Sample records for high-heat flux electronics

  1. High flux heat exchanger

    NASA Astrophysics Data System (ADS)

    Flynn, Edward M.; Mackowski, Michael J.

    1993-01-01

    This interim report documents the results of the first two phases of a four-phase program to develop a high flux heat exchanger for cooling future high performance aircraft electronics. Phase 1 defines future needs for high flux heat removal in advanced military electronics systems. The results are sorted by broad application categories: (1) commercial digital systems, (2) military data processors, (3) power processors, and (4) radar and optical systems. For applications expected to be fielded in five to ten years, the outlook is for steady state flux levels of 30-50 W/sq cm for digital processors and several hundred W/sq cm for power control applications. In Phase 1, a trade study was conducted on emerging cooling technologies which could remove a steady state chip heat flux of 100 W/sq cm while holding chip junction temperature to 90 C. Constraints imposed on heat exchanger design, in order to reflect operation in a fighter aircraft environment, included a practical lower limit on coolant supply temperature, the preference for a nontoxic, nonflammable, and nonfreezing coolant, the need to minimize weight and volume, and operation in an accelerating environment. The trade study recommended the Compact High Intensity Cooler (CHIC) for design, fabrication, and test in the final two phases of this program.

  2. Transport coefficients and heat fluxes in non-equilibrium high-temperature flows with electronic excitation

    NASA Astrophysics Data System (ADS)

    Istomin, V. A.; Kustova, E. V.

    2017-02-01

    The influence of electronic excitation on transport processes in non-equilibrium high-temperature ionized mixture flows is studied. Two five-component mixtures, N 2 / N2 + / N / N + / e - and O 2 / O2 + / O / O + / e - , are considered taking into account the electronic degrees of freedom for atomic species as well as the rotational-vibrational-electronic degrees of freedom for molecular species, both neutral and ionized. Using the modified Chapman-Enskog method, the transport coefficients (thermal conductivity, shear viscosity and bulk viscosity, diffusion and thermal diffusion) are calculated in the temperature range 500-50 000 K. Thermal conductivity and bulk viscosity coefficients are strongly affected by electronic states, especially for neutral atomic species. Shear viscosity, diffusion, and thermal diffusion coefficients are not sensible to electronic excitation if the size of excited states is assumed to be constant. The limits of applicability for the Stokes relation are discussed; at high temperatures, this relation is violated not only for molecular species but also for electronically excited atomic gases. Two test cases of strongly non-equilibrium flows behind plane shock waves corresponding to the spacecraft re-entry (Hermes and Fire II) are simulated numerically. Fluid-dynamic variables and heat fluxes are evaluated in gases with electronic excitation. In inviscid flows without chemical-radiative coupling, the flow-field is weakly affected by electronic states; however, in viscous flows, their influence can be more important, in particular, on the convective heat flux. The contribution of different dissipative processes to the heat transfer is evaluated as well as the effect of reaction rate coefficients. The competition of diffusion and heat conduction processes reduces the overall effect of electronic excitation on the convective heating, especially for the Fire II test case. It is shown that reliable models of chemical reaction rates are of great

  3. Structures for handling high heat fluxes

    NASA Astrophysics Data System (ADS)

    Watson, R. D.

    1990-12-01

    The divertor is reconized as one of the main performance limiting components for ITER. This paper reviews the critical issues for structures that are designed to withstand heat fluxes > 5 MW/m 2. High velocity, sub-cooled water with twisted tape inserts for enhanced heat transfer provides a critical heat flux limit of 40-60 MW/m 2. Uncertainties in physics and engineering heat flux peaking factors require that the design heat flux not exceed 10 MW/m 2 to maintain an adequate burnout safety margin. Armor tiles and heat sink materials must have a well matched thermal expansion coefficient to minimize stresses. The divertor lifetime from sputtering erosion is highly uncertain. The number of disruptions specified for ITER must be reduced to achieve a credible design. In-situ plasma spray repair with thick metallic coatings may reduce the problems of erosion. Runaway electrons in ITER have the potential to melt actively cooled components in a single event. A water leak is a serious accident because of steam reactions with hot carbon, beryllium, or tungsten that can mobilize large amounts of tritium and radioactive elements. If the plasma does not shutdown immediately, the divertor can melt in 1-10 s after a loss of coolant accident. Very high reliability of carbon tile braze joints will be required to achieve adequate safety and performance goals. Most of these critical issues will be addressed in the near future by operation of the Tore Supra pump limiters and the JET pumped divertor. An accurate understanding of the power flow out of edge of a DT burning plasma is essential to successful design of high heat flux components.

  4. Advanced high temperature heat flux sensors

    NASA Technical Reports Server (NTRS)

    Atkinson, W.; Hobart, H. F.; Strange, R. R.

    1983-01-01

    To fully characterize advanced high temperature heat flux sensors, calibration and testing is required at full engine temperature. This required the development of unique high temperature heat flux test facilities. These facilities were developed, are in place, and are being used for advanced heat flux sensor development.

  5. Nanoporous membrane device for ultra high heat flux thermal management

    NASA Astrophysics Data System (ADS)

    Hanks, Daniel F.; Lu, Zhengmao; Sircar, Jay; Salamon, Todd R.; Antao, Dion S.; Bagnall, Kevin R.; Barabadi, Banafsheh; Wang, Evelyn N.

    2018-02-01

    High power density electronics are severely limited by current thermal management solutions which are unable to dissipate the necessary heat flux while maintaining safe junction temperatures for reliable operation. We designed, fabricated, and experimentally characterized a microfluidic device for ultra-high heat flux dissipation using evaporation from a nanoporous silicon membrane. With 100 nm diameter pores, the membrane can generate high capillary pressure even with low surface tension fluids such as pentane and R245fa. The suspended ultra-thin membrane structure facilitates efficient liquid transport with minimal viscous pressure losses. We fabricated the membrane in silicon using interference lithography and reactive ion etching and then bonded it to a high permeability silicon microchannel array to create a biporous wick which achieves high capillary pressure with enhanced permeability. The back side consisted of a thin film platinum heater and resistive temperature sensors to emulate the heat dissipation in transistors and measure the temperature, respectively. We experimentally characterized the devices in pure vapor-ambient conditions in an environmental chamber. Accordingly, we demonstrated heat fluxes of 665 ± 74 W/cm2 using pentane over an area of 0.172 mm × 10 mm with a temperature rise of 28.5 ± 1.8 K from the heated substrate to ambient vapor. This heat flux, which is normalized by the evaporation area, is the highest reported to date in the pure evaporation regime, that is, without nucleate boiling. The experimental results are in good agreement with a high fidelity model which captures heat conduction in the suspended membrane structure as well as non-equilibrium and sub-continuum effects at the liquid-vapor interface. This work suggests that evaporative membrane-based approaches can be promising towards realizing an efficient, high flux thermal management strategy over large areas for high-performance electronics.

  6. Electron heat flux dropouts in the solar wind - Evidence for interplanetary magnetic field reconnection?

    NASA Technical Reports Server (NTRS)

    Mccomas, D. J.; Gosling, J. T.; Phillips, J. L.; Bame, S. J.; Luhmann, J. G.; Smith, E. J.

    1989-01-01

    An examination of ISEE-3 data from 1978 reveal 25 electron heat flux dropout events ranging in duration from 20 min to over 11 hours. The heat flux dropouts are found to occur in association with high plasma densities, low plasma velocities, low ion and electron temperatures, and low magnetic field magnitudes. It is suggested that the heat flux dropout intervals may indicate that the spacecraft is sampling plasma regimes which are magnetically disconnected from the sun and instead are connected to the outer heliosphere at both ends.

  7. Recent High Heat Flux Tests on W-Rod-Armored Mockups

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    NYGREN,RICHARD E.; YOUCHISON,DENNIS L.; MCDONALD,JIMMIE M.

    2000-07-18

    In the authors initial high heat flux tests on small mockups armored with W rods, done in the small electron beam facility (EBTS) at Sandia National Laboratories, the mockups exhibited excellent thermal performance. However, to reach high heat fluxes, they reduced the heated area to only a portion ({approximately}25%) of the sample. They have now begun tests in their larger electron beam facility, EB 1200, where the available power (1.2 MW) is more than enough to heat the entire surface area of the small mockups. The initial results indicate that, at a given power, the surface temperatures of rods inmore » the EB 1200 tests is somewhat higher than was observed in the EBTS tests. Also, it appears that one mockup (PW-10) has higher surface temperatures than other mockups with similar height (10mm) W rods, and that the previously reported values of absorbed heat flux on this mockup were too high. In the tests in EB 1200 of a second mockup, PW-4, absorbed heat fluxes of {approximately}22MW/m{sup 2} were reached but the corresponding surface temperatures were somewhat higher than in EBTS. A further conclusion is that the simple 1-D model initially used in evaluating some of the results from the EBTS testing was not adequate, and 3-D thermal modeling will be needed to interpret the results.« less

  8. High heat flux loop heat pipes

    NASA Astrophysics Data System (ADS)

    North, Mark T.; Sarraf, David B.; Rosenfeld, John H.; Maidanik, Yuri F.; Vershinin, Sergey

    1997-01-01

    Loop Heat Pipes (LHPs) can transport very large thermal power loads, over long distances, through flexible, small diameter tubes and against high gravitational heads. While recent LHPs have transported as much as 1500 W, the peak heat flux through a LHP's evaporator has been limited to about 0.07 MW/m2. This limitation is due to the arrangement of vapor passages next to the heat load which is one of the conditions necessary to ensure self priming of the device. This paper describes work aimed at raising this limit by threefold to tenfold. Two approaches were pursued. One optimized the vapor passage geometry for the high heat flux conditions. The geometry improved the heat flow into the wick and working fluid. This approach also employed a finer pored wick to support higher vapor flow losses. The second approach used a bidisperse wick material within the circumferential vapor passages. The bidisperse material increased the thermal conductivity and the evaporative surface area in the region of highest heat flux, while providing a flow path for the vapor. Proof-of-concept devices were fabricated and tested for each approach. Both devices operated as designed and both demonstrated operation at a heat flux of 0.70 MW/m2. This performance exceeded the known state of the art by a factor of more than six for both conventional heat pipes and for loop heat pipes using ammonia. In addition, the bidisperse-wick device demonstrated boiling heat transfer coefficients up to 100,000 W/m2.K, and the fine pored device demonstrated an orientation independence with its performance essentially unaffected by whether its evaporator was positioned above, below or level with the condenser.

  9. The role of electron heat flux in guide-field magnetic reconnection

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Hesse, Michael; Kuznetsova, Masha; Birn, Joachim

    2004-12-01

    A combination of analytical theory and particle-in-cell simulations are employed in order to investigate the electron dynamics near and at the site of guide field magnetic reconnection. A detailed analysis of the contributions to the reconnection electric field shows that both bulk inertia and pressure-based quasiviscous processes are important for the electrons. Analytic scaling demonstrates that conventional approximations for the electron pressure tensor behavior in the dissipation region fail, and that heat flux contributions need to be accounted for. Based on the evolution equation of the heat flux three tensor, which is derived in this paper, an approximate form ofmore » the relevant heat flux contributions to the pressure tensor is developed, which reproduces the numerical modeling result reasonably well. Based on this approximation, it is possible to develop a scaling of the electron current layer in the central dissipation region. It is shown that the pressure tensor contributions become important at the scale length defined by the electron Larmor radius in the guide magnetic field.« less

  10. Heat-Flux Measurements in Laser-Produced Plasmas Using Thomson Scattering from Electron Plasma Waves

    NASA Astrophysics Data System (ADS)

    Henchen, R. J.; Goncharov, V. N.; Cao, D.; Katz, J.; Froula, D. H.; Rozmus, W.

    2017-10-01

    An experiment was designed to measure heat flux in coronal plasmas using collective Thomson scattering. Adjustments to the electron distribution function resulting from heat flux affect the shape of the collective Thomson scattering features through wave-particle resonance. The amplitude of the Spitzer-Härm electron distribution function correction term (f1) was varied to match the data and determines the value of the heat flux. Independent measurements of temperature and density obtained from Thomson scattering were used to infer the classical heat flux (q = - κ∇Te) . Time-resolved Thomson-scattering data were obtained at five locations in the corona along the target normal in a blowoff plasma formed from a planar Al target with 1.5 kJ of 351-nm laser light in a 2-ns square pulse. The flux measured through the Thomson-scattering spectra is a factor of 5 less than the κ∇Te measurements. The lack of collisions of heat-carrying electrons suggests a nonlocal model is needed to accurately describe the heat flux. This material is based upon work supported by the Department of Energy National Nuclear Security Administration under Award Number DE-NA0001944.

  11. High heat flux issues for plasma-facing components in fusion reactors

    NASA Astrophysics Data System (ADS)

    Watson, Robert D.

    1993-02-01

    Plasma facing components in tokamak fusion reactors are faced with a number of difficult high heat flux issues. These components include: first wall armor tiles, pumped limiters, diverter plates, rf antennae structure, and diagnostic probes. Peak heat fluxes are 15 - 30 MW/m2 for diverter plates, which will operate for 100 - 1000 seconds in future tokamaks. Disruption heat fluxes can approach 100,000 MW/m2 for 0.1 ms. Diverter plates are water-cooled heat sinks with armor tiles brazed on to the plasma facing side. Heat sink materials include OFHC, GlidcopTM, TZM, Mo-41Re, and niobium alloys. Armor tile materials include: carbon fiber composites, beryllium, silicon carbide, tungsten, and molybdenum. Tile thickness range from 2 - 10 mm, and heat sinks are 1 - 3 mm. A twisted tape insert is used to enhance heat transfer and increase the burnout safety margin from critical heat flux limits to 50 - 60 MW/m2 with water at 10 m/s and 4 MPa. Tests using rastered electron beams have shown thermal fatigue failures from cracks at the brazed interface between tiles and the heat sink after only 1000 cycles at 10 - 15 MW/m2. These fatigue lifetimes need to be increased an order of magnitude to meet future requirements. Other critical issues for plasma facing components include: surface erosion from sputtering and disruption erosion, eddy current forces and runaway electron impact from disruptions, neutron damage, tritium retention and release, remote maintenance of radioactive components, corrosion-erosion, and loss-of-coolant accidents.

  12. High heat flux measurements and experimental calibrations/characterizations

    NASA Technical Reports Server (NTRS)

    Kidd, Carl T.

    1992-01-01

    Recent progress in techniques employed in the measurement of very high heat-transfer rates in reentry-type facilities at the Arnold Engineering Development Center (AEDC) is described. These advances include thermal analyses applied to transducer concepts used to make these measurements; improved heat-flux sensor fabrication methods, equipment, and procedures for determining the experimental time response of individual sensors; performance of absolute heat-flux calibrations at levels above 2,000 Btu/cu ft-sec (2.27 kW/cu cm); and innovative methods of performing in-situ run-to-run characterizations of heat-flux probes installed in the test facility. Graphical illustrations of the results of extensive thermal analyses of the null-point calorimeter and coaxial surface thermocouple concepts with application to measurements in aerothermal test environments are presented. Results of time response experiments and absolute calibrations of null-point calorimeters and coaxial thermocouples performed in the laboratory at intermediate to high heat-flux levels are shown. Typical AEDC high-enthalpy arc heater heat-flux data recently obtained with a Calspan-fabricated null-point probe model are included.

  13. Control Mechanisms of the Electron Heat Flux in the Solar Wind: Observations in Comparison to Numerical Simulations

    NASA Astrophysics Data System (ADS)

    Stverak, S.; Hellinger, P.; Landi, S.; Travnicek, P. M.; Maksimovic, M.

    2017-12-01

    Recent understanding of the heat transport and dissipation in the expanding solar wind propose number of complex control mechanisms down to the electron kinetic scales. We investigate the evolution of electron heat flux properties and constraints along the expansion using in situ observations from Helios spacecraft in comparison to numerical kinetic simulations. In particular we focus on the roles of Coulomb collisions and wave-particle interactions in shaping the electron velocity distribution functions and thus controlling the heat transported by the electron heat flux. We show the general evolution of the electron heat flux to be driven namely by the Coulomb collisions. Locally we demonstrate the wave-particle interactions related to the kinetic plasma instabilities to be providing effective constraints in case of extreme heat flux levels.

  14. Physics-Based Modeling and Measurement of High-Flux Condensation Heat Transfer

    DTIC Science & Technology

    2011-09-01

    TRANSFER (Contract No. N000140811139) by Prof. Issam Mudawar Sung-Min Kim Joseph Kim Boiling and Two-Phase Flow Laboratory School of...Final 01-10-2008 to 30-09-2011 Physics-Based Modeling and Measurement of High-Flux Condensation Heat Transfer NA N00014-08-1-1139 NA NA NA NA Mudawar ...respectively. phase change, condensation, electronics cooling, micro-channel, high-flux U U U UU 107 Mudawar , Issam 765-494-5705 Reset PHYSICS-BASED

  15. Modeling of a heat sink and high heat flux vapor chamber

    NASA Astrophysics Data System (ADS)

    Vadnjal, Aleksander

    An increasing demand for a higher heat flux removal capability within a smaller volume for high power electronics led us to focus on a novel cold plate design. A high heat flux evaporator and micro channel heat sink are the main components of a cold plate which is capable of removing couple of 100 W/cm2. In order to describe performance of such porous media device a proper modeling has to be addressed. A universal approach based on the volume average theory (VAT) to transport phenomena in porous media is shown. An approach on how to treat the closure for momentum and energy equations is addressed and a proper definition for friction factors and heat transfer coefficients are discussed. A numerical scheme using a solution to Navier-Stokes equations over a representative elementary volume (REV) and the use of VAT is developed to show how to compute friction factors and heat transfer coefficients. The calculation show good agreement with the experimental data. For the heat transfer coefficient closure, a proper average for both fluid and solid is investigated. Different types of heating are also investigated in order to determine how it influences the heat transfer coefficient. A higher heat fluxes in small area condensers led us to the micro channels in contrast to the classical heat fin design. A micro channel can have various shapes to enhance heat transfer, but the shape that will lead to a higher heat flux removal with a moderate pumping power needs to be determined. The standard micro-channel terminology is usually used for channels with a simple cross section, e.g. square, round, triangle, etc., but here the micro channel cross section is going to be expanded to describe more complicated and interconnected micro scale channel cross sections. The micro channel geometries explored are pin fins (in-line and staggered) and sintered porous micro channels. The problem solved here is a conjugate problem involving two heat transfer mechanisms; (1) porous media

  16. Baseline high heat flux and plasma facing materials for fusion

    NASA Astrophysics Data System (ADS)

    Ueda, Y.; Schmid, K.; Balden, M.; Coenen, J. W.; Loewenhoff, Th.; Ito, A.; Hasegawa, A.; Hardie, C.; Porton, M.; Gilbert, M.

    2017-09-01

    In fusion reactors, surfaces of plasma facing components (PFCs) are exposed to high heat and particle flux. Tungsten and Copper alloys are primary candidates for plasma facing materials (PFMs) and coolant tube materials, respectively, mainly due to high thermal conductivity and, in the case of tungsten, its high melting point. In this paper, recent understandings and future issues on responses of tungsten and Cu alloys to fusion environments (high particle flux (including T and He), high heat flux, and high neutron doses) are reviewed. This review paper includes; Tritium retention in tungsten (K. Schmid and M. Balden), Impact of stationary and transient heat loads on tungsten (J.W. Coenen and Th. Loewenhoff), Helium effects on surface morphology of tungsten (Y. Ueda and A. Ito), Neutron radiation effects in tungsten (A. Hasegawa), and Copper and copper alloys development for high heat flux components (C. Hardie, M. Porton, and M. Gilbert).

  17. Remote high-temperature insulatorless heat-flux gauge

    DOEpatents

    Noel, B.W.

    1993-12-28

    A remote optical heat-flux gauge for use in extremely high temperature environments is described. This application is possible because of the use of thermographic phosphors as the sensing media, and the omission of the need for an intervening layer of insulator between phosphor layers. The gauge has no electrical leads, but is interrogated with ultraviolet or laser light. The luminescence emitted by the two phosphor layers, which is indicative of the temperature of the layers, is collected and analyzed in order to determine the heat flux incident on the surface being investigated. The two layers of thermographic phosphor must be of different materials to assure that the spectral lines collected will be distinguishable. Spatial heat-flux measurements can be made by scanning the light across the surface of the gauge. 3 figures.

  18. Remote high-temperature insulatorless heat-flux gauge

    DOEpatents

    Noel, Bruce W.

    1993-01-01

    A remote optical heat-flux gauge for use in extremely high temperature environments is described. This application is possible because of the use of thermographic phosphors as the sensing media, and the omission of the need for an intervening layer of insulator between phosphor layers. The gauge has no electrical leads, but is interrogated with ultraviolet or laser light. The luminescence emitted by the two phosphor layers, which is indicative of the temperature of the layers, is collected and analyzed in order to determine the heat flux incident on the surface being investigated. The two layers of thermographic phosphor must be of different materials to assure that the spectral lines collected will be distinguishable. Spatial heat-flux measurements can be made by scanning the light across the surface of the gauge.

  19. New low-cost high heat flux source

    NASA Astrophysics Data System (ADS)

    Cheng, Dah Yu

    1993-11-01

    Intense heat sources are needed to address new manufacturing techniques, such as, the Rapid Thermal Process for silicon wafer manufacturing. The current technology of high heat flux sources is the laser for its ability to do welding and cutting is well-known. The laser with its coherent radiation allows an image to be focused down to very small sizes to reach extremely high heat flux. But the laser also has problems: it is inefficient in its use because of its singular wave length and brings up OSHA safety related problems. Also heavy industrial manufacturing requires much higher total energy in addition to the high heat flux which makes the current laser system too slow to be economical. The system I am proposing starts with a parabolic curve. If the curve is rotated about the axis of the parabola, it generates the classical parabolic reflector as we know it. On the other hand, when the curve is rotated about the chord, a line passing through the focal point and perpendicular to the axis, generates a new surface called the Orthogonal Parabolic Surface. A new optical reflector geometry is presented which integrates a linear white light (continuum spectra) source through a coherent path to be focused to a very small area.

  20. Diamond Microchannel Heat Sink Designs For High Heat Flux Thermal Control

    NASA Astrophysics Data System (ADS)

    Corbin, Michael V.; DeBenedictis, Matthew M.; James, David B.; LeBlanc, Stephen P.; Paradis, Leo R.

    2002-08-01

    Directed energy weapons, wide band gap semiconductor based radars, and other powerful systems present significant thermal control challenges to component designers. heat Flux levels approaching 2000 W/cm(2) are encountered at the base of laser diodes, and levels as high as 500 WI /cm(2) are expected in laser slabs and power amplifier tube collectors. These impressive heat flux levels frequently combine with strict operating temperature requirements to further compound the thermal control problem. Many investigators have suggested the use of diamond heat spreaders to reduce flux levels at or near to its source, and some have suggested that diamond microchannel heat sinks ultimately may play a significant role in the solution of these problems. Design engineers at Raytheon Company have investigated the application of all-diamond microchannel heat sinks to representative high heat flux problems and have found the approach promising. Diamond microchannel fabrication feasibility has been demonstrated; integration into packaging systems and the accompanying material compatibility issues have been addressed; and thermal and hydrodynamic performance predictions have been made for selected, possible applications. An example of a practical, all diamond microchannel heat sink has been fabricated, and another is in process and will be performance tested. The heat sink assembly is made entirely of optical quality, CVD diamond and is of sufficient strength to withstand the thermal and pressure-induced mechanical loads associated with manufacture and use in tactical weapons environment. The work presented describes the development program's accomplishments to date, and highlights many of the areas for future study.

  1. Critical role of electron heat flux on Bohm criterion

    DOE PAGES

    Tang, Xianzhu; Guo, Zehua

    2016-12-05

    Bohm criterion, originally derived for an isothermal-electron and cold-ion plasma, is often used as a rule of thumb for more general plasmas. Here, we establish a more precise determination of the Bohm criterion that are quantitatively useful for understanding and modeling collisional plasmas that still have collisional mean-free-path much greater than plasma Debye length. Specifically, it is shown that electron heat flux, rather than the isothermal electron assumption, is what sets the Bohm speed to bemore » $$\\sqrt{k_B(T_e||+3T_i||)/m_i}$$ with T e,i∥ the electron and ion parallel temperature at the sheath entrance and m i the ion mass.« less

  2. Critical role of electron heat flux on Bohm criterion

    NASA Astrophysics Data System (ADS)

    Tang, Xian-Zhu; Guo, Zehua

    2016-12-01

    Bohm criterion, originally derived for an isothermal-electron and cold-ion plasma, is often used as a rule of thumb for more general plasmas. Here, we establish a more precise determination of the Bohm criterion that are quantitatively useful for understanding and modeling collisional plasmas that still have collisional mean-free-path much greater than plasma Debye length. Specifically, it is shown that electron heat flux, rather than the isothermal electron assumption, is what sets the Bohm speed to be √{ k B ( T e ∥ + 3 T i ∥ ) / m i } with T e , i ∥ the electron and ion parallel temperature at the sheath entrance and mi the ion mass.

  3. Investigation of ion and electron heat transport of high- T e ECH heated discharges in the large helical device

    DOE PAGES

    Pablant, N. A.; Satake, S.; Yokoyama, M.; ...

    2016-01-28

    An analysis of the radial electric field and heat transport, both for ions and electrons, is presented for a high-more » $${{T}_{\\text{e}}}$$ electron cyclotron heated (ECH) discharge on the large helical device (LHD). Transport analysis is done using the task3d transport suite utilizing experimentally measured profiles for both ions and electrons. Ion temperature and perpendicular flow profiles are measured using the recently installed x-ray imaging crystal spectrometer diagnostic (XICS), while electron temperature and density profiles are measured using Thomson scattering. The analysis also includes calculated ECH power deposition profiles as determined through the travis ray-tracing code. This is the first time on LHD that this type of integrated transport analysis with measured ion temperature profiles has been performed without NBI, allowing the heat transport properties of plasmas with only ECH heating to be more clearly examined. For this study, a plasma discharge is chosen which develops a high central electron temperature ($${{T}_{\\text{eo}}}=9$$ keV) at moderately low densities ($${{n}_{\\text{eo}}}=1.5\\times {{10}^{19}}$$ m-3). The experimentally determined transport properties from task3d are compared to neoclassical predictions as calculated by the gsrake and fortec-3d codes. The predicted electron fluxes are seen to be an order of magnitude less than the measured fluxes, indicating that electron transport is largely anomalous, while the neoclassical and measured ion heat fluxes are of the same magnitude. Neoclassical predictions of a strong positive ambipolar electric field ($${{E}_{\\text{r}}}$$ ) in the plasma core are validated through comparisons to perpendicular flow measurements from the XICS diagnostic. Furthermore, this provides confidence that the predictions are producing physically meaningful results for the particle fluxes and radial electric field, which are a key component in correctly predicting plasma confinement.« less

  4. EU Development of High Heat Flux Components

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Linke, J.; Lorenzetto, P.; Majerus, P.

    2005-04-15

    The development of plasma facing components for next step fusion devices in Europe is strongly focused to ITER. Here a wide spectrum of different design options for the divertor target and the first wall have been investigated with tungsten, CFC, and beryllium armor. Electron beam simulation experiments have been used to determine the performance of high heat flux components under ITER specific thermal loads. Beside thermal fatigue loads with power density levels up to 20 MWm{sup -2}, off-normal events are a serious concern for the lifetime of plasma facing components. These phenomena are expected to occur on a time scalemore » of a few milliseconds (plasma disruptions) or several hundred milliseconds (vertical displacement events) and have been identified as a major source for the production of neutron activated metallic or tritium enriched carbon dust which is of serious importance from a safety point of view.The irradiation induced material degradation is another critical concern for future D-T-burning fusion devices. In ITER the integrated neutron fluence to the first wall and the divertor armour will remain in the order of 1 dpa and 0.7 dpa, respectively. This value is low compared to future commercial fusion reactors; nevertheless, a nonnegligible degradation of the materials has been detected, both for mechanical and thermal properties, in particular for the thermal conductivity of carbon based materials. Beside the degradation of individual material properties, the high heat flux performance of actively cooled plasma facing components has been investigated under ITER specific thermal and neutron loads.« less

  5. Measurement of local high-level, transient surface heat flux

    NASA Technical Reports Server (NTRS)

    Liebert, Curt H.

    1988-01-01

    This study is part of a continuing investigation to develop methods for measuring local transient surface heat flux. A method is presented for simultaneous measurements of dual heat fluxes at a surface location by considering the heat flux as a separate function of heat stored and heat conducted within a heat flux gage. Surface heat flux information is obtained from transient temperature measurements taken at points within the gage. Heat flux was determined over a range of 4 to 22 MW/sq m. It was concluded that the method is feasible. Possible applications are for heat flux measurements on the turbine blade surfaces of space shuttle main engine turbopumps and on the component surfaces of rocket and advanced gas turbine engines and for testing sensors in heat flux gage calibrators.

  6. Heat Flux Sensor

    NASA Technical Reports Server (NTRS)

    1994-01-01

    A heat flux microsensor developed under a NASP Small Business Innovation Research (SBIR) has a wide range of potential commercial applications. Vatell Corporation originally designed microsensors for use in very high temperatures. The company then used the technology to develop heat flux sensors to measure the rate of heat energy flowing in and out of a surface as well as readings on the surface temperature. Additional major advantages include response to heat flux in less than 10 microseconds and the ability to withstand temperatures up to 1,200 degrees centigrade. Commercial applications are used in high speed aerodynamics, supersonic combustion, blade cooling, and mass flow measurements, etc.

  7. Evaporation on/in Capillary Structures of High Heat Flux Two-Phase Devices

    NASA Technical Reports Server (NTRS)

    Faghri, Amir; Khrustalev, Dmitry

    1996-01-01

    Two-phase devices (heat pipes, capillary pumped loops, loop heat pipes, and evaporators) have become recognized as key elements in thermal control systems of space platforms. Capillary and porous structures are necessary and widely used in these devices, especially in high heat flux and zero-g applications, to provide fluid transport and enhanced heat transfer during vaporization and condensation. However, some unexpected critical phenomena, such as dryout in long heat pipe evaporators and high thermal resistance of loop heat pipe evaporators with high heat fluxes, are possible and have been encountered in the use of two-phase devices in the low gravity environment. Therefore, a detailed fundamental investigation is proposed to better understand the fluid behavior in capillary-porous structures during vaporization at high heat fluxes. The present paper addresses some theoretical aspects of this investigation.

  8. Electron heating within interaction zones of simple high-speed solar wind streams

    NASA Technical Reports Server (NTRS)

    Feldman, W. C.; Asbridge, J. R.; Bame, S. J.; Gosling, J. T.; Lemons, D. S.

    1978-01-01

    In the present paper, electron heating within the high-speed portions of three simple stream-stream interaction zones is studied to further our understanding of the physics of heat flux regulation in interplanetary space. To this end, the thermal signals present in the compressions at the leading edges of the simple high-speed streams are analyzed, showing that the data are inconsistent with the Spitzer conductivity. Instead, a polynomial law is found to apply. Its implication concerning the mechanism of interplanetary heat conduction is discussed, and the results of applying this conductivity law to high-speed flows inside of 1 AU are studied. A self-consistent model of the radial evolution of electrons in the high-speed solar wind is proposed.

  9. On the use of flat tile armour in high heat flux components

    NASA Astrophysics Data System (ADS)

    Merola, M.; Vieider, G.

    1998-10-01

    The possibility to have a flat tile geometry for those high heat flux components subjected to a convective heat flux (namely the divertor dump target, lower vertical target, and the limiter) has been investigated. Because of the glancing incidence of the power load, if an armour tile falls off an extremely high heat flux hits the leading edge of the adjacent tile. As a result a rapid temperature increase occurs in the armour-heat sink joint. The heat flux to the water coolant also increases rapidly up to a factor of 1.7 and 2.3 for a beryllium and CFC armour, respectively, thus causing possible critical heat flux problems. Thermal stresses in the armour-heat sink joint double in less than 0.4 s and triplicate after 1 s thus leading to a possible cascade failure. Therefore the use of a flat tile geometry for these components does not seem to be appropriate. In this case a monoblock geometry gives a much more robust solution.

  10. Momentum transport and nonlocality in heat-flux-driven magnetic reconnection in high-energy-density plasmas.

    PubMed

    Liu, Chang; Fox, William; Bhattacharjee, Amitava; Thomas, Alexander G R; Joglekar, Archis S

    2017-10-01

    Recent theory has demonstrated a novel physics regime for magnetic reconnection in high-energy-density plasmas where the magnetic field is advected by heat flux via the Nernst effect. Here we elucidate the physics of the electron dissipation layer in this regime. Through fully kinetic simulation and a generalized Ohm's law derived from first principles, we show that momentum transport due to a nonlocal effect, the heat-flux-viscosity, provides the dissipation mechanism for magnetic reconnection. Scaling analysis, and simulations show that the reconnection process comprises a magnetic field compression stage and quasisteady reconnection stage, and the characteristic width of the current sheet in this regime is several electron mean-free paths. These results show the important interplay between nonlocal transport effects and generation of anisotropic components to the distribution function.

  11. High geothermal heat flux measured below the West Antarctic Ice Sheet

    PubMed Central

    Fisher, Andrew T.; Mankoff, Kenneth D.; Tulaczyk, Slawek M.; Tyler, Scott W.; Foley, Neil

    2015-01-01

    The geothermal heat flux is a critical thermal boundary condition that influences the melting, flow, and mass balance of ice sheets, but measurements of this parameter are difficult to make in ice-covered regions. We report the first direct measurement of geothermal heat flux into the base of the West Antarctic Ice Sheet (WAIS), below Subglacial Lake Whillans, determined from the thermal gradient and the thermal conductivity of sediment under the lake. The heat flux at this site is 285 ± 80 mW/m2, significantly higher than the continental and regional averages estimated for this site using regional geophysical and glaciological models. Independent temperature measurements in the ice indicate an upward heat flux through the WAIS of 105 ± 13 mW/m2. The difference between these heat flux values could contribute to basal melting and/or be advected from Subglacial Lake Whillans by flowing water. The high geothermal heat flux may help to explain why ice streams and subglacial lakes are so abundant and dynamic in this region. PMID:26601210

  12. High geothermal heat flux measured below the West Antarctic Ice Sheet.

    PubMed

    Fisher, Andrew T; Mankoff, Kenneth D; Tulaczyk, Slawek M; Tyler, Scott W; Foley, Neil

    2015-07-01

    The geothermal heat flux is a critical thermal boundary condition that influences the melting, flow, and mass balance of ice sheets, but measurements of this parameter are difficult to make in ice-covered regions. We report the first direct measurement of geothermal heat flux into the base of the West Antarctic Ice Sheet (WAIS), below Subglacial Lake Whillans, determined from the thermal gradient and the thermal conductivity of sediment under the lake. The heat flux at this site is 285 ± 80 mW/m(2), significantly higher than the continental and regional averages estimated for this site using regional geophysical and glaciological models. Independent temperature measurements in the ice indicate an upward heat flux through the WAIS of 105 ± 13 mW/m(2). The difference between these heat flux values could contribute to basal melting and/or be advected from Subglacial Lake Whillans by flowing water. The high geothermal heat flux may help to explain why ice streams and subglacial lakes are so abundant and dynamic in this region.

  13. Development of advanced high-temperature heat flux sensors. Phase 2: Verification testing

    NASA Technical Reports Server (NTRS)

    Atkinson, W. H.; Cyr, M. A.; Strange, R. R.

    1985-01-01

    A two-phase program is conducted to develop heat flux sensors capable of making heat flux measurements throughout the hot section of gas turbine engines. In Phase 1, three types of heat flux sensors are selected; embedded thermocouple, laminated, and Gardon gauge sensors. A demonstration of the ability of these sensors to operate in an actual engine environment is reported. A segmented liner of each of two combustors being used in the Broad Specification Fuels Combustor program is instrumented with the three types of heat flux sensors then tested in a high pressure combustor rig. Radiometer probes are also used to measure the radiant heat loads to more fully characterize the combustor environment. Test results show the heat flux sensors to be in good agreement with radiometer probes and the predicted data trends. In general, heat flux sensors have strong potential for use in combustor development programs.

  14. Institute for High Heat Flux Removal (IHHFR). Phases I, II, and III

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Boyd, Ronald D.

    2014-08-31

    The IHHFR focused on interdisciplinary applications as it relates to high heat flux engineering issues and problems which arise due to engineering systems being miniaturized, optimized, or requiring increased high heat flux performance. The work in the IHHFR focused on water as a coolant and includes: (1) the development, design, and construction of the high heat flux flow loop and facility; (2) test section development, design, and fabrication; and, (3) single-side heat flux experiments to produce 2-D boiling curves and 3-D conjugate heat transfer measurements for single-side heated test sections. This work provides data for comparisons with previously developed andmore » new single-side heated correlations and approaches that address the single-side heated effect on heat transfer. In addition, this work includes the addition of single-side heated circular TS and a monoblock test section with a helical wire insert. Finally, the present work includes: (1) data base expansion for the monoblock with a helical wire insert (only for the latter geometry), (2) prediction and verification using finite element, (3) monoblock model and methodology development analyses, and (4) an alternate model development for a hypervapotron and related conjugate heat transfer controlling parameters.« less

  15. Automated Heat-Flux-Calibration Facility

    NASA Technical Reports Server (NTRS)

    Liebert, Curt H.; Weikle, Donald H.

    1989-01-01

    Computer control speeds operation of equipment and processing of measurements. New heat-flux-calibration facility developed at Lewis Research Center. Used for fast-transient heat-transfer testing, durability testing, and calibration of heat-flux gauges. Calibrations performed at constant or transient heat fluxes ranging from 1 to 6 MW/m2 and at temperatures ranging from 80 K to melting temperatures of most materials. Facility developed because there is need to build and calibrate very-small heat-flux gauges for Space Shuttle main engine (SSME).Includes lamp head attached to side of service module, an argon-gas-recirculation module, reflector, heat exchanger, and high-speed positioning system. This type of automated heat-flux calibration facility installed in industrial plants for onsite calibration of heat-flux gauges measuring fluxes of heat in advanced gas-turbine and rocket engines.

  16. Momentum transport and nonlocality in heat-flux-driven magnetic reconnection in high-energy-density plasmas

    DOE PAGES

    Liu, Chang; Fox, William; Bhattacharjee, Amitava; ...

    2017-10-06

    Recent theory has demonstrated a novel physics regime for magnetic reconnection in high-energy-density plasmas where the magnetic field is advected by heat flux via the Nernst effect. In this paper, we elucidate the physics of the electron dissipation layer in this regime. Through fully kinetic simulation and a generalized Ohm's law derived from first principles, we show that momentum transport due to a nonlocal effect, the heat-flux-viscosity, provides the dissipation mechanism for magnetic reconnection. Scaling analysis, and simulations show that the reconnection process comprises a magnetic field compression stage and quasisteady reconnection stage, and the characteristic width of the currentmore » sheet in this regime is several electron mean-free paths. Finally, these results show the important interplay between nonlocal transport effects and generation of anisotropic components to the distribution function.« less

  17. Light-intensity modulator withstands high heat fluxes

    NASA Technical Reports Server (NTRS)

    Maples, H. G.; Strass, H. K.

    1966-01-01

    Mechanism modulates and controls the intensity of luminous radiation in light beams associated with high-intensity heat flux. This modulator incorporates two fluid-cooled, externally grooved, contracting metal cylinders which when rotated about their longitudinal axes present a circular aperture of varying size depending on the degree of rotation.

  18. Divertor heat flux mitigation in the National Spherical Torus Experimenta)

    NASA Astrophysics Data System (ADS)

    Soukhanovskii, V. A.; Maingi, R.; Gates, D. A.; Menard, J. E.; Paul, S. F.; Raman, R.; Roquemore, A. L.; Bell, M. G.; Bell, R. E.; Boedo, J. A.; Bush, C. E.; Kaita, R.; Kugel, H. W.; Leblanc, B. P.; Mueller, D.; NSTX Team

    2009-02-01

    Steady-state handling of divertor heat flux is a critical issue for both ITER and spherical torus-based devices with compact high power density divertors. Significant reduction of heat flux to the divertor plate has been achieved simultaneously with favorable core and pedestal confinement and stability properties in a highly shaped lower single null configuration in the National Spherical Torus Experiment (NSTX) [M. Ono et al., Nucl. Fusion 40, 557 2000] using high magnetic flux expansion at the divertor strike point and the radiative divertor technique. A partial detachment of the outer strike point was achieved with divertor deuterium injection leading to peak flux reduction from 4-6MWm-2to0.5-2MWm-2 in small-ELM 0.8-1.0MA, 4-6MW neutral beam injection-heated H-mode discharges. A self-consistent picture of the outer strike point partial detachment was evident from divertor heat flux profiles and recombination, particle flux and neutral pressure measurements. Analytic scrape-off layer parallel transport models were used for interpretation of NSTX detachment experiments. The modeling showed that the observed peak heat flux reduction and detachment are possible with high radiated power and momentum loss fractions, achievable with divertor gas injection, and nearly impossible to achieve with main electron density, divertor neutral density or recombination increases alone.

  19. Air-Cooled Heat Exchanger for High-Temperature Power Electronics: Preprint

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Waye, S. K.; Lustbader, J.; Musselman, M.

    2015-05-06

    This work demonstrates a direct air-cooled heat exchanger strategy for high-temperature power electronic devices with an application specific to automotive traction drive inverters. We present experimental heat dissipation and system pressure curves versus flow rate for baseline and optimized sub-module assemblies containing two ceramic resistance heaters that provide device heat fluxes. The maximum allowable junction temperature was set to 175 deg.C. Results were extrapolated to the inverter scale and combined with balance-of-inverter components to estimate inverter power density and specific power. The results exceeded the goal of 12 kW/L and 12 kW/kg for power density and specific power, respectively.

  20. Numerical simulation of heat fluxes in a two-temperature plasma at shock tube walls

    NASA Astrophysics Data System (ADS)

    Kuznetsov, E. A.; Poniaev, S. A.

    2015-12-01

    Numerical simulation of a two-temperature three-component Xenon plasma flow is presented. A solver based on the OpenFOAM CFD software package is developed. The heat flux at the shock tube end wall is calculated and compared with experimental data. It is shown that the heat flux due to electrons can be as high as 14% of the total heat flux.

  1. Ultrahigh Flux Thin Film Boiling Heat Transfer Through Nanoporous Membranes.

    PubMed

    Wang, Qingyang; Chen, Renkun

    2018-05-09

    Phase change heat transfer is fundamentally important for thermal energy conversion and management, such as in electronics with power density over 1 kW/cm 2 . The critical heat flux (CHF) of phase change heat transfer, either evaporation or boiling, is limited by vapor flux from the liquid-vapor interface, known as the upper limit of heat flux. This limit could in theory be greater than 1 kW/cm 2 on a planar surface, but its experimental realization has remained elusive. Here, we utilized nanoporous membranes to realize a new "thin film boiling" regime that resulted in an unprecedentedly high CHF of over 1.2 kW/cm 2 on a planar surface, which is within a factor of 4 of the theoretical limit, and can be increased to a higher value if mechanical strength of the membranes can be improved (demonstrated with 1.85 kW/cm 2 CHF in this work). The liquid supply is achieved through a simple nanoporous membrane that supports the liquid film where its thickness automatically decreases as heat flux increases. The thin film configuration reduces the conductive thermal resistance, leads to high frequency bubble departure, and provides separate liquid-vapor pathways, therefore significantly enhances the heat transfer. Our work provides a new nanostructuring approach to achieve ultrahigh heat flux in phase change heat transfer and will benefit both theoretical understanding and application in thermal management of high power devices of boiling heat transfer.

  2. Heat-Flux Measurements from Collective Thomson-Scattering Spectra

    NASA Astrophysics Data System (ADS)

    Henchen, R. J.; Hu, S. X.; Katz, J.; Froula, D. H.; Rozmus, W.

    2015-11-01

    Collective Thomson scattering was used to measure heat flux in coronal plasmas. The relative amplitude of the Thomson-scattered power into the up- and downshifted electron plasma wave features was used to determine the flux of electrons moving along the temperature gradient at three to four times the electron thermal velocity. Simultaneously, the ion-acoustic wave features were measured. Their relative amplitude is used to measure the flux of the return-current electrons. The frequencies of these ion-acoustic and electron plasma wave features provide local measurements of the electron temperature and density. These spectra were obtained at five locations along the temperature gradient in a laser-produced blowoff plasma. These measurements of plasma parameters are used to infer the Spitzer -Härm flux qSH = - κ∇Te and are in good agreement with the values of the heat flux measured from the scattering-feature asymmetries. This material is based upon work supported by the Department of Energy National Nuclear Security Administration under Award Number DE-NA0001944.

  3. A unique high heat flux facility for testing hypersonic engine components

    NASA Technical Reports Server (NTRS)

    Melis, Matthew E.; Gladden, Herbert J.

    1990-01-01

    This paper describes the Hot Gas Facility, a unique, reliable, and cost-effective high-heat-flux facility for testing hypersonic engine components developed at the NASA Lewis Research Center. The Hot Gas Facility is capable of providing heat fluxes ranging from 200 Btu/sq ft per sec on flat surfaces up to 8000 Btu/sq ft per sec at a leading edge stagnation point. The usefulness of the Hot Gas Facility for the NASP community was demonstrated by testing hydrogen-cooled structures over a range of temperatures and pressures. Ranges of the Reynolds numbers, Prandtl numbers, enthalpy, and heat fluxes similar to those expected during hypersonic flights were achieved.

  4. Performance of thermal barrier coatings in high heat flux environments

    NASA Technical Reports Server (NTRS)

    Miller, R. A.; Berndt, C. C.

    1984-01-01

    Thermal barrier coatings were exposed to the high temperature and high heat flux produced by a 30 kW plasma torch. Analysis of the specimen heating rates indicates that the temperature drop across the thickness of the 0.038 cm ceramic layer was about 1100 C after 0.5 sec in the flame. An as-sprayed ZrO2-8%Y2O3 specimens survived 3000 of the 0.5 sec cycles with failing. Surface spalling was observed when 2.5 sec cycles were employed but this was attributed to uneven heating caused by surface roughness. This surface spalling was prevented by smoothing the surface with silicon carbide paper or by laser glazing. A coated specimen with no surface modification but which was heat treated in argon also did not surface spall. Heat treatment in air led to spalling in as early as 2 cycle from heating stresses. Failures at edges were investigated and shown to be a minor source of concern. Ceramic coatings formed from ZrO2-12%Y2O3 or ZrO2-20%Y2O3 were shown to be unsuited for use under the high heat flux conditions of this study.

  5. High-resolution hot-film measurement of surface heat flux to an impinging jet

    NASA Astrophysics Data System (ADS)

    O'Donovan, T. S.; Persoons, T.; Murray, D. B.

    2011-10-01

    To investigate the complex coupling between surface heat transfer and local fluid velocity in convective heat transfer, advanced techniques are required to measure the surface heat flux at high spatial and temporal resolution. Several established flow velocity techniques such as laser Doppler anemometry, particle image velocimetry and hot wire anemometry can measure fluid velocities at high spatial resolution (µm) and have a high-frequency response (up to 100 kHz) characteristic. Equivalent advanced surface heat transfer measurement techniques, however, are not available; even the latest advances in high speed thermal imaging do not offer equivalent data capture rates. The current research presents a method of measuring point surface heat flux with a hot film that is flush mounted on a heated flat surface. The film works in conjunction with a constant temperature anemometer which has a bandwidth of 100 kHz. The bandwidth of this technique therefore is likely to be in excess of more established surface heat flux measurement techniques. Although the frequency response of the sensor is not reported here, it is expected to be significantly less than 100 kHz due to its physical size and capacitance. To demonstrate the efficacy of the technique, a cooling impinging air jet is directed at the heated surface, and the power required to maintain the hot-film temperature is related to the local heat flux to the fluid air flow. The technique is validated experimentally using a more established surface heat flux measurement technique. The thermal performance of the sensor is also investigated numerically. It has been shown that, with some limitations, the measurement technique accurately measures the surface heat transfer to an impinging air jet with improved spatial resolution for a wide range of experimental parameters.

  6. Critical Heat Flux Phenomena at HighPressure & Low Mass Fluxes: NEUP Final Report Part I: Experiments

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Corradini, Michael; Wu, Qiao

    2015-04-30

    This report is a preliminary document presenting an overview of the Critical Heat Flux (CHF) phenomenon, the High Pressure Critical Heat Flux facility (HPCHF), preliminary CHF data acquired, and the future direction of the research. The HPCHF facility has been designed and built to study CHF at high pressure and low mass flux ranges in a rod bundle prototypical of conceptual Small Modular Reactor (SMR) designs. The rod bundle is comprised of four electrically heated rods in a 2x2 square rod bundle with a prototypic chopped-cosine axial power profile and equipped with thermocouples at various axial and circumferential positions embeddedmore » in each rod for CHF detection. Experimental test parameters for CHF detection range from pressures of ~80 – 160 bar, mass fluxes of ~400 – 1500 kg/m2s, and inlet water subcooling from ~30 – 70°C. The preliminary data base established will be further extended in the future along with comparisons to existing CHF correlations, models, etc. whose application ranges may be applicable to the conditions of SMRs.« less

  7. High-Heat-Flux Cyclic Durability of Thermal and Environmental Barrier Coatings

    NASA Technical Reports Server (NTRS)

    Zhu, Dongming; Ghosn, Louis L.; Miller, Robert A.

    2007-01-01

    Advanced ceramic thermal and environmental barrier coatings will play an increasingly important role in future gas turbine engines because of their ability to protect the engine components and further raise engine temperatures. For the supersonic vehicles currently envisioned in the NASA fundamental aeronautics program, advanced gas turbine engines will be used to provide high power density thrust during the extended supersonic flight of the aircraft, while meeting stringent low emission requirements. Advanced ceramic coating systems are critical to the performance, life and durability of the hot-section components of the engine systems. In this work, the laser and burner rig based high-heat-flux testing approaches were developed to investigate the coating cyclic response and failure mechanisms under simulated supersonic long-duration cruise mission. The accelerated coating cracking and delamination mechanism under the engine high-heat-flux, and extended supersonic cruise time conditions will be addressed. A coating life prediction framework may be realized by examining the crack initiation and propagation in conjunction with environmental degradation under high-heat-flux test conditions.

  8. A low-frequency wave motion mechanism enables efficient energy transport in carbon nanotubes at high heat fluxes.

    PubMed

    Zhang, Xiaoliang; Hu, Ming; Poulikakos, Dimos

    2012-07-11

    The great majority of investigations of thermal transport in carbon nanotubes (CNTs) in the open literature focus on low heat fluxes, that is, in the regime of validity of the Fourier heat conduction law. In this paper, by performing nonequilibrium molecular dynamics simulations we investigated thermal transport in a single-walled CNT bridging two Si slabs under constant high heat flux. An anomalous wave-like kinetic energy profile was observed, and a previously unexplored, wave-dominated energy transport mechanism is identified for high heat fluxes in CNTs, originated from excited low frequency transverse acoustic waves. The transported energy, in terms of a one-dimensional low frequency mechanical wave, is quantified as a function of the total heat flux applied and is compared to the energy transported by traditional Fourier heat conduction. The results show that the low frequency wave actually overtakes traditional Fourier heat conduction and efficiently transports the energy at high heat flux. Our findings reveal an important new mechanism for high heat flux energy transport in low-dimensional nanostructures, such as one-dimensional (1-D) nanotubes and nanowires, which could be very relevant to high heat flux dissipation such as in micro/nanoelectronics applications.

  9. Electromagnetic Control of High Heat-Flux Spray Impingement Boiling Under Microgravity Conditions

    DTIC Science & Technology

    2007-03-01

    impingement boiling ( Mudawar , 2000; Chow et al., 1997; Tilton, 1989). With water as the working fluid, spray cooling has achieved a heat flux on the...Stebbins, C. J., and Mudawar , I., 1996. "Mapping of Impact and Heat Transfer Regimes of Water Drops Impinging on a Polished Surface," Int. J. Heat and Mass...34 Proceedings of SAE 2004 Power Systems Conference, 2004-01-3204, Reno NV, November, pp. 309-317. Mudawar , 1., 2000. "Assessment of High-heat Flux

  10. Electron Heat Flux in Pressure Balance Structures at Ulysses

    NASA Technical Reports Server (NTRS)

    Yamauchi, Yohei; Suess, Steven T.; Sakurai, Takashi; Whitaker, Ann F. (Technical Monitor)

    2001-01-01

    Pressure balance structures (PBSs) are a common feature in the high-latitude solar wind near solar minimum. Rom previous studies, PBSs are believed to be remnants of coronal plumes and be related to network activity such as magnetic reconnection in the photosphere. We investigated the magnetic structures of the PBSs, applying a minimum variance analysis to Ulysses/Magnetometer data. At 2001 AGU Spring meeting, we reported that PBSs have structures like current sheets or plasmoids, and suggested that they are associated with network activity at the base of polar plumes. In this paper, we have analyzed high-energy electron data at Ulysses/SWOOPS to see whether bi-directional electron flow exists and confirm the conclusions more precisely. As a result, although most events show a typical flux directed away from the Sun, we have obtained evidence that some PBSs show bi-directional electron flux and others show an isotropic distribution of electron pitch angles. The evidence shows that plasmoids are flowing away from the Sun, changing their flow direction dynamically in a way not caused by Alfven waves. From this, we have concluded that PBSs are generated due to network activity at the base of polar plumes and their magnetic structures axe current sheets or plasmoids.

  11. Electron Heating and Acceleration from High Amplitude Driven Alfvén Waves in the LAPD

    NASA Astrophysics Data System (ADS)

    Auerbach, David; Carter, Troy; Brugman, Brian

    2006-10-01

    High amplitude (δB/B ˜1 %) shear Alfvén waves are generated in the Large Plasma Device Upgrade (LAPD) at UCLA, and elevated electron temperatures and high energy electrons are observed using triple probes and Langmuir current traces. The Poynting flux of the observed waves is calculated, and wave power is compared to estimates of power input required to cause the observed heating. Theoretical calculations of power transfer from wave to plasma due to Landau damping and collisional heating are also presented and compared to experimental measurements. Heating by antenna near field effects is also being explored. The density and potential structures of these waves are explored using interferometer and triple probe measurements. Applications to Auroral generation and plasma heating are discussed.

  12. GRCop-84: A High Temperature Copper-based Alloy For High Heat Flux Applications

    NASA Technical Reports Server (NTRS)

    Ellis, David L.

    2005-01-01

    While designed for rocket engine main combustion chamber liners, GRCop-84 (Cu-8 at.% Cr-4 at.% Nb) offers potential for high heat flux applications in industrial applications requiring a temperature capability up to approximately 700 C (1292 F). GRCop-84 is a copper-based alloy with excellent elevated temperature strength, good creep resistance, long LCF lives and enhanced oxidation resistance. It also has a lower thermal expansion than copper and many other low alloy copper-based alloys. GRCop-84 can be manufactured into a variety of shapes such as tubing, bar, plate and sheet using standard production techniques and requires no special production techniques. GRCop-84 forms well, so conventional fabrication methods including stamping and bending can be used. GRCop-84 has demonstrated an ability to be friction stir welded, brazed, inertia welded, diffusion bonded and electron beam welded for joining to itself and other materials. Potential applications include plastic injection molds, resistance welding electrodes and holders, permanent metal casting molds, vacuum plasma spray nozzles and high temperature heat exchanger applications.

  13. Quasi-passive heat sink for high-power laser diodes

    NASA Astrophysics Data System (ADS)

    Vetrovec, John

    2009-02-01

    We report on a novel heat sink for high-power laser diodes offering unparalleled capacity in high-heat flux handling and temperature control. The heat sink uses a liquid coolant flowing at high speed in a miniature closed and sealed loop. Diode waste heat is received at high flux and transferred to environment, coolant fluid, heat pipe, or structure at a reduced flux. When pumping solid-state or alkali vapor lasers, diode wavelength can be electronically tuned to the absorption features of the laser gain medium. This paper presents the heat sink physics, engineering design, performance modeling, and configurations.

  14. Thermal management of high heat flux electronic components in space and aircraft systems, phase 1

    NASA Astrophysics Data System (ADS)

    Iversen, Arthur H.

    1991-03-01

    The objectives of this Phase 1 program were to analyze, design, construct and demonstrate the application of curved surface cooling to power devices with the goal of demonstrating greater than 200 W/sq cm chip dissipation while maintaining junction temperatures within specification. Major components of the experiment comprised the test fixture for mounting the device under test and the cooling loop equipment and instrumentation. The work conducted in this Phase 1 study was to establish the basic parameters for the design of an entire class of efficient, compact, lightweight and cost competitive power conversion/conditioning systems for space, aircraft and general DOD requirements. This has been accomplished. Chip power dissipation of greater than 400 W/sq cm was demonstrated, and a general packaging and the thermal management design has been devised to meet the above requirements. The power limit reached was dictated by the junction temperature and not power dissipation, i.e., critical heat flux. The key to the packaging design is a basic construction concept that provides low junction to fluid thermal resistance. High heat flux dissipation without low thermal resistance is useless because excessive junction temperatures will results.

  15. Hypersonic engine component experiments in high heat flux, supersonic flow environment

    NASA Technical Reports Server (NTRS)

    Gladden, Herbert J.; Melis, Matthew E.

    1993-01-01

    A major concern in advancing the state-of-the-art technologies for hypersonic vehicles is the development of an aeropropulsion system capable of withstanding the sustained high thermal loads expected during hypersonic flight. Even though progress has been made in the computational understanding of fluid dynamics and the physics/chemistry of high speed flight, there is also a need for experimental facilities capable of providing a high heat flux environment for testing component concepts and verifying/calibrating these analyses. A hydrogen/oxygen rocket engine heat source was developed at the NASA Lewis Research Center as one element in a series of facilities at national laboratories designed to fulfill this need. This 'Hot Gas Facility' is capable of providing heat fluxes up to 450 w/sq cm on flat surfaces and up to 5,000 w/sq cm at the leading edge stagnation point of a strut in a supersonic flow stream. Gas temperatures up to 3050 K can also be attained. Two recent experimental programs conducted in this facility are discussed. The objective of the first experiment is to evaluate the erosion and oxidation characteristics of a coating on a cowl leading edge (or strut leading edge) in a supersonic, high heat flux environment. Macrophotographic data from a coated leading edge model show progressive degradation over several thermal cycles at aerothermal conditions representative of high Mach number flight. The objective of the second experiment is to assess the capability of cooling a porous surface exposed to a high temperature, high velocity flow environment and to provide a heat transfer data base for a design procedure. Experimental results from transpiration cooled surfaces in a supersonic flow environment are presented.

  16. Integrated computational study of ultra-high heat flux cooling using cryogenic micro-solid nitrogen spray

    NASA Astrophysics Data System (ADS)

    Ishimoto, Jun; Oh, U.; Tan, Daisuke

    2012-10-01

    A new type of ultra-high heat flux cooling system using the atomized spray of cryogenic micro-solid nitrogen (SN2) particles produced by a superadiabatic two-fluid nozzle was developed and numerically investigated for application to next generation super computer processor thermal management. The fundamental characteristics of heat transfer and cooling performance of micro-solid nitrogen particulate spray impinging on a heated substrate were numerically investigated and experimentally measured by a new type of integrated computational-experimental technique. The employed Computational Fluid Dynamics (CFD) analysis based on the Euler-Lagrange model is focused on the cryogenic spray behavior of atomized particulate micro-solid nitrogen and also on its ultra-high heat flux cooling characteristics. Based on the numerically predicted performance, a new type of cryogenic spray cooling technique for application to a ultra-high heat power density device was developed. In the present integrated computation, it is clarified that the cryogenic micro-solid spray cooling characteristics are affected by several factors of the heat transfer process of micro-solid spray which impinges on heated surface as well as by atomization behavior of micro-solid particles. When micro-SN2 spraying cooling was used, an ultra-high cooling heat flux level was achieved during operation, a better cooling performance than that with liquid nitrogen (LN2) spray cooling. As micro-SN2 cooling has the advantage of direct latent heat transport which avoids the film boiling state, the ultra-short time scale heat transfer in a thin boundary layer is more possible than in LN2 spray. The present numerical prediction of the micro-SN2 spray cooling heat flux profile can reasonably reproduce the measurement results of cooling wall heat flux profiles. The application of micro-solid spray as a refrigerant for next generation computer processors is anticipated, and its ultra-high heat flux technology is expected

  17. Miniature high temperature plug-type heat flux gauges

    NASA Technical Reports Server (NTRS)

    Liebert, Curt H.

    1992-01-01

    The objective is to describe continuing efforts to develop methods for measuring surface heat flux, gauge active surface temperature, and heat transfer coefficient quantities. The methodology involves inventing a procedure for fabricating improved plug-type heat flux gauges and also for formulating inverse heat conduction models and calculation procedures. These models and procedures are required for making indirect measurements of these quantities from direct temperature measurements at gauge interior locations. Measurements of these quantities were made in a turbine blade thermal cycling tester (TBT) located at MSFC. The TBT partially simulates the turbopump turbine environment in the Space Shuttle Main Engine. After the TBT test, experiments were performed in an arc lamp to analyze gauge quality.

  18. High temperature thermocouple and heat flux gauge using a unique thin film-hardware hot juncture

    NASA Technical Reports Server (NTRS)

    Liebert, C. H.; Holanda, R.; Hippensteele, S. A.; Andracchio, C. A.

    1984-01-01

    A special thin film-hardware material thermocouple (TC) and heat flux gauge concept for a reasonably high temperature and high flux flat plate heat transfer experiment was fabricated and tested to gauge temperatures of 911 K. This concept was developed for minimal disturbance of boundary layer temperature and flow over the plates and minimal disturbance of heat flux through the plates. Comparison of special heat flux gauge Stanton number output at steady-state conditions with benchmark literature data was good and agreement was within a calculated uncertainty of the measurement system. Also, good agreement of special TC and standard TC outputs was obtained and the results are encouraging. Oxidation of thin film thermoelements was a primary failure mode after about 5 of operation.

  19. High-temperature thermocouple and heat flux gauge using a unique thin film-hardware hot junction

    NASA Technical Reports Server (NTRS)

    Liebert, C. H.; Holanda, R.; Hippensteele, S. A.; Andracchio, C. A.

    1985-01-01

    A special thin film-hardware material thermocouple (TC) and heat flux gauge concept for a reasonably high temperature and high flux flat plate heat transfer experiment was fabricated and tested to gauge temperatures of 911 K. This concept was developed for minimal disturbance of boundary layer temperature and flow over the plates and minimal disturbance of heat flux through the plates. Comparison of special heat flux gauge Stanton number output at steady-state conditions with benchmark literature data was good and agreement was within a calculated uncertainty of the measurement system. Also, good agreement of special TC and standard TC outputs was obtained and the results are encouraging. Oxidation of thin film thermoelements was a primary failure mode after about 5 of operation.

  20. Monitoring Delamination of Thermal Barrier Coatings During Interrupted High-Heat-Flux Laser Testing using Luminescence Imaging

    NASA Technical Reports Server (NTRS)

    Eldridge, Jeffrey I.; Zhu, Dongming; Wolfe, Douglas E.

    2011-01-01

    This presentation showed progress made in extending luminescence-base delamination monitoring to TBCs exposed to high heat fluxes, which is an environment that much better simulates actual turbine engine conditions. This was done by performing upconversion luminescence imaging during interruptions in laser testing, where a high-power CO2 laser was employed to create the desired heat flux. Upconverison luminescence refers to luminescence where the emission is at a higher energy (shorter wavelength) than the excitation. Since there will be negligible background emission at higher energies than the excitation, this methods produces superb contrast. Delamination contrast is produced because both the excitation and emission wavelengths are reflected at delamination cracks so that substantially higher luminescence intensity is observed in regions containing delamination cracks. Erbium was selected as the dopant for luminescence specifically because it exhibits upconversion luminescence. The high power CO2 10.6 micron wavelength laser facility at NASA GRC was used to produce the heat flux in combination with forced air backside cooling. Testing was performed at a lower (95 W/sq cm) and higher (125 W/sq cm) heat flux as well as furnace cycling at 1163C for comparison. The lower heat flux showed the same general behavior as furnace cycling, a gradual, "spotty" increase in luminescence associated with debond progression; however, a significant difference was a pronounced incubation period followed by acceleration delamination progression. These results indicate that extrapolating behavior from furnace cycling measurements will grossly overestimate remaining life under high heat flux conditions. The higher heat flux results were not only accelerated, but much different in character. Extreme bond coat rumpling occurred, and delamination propagation extended over much larger areas before precipitating macroscopic TBC failure. This indicates that under the higher heat flux (and

  1. Sensors for Metering Heat Flux Area Density and Metrological Equipment for the Heat Flux Density Measurement

    NASA Astrophysics Data System (ADS)

    Doronin, D. O.

    2018-04-01

    The demand in measuring and studies of heat conduction of various media is very urgent now. This article considers the problem of heat conduction monitoring and measurement in various media and materials in any industries and branches of science as well as metrological support of the heat flux measurement equipment. The main study objects are both the sensors manufactured and facilities onto which these sensors will be installed: different cladding structures of the buildings, awnings, rocket fairings, boiler units, internal combustion engines. The Company develops and manufactures different types of heat flux sensors: thermocouple, thin-film, heterogeneous gradient as well as metrological equipment for the gauging calibration of the heat flux density measurement. The calibration shall be performed using both referencing method in the unit and by fixed setting of the heat flux in the unit. To manufacture heterogeneous heat flux gradient sensors (HHFGS) the Company developed and designed a number of units: diffusion welding unit, HHFGS cutting unit. Rather good quality HHFGS prototypes were obtained. At this stage the factory tests on the equipment for the heat flux density measurement equipment are planned. A high-sensitivity heat flux sensor was produced, now it is tested at the Construction Physics Research Institute (Moscow). It became possible to create thin-film heat flux sensors with the sensitivity not worse than that of the sensors manufactured by Captec Company (France). The Company has sufficient premises to supply the market with a wide range of sensors, to master new sensor manufacture technologies which will enable their application range.

  2. Latent Heat in Soil Heat Flux Measurements

    USDA-ARS?s Scientific Manuscript database

    The surface energy balance includes a term for soil heat flux. Soil heat flux is difficult to measure because it includes conduction and convection heat transfer processes. Accurate representation of soil heat flux is an important consideration in many modeling and measurement applications. Yet, the...

  3. Classical Heat-Flux Measurements in Coronal Plasmas from Collective Thomson-Scattering Spectra

    NASA Astrophysics Data System (ADS)

    Henchen, R. J.; Hu, S. X.; Katz, J.; Froula, D. H.; Rozmus, W.

    2016-10-01

    Collective Thomson scattering was used to measure heat flux in coronal plasmas. The relative amplitude of the Thomson-scattered power into the up- and downshifted electron plasma wave features was used to determine the flux of electrons moving along the temperature gradient at three to four times the electron thermal velocity. Simultaneously, the ion-acoustic wave features were measured. Their relative amplitude was used to measure the flux of the return-current electrons. The frequencies of these ion-acoustic and electron plasma wave features provide local measurements of the electron temperature and density. These spectra were obtained at five locations along the temperature gradient in a laser-produced blowoff plasma. These measurements of plasma parameters are used to infer the Spitzer-Härm flux (qSH = - κ∇Te ) and are in good agreement with the values of the heat flux measured from the scattering-feature asymmetries. Additional experiments probed plasma waves perpendicular to the temperature gradient. The data show small effects resulting from heat flux compared to probing waves along the temperature gradient. This material is based upon work supported by the Department of Energy National Nuclear Security Administration under Award Number DE-NA0001944.

  4. Development of advanced high-temperature heat flux sensors

    NASA Technical Reports Server (NTRS)

    Atkinson, W. H.; Strange, R. R.

    1982-01-01

    Various configurations of high temperature, heat flux sensors were studied to determine their suitability for use in experimental combustor liners of advanced aircraft gas turbine engines. It was determined that embedded thermocouple sensors, laminated sensors, and Gardon gauge sensors, were the most viable candidates. Sensors of all three types were fabricated, calibrated, and endurance tested. All three types of sensors met the fabricability survivability, and accuracy requirements established for their application.

  5. Effects of heat/citric acid reprocessing on high-flux polysulfone dialyzers.

    PubMed

    Cornelius, Rena M; McClung, W Glenn; Richardson, Robert M A; Estridge, Charles; Plaskos, Nicholas; Yip, Christopher M; Brash, John L

    2002-01-01

    The surface features, morphology, and tensile properties of fibers obtained from pristine, reprocessed, and reused Fresenius Polysulfone High-Flux (Hemoflow F80A) hemodialyzers have been studied. Scanning electron microscopy of the dialyzer fibers revealed a dense skin layer on the inner surface of the membrane and a relatively thick porous layer on the outer surface. Transmission electron microscopy and atomic force microscopy showed an alteration in membrane morphology due to reprocessing and reuse, or to a deposition of blood-borne material on the membrane that is not removed with reprocessing. Fluorescent microscopy images also showed that a fluorescent material not removed by heat/citric acid reprocessing builds up with continued use of the dialyzers. The tensile properties of the dialyzer fibers were not affected by the heat/citric acid reprocessing procedure. The protein layers formed on pristine and reused hemodialyzer membranes during clinical use were also studied using sodium dodecyl sulfate polyacrylamide gel electrophoresis and immunoblotting. A considerable amount of protein was found on the blood side of single and multiple use dialyzers. Proteins adsorbed on the dialysate side of the membrane were predominantly in the molecular weight region below 30 kDa. Little protein was detected on the membranes of reprocessed hemodialyzers.

  6. Heat flux viscosity in collisional magnetized plasmas

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Liu, C., E-mail: cliu@pppl.gov; Fox, W.; Bhattacharjee, A.

    2015-05-15

    Momentum transport in collisional magnetized plasmas due to gradients in the heat flux, a “heat flux viscosity,” is demonstrated. Even though no net particle flux is associated with a heat flux, in a plasma there can still be momentum transport owing to the velocity dependence of the Coulomb collision frequency, analogous to the thermal force. This heat-flux viscosity may play an important role in numerous plasma environments, in particular, in strongly driven high-energy-density plasma, where strong heat flux can dominate over ordinary plasma flows. The heat flux viscosity can influence the dynamics of the magnetic field in plasmas through themore » generalized Ohm's law and may therefore play an important role as a dissipation mechanism allowing magnetic field line reconnection. The heat flux viscosity is calculated directly using the finite-difference method of Epperlein and Haines [Phys. Fluids 29, 1029 (1986)], which is shown to be more accurate than Braginskii's method [S. I. Braginskii, Rev. Plasma Phys. 1, 205 (1965)], and confirmed with one-dimensional collisional particle-in-cell simulations. The resulting transport coefficients are tabulated for ease of application.« less

  7. Single-side conduction modeling for high heat flux coolant channels

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Boyd, R.D. Sr.

    In the development of plasma-facing components (PFCs), most investigators have erroneously postulated negligible water critical heat flux dependence on the coolant channel length-to-diameter (L/D) ratio above a constant value of L/D. Although encouraging results have been obtained in characterizing peaking factors for local two-dimensional boiling curves and critical heat flux, additional experimental data and theoretical model development are needed to validate the applicability to PFCs. Both these and related issues will affect the flow boiling correlation and data reduction associated with the development of PFCs for fusion reactors and other physical problems that are dependent on conduction modeling in themore » heat flux spectrum of applications. Both exact solutions and numerical conjugate analyses are presented for a one-side heated (OSH) geometry. The results show (a) the coexistence of three flow regimes inside an OSH circular geometry, (b) the correlational dependence of the inside wall heat flux and temperature, and (c) inaccuracies that could arise in some data reduction procedures.« less

  8. Quantitative method for measuring heat flux emitted from a cryogenic object

    DOEpatents

    Duncan, Robert V.

    1993-01-01

    The present invention is a quantitative method for measuring the total heat flux, and of deriving the total power dissipation, of a heat-fluxing object which includes the steps of placing an electrical noise-emitting heat-fluxing object in a liquid helium bath and measuring the superfluid transition temperature of the bath. The temperature of the liquid helium bath is thereafter reduced until some measurable parameter, such as the electrical noise, exhibited by the heat-fluxing object or a temperature-dependent resistive thin film in intimate contact with the heat-fluxing object, becomes greatly reduced. The temperature of the liquid helum bath is measured at this point. The difference between the superfluid transition temperature of the liquid helium bath surrounding the heat-fluxing object, and the temperature of the liquid helium bath when the electrical noise emitted by the heat-fluxing object becomes greatly reduced, is determined. The total heat flux from the heat-fluxing object is determined as a function of this difference between these temperatures. In certain applications, the technique can be used to optimize thermal design parameters of cryogenic electronics, for example, Josephson junction and infra-red sensing devices.

  9. Quantitative method for measuring heat flux emitted from a cryogenic object

    DOEpatents

    Duncan, R.V.

    1993-03-16

    The present invention is a quantitative method for measuring the total heat flux, and of deriving the total power dissipation, of a heat-fluxing object which includes the steps of placing an electrical noise-emitting heat-fluxing object in a liquid helium bath and measuring the superfluid transition temperature of the bath. The temperature of the liquid helium bath is thereafter reduced until some measurable parameter, such as the electrical noise, exhibited by the heat-fluxing object or a temperature-dependent resistive thin film in intimate contact with the heat-fluxing object, becomes greatly reduced. The temperature of the liquid helum bath is measured at this point. The difference between the superfluid transition temperature of the liquid helium bath surrounding the heat-fluxing object, and the temperature of the liquid helium bath when the electrical noise emitted by the heat-fluxing object becomes greatly reduced, is determined. The total heat flux from the heat-fluxing object is determined as a function of this difference between these temperatures. In certain applications, the technique can be used to optimize thermal design parameters of cryogenic electronics, for example, Josephson junction and infrared sensing devices.

  10. Miniature Convection Cooled Plug-type Heat Flux Gauges

    NASA Technical Reports Server (NTRS)

    Liebert, Curt H.

    1994-01-01

    Tests and analysis of a new miniature plug-type heat flux gauge configuration are described. This gauge can simultaneously measure heat flux on two opposed active surfaces when heat flux levels are equal to or greater than about 0.2 MW/m(sup 2). The performance of this dual active surface gauge was investigated over a wide transient and steady heat flux and temperature range. The tests were performed by radiatively heating the front surface with an argon arc lamp while the back surface was convection cooled with air. Accuracy is about +20 percent. The gauge is responsive to fast heat flux transients and is designed to withstand the high temperature (1300 K), high pressure (15 MPa), erosive and corrosive environments in modern engines. This gauge can be used to measure heat flux on the surfaces of internally cooled apparatus such as turbine blades and combustors used in jet propulsion systems and on the surfaces of hypersonic vehicles. Heat flux measurement accuracy is not compromised when design considerations call for various size gauges to be fabricated into alloys of various shapes and properties. Significant gauge temperature reductions (120 K), which can lead to potential gauge durability improvement, were obtained when the gauges were air-cooled by forced convection.

  11. Heat flux microsensor measurements and calibrations

    NASA Technical Reports Server (NTRS)

    Terrell, James P.; Hager, Jon M.; Onishi, Shinzo; Diller, Thomas E.

    1992-01-01

    A new thin-film heat flux gage has been fabricated specifically for severe high temperature operation using platinum and platinum-10 percent rhodium for the thermocouple elements. Radiation calibrations of this gage were performed at the AEDC facility over the available heat flux range (approx. 1.0 - 1,000 W/cu cm). The gage output was linear with heat flux with a slight increase in sensitivity with increasing surface temperature. Survivability of gages was demonstrated in quench tests from 500 C into liquid nitrogen. Successful operation of gages to surface temperatures of 750 C has been achieved. No additional cooling of the gages is required because the gages are always at the same temperature as the substrate material. A video of oxyacetylene flame tests with real-time heat flux and temperature output is available.

  12. Pyrolytic graphite gauge for measuring heat flux

    NASA Technical Reports Server (NTRS)

    Bunker, Robert C. (Inventor); Ewing, Mark E. (Inventor); Shipley, John L. (Inventor)

    2002-01-01

    A gauge for measuring heat flux, especially heat flux encountered in a high temperature environment, is provided. The gauge includes at least one thermocouple and an anisotropic pyrolytic graphite body that covers at least part of, and optionally encases the thermocouple. Heat flux is incident on the anisotropic pyrolytic graphite body by arranging the gauge so that the gauge surface on which convective and radiative fluxes are incident is perpendicular to the basal planes of the pyrolytic graphite. The conductivity of the pyrolytic graphite permits energy, transferred into the pyrolytic graphite body in the form of heat flux on the incident (or facing) surface, to be quickly distributed through the entire pyrolytic graphite body, resulting in small substantially instantaneous temperature gradients. Temperature changes to the body can thereby be measured by the thermocouple, and reduced to quantify the heat flux incident to the body.

  13. Design and performance of vacuum system for high heat flux test facility

    NASA Astrophysics Data System (ADS)

    Swamy Kidambi, Rajamannar; Mokaria, Prakash; Khirwadkar, Samir; Belsare, Sunil; Khan, M. S.; Patel, Tushar; Krishnan, Deepu S.

    2017-04-01

    High heat flux test facility (HHFTF) at IPR is used for testing thermal performance of plasma facing materials or components. It consists of various subsystems like vacuum system, high power electron beam system, diagnostic and calibration system, data acquisition and control system and high pressure high temperature water circulation system. Vacuum system consists of large D-shaped chamber, target handling system, pumping systems and support structure. The net volume of vacuum chamber is 5 m3 was maintained at the base pressure of the order of 10-6 mbar for operation of electron gun with minimum beam diameter which is achieved with turbo-molecular pump (TMP) and cryo pump. A variable conductance gate valve is used for maintaining required vacuum in the chamber. Initial pumping of the chamber was carried out by using suitable rotary and root pumps. PXI and PLC based faster real time data acquisition and control system is implemented for performing the various operations like remote operation, online vacuum data measurements, display and status indication of all vacuum equipments. This paper describes in detail the design and implementation of various vacuum system for HHFTF.

  14. Electron-phonon mediated heat flow in disordered graphene

    NASA Astrophysics Data System (ADS)

    Chen, Wei; Clerk, Aashish A.

    2012-09-01

    We calculate the heat flux and electron-phonon thermal conductance in a disordered graphene sheet, going beyond a Fermi’s golden rule approach to fully account for the modification of the electron-phonon interaction by disorder. Using the Keldysh technique combined with standard impurity averaging methods in the regime kFl≫1 (where kF is the Fermi wave vector and l is the mean free path), we consider both scalar potential (i.e., deformation potential) and vector-potential couplings between electrons and phonons. We also consider the effects of electronic screening at the Thomas-Fermi level. We find that the temperature dependence of the heat flux and thermal conductance is sensitive to the presence of disorder and screening, and reflects the underlying chiral nature of electrons in graphene and the corresponding modification of their diffusive behavior. In the case of weak screening, disorder enhances the low-temperature heat flux over the clean system (changing the associated power law from T4 to T3), and the deformation potential dominates. For strong screening, both the deformation potential and vector-potential couplings make comparable contributions, and the low-temperature heat flux obeys a T5 power law.

  15. Latent heat sink in soil heat flux measurements

    USDA-ARS?s Scientific Manuscript database

    The surface energy balance includes a term for soil heat flux. Soil heat flux is difficult to measure because it includes conduction and convection heat transfer processes. Accurate representation of soil heat flux is an important consideration in many modeling and measurement applications. Yet, the...

  16. Heat flux microsensor measurements

    NASA Technical Reports Server (NTRS)

    Terrell, J. P.; Hager, J. M.; Onishi, S.; Diller, T. E.

    1992-01-01

    A thin-film heat flux sensor has been fabricated on a stainless steel substrate. The thermocouple elements of the heat flux sensor were nickel and nichrome, and the temperature resistance sensor was platinum. The completed heat flux microsensor was calibrated at the AEDC radiation facility. The gage output was linear with heat flux with no apparent temperature effect on sensitivity. The gage was used for heat flux measurements at the NASA Langley Vitiated Air Test Facility. Vitiated air was expanded to Mach 3.0 and hydrogen fuel was injected. Measurements were made on the wall of a diverging duct downstream of the injector during all stages of the hydrogen combustion tests. Because the wall and the gage were not actively cooled, the wall temperature reached over 1000 C (1900 F) during the most severe test.

  17. Heat fluxes across the Antarctic Circumpolar Current

    NASA Astrophysics Data System (ADS)

    Ferrari, Ramiro; Provost, Christine; Hyang Park, Young; Sennéchael, Nathalie; Garric, Gilles; Bourdallé-Badie, Romain

    2014-05-01

    Determining the processes responsible for the Southern Ocean heat balance is fundamental to our understanding of the weather and climate systems. Therefore, in the last decades, various studies aimed at analyzing the major mechanisms of the oceanic poleward heat flux in this region. Previous works stipulated that the cross-stream heat flux due to the mesoscale transient eddies was responsible for the total meridional heat transport across the Antarctic Circumpolar Current (ACC). Several numerical modelling and current meters data studies have recently challenged this idea. These showed that the heat flux due to the mean flow in the southern part of the Antarctic Circumpolar Current could be larger than the eddy heat flux contribution by two orders of magnitude. Eddy heat flux and heat flux by the mean flow distributions of were examined in Drake Passage using in situ measurements collected during the DRAKE 2006-9 project (from January 2006 to March 2009), available observations from the historical DRAKE 79 experiment and high resolution model outputs (ORCA 12, MERCATOR). The Drake Passage estimations provided a limited view of heat transport in the Southern Ocean. The small spatial scales shown by the model derived heat flux by the mean flow indicate that circumpolar extrapolations from a single point observation are perilous. The importance of the heat flux due by the mean flow should be further investigated using other in situ observations and numerical model outputs. Similar situation has been observed, with important implication for heat flux due to the mean flow, in other topographically constricted regions with strong flow across prominent submarine ridges (choke points). We have estimated the heat flux due to the mean flow revisiting other ACC mooring sites where in situ time series are available, e.g. south of Australia (Tasmania) (Phillips and Rintoul, 2000), southeast of New Zealand (Campbell Plateau) (Bryden and Heath, 1985). Heat fluxes due to the mean

  18. Behavior of Brazed W/Cu Mockup Under High Heat Flux Loads

    NASA Astrophysics Data System (ADS)

    Chen, Lei; Lian, Youyun; Liu, Xiang

    2014-03-01

    In order to transfer the heat from the armor to the coolant, tungsten has to be connected with a copper heat sink. The joint technology is the most critical issue for manufacturing plasma facing components. Consequently, the reliability of the joints should be verified by a great number of high-heat-flux (HHF) tests to simulate the real load conditions. W/Cu brazed joint technology with sliver free filler metal CuMnNi has been developed at Southwestern Institute of Physics (SWIP). Screening and thermal fatigue tests of one small-scale flat tile W/CuCrZr mockup were performed on a 60 kW electron-beam Material testing scenario (EMS-60) constructed recently at SWIP. The module successfully survived screening test with the absorbed power density (Pabs) of 2 MW/m2 to 10 MW/m2 and the following 1000 cycles at Pabs of 7.2 MW/m2 without hot spots and overheating zones during the whole test campaign. Metallurgy and SEM observations did not find any cracks at both sides and the interface, indicating a good bonding of W and CuCrZr alloy. In addition, finite element simulations by ANSYS 12.0 under experimental load conditions were performed and compared with experimental results.

  19. Momentum transport and non-local transport in heat-flux-driven magnetic reconnection in HEDP

    NASA Astrophysics Data System (ADS)

    Liu, Chang; Fox, Will; Bhattacharjee, Amitava

    2016-10-01

    Strong magnetic fields are readily generated in high-energy-density plasmas and can affect the heat confinement properties of the plasma. Magnetic reconnection can in turn be important as an inverse process, which destroys or reconfigures the magnetic field. Recent theory has demonstrated a novel physics regime for reconnection in high-energy-density plasmas where the magnetic field is advected into the reconnection layer by plasma heat flux via the Nernst effect. In this work we elucidate the physics of the electron dissipation layer in this heat-flux-driven regime. Through fully kinetic simulation and a new generalized Ohm's law, we show that momentum transport due to the heat-flux-viscosity effect provides the dissipation mechanism to allow magnetic field line reconnection. Scaling analysis and simulations show that the characteristic width of the current sheet in this regime is several electron mean-free-paths. These results additionally show a coupling between non-local transport and momentum transport, which in turn affects the dynamics of the magnetic field. This work was supported by the U.S. Department of Energy under Contract No. DE-SC0008655.

  20. Measurements of plasma sheath heat flux in the Alcator C-Mod divertor

    NASA Astrophysics Data System (ADS)

    Brunner, Dan; Labombard, Brian; Terry, Jim; Reinke, Matt

    2010-11-01

    Heat flux is one of the most important parameters controlling the lifetime of first-wall components in fusion experiments and reactors. The sheath heat flux coefficient (γ) is a parameter relating heat flux (from a plasma to a material surface) to the electron temperature and ion saturation current. Being such a simple expression for a kinetic process, it is of great interest to plasma edge fluid modelers. Under the assumptions of equal ion and electron temperatures, no secondary electron emission, and no net current to the surface the value of γ is approximately 7 [1]. Alcator C-Mod provides a unique opportunity among today's experiments to measure reactor-relevant heat fluxes (100's of MW/m^2 parallel to the magnetic field) in reactor-like divertor geometry. Motivated by the DoE 2010 joint milestone to measure heat flux footprints, the lower outer divertor of Alcator has been instrumented with a suite of Langmuir probes, novel surface thermocouples, and calorimeters in tiles purposefully ramped to eliminate shadowing; all within view of an IR camera. Initial results indicate that the experimentally inferred values of γ are found to agree with simple theory in the sheath limited regime and diverges to lower values as the density increases.

  1. Heat deposition analysis for the High Flux Isotope Reactor’s HEU and LEU core models

    DOE PAGES

    Davidson, Eva E.; Betzler, Benjamin R.; Chandler, David; ...

    2017-08-01

    The High Flux Isotope Reactor at Oak Ridge National Laboratory is an 85 MW th pressurized light-water-cooled and -moderated flux-trap type research reactor. The reactor is used to conduct numerous experiments, advancing various scientific and engineering disciplines. As part of an ongoing program sponsored by the US Department of Energy National Nuclear Security Administration Office of Material Management and Minimization, studies are being performed to assess the feasibility of converting the reactor’s highly enriched uranium fuel to low-enriched uranium fuel. To support this conversion project, reference models with representative experiment target loading and explicit fuel plate representation were developed andmore » benchmarked for both fuels to (1) allow for consistent comparison between designs for both fuel types and (2) assess the potential impact of low-enriched uranium conversion. These high-fidelity models were used to conduct heat deposition analyses at the beginning and end of the reactor cycle and are presented herein. This article (1) discusses the High Flux Isotope Reactor models developed to facilitate detailed heat deposition analyses of the reactor’s highly enriched and low-enriched uranium cores, (2) examines the computational approach for performing heat deposition analysis, which includes a discussion on the methodology for calculating the amount of energy released per fission, heating rates, power and volumetric heating rates, and (3) provides results calculated throughout various regions of the highly enriched and low-enriched uranium core at the beginning and end of the reactor cycle. These are the first detailed high-fidelity heat deposition analyses for the High Flux Isotope Reactor’s highly enriched and low-enriched core models with explicit fuel plate representation. Lastly, these analyses are used to compare heat distributions obtained for both fuel designs at the beginning and end of the reactor cycle, and they are essential

  2. Quasi-exospheric heat flux of solar-wind electrons

    NASA Technical Reports Server (NTRS)

    Eviatar, A.; Schultz, M.

    1975-01-01

    Density, bulk-velocity, and heat-flow moments are calculated for truncated Maxwellian distributions representing the cool and hot populations of solar-wind electrons, as realized at the base of a hypothetical exosphere. The electrostatic potential is thus calculated by requiring charge quasi-neutrality and the absence of electrical current. Plasma-kinetic coupling of the cool-electron and proton bulk velocities leads to an increase in the electrostatic potential and a decrease in the heat-flow moment.

  3. High Heat Flux Surface Coke Deposition and Removal Assessment

    DTIC Science & Technology

    2015-01-01

    Technical Paper 3. DATES COVERED (From - To) January 2015- May 2015 4. TITLE AND SUBTITLE High Heat Flux Surface Coke Deposition and Removal Assessment... coke ) form. Coke has a much lower thermal conductivity than copper - thicknesses of only a few millionths of an inch can cause liner temperatures to...increase to dangerous levels. Moreover, reusing launch vehicles and main engines increases the likelihood that unsafe levels of coke will be

  4. Investigation of Instabilities and Heat Transfer Phenomena in Supercritical Fuels at High Heat Flux and Temperatures

    NASA Technical Reports Server (NTRS)

    Linne, Diane L.; Meyer, Michael L.; Braun, Donald C.; Keller, Dennis J.

    2000-01-01

    A series of heated tube experiments was performed to investigate fluid instabilities that occur during heating of supercritical fluids. In these tests, JP-7 flowed vertically through small diameter tubes at supercritical pressures. Test section heated length, diameter, mass flow rate, inlet temperature, and heat flux were varied in an effort to determine the range of conditions that trigger the instabilities. Heat flux was varied up to 4 BTU/sq in./s, and test section wall temperatures reached as high as 1950 F. A statistical model was generated to explain the trends and effects of the control variables. The model included no direct linear effect of heat flux on the occurrence of the instabilities. All terms involving inlet temperature were negative, and all terms involving mass flow rate were positive. Multiple tests at conditions that produced instabilities provided inconsistent results. These inconsistencies limit the use of the model as a predictive tool. Physical variables that had been previously postulated to control the onset of the instabilities, such as film temperature, velocity, buoyancy, and wall-to-bulk temperature ratio, were evaluated here. Film temperatures at or near critical occurred during both stable and unstable tests. All tests at the highest velocity were stable, but there was no functional relationship found between the instabilities and velocity, or a combination of velocity and temperature ratio. Finally, all of the unstable tests had significant buoyancy at the inlet of the test section, but many stable tests also had significant buoyancy forces.

  5. Heat flux modeling using ion drift effects in DIII-D H-mode plasmas with resonant magnetic perturbations

    DOE PAGES

    Wingen, Andreas; Schmitz, Oliver; Evans, Todd E.; ...

    2014-01-01

    The heat flux patterns measured in low-collisionality DIII-D H-mode plasmas strongly deviate from simultaneously measured CII emission patterns, used as indicator of particle flux, during applied resonant magnetic perturbations. While the CII emission clearly shows typical striations, which are similar to magnetic footprint patterns obtained from vacuum field line tracing, the heat flux is usually dominated by one large peak at the strike point position. The vacuum approximation, which only considers applied magnetic fields and neglects plasma response and plasma effects, cannot explain the shape of the observed heat flux pattern. One possible explanation is the effect of particle drifts.more » This is included in the field line equations and the results are discussed with reference to the measurement. Electrons and ions show di fferent drift motions at thermal energy levels in a guiding center approximation. While electrons hardly deviate from the field lines, ions can drift several centimetres away from field line flux surfaces. A model is presented in which an ion heat flux, based on the ion drift motion from various kinetic energies as they contribute to a thermal Maxwellian distribution, is calculated. The simulated heat flux is directly compared to measurements with a varying edge safety factor q95. This analysis provides evidence for the dominate e ect of high-energy ions in carrying heat from the plasma inside the separatrix to the target. High-energy ions are deposited close to the unperturbed strike line while low-energy ions can travel into the striated magnetic topology.« less

  6. Experimental and analytical studies of high heat flux components for fusion experimental reactor

    NASA Astrophysics Data System (ADS)

    Araki, Masanori

    1993-03-01

    In this report, the experimental and analytical results concerning the development of plasma facing components of ITER are described. With respect to developing high heat removal structures for the divertor plates, an externally-finned swirl tube was developed based on the results of critical heat flux (CHF) experiments on various tube structures. As the result, the burnout heat flux, which also indicates incident CHF, of 41 (+/-) 1 MW/sq m was achieved in the externally-finned swirl tube. The applicability of existing CHF correlations based on uniform heating conditions was evaluated by comparing the CHF experimental data with the smooth and the externally-finned tubes under one-sided heating condition. As the results, experimentally determined CHF data for straight tube show good agreement, for the externally-finned tube, no existing correlations are available for prediction of the CHF. With respect to the evaluation of the bonds between carbon-based material and heat sink metal, results of brazing tests were compared with the analytical results by three dimensional model with temperature-dependent thermal and mechanical properties. Analytical results showed that residual stresses from brazing can be estimated by the analytical three directional stress values instead of the equivalent stress value applied. In the analytical study on the separatrix sweeping for effectively reducing surface heat fluxes on the divertor plate, thermal response of the divertor plate was analyzed under ITER relevant heat flux conditions and has been tested. As the result, it has been demonstrated that application of the sweeping technique is very effective for improvement in the power handling capability of the divertor plate and that the divertor mock-up has withstood a large number of additional cyclic heat loads.

  7. Testing of active heat sink for advanced high-power laser diodes

    NASA Astrophysics Data System (ADS)

    Vetrovec, John; Copeland, Drew A.; Feeler, Ryan; Junghans, Jeremy

    2011-03-01

    We report on the development of a novel active heat sink for high-power laser diodes offering unparalleled capacity in high-heat flux handling and temperature control. The heat sink employs convective heat transfer by a liquid metal flowing at high speed inside a miniature sealed flow loop. Liquid metal flow in the loop is maintained electromagnetically without any moving parts. Thermal conductance of the heat sink is electronically adjustable, allowing for precise control of diode temperature and the laser light wavelength. This paper presents the principles and challenges of liquid metal cooling, and data from testing at high heat flux and high heat loads.

  8. Superlattice-based thin-film thermoelectric modules with high cooling fluxes

    PubMed Central

    Bulman, Gary; Barletta, Phil; Lewis, Jay; Baldasaro, Nicholas; Manno, Michael; Bar-Cohen, Avram; Yang, Bao

    2016-01-01

    In present-day high-performance electronic components, the generated heat loads result in unacceptably high junction temperatures and reduced component lifetimes. Thermoelectric modules can, in principle, enhance heat removal and reduce the temperatures of such electronic devices. However, state-of-the-art bulk thermoelectric modules have a maximum cooling flux qmax of only about 10 W cm−2, while state-of-the art commercial thin-film modules have a qmax <100 W cm−2. Such flux values are insufficient for thermal management of modern high-power devices. Here we show that cooling fluxes of 258 W cm−2 can be achieved in thin-film Bi2Te3-based superlattice thermoelectric modules. These devices utilize a p-type Sb2Te3/Bi2Te3 superlattice and n-type δ-doped Bi2Te3−xSex, both of which are grown heteroepitaxially using metalorganic chemical vapour deposition. We anticipate that the demonstration of these high-cooling-flux modules will have far-reaching impacts in diverse applications, such as advanced computer processors, radio-frequency power devices, quantum cascade lasers and DNA micro-arrays. PMID:26757675

  9. Manufacturing and High Heat Flux Testing of Brazed Flat-Type W/CuCrZr Plasma Facing Components

    NASA Astrophysics Data System (ADS)

    Lian, Youyun; Liu, Xiang; Feng, Fan; Chen, Lei; Cheng, Zhengkui; Wang, Jin; Chen, Jiming

    2016-02-01

    Water-cooled flat-type W/CuCrZr plasma facing components with an interlayer of oxygen-free copper (OFC) have been developed by using vacuum brazing route. The OFC layer for the accommodation of thermal stresses was cast onto the surface of W at a temperature range of 1150 °C-1200 °C in a vacuum furnace. The W/OFC cast tiles were vacuum brazed to a CuCrZr heat sink at 940 °C using the silver-free filler material CuMnSiCr. The microstructure, bonding strength, and high heat flux properties of the brazed W/CuCrZr joint samples were investigated. The W/Cu joint exhibits an average tensile strength of 134 MPa, which is about the same strength as pure annealed copper. High heat flux tests were performed in the electron beam facility EMS-60. Experimental results indicated that the brazed W/CuCrZr mock-up experienced screening tests of up to 15 MW/m2 and cyclic tests of 9 MW/m2 for 1000 cycles without visible damage. supported by National Natural Science Foundation of China (No. 11205049) and the National Magnetic Confinement Fusion Science Program of China (No. 2011GB110004)

  10. High heat flux properties of pure tungsten and plasma sprayed tungsten coatings

    NASA Astrophysics Data System (ADS)

    Liu, X.; Tamura, S.; Tokunaga, K.; Yoshida, N.; Noda, N.; Yang, L.; Xu, Z.

    2004-08-01

    High heat flux properties of pure tungsten and plasma sprayed tungsten coatings on carbon substrates have been studied by annealing and cyclic heat loading. The recrystallization temperature and an activation energy QR=126 kJ/mol for grain growth of tungsten coating by vacuum plasma spray (VPS) were estimated, and the microstructural changes of multi-layer tungsten and rhenium interface pre-deposited by physical vapor deposition (PVD) with anneal temperature were investigated. Cyclic load tests indicated that pure tungsten and VPS-tungsten coating could withstand 1000 cycles at 33-35 MW/m 2 heat flux and 3 s pulse duration, and inert gas plasma spray (IPS)-tungsten coating showed local cracks by 300 cycles but did not induce failure by further cycles. However, the failure of pure tungsten and VPS-tungsten coating by fatigue cracking was observed under higher heat load (55-60 MW/m 2) for 420 and 230 cycles, respectively.

  11. Liquid metal heat sink for high-power laser diodes

    NASA Astrophysics Data System (ADS)

    Vetrovec, John; Litt, Amardeep S.; Copeland, Drew A.; Junghans, Jeremy; Durkee, Roger

    2013-02-01

    We report on the development of a novel, ultra-low thermal resistance active heat sink (AHS) for thermal management of high-power laser diodes (HPLD) and other electronic and photonic components. AHS uses a liquid metal coolant flowing at high speed in a miniature closed and sealed loop. The liquid metal coolant receives waste heat from an HPLD at high flux and transfers it at much reduced flux to environment, primary coolant fluid, heat pipe, or structure. Liquid metal flow is maintained electromagnetically without any moving parts. Velocity of liquid metal flow can be controlled electronically, thus allowing for temperature control of HPLD wavelength. This feature also enables operation at a stable wavelength over a broad range of ambient conditions. Results from testing an HPLD cooled by AHS are presented.

  12. Particle-In-Cell simulation concerning heat-flux mitigation using electromagnetic fields

    NASA Astrophysics Data System (ADS)

    Lüskow, Karl Felix; Duras, Julia; Kemnitz, Stefan; Kahnfeld, Daniel; Matthias, Paul; Bandelow, Gunnas; Schneider, Ralf; Konigorski, Detlev

    2016-10-01

    In space missions enormous amount of money is spent for the thermal protection system for re-entry. To avoid complex materials and save money one idea is to reduce the heat-flux towards the spacecraft. The partially-ionized gas can be controlled by electromagnetic fields. For first-principle tests partially ionized argon flow from an arc-jet was used to measure the heat-flux mitigation created by an external magnetic field. In the successful experiment a reduction of 85% was measured. In this work the Particle-in-Cell (PIC) method was used to simulate this experiment. PIC is able to reproduce the heat flux mitigation qualitatively. The main mechanism is identified as a changed electron transport and by this, modified electron density due to the reaction to the applied magnetic field. Ions follow due to quasi-neutrality and influence then strongly by charge exchange collisions the neutrals dynamics and heat deposition. This work was supported by the German Space Agency DLR through Project 50RS1508.

  13. High flux, narrow bandwidth compton light sources via extended laser-electron interactions

    DOEpatents

    Barty, V P

    2015-01-13

    New configurations of lasers and electron beams efficiently and robustly produce high flux beams of bright, tunable, polarized quasi-monoenergetic x-rays and gamma-rays via laser-Compton scattering. Specifically, the use of long-duration, pulsed lasers and closely-spaced, low-charge and low emittance bunches of electron beams increase the spectral flux of the Compton-scattered x-rays and gamma rays, increase efficiency of the laser-electron interaction and significantly reduce the overall complexity of Compton based light sources.

  14. Nonlocal electron energy transport and flux inhibition in laser produced plasmas in one and two dimensions

    NASA Astrophysics Data System (ADS)

    Manheimer, Wallace

    2011-10-01

    As the mean free path of the heat conducting electrons in laser produced plasmas can, at certain points, be greater than the temperature gradient scale length, the classical, local model can be invalid. More energetic electrons can advance ahead of the main heat front and preheat the fusion target. Also, experiments show that the main heat front does not propagate as rapidly as classical theory would predict, so there is heat flux inhibition. This latter effect is usually treated by limiting the flux to some arbitrary fraction f of the free streaming flux; f's have ranged from 0.03 to 0.3. However the choice of flux limit is arbitrary and the choice affects plasma temperature, which in turn affects thresholds for laser plasma instabilities; too low a limit has given too high a temperature and false optimism regarding instability threshold. We have developed a velocity dependent Krook model for nonlocal electron energy transport. It shows preheat and flux limitation are not separate effects, but are two sides of the same coin. The model gives an analytic solution for the nonlocal electron energy flux, and it is relatively simple and inexpensive to incorporate in a fluid simulation run at the ion time scale. It shows that in some sense, preheat is subtracted from the main electron energy flux, thereby giving rise to flux limitation. We have developed the theory and compared it with Fokker Planck simulations of simple configurations. We have incorporated the model into our code FAST2D and used it to model foil acceleration and evaluate and compare a number of competing physical effects in one and two dimensions, and compared with experiments. We have investigated the effect on spherical implosions, especially the effect on corona temperature, pressure, fuel adiabat and preheat, and ultimately gain. Supported by ONR and NNSA/DoE.

  15. Fundamentals of heat measurement. [heat flux transducers

    NASA Technical Reports Server (NTRS)

    Gerashchenko, O. A.

    1979-01-01

    Various methods and devices for obtaining experimental data on heat flux density over wide ranges of temperature and pressure are examined. Laboratory tests and device fabrication details are supplemented by theoretical analyses of heat-conduction and thermoelectric effects, providing design guidelines and information relevant to further research and development. A theory defining the measure of correspondence between transducer signal and the measured heat flux is established for individual (isolated) heat flux transducers subject to space and time-dependent loading. An analysis of the properties of stacked (series-connected) transducers of various types (sandwich-type, plane, and spiral) is used to derive a similarity theory providing general governing relationships. The transducers examined are used in 36 types of derivative devices involving direct heat loss measurements, heat conduction studies, radiation pyrometry, calorimetry in medicine and industry and nuclear reactor dosimetry.

  16. QUANTIFICATION OF HEAT FLUX FROM A REACTING THERMITE SPRAY

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Eric Nixon; Michelle Pantoya

    2009-07-01

    Characterizing the combustion behaviors of energetic materials requires diagnostic tools that are often not readily or commercially available. For example, a jet of thermite spray provides a high temperature and pressure reaction that can also be highly corrosive and promote undesirable conditions for the survivability of any sensor. Developing a diagnostic to quantify heat flux from a thermite spray is the objective of this study. Quick response sensors such as thin film heat flux sensors can not survive the harsh conditions of the spray, but more rugged sensors lack the response time for the resolution desired. A sensor that willmore » allow for adequate response time while surviving the entire test duration was constructed. The sensor outputs interior temperatures of the probes at known locations and utilizes an inverse heat conduction code to calculate heat flux values. The details of this device are discussed and illustrated. Temperature and heat flux measurements of various thermite spray conditions are reported. Results indicate that this newly developed energetic material heat flux sensor provides quantitative data with good repeatability.« less

  17. High geothermal heat flux in close proximity to the Northeast Greenland Ice Stream.

    PubMed

    Rysgaard, Søren; Bendtsen, Jørgen; Mortensen, John; Sejr, Mikael K

    2018-01-22

    The Greenland ice sheet (GIS) is losing mass at an increasing rate due to surface melt and flow acceleration in outlet glaciers. Currently, there is a large disagreement between observed and simulated ice flow, which may arise from inaccurate parameterization of basal motion, subglacial hydrology or geothermal heat sources. Recently it was suggested that there may be a hidden heat source beneath GIS caused by a higher than expected geothermal heat flux (GHF) from the Earth's interior. Here we present the first direct measurements of GHF from beneath a deep fjord basin in Northeast Greenland. Temperature and salinity time series (2005-2015) in the deep stagnant basin water are used to quantify a GHF of 93 ± 21 mW m -2 which confirm previous indirect estimated values below GIS. A compilation of heat flux recordings from Greenland show the existence of geothermal heat sources beneath GIS and could explain high glacial ice speed areas such as the Northeast Greenland ice stream.

  18. Design and Characterization of a High Resolution Microfluidic Heat Flux Sensor with Thermal Modulation

    PubMed Central

    Nam, Sung-Ki; Kim, Jung-Kyun; Cho, Sung-Cheon; Lee, Sun-Kyu

    2010-01-01

    A complementary metal-oxide semiconductor-compatible process was used in the design and fabrication of a suspended membrane microfluidic heat flux sensor with a thermopile for the purpose of measuring the heat flow rate. The combination of a thirty-junction gold and nickel thermoelectric sensor with an ultralow noise preamplifier, a low pass filter, and a lock-in amplifier can yield a resolution 20 nW with a sensitivity of 461 V/W. The thermal modulation method is used to eliminate low-frequency noise from the sensor output, and various amounts of fluidic heat were applied to the sensor to investigate its suitability for microfluidic applications. For sensor design and analysis of signal output, a method of modeling and simulating electro-thermal behavior in a microfluidic heat flux sensor with an integrated electronic circuit is presented and validated. The electro-thermal domain model was constructed by using system dynamics, particularly the bond graph. The electro-thermal domain system model in which the thermal and the electrical domains are coupled expresses the heat generation of samples and converts thermal input to electrical output. The proposed electro-thermal domain system model is in good agreement with the measured output voltage response in both the transient and the steady state. PMID:22163568

  19. Development of Advanced Thermal and Environmental Barrier Coatings Using a High-Heat-Flux Testing Approach

    NASA Technical Reports Server (NTRS)

    Zhu, Dongming; Miller, Robert A.

    2003-01-01

    The development of low conductivity, robust thermal and environmental barrier coatings requires advanced testing techniques that can accurately and effectively evaluate coating thermal conductivity and cyclic resistance at very high surface temperatures (up to 1700 C) under large thermal gradients. In this study, a laser high-heat-flux test approach is established for evaluating advanced low conductivity, high temperature capability thermal and environmental barrier coatings under the NASA Ultra Efficient Engine Technology (UEET) program. The test approach emphasizes the real-time monitoring and assessment of the coating thermal conductivity, which initially rises under the steady-state high temperature thermal gradient test due to coating sintering, and later drops under the cyclic thermal gradient test due to coating cracking/delamination. The coating system is then evaluated based on damage accumulation and failure after the combined steady-state and cyclic thermal gradient tests. The lattice and radiation thermal conductivity of advanced ceramic coatings can also be evaluated using laser heat-flux techniques. The external radiation resistance of the coating is assessed based on the measured specimen temperature response under a laser- heated intense radiation-flux source. The coating internal radiation contribution is investigated based on the measured apparent coating conductivity increases with the coating surface test temperature under large thermal gradient test conditions. Since an increased radiation contribution is observed at these very high surface test temperatures, by varying the laser heat-flux and coating average test temperature, the complex relation between the lattice and radiation conductivity as a function of surface and interface test temperature may be derived.

  20. A laser-induced heat flux technique for convective heat transfer measurements in high speed flows

    NASA Technical Reports Server (NTRS)

    Porro, A. R.; Keith, T. G., Jr.; Hingst, W. R.

    1991-01-01

    A technique is developed to measure the local convective heat transfer coefficient on a model surface in a supersonic flow field. The technique uses a laser to apply a discrete local heat flux at the model test surface, and an infrared camera system determines the local temperature distribution due to the heating. From this temperature distribution and an analysis of the heating process, a local convective heat transfer coefficient is determined. The technique was used to measure the local surface convective heat transfer coefficient distribution on a flat plate at nominal Mach numbers of 2.5, 3.0, 3.5, and 4.0. The flat plate boundary layer initially was laminar and became transitional in the measurement region. The experimentally determined convective heat transfer coefficients were generally higher than the theoretical predictions for flat plate laminar boundary layers. However, the results indicate that this nonintrusive optical measurement technique has the potential to measure surface convective heat transfer coefficients in high speed flow fields.

  1. A laser-induced heat flux technique for convective heat transfer measurements in high speed flows

    NASA Technical Reports Server (NTRS)

    Porro, A. R.; Keith, T. G., Jr.; Hingst, W. R.

    1991-01-01

    A technique is developed to measure the local convective heat transfer coefficient on a model surface in a supersonic flow field. The technique uses a laser to apply a discrete local heat flux at the model test surface, and an infrared camera system determines the local temperature distribution due to the heating. From this temperature distribution and an analysis of the heating process, a local convective heat transfer coefficient is determined. The technique was used to measure the local surface convective heat transfer coefficient distribution on a flat plate at nominal Mach numbers of 2.5, 3.0, 3.5, and 4.0. The flat plate boundary layer initially was laminar and became transitional in the measurement region. The experimentally determined convective heat transfer coefficients were generally higher than the theoretical predictions for flat plate laminar boundary layers. However, the results indicate that this nonintrusive optical measurement technique has the potential to measure surface convective heat transfer coefficients in high-speed flowfields.

  2. Evaluation of cooling concepts and specimen geometries for high heat flux tests on neutron irradiated divertor elements

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Linke, J.; Bolt. H.; Breitbach, G.

    1994-12-31

    To assess the lifetime and the long term heat removal capabilities of plasma facing components in future thermonuclear fusion reactors such as ITER, neutron irradiation and subsequent high heat flux tests will be most essential. The effect of neutron damage will be simulated in material test reactors (such as the HFR-Petten) in a fission neutron environment. To investigate the heat loads during normal and off-normal operation scenarios a 60 kW electron beam test stand (Juelich Divertor Test Facility in Hot Cells, JUDITH) has been installed in a hot cell which can be operated by remote handling techniques. In this facilitymore » inertially cooled test coupons can be handled as well as small actively cooled divertor mock-ups. A special clamping mechanism for small test coupons (25 mm x 25 mm x 35 mm) with an integrated coolant channel within a copper or TZM heat sink has been developed and tested in an electron beam test bed. This method is an attractive alternative to costly large scale tests on complete divertor modules. The temperature and stress fields in individual CFC or beryllium tiles brazed to metallic heat sink (e.g. copper or TZM) can be investigated before and after neutron irradiation with moderate efforts.« less

  3. Interplanetary magnetic field connection to the sun during electron heat flux dropouts in the solar wind

    NASA Technical Reports Server (NTRS)

    Lin, R. P.; Kahler, S. W.

    1992-01-01

    The paper discusses observations of 2- to 8.5-keV electrons, made by measurements aboard the ISEE 3 spacecraft during the periods of heat flux decreases (HFDs) reported by McComas et al. (1989). In at least eight of the total of 25 HFDs observed, strong streaming of electrons that were equal to or greater than 2 keV outward from the sun was recorded. In one HFD, an impulsive solar electron event was observed with an associated type III radio burst, which could be tracked from the sun to about 1 AU. It is concluded that, in many HFDs, the interplanetary field is still connected to the sun and that some energy-dependent process may produce HFDs without significantly perturbing electrons of higher energies.

  4. High Flux Heat Exchanger

    DTIC Science & Technology

    1993-01-01

    maximum jet velocity (6.36 m/s), and maximum number of jets (nine). Wadsworth and Mudawar [49] describe the use of a single slotted nozzle to provide...H00503 (ASME), pp. 121-128, 1989. 40 49. D. C. Wadsworth and I. Mudawar , "Cooling of a Multichip Electronic Module by Means of Confined Two-Dimensional...Jets of Dielectric Liquid," HTD-Vol. 111, Heat Transfer in Electrglif, Book No. H00503 (ASME), pp. 79-87, 1989. 50. D.C. Wadsworth and I. Mudawar

  5. Micro-Columnated Loop Heat Pipe: The Future of Electronic Substrates

    NASA Astrophysics Data System (ADS)

    Dhillon, Navdeep Singh

    The modern world is run by semiconductor-based electronic systems. Due to continuous improvements in semiconductor device fabrication, there is a clear trend in the market towards the development of electronic devices and components that not only deliver enhanced computing power, but are also more compact. Thermal management has emerged as the primary challenge in this scenario where heat flux dissipation of electronic chips is increasing exponentially, but conventional cooling solutions such as conduction and convection are no longer feasible. To keep device junction temperatures within the safe operating limit, there is an urgent requirement for ultra-high-conductivity thermal substrates that not only absorb and transport large heat fluxes, but can also provide localized cooling to thermal hotspots. This dissertation describes the design, modeling, and fabrication of a phase change-based, planar, ultra-thin, passive thermal transport system that is inspired by the concept of loop heat pipes and capillary pumped loops. Fabricated on silicon and Pyrex wafers using microfabrication techniques, the micro-columnated loop heat pipe (muCLHP) can be integrated directly with densely packed or multiply-stacked electronic substrates, to provide localized high-heat-flux thermal management. The muCLHP employs a dual-scale coherent porous silicon(CPS)-based micro-columnated wicking structure, where the primary CPS wick provides large capillary forces for fluid transport, while a secondary surface-wick maximizes the rate of thin-film evaporation. To overcome the wick thickness limitation encountered in conventional loop heat pipes, strategies based on MEMS surface micromachining techniques were developed to reduce parasitic heat flow from the evaporator to the compensation chamber of the device. Finite element analysis was used to confirm this reduction in a planar evaporator design, thus enabling the generation of a large motive temperature head for continuous device operation

  6. Thermal performance analysis of a flat heat pipe working with carbon nanotube-water nanofluid for cooling of a high heat flux heater

    NASA Astrophysics Data System (ADS)

    Arya, A.; Sarafraz, M. M.; Shahmiri, S.; Madani, S. A. H.; Nikkhah, V.; Nakhjavani, S. M.

    2018-04-01

    Experimental investigation on the thermal performance of a flat heat pipe working with carbon nanotube nanofluid is conducted. It is used for cooling a heater working at high heat flux conditions up to 190 kW/m2. The heat pipe is fabricated from aluminium and is equipped with rectangular fin for efficient cooling of condenser section. Inside the heat pipe, a screen mesh was inserted as a wick structure to facilitate the capillary action of working fluid. Influence of different operating parameters such as heat flux, mass concentration of carbon nanotubes and filling ratio of working fluid on thermal performance of heat pipe and its thermal resistance are investigated. Results showed that with an increase in heat flux, the heat transfer coefficient in evaporator section of the heat pipe increases. For filling ratio, however, there is an optimum value, which was 0.8 for the test heat pipe. In addition, CNT/water enhanced the heat transfer coefficient up to 40% over the deionized water. Carbon nanotubes intensified the thermal performance of wick structure by creating a fouling layer on screen mesh structure, which changes the contact angle of liquid with the surface, intensifying the capillary forces.

  7. Prompt Ion Outflows and Artificial Ducts during High-Power HF Heating at HAARP: Effect of Suprathermal Electrons?

    NASA Astrophysics Data System (ADS)

    Mishin, E. V.; Milikh, G. M.

    2014-12-01

    In situ observations from the DMSP and Demeter satellites established that high-power HF heating of the ionosphere F-region results in significant ion outflows associated with 10-30% density enhancements in the topside ionosphere magnetically-conjugate to the heated region. As follows from the SAMI2 two-fluid model calculations, their formation time should exceed 5-7 minutes. However, specially designed DMSP-HAARP experiments have shown that artificial ducts and ion outflows appear on the topside within 2 minutes. We describe the results of these observations and present a semi-quantitative explanation of the fast timescale due to suprathermal electrons accelerated by HF-induced plasma turbulence. There are two possible effects of suprathermal electrons: (1) the increase of the ambipolar electric field over the usual thermal ambipolar diffusion and (2) excitation of heat flux-driven plasma instability resulting in an anomalous electron-ion momentum exchange. Both effects result in faster upward ion flows.

  8. Calibration of High Heat Flux Sensors at NIST

    PubMed Central

    Murthy, A. V.; Tsai, B. K.; Gibson, C. E.

    1997-01-01

    An ongoing program at the National Institute of Standards and Technology (NIST) is aimed at improving and standardizing heat-flux sensor calibration methods. The current calibration needs of U.S. science and industry exceed the current NIST capability of 40 kW/m2 irradiance. In achieving this goal, as well as meeting lower-level non-radiative heat flux calibration needs of science and industry, three different types of calibration facilities currently are under development at NIST: convection, conduction, and radiation. This paper describes the research activities associated with the NIST Radiation Calibration Facility. Two different techniques, transfer and absolute, are presented. The transfer calibration technique employs a transfer standard calibrated with reference to a radiometric standard for calibrating the sensors using a graphite tube blackbody. Plans for an absolute calibration facility include the use of a spherical blackbody and a cooled aperture and sensor-housing assembly to calibrate the sensors in a low convective environment. PMID:27805156

  9. High heat flux testing of CFC composites for the tokamak physics experiment

    NASA Astrophysics Data System (ADS)

    Valentine, P. G.; Nygren, R. E.; Burns, R. W.; Rocket, P. D.; Colleraine, A. P.; Lederich, R. J.; Bradley, J. T.

    1996-10-01

    High heat flux (HHF) testing of carbon fiber reinforced carbon composites (CFC's) was conducted under the General Atomics program to develop plasma-facing components (PFC's) for Princeton Plasma Physics Laboratory's tokamak physics experiment (TPX). As part of the process of selecting TPX CFC materials, a series of HHF tests were conducted with the 30 kW electron beam test system (EBTS) facility at Sandia National Laboratories, and with the plasma disruption simulator I (PLADIS-I) facility at the University of New Mexico. The purpose of the tests was to make assessments of the thermal performance and erosion behavior of CFC materials. Tests were conducted with 42 different CFC materials. In general, the CFC materials withstood the rapid thermal pulse environments without fracturing, delaminating, or degrading in a non-uniform manner; significant differences in thermal performance, erosion behavior, vapor evolution, etc. were observed and preliminary findings are presented below. The CFC's exposed to the hydrogen plasma pulses in PLADIS-I exhibited greater erosion rates than the CFC materials exposed to the electron-beam pulses in EBTS. The results obtained support the continued consideration of a variety of CFC composites for TPX PFC components.

  10. A diagnostic for quantifying heat flux from a thermite spray

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    E. P. Nixon; M. L. Pantoya; D. J. Prentice

    2010-02-01

    Characterizing the combustion behaviors of energetic materials requires diagnostic tools that are often not readily or commercially available. For example, a jet of thermite spray provides a high temperature and pressure reaction that can also be highly corrosive and promote undesirable conditions for the survivability of any sensor. Developing a diagnostic to quantify heat flux from a thermite spray is the objective of this study. Quick response sensors such as thin film heat flux sensors cannot survive the harsh conditions of the spray, but more rugged sensors lack the response time for the resolution desired. A sensor that will allowmore » for adequate response time while surviving the entire test duration was constructed. The sensor outputs interior temperatures of the probes at known locations and utilizes an inverse heat conduction code to calculate heat flux values. The details of this device are discussed and illustrated. Temperature and heat flux measurements of various thermite sprays are reported. Results indicate that this newly designed heat flux sensor provides quantitative data with good repeatability suitable for characterizing energetic material combustion.« less

  11. Thermotronics: Towards Nanocircuits to Manage Radiative Heat Flux

    NASA Astrophysics Data System (ADS)

    Ben-Abdallah, Philippe; Biehs, Svend-Age

    2017-02-01

    The control of electric currents in solids is at the origin of the modern electronics revolution that has driven our daily life since the second half of 20th century. Surprisingly, to date, there is no thermal analogue for a control of heat flux. Here, we summarise the very last developments carried out in this direction to control heat exchanges by radiation both in near and far-field in complex architecture networks.

  12. Numerical Analysis of a Radiant Heat Flux Calibration System

    NASA Technical Reports Server (NTRS)

    Jiang, Shanjuan; Horn, Thomas J.; Dhir, V. K.

    1998-01-01

    A radiant heat flux gage calibration system exists in the Flight Loads Laboratory at NASA's Dryden Flight Research Center. This calibration system must be well understood if the heat flux gages calibrated in it are to provide useful data during radiant heating ground tests or flight tests of high speed aerospace vehicles. A part of the calibration system characterization process is to develop a numerical model of the flat plate heater element and heat flux gage, which will help identify errors due to convection, heater element erosion, and other factors. A 2-dimensional mathematical model of the gage-plate system has been developed to simulate the combined problem involving convection, radiation and mass loss by chemical reaction. A fourth order finite difference scheme is used to solve the steady state governing equations and determine the temperature distribution in the gage and plate, incident heat flux on the gage face, and flat plate erosion. Initial gage heat flux predictions from the model are found to be within 17% of experimental results.

  13. Geometrical correction factors for heat flux meters

    NASA Technical Reports Server (NTRS)

    Baumeister, K. J.; Papell, S. S.

    1974-01-01

    General formulas are derived for determining gage averaging errors of strip-type heat flux meters used in the measurement of one-dimensional heat flux distributions. The local averaging error e(x) is defined as the difference between the measured value of the heat flux and the local value which occurs at the center of the gage. In terms of e(x), a correction procedure is presented which allows a better estimate for the true value of the local heat flux. For many practical problems, it is possible to use relatively large gages to obtain acceptable heat flux measurements.

  14. Boiling Heat-Transfer Processes and Their Application in the Cooling of High Heat Flux Devices

    DTIC Science & Technology

    1993-06-01

    1991, pp. 395-397. 385. Galloway, J. E. and Mudawar , 1. "Critical Heat Flux Enhancement by Means of Liquid Subcooling and Centrifugal Force Induced...Flow Boiling Heat Transfer for a Spirally Fluted Tube." Heat Tran~ler Engineering, Vol. 13, No.1, 1992, pp. 42-52. 390. Willingham, T. C. and Mudawar

  15. Apparatus for measuring high-flux heat transfer in radiatively heated compact exchangers

    NASA Technical Reports Server (NTRS)

    Olson, Douglas A.

    1989-01-01

    An apparatus is described which can deliver uniform heat flux densities of up to 80 W/sq cm over an area 7.8 cm x 15.2 cm for use in measuring the heat transfer and pressure drop in thin (6 mm or less), compact heat exchangers. Helium gas at flow rates of 0 to 40 kg/h and pressures to 6.9 MPa (1000 psi) is the working fluid. The instrumentation used in the apparatus and the methods for analyzing the data is described. The apparatus will be used initially to test the performance of prototype cooling jackets for the engine struts of the National Aerospace Plane (NASP).

  16. Diffusion, Fluxes, Friction Forces, and Joule Heating in Two-Temperature Multicomponent Magnetohydrodynamics

    NASA Technical Reports Server (NTRS)

    Chang, C. H.

    1999-01-01

    The relationship between Joule heating, diffusion fluxes, and friction forces has been studied for both total and electron thermal energy equations, using general expressions for multicomponent diffusion in two-temperature plasmas with the velocity dependent Lorentz force acting on charged species in a magnetic field. It is shown that the derivation of Joule heating terms requires both diffusion fluxes and friction between species which represents the resistance experienced by the species moving at different relative velocities. It is also shown that the familiar Joule heating term in the electron thermal energy equation includes artificial effects produced by switching the convective velocity from the species velocity to the mass-weighted velocity, and thus should not be ignored even when there is no net energy dissipation.

  17. The Influence of a Sandy Substrate, Seagrass, or Highly Turbid Water on Albedo and Surface Heat Flux

    NASA Astrophysics Data System (ADS)

    Fogarty, M. C.; Fewings, M. R.; Paget, A. C.; Dierssen, H. M.

    2018-01-01

    Sea-surface albedo is a combination of surface-reflected and water-leaving irradiance, but water-leaving irradiance typically contributes less than 15% of the total albedo in open-ocean conditions. In coastal systems, however, the bottom substrate or suspended particulate matter can increase the amount of backscattered light, thereby increasing albedo and decreasing net shortwave surface heat flux. Here a sensitivity analysis using observations and models predicts the effect of light scattering on albedo and the net shortwave heat flux for three test cases: a bright sand bottom, a seagrass canopy, and turbid water. After scaling to the full solar shortwave spectrum, daytime average albedo for the test cases is up to 0.20 and exceeds the value of 0.05 predicted using a commonly applied parameterization. Daytime net shortwave heat flux into the water is significantly reduced, particularly for waters with bright sediments, dense horizontal seagrass canopies < 0.25 m from the sea surface, or highly turbid waters with suspended particulate matter concentration ≥ 50 g m-3. Observations of a more vertical seagrass canopy within 0.2 and 1 m of the surface indicate the increase in albedo compared to the common parameterization is negligible. Therefore, we suggest that the commonly applied albedo lookup table can be used in coastal heat flux estimates in water as shallow as 1 m unless the bottom substrate is highly reflective or the water is highly turbid. Our model results provide guidance to researchers who need to determine albedo in highly reflective or highly turbid conditions but have no direct observations.

  18. Environmental Barrier Coating Fracture, Fatigue and High-Heat-Flux Durability Modeling and Stochastic Progressive Damage Simulation

    NASA Technical Reports Server (NTRS)

    Zhu, Dongming; Nemeth, Noel N.

    2017-01-01

    Advanced environmental barrier coatings will play an increasingly important role in future gas turbine engines because of their ability to protect emerging light-weight SiC/SiC ceramic matrix composite (CMC) engine components, further raising engine operating temperatures and performance. Because the environmental barrier coating systems are critical to the performance, reliability and durability of these hot-section ceramic engine components, a prime-reliant coating system along with established life design methodology are required for the hot-section ceramic component insertion into engine service. In this paper, we have first summarized some observations of high temperature, high-heat-flux environmental degradation and failure mechanisms of environmental barrier coating systems in laboratory simulated engine environment tests. In particular, the coating surface cracking morphologies and associated subsequent delamination mechanisms under the engine level high-heat-flux, combustion steam, and mechanical creep and fatigue loading conditions will be discussed. The EBC compostion and archtechture improvements based on advanced high heat flux environmental testing, and the modeling advances based on the integrated Finite Element Analysis Micromechanics Analysis Code/Ceramics Analysis and Reliability Evaluation of Structures (FEAMAC/CARES) program will also be highlighted. The stochastic progressive damage simulation successfully predicts mud flat damage pattern in EBCs on coated 3-D specimens, and a 2-D model of through-the-thickness cross-section. A 2-parameter Weibull distribution was assumed in characterizing the coating layer stochastic strength response and the formation of damage was therefore modeled. The damage initiation and coalescence into progressively smaller mudflat crack cells was demonstrated. A coating life prediction framework may be realized by examining the surface crack initiation and delamination propagation in conjunction with environmental

  19. Mitigation of divertor heat flux by high-frequency ELM pacing with non-fuel pellet injection in DIII-D

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Bortolon, A.; Maingi, R.; Mansfield, D. K.

    Experiments have been conducted on DIII-D investigating high repetition rate injection of non-fuel pellets as a tool for pacing Edge Localized Modes (ELMs) and mitigating their transient divertor heat loads. Effective ELM pacing was obtained with injection of Li granules in different H-mode scenarios, at frequencies 3–5 times larger than the natural ELM frequency, with subsequent reduction of strike-point heat flux. However, in scenarios with high pedestal density (~6 × 10 19 m –3), the magnitude of granule triggered ELMs shows a broad distribution, in terms of stored energy loss and peak heat flux, challenging the effectiveness of ELM mitigation.more » Furthermore, transient heat-flux deposition correlated with granule injections was observed far from the strike-points. As a result, field line tracing suggest this phenomenon to be consistent with particle loss into the mid-plane far scrape-off layer, at toroidal location of the granule injection.« less

  20. Mitigation of divertor heat flux by high-frequency ELM pacing with non-fuel pellet injection in DIII-D

    DOE PAGES

    Bortolon, A.; Maingi, R.; Mansfield, D. K.; ...

    2017-03-23

    Experiments have been conducted on DIII-D investigating high repetition rate injection of non-fuel pellets as a tool for pacing Edge Localized Modes (ELMs) and mitigating their transient divertor heat loads. Effective ELM pacing was obtained with injection of Li granules in different H-mode scenarios, at frequencies 3–5 times larger than the natural ELM frequency, with subsequent reduction of strike-point heat flux. However, in scenarios with high pedestal density (~6 × 10 19 m –3), the magnitude of granule triggered ELMs shows a broad distribution, in terms of stored energy loss and peak heat flux, challenging the effectiveness of ELM mitigation.more » Furthermore, transient heat-flux deposition correlated with granule injections was observed far from the strike-points. As a result, field line tracing suggest this phenomenon to be consistent with particle loss into the mid-plane far scrape-off layer, at toroidal location of the granule injection.« less

  1. Understanding of flux-limited behaviors of heat transport in nonlinear regime

    NASA Astrophysics Data System (ADS)

    Guo, Yangyu; Jou, David; Wang, Moran

    2016-01-01

    The classical Fourier's law of heat transport breaks down in highly nonequilibrium situations as in nanoscale heat transport, where nonlinear effects become important. The present work is aimed at exploring the flux-limited behaviors based on a categorization of existing nonlinear heat transport models in terms of their theoretical foundations. Different saturation heat fluxes are obtained, whereas the same qualitative variation trend of heat flux versus exerted temperature gradient is got in diverse nonlinear models. The phonon hydrodynamic model is proposed to act as a standard to evaluate other heat flux limiters because of its more rigorous physical foundation. A deeper knowledge is thus achieved about the phenomenological generalized heat transport models. The present work provides deeper understanding and accurate modeling of nonlocal and nonlinear heat transport beyond the diffusive limit.

  2. Heat flux measurements on ceramics with thin film thermocouples

    NASA Technical Reports Server (NTRS)

    Holanda, Raymond; Anderson, Robert C.; Liebert, Curt H.

    1993-01-01

    Two methods were devised to measure heat flux through a thick ceramic using thin film thermocouples. The thermocouples were deposited on the front and back face of a flat ceramic substrate. The heat flux was applied to the front surface of the ceramic using an arc lamp Heat Flux Calibration Facility. Silicon nitride and mullite ceramics were used; two thicknesses of each material was tested, with ceramic temperatures to 1500 C. Heat flux ranged from 0.05-2.5 MW/m2(sup 2). One method for heat flux determination used an approximation technique to calculate instantaneous values of heat flux vs time; the other method used an extrapolation technique to determine the steady state heat flux from a record of transient data. Neither method measures heat flux in real time but the techniques may easily be adapted for quasi-real time measurement. In cases where a significant portion of the transient heat flux data is available, the calculated transient heat flux is seen to approach the extrapolated steady state heat flux value as expected.

  3. Study on coal char ignition by radiant heat flux.

    NASA Astrophysics Data System (ADS)

    Korotkikh, A. G.; Slyusarskiy, K. V.

    2017-11-01

    The study on coal char ignition by CO2-continuous laser was carried out. The coal char samples of T-grade bituminous coal and 2B-grade lignite were studied via CO2-laser ignition setup. Ignition delay times were determined at ambient condition in heat flux density range 90-200 W/cm2. The average ignition delay time value for lignite samples were 2 times lower while this difference is larger in high heat flux region and lower in low heat flux region. The kinetic constants for overall oxidation reaction were determined using analytic solution of simplified one-dimensional heat transfer equation with radiant heat transfer boundary condition. The activation energy for lignite char was found to be less than it is for bituminous coal char by approximately 20 %.

  4. GEM-CEDAR Challenge: Poynting Flux at DMSP and Modeled Joule Heat

    NASA Technical Reports Server (NTRS)

    Rastaetter, Lutz; Shim, Ja Soon; Kuznetsova, Maria M.; Kilcommons, Liam M.; Knipp, Delores J.; Codrescu, Mihail; Fuller-Rowell, Tim; Emery, Barbara; Weimer, Daniel R.; Cosgrove, Russell; hide

    2016-01-01

    Poynting flux into the ionosphere measures the electromagnetic energy coming from the magnetosphere. This energy flux can vary greatly between quiet times and geomagnetic active times. As part of the Geospace Environment Modeling-coupling energetics and dynamics of atmospheric regions modeling challenge, physics-based models of the 3-D ionosphere and ionospheric electrodynamics solvers of magnetosphere models that specify Joule heat and empirical models specifying Poynting flux were run for six geomagnetic storm events of varying intensity. We compared model results with Poynting flux values along the DMSP-15 satellite track computed from ion drift meter and magnetic field observations. Although being a different quantity, Joule heat can in practice be correlated to incoming Poynting flux because the energy is dissipated primarily in high latitudes where Poynting flux is being deposited. Within the physics-based model group, we find mixed results with some models overestimating Joule heat and some models agreeing better with observed Poynting flux rates as integrated over auroral passes. In contrast, empirical models tend to underestimate integrated Poynting flux values. Modeled Joule heat or Poynting flux patterns often resemble the observed Poynting flux patterns on a large scale, but amplitudes can differ by a factor of 2 or larger due to the highly localized nature of observed Poynting flux deposition that is not captured by the models. In addition, the positioning of modeled patterns appear to be randomly shifted against the observed Poynting flux energy input. This study is the first to compare Poynting flux and Joule heat in a large variety of models of the ionosphere.

  5. Pool boiling with high heat flux enabled by a porous artery structure

    NASA Astrophysics Data System (ADS)

    Bai, Lizhan; Zhang, Lianpei; Lin, Guiping; Peterson, G. P.

    2016-06-01

    A porous artery structure utilizing the concept of "phase separation and modulation" is proposed to enhance the critical heat flux of pool boiling. A series of experiments were conducted on a range of test articles in which multiple rectangular arteries were machined directly into the top surface of a 10.0 mm diameter copper rod. The arteries were then covered by a 2.0 mm thickness microporous copper plate through silver brazing. The pool wall was fabricated from transparent Pyrex glass to allow a visualization study, and water was used as the working fluid. Experimental results confirmed that the porous artery structure provided individual flow paths for the liquid supply and vapor venting, and avoided the detrimental effects of the liquid/vapor counter flow. As a result, a maximum heat flux of 610 W/cm2 over a heating area of 0.78 cm2 was achieved with no indication of dryout, prior to reaching the heater design temperature limit. Following the experimental tests, the mechanisms responsible for the boiling critical heat flux and performance enhancement of the porous artery structure were analyzed.

  6. Diamond-based heat spreaders for power electronic packaging applications

    NASA Astrophysics Data System (ADS)

    Guillemet, Thomas

    As any semiconductor-based devices, power electronic packages are driven by the constant increase of operating speed (higher frequency), integration level (higher power), and decrease in feature size (higher packing density). Although research and innovation efforts have kept these trends continuous for now more than fifty years, the electronic packaging technology is currently facing a challenge that must be addressed in order to move toward any further improvements in terms of performances or miniaturization: thermal management. Thermal issues in high-power packages strongly affect their reliability and lifetime and have now become one of the major limiting factors of power modules development. Thus, there is a strong need for materials that can sustain higher heat flux levels while safely integrating into the electronic package architecture. In such context, diamond is an attractive candidate because of its outstanding thermal conductivity, low thermal expansion, and high electrical resistivity. Its low heat capacity relative to metals such as aluminum or copper makes it however preferable for heat spreading applications (as a heat-spreader) rather than for dissipating the heat flux itself (as a heat sink). In this study, a dual diamond-based heat-spreading solution is proposed. Polycrystalline diamond films were grown through laser-assisted combustion synthesis on electronic substrates (in the U.S) while, in parallel, diamond-reinforced copper-matrix composite films were fabricated through tape casting and hot pressing (in France). These two types of diamond-based heat-spreading films were characterized and their microstructure and chemical composition were related to their thermal performances. Particular emphasize was put on the influence of interfaces on the thermal properties of the materials, either inside a single material (grain boundaries) or between dissimilar materials (film/substrate interface, matrix/reinforcement interface). Finally, the packaging

  7. High-heat-flux testing of irradiated tungsten-based materials for fusion applications using infrared plasma arc lamps

    DOE PAGES

    Sabau, Adrian S.; Ohriner, Evan K.; Kiggans, Jim; ...

    2014-11-01

    Testing of advanced materials and component mock-ups under prototypical fusion high-heat-flux conditions, while historically a mainstay of fusion research, has proved to be quite challenging, especially for irradiated materials. A new high-heat-flux–testing (HHFT) facility based on water-wall plasma arc lamps (PALs) is now introduced for materials and small-component testing. Two PAL systems, utilizing a 12 000°C plasma arc contained in a quartz tube cooled by a spiral water flow over the inside tube surface, provide maximum incident heat fluxes of 4.2 and 27 MW/m 2 over areas of 9×12 and 1×10 cm 2, respectively. This paper will present the overallmore » design and implementation of a PAL-based irradiated material target station (IMTS). The IMTS is primarily designed for testing the effects of heat flux or thermal cycling on material coupons of interest, such as those for plasma-facing components. Temperature results are shown for thermal cycling under HHFT of tungsten coupon specimens that were neutron irradiated in HFIR. Finally, radiological surveys indicated minimal contamination of the 36×36×18 cm test section, demonstrating the capability of the new facility to handle irradiated specimens at high temperature.« less

  8. Fast plasma shutdown by killer pellet injection in JT-60U with reduced heat flux on the divertor plate and avoiding runaway electron generation

    NASA Astrophysics Data System (ADS)

    Yoshino, R.; Kondoh, T.; Neyatani, Y.; Itami, K.; Kawano, Y.; Isei, N.

    1997-02-01

    A killer pellet is an impurity pellet that is injected into a tokamak plasma in order to terminate a discharge without causing serious damage to the tokamak machine. In JT-60U neon ice pellets have been injected into OH and NB heated plasmas and fast plasma shutdowns have been demonstrated without large vertical displacement. The heat pulse on the divertor plate has been greatly reduced by killer pellet injection (KPI), but a low-power heat flux tail with a long time duration is observed. The total energy on the divertor plate increases with longer heat flux tail, so it has been reduced by shortening the tail. Runaway electron (RE) generation has been observed just after KPI and/or in the later phase of the plasma current quench. However, RE generation has been avoided when large magnetic perturbations are excited. These experimental results clearly show that KPI is a credible fast shutdown method avoiding large vertical displacement, reducing heat flux on the divertor plate, and avoiding (or minimizing) RE generation.

  9. Heat flux measurement in SSME turbine blade tester

    NASA Astrophysics Data System (ADS)

    Liebert, Curt H.

    1990-11-01

    Surface heat flux values were measured in the turbine blade thermal cycling tester located at NASA-Marshall. This is the first time heat flux has been measured in a space shuttle main engine turbopump environment. Plots of transient and quasi-steady state heat flux data over a range of about 0 to 15 MW/sq m are presented. Data were obtained with a miniature heat flux gage device developed at NASA-Lewis. The results from these tests are being incorporated into turbine design models. Also, these gages are being considered for airfoil surface heat flux measurement on turbine vanes mounted in SSME turbopump test bed engine nozzles at Marshall. Heat flux effects that might be observed on degraded vanes are discussed.

  10. Heat flux measurement in SSME turbine blade tester

    NASA Astrophysics Data System (ADS)

    Liebert, Curt H.

    Surface heat flux values were measured in the turbine blade thermal cycling tester located at NASA-Marshall. This is the first time heat flux has been measured in a space shuttle main engine turbopump environment. Plots of transient and quasi-steady state heat flux data over a range of about 0 to 15 MW/sq m are presented. Data were obtained with a miniature heat flux gage device developed at NASA-Lewis. The results from these tests are being incorporated into turbine design models. Also, these gages are being considered for airfoil surface heat flux measurement on turbine vanes mounted in SSME turbopump test bed engine nozzles at Marshall. Heat flux effects that might be observed on degraded vanes are discussed.

  11. Fabrication of Thin Film Heat Flux Sensors

    NASA Technical Reports Server (NTRS)

    Will, Herbert A.

    1992-01-01

    Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied to propulsion system materials and components. The sensors can provide steady state and fast transient heat flux information. Fabrication of the sensor does not require any matching of the mounting surface. Heat flux is proportional to the temperature difference across the upper and lower surfaces of an insulation material. The sensor consists of an array of thermocouples on the upper and lower surfaces of a thin insulating layer. The thermocouples for the sensor are connected in a thermopile arrangement. A 100 thermocouple pair heat flux sensor has been fabricated on silicon wafers. The sensor produced an output voltage of 200-400 microvolts when exposed to a hot air heat gun. A 20 element thermocouple pair heat flux sensor has been fabricated on aluminum oxide sheet. Thermocouples are Pt-Pt/Rh with silicon dioxide as the insulating material. This sensor produced an output of 28 microvolts when exposed to the radiation of a furnace operating at 1000 C. Work is also underway to put this type of heat flux sensor on metal surfaces.

  12. Experimental results and a self-consistent model of evaporation and high heat flux extraction by evaporating flow in a micro-grooved blade

    NASA Astrophysics Data System (ADS)

    Monazami, Reza; Saadat, Mehdi; Zhu, Jianzhong; Haj-Hariri, Hossein

    2015-11-01

    The problem of evaporation from a vertical micro-grooved blade heated from above is investigated. The required superheat to handle the incoming flux is calculated using the results of the study by Monazami and Haj-Hariri (2012). The relation between the applied heat flux, dry-out length and the maximum equilibrium temperature for several geometries and working fluids are studied. Furthermore, a computational study of the evaporating meniscus is conducted to evaluate the evaporation rates and dissipated heat flux at the liquid-vapor interface. The computational study accounts for the flow and heat transfer in both liquid and vapor phases. The results of this study indicate that the micro-grooved structure can dissipate heat fluxes as high as 10MW/m2 for superheats as low as 5 degrees Kelvin. Experiments are conducted to verify the computational and analytical results. The findings of this work are applicable to the design of thermal management systems for high heat flux applications. Partially supported by the MAXNET Energy Partnership (Max Planck Institute and UVA).

  13. A new heat flux model for the Antarctic Peninsula incorporating spatially variable upper crustal radiogenic heat production

    NASA Astrophysics Data System (ADS)

    Burton-Johnson, A.; Halpin, J. A.; Whittaker, J. M.; Graham, F. S.; Watson, S. J.

    2017-06-01

    A new method for modeling heat flux shows that the upper crust contributes up to 70% of the Antarctic Peninsula's subglacial heat flux and that heat flux values are more variable at smaller spatial resolutions than geophysical methods can resolve. Results indicate a higher heat flux on the east and south of the Peninsula (mean 81 mW m-2) where silicic rocks predominate, than on the west and north (mean 67 mW m-2) where volcanic arc and quartzose sediments are dominant. While the data supports the contribution of heat-producing element-enriched granitic rocks to high heat flux values, sedimentary rocks can be of comparative importance dependent on their provenance and petrography. Models of subglacial heat flux must utilize a heterogeneous upper crust with variable radioactive heat production if they are to accurately predict basal conditions of the ice sheet. Our new methodology and data set facilitate improved numerical model simulations of ice sheet dynamics.Plain Language SummaryAs the climate changes, the Antarctic ice sheet represents the single largest potential source of sea level rise. However, one key parameter controlling how the ice sheet flows remains poorly constrained: the effect of <span class="hlt">heat</span> derived from the Earth's geology on the base of the ice sheet (known as subglacial <span class="hlt">heat</span> <span class="hlt">flux</span>). Although this may not seem like a lot of <span class="hlt">heat</span>, under slow-flowing ice, this "<span class="hlt">heat</span> <span class="hlt">flux</span>" can control how well the ice sheet can flow over the rocks and even lead to melting of the ice at its base. Current models for Antarctica's <span class="hlt">heat</span> <span class="hlt">flux</span> use geophysics to determine how thin the crust is and consequently how easily <span class="hlt">heat</span> from the Earth's mantle can warm the surface. We show here that <span class="hlt">heat</span> produced by radioactive decay within the Earth's crust can have an even greater and much more variable contribution to the subglacial <span class="hlt">heat</span> <span class="hlt">flux</span> than estimated by these previous models. We present a new methodology allowing this crustal <span class="hlt">heat</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1235747-role-surface-heat-fluxes-underneath-cold-pools','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1235747-role-surface-heat-fluxes-underneath-cold-pools"><span>Role of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Gentine, Pierre; Garelli, Alix; Park, Seung -Bu; ...</p> <p>2016-01-05</p> <p>In this paper, the role of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools is investigated using cloud–resolving simulations with either interactive or horizontally homogenous surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> over an ocean and a simplified land surface. Over the ocean, there are limited changes in the distribution of the cold pool temperature, humidity, and gust front velocity, yet interactive <span class="hlt">heat</span> <span class="hlt">fluxes</span> induce more cold pools, which are smaller, and convection is then less organized. Correspondingly, the updraft mass <span class="hlt">flux</span> and lateral entrainment are modified. Over the land surface, the <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools drastically impact the cold pool characteristics with more numerousmore » and smaller pools, which are warmer and more humid and accompanied by smaller gust front velocities. The interactive <span class="hlt">fluxes</span> also modify the updraft mass <span class="hlt">flux</span> and reduce convective organization. These results emphasize the importance of interactive surface <span class="hlt">fluxes</span> instead of prescribed <span class="hlt">flux</span> boundary conditions, as well as the formulation of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>, when studying convection.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4819715','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4819715"><span>Role of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Garelli, Alix; Park, Seung‐Bu; Nie, Ji; Torri, Giuseppe; Kuang, Zhiming</p> <p>2016-01-01</p> <p>Abstract The role of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools is investigated using cloud‐resolving simulations with either interactive or horizontally homogenous surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> over an ocean and a simplified land surface. Over the ocean, there are limited changes in the distribution of the cold pool temperature, humidity, and gust front velocity, yet interactive <span class="hlt">heat</span> <span class="hlt">fluxes</span> induce more cold pools, which are smaller, and convection is then less organized. Correspondingly, the updraft mass <span class="hlt">flux</span> and lateral entrainment are modified. Over the land surface, the <span class="hlt">heat</span> <span class="hlt">fluxes</span> underneath cold pools drastically impact the cold pool characteristics with more numerous and smaller pools, which are warmer and more humid and accompanied by smaller gust front velocities. The interactive <span class="hlt">fluxes</span> also modify the updraft mass <span class="hlt">flux</span> and reduce convective organization. These results emphasize the importance of interactive surface <span class="hlt">fluxes</span> instead of prescribed <span class="hlt">flux</span> boundary conditions, as well as the formulation of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>, when studying convection. PMID:27134320</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA583176','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA583176"><span>Nanoengineered Surfaces for <span class="hlt">High</span> <span class="hlt">Flux</span> Thin Film Evaporation</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2013-07-15</p> <p>for a variety of <span class="hlt">heat</span> transfer and resource conserving applications. References 1. Mudawar , I., Assessment of <span class="hlt">high-heat-flux</span> thermal...M.B. and I. Mudawar , <span class="hlt">High-flux</span> boiling in low-flow rate, low-pressure drop mini- channel and microchannel <span class="hlt">heat</span> sinks. International Journal of <span class="hlt">Heat</span>...pressure drop elements and fabricated nucleation sites. Journal of <span class="hlt">Heat</span> Transfer, 2006. 128(4): p. 389-396. 7. Qu, W. and I. Mudawar , Measurement and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910015008','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910015008"><span>Calibrator tests of <span class="hlt">heat</span> <span class="hlt">flux</span> gauges mounted in SSME blades</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Liebert, Curt H.</p> <p>1989-01-01</p> <p>Measurements of <span class="hlt">heat</span> <span class="hlt">flux</span> to space shuttle main engine (SSME) turbine blade surfaces are being made in the Lewis <span class="hlt">heat</span> <span class="hlt">flux</span> calibration facility. Surface <span class="hlt">heat</span> <span class="hlt">flux</span> information is obtained from transient temperature measurements taken at points within the gauge. A 100-kW Vortek arc lamp is used as a source of thermal radiant energy. Thermoplugs, with diameters of about 0.190 cm and lengths varying from about 0.190 to 0.320 cm, are being investigated. The thermoplug is surrounded on all surfaces except the active surface by a pocket of air located in the circular annulus and under the back cover. Since the thermoplug is insulated, it is assumed that <span class="hlt">heat</span> is conducted in a one-dimensional manner from the hot active surface to the cooler back side of the thermoplug. It is concluded that the miniature plug-type gauge concept is feasible for measurement of blade surface <span class="hlt">heat</span> <span class="hlt">flux</span>. It is suggested that it is important to measure <span class="hlt">heat</span> <span class="hlt">flux</span> near the hub on the suction surface and at the throat on SSME blades rotating in engines because stress and <span class="hlt">heat</span> transfer coefficients are <span class="hlt">high</span> in this region.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/6713305-third-law-thermodynamics-presence-heat-flux','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/6713305-third-law-thermodynamics-presence-heat-flux"><span>Third law of thermodynamics in the presence of a <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Camacho, J.</p> <p>1995-01-01</p> <p>Following a maximum entropy formalism, we study a one-dimensional crystal under a <span class="hlt">heat</span> <span class="hlt">flux</span>. We obtain the phonon distribution function and evaluate the nonequilibrium temperature, the specific <span class="hlt">heat</span>, and the entropy as functions of the internal energy and the <span class="hlt">heat</span> <span class="hlt">flux</span>, in both the quantum and the classical limits. Some analogies between the behavior of equilibrium systems at low absolute temperature and nonequilibrium steady states under <span class="hlt">high</span> values of the <span class="hlt">heat</span> <span class="hlt">flux</span> are shown, which point to a possible generalization of the third law in nonequilibrium situations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NucFu..57k6016X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NucFu..57k6016X"><span>Divertor <span class="hlt">heat</span> <span class="hlt">flux</span> simulations in ELMy H-mode discharges of EAST</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xia, T. Y.; Xu, X. Q.; Wu, Y. B.; Huang, Y. Q.; Wang, L.; Zheng, Z.; Liu, J. B.; Zang, Q.; Li, Y. Y.; Zhao, D.; EAST Team</p> <p>2017-11-01</p> <p>This paper presents <span class="hlt">heat</span> <span class="hlt">flux</span> simulations for the ELMy H-mode on the Experimental Advanced Superconducting Tokamak (EAST) using a six-field two-fluid model in BOUT++. Three EAST ELMy H-mode discharges with different plasma currents I p and geometries are studied. The trend of the scrape-off layer width λq with I p is reproduced by the simulation. The simulated width is only half of that derived from the EAST scaling law, but agrees well with the international multi-machine scaling law. Note that there is no radio-frequency (RF) <span class="hlt">heating</span> scheme in the simulations, and RF <span class="hlt">heating</span> can change the boundary topology and increase the <span class="hlt">flux</span> expansion. Anomalous <span class="hlt">electron</span> transport is found to contribute to the divertor <span class="hlt">heat</span> <span class="hlt">fluxes</span>. A coherent mode is found in the edge region in simulations. The frequency and poloidal wave number kθ are in the range of the edge coherent mode in EAST. The magnetic fluctuations of the mode are smaller than the electric field fluctuations. Statistical analysis of the type of turbulence shows that the turbulence transport type (blobby or turbulent) does not influence the <span class="hlt">heat</span> <span class="hlt">flux</span> width scaling. The two-point model differs from the simulation results but the drift-based model shows good agreement with simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22490062-heat-flux-plasma-flow-far-scrape-off-layer-inboard-poloidal-field-null-configuration-quest','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22490062-heat-flux-plasma-flow-far-scrape-off-layer-inboard-poloidal-field-null-configuration-quest"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> and plasma flow in the far scrape-off layer of the inboard poloidal field null configuration in QUEST</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Onchi, T.; Zushi, H.; Hanada, K.</p> <p>2015-08-15</p> <p><span class="hlt">Heat</span> <span class="hlt">flux</span> and plasma flow in the scrape-off layer (SOL) are examined for the inboard poloidal field null (IPN) configuration of the spherical tokamak QUEST. In the plasma current (I{sub p}) ramp-up phase, <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> (>1 MW/m{sup 2}) and supersonic flow (Mach number M > 1) are found to be present simultaneously in the far-SOL. The <span class="hlt">heat</span> <span class="hlt">flux</span> is generated by energetic <span class="hlt">electrons</span> excursed from the last closed <span class="hlt">flux</span> surface. Supersonic flows in the poloidal and toroidal directions are correlated with each other. In the quasi-steady state, sawtooth-like oscillation of I{sub p} at 20 Hz is observed. <span class="hlt">Heat</span> <span class="hlt">flux</span> and subsonic plasma flowmore » in the far-SOL are modified corresponding to the I{sub p}-oscillation. The <span class="hlt">heat</span> flow caused by motion of energetic <span class="hlt">electrons</span> and the bulk-particle transport to the far-SOL is enhanced during the low-I{sub p} phase. Modification of plasma flow in the far SOL occurs earlier than the I{sub p} crash. The M–I{sub p} curve has a limit-cycle characteristic with sawtooth-like oscillation. Such a core–SOL relationship indicates that the far-SOL flow plays an important role in sustaining the oscillation of I{sub p} in the IPN configuration.« less</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_7 --> <div id="page_8" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="141"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PPCF...60f5002K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PPCF...60f5002K"><span>Intermittent <span class="hlt">electron</span> density and temperature fluctuations and associated <span class="hlt">fluxes</span> in the Alcator C-Mod scrape-off layer</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kube, R.; Garcia, O. E.; Theodorsen, A.; Brunner, D.; Kuang, A. Q.; LaBombard, B.; Terry, J. L.</p> <p>2018-06-01</p> <p>The Alcator C-Mod mirror Langmuir probe system has been used to sample data time series of fluctuating plasma parameters in the outboard mid-plane far scrape-off layer. We present a statistical analysis of one second long time series of <span class="hlt">electron</span> density, temperature, radial electric drift velocity and the corresponding particle and <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span>. These are sampled during stationary plasma conditions in an ohmically <span class="hlt">heated</span>, lower single null diverted discharge. The <span class="hlt">electron</span> density and temperature are strongly correlated and feature fluctuation statistics similar to the ion saturation current. Both <span class="hlt">electron</span> density and temperature time series are dominated by intermittent, large-amplitude burst with an exponential distribution of both burst amplitudes and waiting times between them. The characteristic time scale of the large-amplitude bursts is approximately 15 μ {{s}}. Large-amplitude velocity fluctuations feature a slightly faster characteristic time scale and appear at a faster rate than <span class="hlt">electron</span> density and temperature fluctuations. Describing these time series as a superposition of uncorrelated exponential pulses, we find that probability distribution functions, power spectral densities as well as auto-correlation functions of the data time series agree well with predictions from the stochastic model. The <span class="hlt">electron</span> particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> present large-amplitude fluctuations. For this low-density plasma, the radial <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">flux</span> is dominated by convection, that is, correlations of fluctuations in the <span class="hlt">electron</span> density and radial velocity. Hot and dense blobs contribute only a minute fraction of the total fluctuation driven <span class="hlt">heat</span> <span class="hlt">flux</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160007555','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160007555"><span>Comparison of <span class="hlt">Heat</span> <span class="hlt">Flux</span> Gages for <span class="hlt">High</span> Enthalpy Flows - NASA Ames and IRS</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Loehle, Stefan; Nawaz, Anuscheh; Herdrich, Georg; Fasoulas, Stefanos; Martinez, Edward; Raiche, George</p> <p>2016-01-01</p> <p>This article is a companion to a paper on <span class="hlt">heat</span> <span class="hlt">flux</span> measurements as initiated under a Space Act Agreement in 2011. The current focus of this collaboration between the Institute of Space Systems (IRS) of the University of Stuttgart and NASA Ames Research Center is the comparison and refinement of diagnostic measurements. A first experimental campaign to test different <span class="hlt">heat</span> <span class="hlt">flux</span> gages in the NASA Interaction <span class="hlt">Heating</span> Facility (IHF) and the Plasmawindkanaele (PWK) at IRS was established. This paper focuses on the results of the measurements conducted at IRS. The tested gages included a at face and hemispherical probe head, a 4" hemispherical slug calorimeter, a null-point calorimeter from Ames and a null-point calorimeter developed for this purpose at IRS. The Ames null-point calorimeter was unfortunately defective upon arrival. The measured <span class="hlt">heat</span> <span class="hlt">fluxes</span> agree fairly well with each other. The reason for discrepancies can be attributed to signal-to-noise levels and the probe geometry.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24679302','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24679302"><span>Magnetic reconnection in plasma under inertial confinement fusion conditions driven by <span class="hlt">heat</span> <span class="hlt">flux</span> effects in Ohm's law.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Joglekar, A S; Thomas, A G R; Fox, W; Bhattacharjee, A</p> <p>2014-03-14</p> <p>In the interaction of <span class="hlt">high</span>-power laser beams with solid density plasma there are a number of mechanisms that generate strong magnetic fields. Such fields subsequently inhibit or redirect <span class="hlt">electron</span> flows, but can themselves be advected by <span class="hlt">heat</span> <span class="hlt">fluxes</span>, resulting in complex interplay between thermal transport and magnetic fields. We show that for <span class="hlt">heating</span> by multiple laser spots reconnection of magnetic field lines can occur, mediated by these <span class="hlt">heat</span> <span class="hlt">fluxes</span>, using a fully implicit 2D Vlasov-Fokker-Planck code. Under such conditions, the reconnection rate is dictated by <span class="hlt">heat</span> flows rather than Alfvènic flows. We find that this mechanism is only relevant in a <span class="hlt">high</span> β plasma. However, the Hall parameter ωcτei can be large so that thermal transport is strongly modified by these magnetic fields, which can impact longer time scale temperature homogeneity and ion dynamics in the system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940011344','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940011344"><span>Explosive Boiling at Very Low <span class="hlt">Heat</span> <span class="hlt">Fluxes</span>: A Microgravity Phenomenon</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hasan, M. M.; Lin, C. S.; Knoll, R. H.; Bentz, M. D.</p> <p>1993-01-01</p> <p>The paper presents experimental observations of explosive boiling from a large (relative to bubble sizes) flat <span class="hlt">heating</span> surface at very low <span class="hlt">heat</span> <span class="hlt">fluxes</span> in microgravity. The explosive boiling is characterized as either a rapid growth of vapor mass over the entire <span class="hlt">heating</span> surface due to the flashing of superheated liquid or a violent boiling spread following the appearance of single bubbles on the <span class="hlt">heating</span> surface. Pool boiling data with saturated Freon 113 was obtained in the microgravity environment of the space shuttle. The unique features of the experimental results are the sustainability of <span class="hlt">high</span> liquid superheat for long periods and the occurrence of explosive boiling at low <span class="hlt">heat</span> <span class="hlt">fluxes</span> (0.2 to 1.2 kW/sq m). For a <span class="hlt">heat</span> <span class="hlt">flux</span> of 1.0 kW/sq m a wall superheat of 17.9 degrees C was attained in ten minutes of <span class="hlt">heating</span>. This was followed by an explosive boiling accompanied with a pressure spike and a violent bulk liquid motion. However, at this <span class="hlt">heat</span> <span class="hlt">flux</span> the vapor blanketing the <span class="hlt">heating</span> surface could not be sustained. Stable nucleate boiling continued following the explosive boiling.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110013332','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110013332"><span>Using Models for How Energetic <span class="hlt">Electrons</span> <span class="hlt">Heat</span> the Atmosphere During Flares</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Allred, Joel</p> <p>2011-01-01</p> <p>Using models for how energetic <span class="hlt">electrons</span> <span class="hlt">heat</span> the atmosphere during flares, we simulate the radiative-hydrodynamic response of the lower solar atmosphere to flare <span class="hlt">heating</span>. The simulations account for much of the non-LTE, optically thick radiative transfer that occurs in the chromosphere. Our models predict an increase in white light continuum during the flare on the order of 20%, but this is <span class="hlt">highly</span> sensitive to the <span class="hlt">electron</span> beam <span class="hlt">flux</span> used in the simulation. We find that a majority of the white light continuum originates in the chromosphere as a result of Balmer and Paschen recombinations, but a significant portion also forms in the photosphere which has been <span class="hlt">heated</span> by radiative backwarming.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/867961','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/867961"><span>Optical <span class="hlt">heat</span> <span class="hlt">flux</span> gauge</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Noel, Bruce W.; Borella, Henry M.; Cates, Michael R.; Turley, W. Dale; MaCarthur, Charles D.; Cala, Gregory C.</p> <p>1991-01-01</p> <p>A <span class="hlt">heat</span> <span class="hlt">flux</span> gauge comprising first and second thermographic phosphor layers separated by a layer of a thermal insulator. The gauge may be mounted on a surface with the first thermographic phosphor in contact with the surface. A light source is directed at the gauge, causing the phosphors to luminesce. The luminescence produced by the phosphors is collected and its spectra analyzed in order to determine the <span class="hlt">heat</span> <span class="hlt">flux</span> on the surface. First and second phosphor layers must be different materials to assure that the spectral lines collected will be distinguishable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2003PlST....5.1887L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2003PlST....5.1887L"><span>Erosion and Modifications of Tungsten-Coated Carbon and Copper Under <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Xiang; S, Tamura; K, Tokunaga; N, Yoshida; Zhang, Fu; Xu, Zeng-yu; Ge, Chang-chun; N, Noda</p> <p>2003-08-01</p> <p>Tungsten-coated carbon and copper was prepared by vacuum plasma spraying (VPS) and inert gas plasma spraying (IPS), respectively. W/CFC (Tungsten/Carbon Fiber-Enhanced material) coating has a diffusion barrier that consists of W and Re multi-layers pre-deposited by physical vapor deposition on carbon fiber-enhanced materials, while W/Cu coating has a graded transition interface. Different grain growth processes of tungsten coatings under stable and transient <span class="hlt">heat</span> loads were observed, their experimental results indicated that the recrystallizing temperature of VPS-W coating was about 1400 °C and a recrystallized columnar layer of about 30 μm thickness was formed by cyclic <span class="hlt">heat</span> loads of 4 ms pulse duration. Erosion and modifications of W/CFC and W/Cu coatings under <span class="hlt">high</span> <span class="hlt">heat</span> load, such as microstructure changes of interface, surface plastic deformations and cracks, were investigated, and the erosion mechanism (erosion products) of these two kinds of tungsten coatings under <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> was also studied.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130014337','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130014337"><span>Thin Film <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensors: Design and Methodology</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fralick, Gustave C.; Wrbanek, John D.</p> <p>2013-01-01</p> <p>Thin Film <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensors: Design and Methodology: (1) <span class="hlt">Heat</span> <span class="hlt">flux</span> is one of a number of parameters, together with pressure, temperature, flow, etc. of interest to engine designers and fluid dynamists, (2) The measurement of <span class="hlt">heat</span> <span class="hlt">flux</span> is of interest in directly determining the cooling requirements of hot section blades and vanes, and (3)In addition, if the surface and gas temperatures are known, the measurement of <span class="hlt">heat</span> <span class="hlt">flux</span> provides a value for the convective <span class="hlt">heat</span> transfer coefficient that can be compared with the value provided by CFD codes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1409276','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1409276"><span>IR-thermography-based investigation of critical <span class="hlt">heat</span> <span class="hlt">flux</span> in subcooled flow boiling of water at atmospheric and <span class="hlt">high</span> pressure conditions</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Bucci, Matteo; Seong, Jee H.; Buongiorno, Jdacopo</p> <p></p> <p>Here we report on MIT’s THM work in Q4 2016 and Q1 2017. The goal of this project is to design, construct and execute tests of flow boiling critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) at <span class="hlt">high</span>-pressure using <span class="hlt">high</span>-resolution and <span class="hlt">high</span>-speed video and infrared (IR) thermometry, to generate unique data to inform the development of and validate mechanistic boiling <span class="hlt">heat</span> transfer and CHF models. In FY2016, a new test section was designed and fabricated. Data was collected at atmospheric conditions at 10, 25 and 50 K subcoolings, and three mass <span class="hlt">fluxes</span>, i.e. 500, 750 and 1000 kg/m2/s. Starting in Q4 2016 and continuingmore » forward, new post-processing techniques have been developed to analyze the data collected. These new algorithms analyze the time-dependent temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> distributions to calculate nucleation site density, nucleation frequency, growth and wait time, dry area fraction, and the complete <span class="hlt">heat</span> <span class="hlt">flux</span> partitioning. In Q1 2017 a new flow boiling loop was designed and constructed to support flow boiling tests up 10 bar pressure and 180 °C. Initial shakedown and testing has been completed. The flow loop and test section are now ready to begin <span class="hlt">high</span>-pressure flow boiling testing.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1994usee.work..203D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1994usee.work..203D"><span>Measurement of a surface <span class="hlt">heat</span> <span class="hlt">flux</span> and temperature</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Davis, R. M.; Antoine, G. J.; Diller, T. E.; Wicks, A. L.</p> <p>1994-04-01</p> <p>The <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor is a new sensor which was recently patented by Virginia Tech and is just starting to be marketed by Vatell Corp. The sensor is made using the thin-film microfabrication techniques directly on the material that is to be measured. It consists of several thin-film layers forming a differential thermopile across a thermal resistance layer. The measured <span class="hlt">heat</span> <span class="hlt">flux</span> q is proportional to the temperature difference across the resistance layer q= k(sub g)/delta(sub g) x (t(sub 1) - T(sub 2)), where k(sub g) is the thermal conductivity and delta (sub g) is the thickness of the thermal resistance layer. Because the gages are sputter coated directly onto the surface, their total thickness is less than 2 micrometers, which is two orders of magnitude thinner than previous gages. The resulting temperature difference across the thermal resistance layer (delta is less than 1 micrometer) is very small even at <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span>. To generate a measurable signal many thermocouple pairs are put in series to form a differential thermopile. The combination of series thermocouple junctions and thin-film design creates a gage with very attractive characteristics. It is not only physically non-intrusive to the flow, but also causes minimal disruption of the surface temperature. Because it is so thin, the response time is less than 20 microsec. Consequently, the frequency response is flat from 0 to over 50 kHz. Moreover, the signal of the <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor is directly proportional to the <span class="hlt">heat</span> <span class="hlt">flux</span>. Therefore, it can easily be used in both steady and transient flows, and it measures both the steady and unsteady components of the surface <span class="hlt">heat</span> <span class="hlt">flux</span>. A version of the <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor has been developed to meet the harsh demands of combustion environments. These gages use platinum and platinum-10 percent rhodium as the thermoelectric materials. The thermal resistance layer is silicon monoxide and a protective coating of Al2O3 is deposited on top of the sensor. The</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940031900','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940031900"><span>Measurement of a surface <span class="hlt">heat</span> <span class="hlt">flux</span> and temperature</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Davis, R. M.; Antoine, G. J.; Diller, T. E.; Wicks, A. L.</p> <p>1994-01-01</p> <p>The <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor is a new sensor which was recently patented by Virginia Tech and is just starting to be marketed by Vatell Corp. The sensor is made using the thin-film microfabrication techniques directly on the material that is to be measured. It consists of several thin-film layers forming a differential thermopile across a thermal resistance layer. The measured <span class="hlt">heat</span> <span class="hlt">flux</span> q is proportional to the temperature difference across the resistance layer q= k(sub g)/delta(sub g) x (t(sub 1) - T(sub 2)), where k(sub g) is the thermal conductivity and delta (sub g) is the thickness of the thermal resistance layer. Because the gages are sputter coated directly onto the surface, their total thickness is less than 2 micrometers, which is two orders of magnitude thinner than previous gages. The resulting temperature difference across the thermal resistance layer (delta is less than 1 micrometer) is very small even at <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span>. To generate a measurable signal many thermocouple pairs are put in series to form a differential thermopile. The combination of series thermocouple junctions and thin-film design creates a gage with very attractive characteristics. It is not only physically non-intrusive to the flow, but also causes minimal disruption of the surface temperature. Because it is so thin, the response time is less than 20 microsec. Consequently, the frequency response is flat from 0 to over 50 kHz. Moreover, the signal of the <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor is directly proportional to the <span class="hlt">heat</span> <span class="hlt">flux</span>. Therefore, it can easily be used in both steady and transient flows, and it measures both the steady and unsteady components of the surface <span class="hlt">heat</span> <span class="hlt">flux</span>. A version of the <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensor has been developed to meet the harsh demands of combustion environments. These gages use platinum and platinum-10 percent rhodium as the thermoelectric materials. The thermal resistance layer is silicon monoxide and a protective coating of Al2O3 is deposited on top of the sensor. The</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130000651','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130000651"><span>Surface Catalysis and Oxidation on Stagnation Point <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements in <span class="hlt">High</span> Enthalpy Arc Jets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Nawaz, Anuscheh; Driver, David M.; Terrazas-Salinas</p> <p>2013-01-01</p> <p><span class="hlt">Heat</span> <span class="hlt">flux</span> sensors are routinely used in arc jet facilities to determine <span class="hlt">heat</span> transfer rates from plasma plume. The goal of this study is to assess the impact of surface composition changes on these <span class="hlt">heat</span> <span class="hlt">flux</span> sensors. Surface compositions can change due to oxidation and material deposition from the arc jet. Systematic surface analyses of the sensors were conducted before and after exposure to plasma. Currently copper is commonly used as surface material. Other surface materials were studied including nickel, constantan gold, platinum and silicon dioxide. The surfaces were exposed to plasma between 0.3 seconds and 3 seconds. Surface changes due to oxidation as well as copper deposition from the arc jets were observed. Results from changes in measured <span class="hlt">heat</span> <span class="hlt">flux</span> as a function of surface catalycity is given, along with a first assessment of enthalpy for these measurements. The use of cupric oxide is recommended for future <span class="hlt">heat</span> <span class="hlt">flux</span> measurements, due to its consistent surface composition arc jets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..19.2080D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..19.2080D"><span>Wind stress and <span class="hlt">heat</span> <span class="hlt">fluxes</span> over a Brazilian Coastal Upwelling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dourado, Marcelo; Candella, Rogério</p> <p>2017-04-01</p> <p>-sea gradient. This could intensifies the sea breeze. At the same time, the latent <span class="hlt">heat</span> <span class="hlt">flux</span> to the atmosphere is reduced. As expected, cold waters from the upwelling imply in the reduction of the evaporation, and so the latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> also reduce significantly. As upwelling events in this region are associated to the presence of the South Atlantic <span class="hlt">high</span> pressure, NE winds, during these periods of cold water the net <span class="hlt">heat</span> <span class="hlt">flux</span> toward the ocean surface is intensified.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011A%26A...531A.162K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011A%26A...531A.162K"><span>Reynolds stress and <span class="hlt">heat</span> <span class="hlt">flux</span> in spherical shell convection</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Käpylä, P. J.; Mantere, M. J.; Guerrero, G.; Brandenburg, A.; Chatterjee, P.</p> <p>2011-07-01</p> <p>Context. Turbulent <span class="hlt">fluxes</span> of angular momentum and enthalpy or <span class="hlt">heat</span> due to rotationally affected convection play a key role in determining differential rotation of stars. Their dependence on latitude and depth has been determined in the past from convection simulations in Cartesian or spherical simulations. Here we perform a systematic comparison between the two geometries as a function of the rotation rate. Aims: Here we want to extend the earlier studies by using spherical wedges to obtain turbulent angular momentum and <span class="hlt">heat</span> transport as functions of the rotation rate from stratified convection. We compare results from spherical and Cartesian models in the same parameter regime in order to study whether restricted geometry introduces artefacts into the results. In particular, we want to clarify whether the sharp equatorial profile of the horizontal Reynolds stress found in earlier Cartesian models is also reproduced in spherical geometry. Methods: We employ direct numerical simulations of turbulent convection in spherical and Cartesian geometries. In order to alleviate the computational cost in the spherical runs, and to reach as <span class="hlt">high</span> spatial resolution as possible, we model only parts of the latitude and longitude. The rotational influence, measured by the Coriolis number or inverse Rossby number, is varied from zero to roughly seven, which is the regime that is likely to be realised in the solar convection zone. Cartesian simulations are performed in overlapping parameter regimes. Results: For slow rotation we find that the radial and latitudinal turbulent angular momentum <span class="hlt">fluxes</span> are directed inward and equatorward, respectively. In the rapid rotation regime the radial <span class="hlt">flux</span> changes sign in accordance with earlier numerical results, but in contradiction with theory. The latitudinal <span class="hlt">flux</span> remains mostly equatorward and develops a maximum close to the equator. In Cartesian simulations this peak can be explained by the strong "banana cells". Their effect in the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1850o0002F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1850o0002F"><span><span class="hlt">Heat</span> transfer experiments with a central receiver tube subjected to unsteady and non-uniform <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fernández-Torrijos, María; Marugán-Cruz, Carolina; Sobrino, Celia; Santana, Domingo</p> <p>2017-06-01</p> <p>In this work, a molten salt test loop to study the <span class="hlt">heat</span> transfer process in external molten salt receivers is described. The experimental installation is formed by a cylindrical molten salt tank, a pump, a flow meter, and an induction heater to generate the <span class="hlt">heat</span> <span class="hlt">flux</span>, which is applied in a small rectangular region of the tube surface. In central tower plants, the external receiver pipe is considered to be under unilateral concentrated solar radiation, because only one side of the pipe receives <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span>. The main advantage of using an induction heater is the control of <span class="hlt">heating</span> in different areas of the tube. In order to measure the effects of a non-homogenous and unsteady <span class="hlt">heat</span> <span class="hlt">flux</span> on the wall temperature distribution a series of experiments have been carried out. 4 K-type thermocouples have been welded at different axial and azimuthal positions of the pipe to obtain the wall temperature distribution. Different temperature measurements have been made varying the <span class="hlt">heat</span> <span class="hlt">flux</span> and water velocity to study their effects on the <span class="hlt">heat</span> transfer process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014JNuM..455..382L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014JNuM..455..382L"><span>Tungsten joining with copper alloy and its <span class="hlt">high</span> <span class="hlt">heat</span> load performance</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Xiang; Lian, Youyun; Chen, Lei; Cheng, Zengkui; Chen, Jiming; Duan, Xuru; Song, Jioupeng; Yu, Yang</p> <p>2014-12-01</p> <p>W-CuCrZr joining technology by using low activation Cu-Mn filler metal was developed at Southwestern Institute of Physics (SWIP) for the manufacturing of divertor components of fusion experiment devices. In addition, a fast W coating technology by chemical vapor deposition (CVD) was also developed and CVD-W/CuCrZr and CVD-W/C mockups with a W coating thickness of 2 mm were prepared. In order to assess their <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> (HHF) performances, a 60 kW <span class="hlt">Electron</span>-beam Material testing Scenario (EMS-60) equipped with a 150 keV <span class="hlt">electron</span> beam welding gun was constructed at SWIP. Experimental results indicated that brazed W/CuCrZr mockups can withstand 8 MW/m2 <span class="hlt">heat</span> <span class="hlt">flux</span> for 1000 cycles without visible damages and CVD-W/CuCrZr mockups with W-Cu gradient interface can survive 1000 cycles under 11 MW/m2 <span class="hlt">heat</span> <span class="hlt">flux</span>. An ultrasonic inspection method for non-destructive tests (NDT) of brazed W/CuCrZr mockups was established and 2 mm defect can be detected. Infinite element analysis and <span class="hlt">heat</span> load tests indicated that 5 mm defect had less noticeable influence on the <span class="hlt">heat</span> transfer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/867881','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/867881"><span>Optical <span class="hlt">heat</span> <span class="hlt">flux</span> gauge</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Noel, Bruce W.; Borella, Henry M.; Cates, Michael R.; Turley, W. Dale; MacArthur, Charles D.; Cala, Gregory C.</p> <p>1991-01-01</p> <p>A <span class="hlt">heat</span> <span class="hlt">flux</span> gauge comprising first and second thermographic phosphor layers separated by a layer of a thermal insulator wherein each thermographic layer comprises a plurality of respective thermographic phosphors. The gauge may be mounted on a surface with the first thermographic phosphor in contact with the surface. A light source is directed at the gauge, causing the phosphors to luminesce. The luminescence produced by the phosphors is collected and its spectra analyzed in order to determine the <span class="hlt">heat</span> <span class="hlt">flux</span> on the surface. First and second phosphor layers must be different materials to assure that the spectral lines collected will be distinguishable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26219636','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26219636"><span>A <span class="hlt">heat</span> <span class="hlt">flux</span> modulator from carbon nanotubes.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Jiang, Shaohui; Zhang, Guang; Xia, Dan; Liu, Changhong; Fan, Shoushan</p> <p>2015-08-28</p> <p>For a <span class="hlt">heat</span> <span class="hlt">flux</span> modulator, the most difficult problem is that the main carriers named 'phonons' have little response to external fields. Of the existing studies on <span class="hlt">heat</span> <span class="hlt">flux</span> modulators, most were theoretical work and the materials systems for the theoretical calculations were artificial lattices. In this paper, we made a <span class="hlt">heat</span> modulator with ultrathin buckypaper which was made of multi-layer carbon nanotube sheets overlapped together, and achieved an on/off ratio whose value was 1.41 using an pendent block in experiments without special optimizations. When the temperatures of the two sides were of appropriate values, we could even see a negative <span class="hlt">heat</span> <span class="hlt">flux</span>. Intuitively, the <span class="hlt">heat</span> <span class="hlt">flux</span> was tuned by the gap between the buckypaper and the pendent gate, and we observed that there was <span class="hlt">heat</span> transferred to the pendent block. The structure of the modulator is similar to a CNT transistor with a contactless gate, hence this type of micromodulator will be easy to manufacture in the future.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930022364','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930022364"><span>Progress in the measurement of SSME turbine <span class="hlt">heat</span> <span class="hlt">flux</span> with plug-type sensors</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Liebert, Curt H.</p> <p>1991-01-01</p> <p>Data reduction was completed for tests of plug-type <span class="hlt">heat</span> <span class="hlt">flux</span> sensors (gauges) in a turbine blade thermal cycling tester (TBT) that is located at NASA/Marshall Space Flight Center, and a typical gauge is illustrated. This is the first time that <span class="hlt">heat</span> <span class="hlt">flux</span> has been measured in a Space Shuttle Main Engine (SSME) Turbopump Turbine environment. The development of the concept for the gauge was performed in a <span class="hlt">heat</span> <span class="hlt">flux</span> measurement facility at Lewis. In this facility, transient and steady state absorbed surface <span class="hlt">heat</span> <span class="hlt">flux</span> information was obtained from transient temperature measurements taken at points within the gauge. A schematic of the TBT is presented, and plots of the absorbed surface <span class="hlt">heat</span> <span class="hlt">flux</span> measured on the three blades tested in the TBT are presented. <span class="hlt">High</span> quality <span class="hlt">heat</span> <span class="hlt">flux</span> values were measured on all three blades. The experiments demonstrated that reliable and durable gauges can be repeatedly fabricated into the airfoils. The experiment <span class="hlt">heat</span> <span class="hlt">flux</span> data are being used for verification of SSME analytical stress, boundary layer, and <span class="hlt">heat</span> transfer design models. Other experimental results and future plans are also presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1084256','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/1084256"><span>Tracking <span class="hlt">heat</span> <span class="hlt">flux</span> sensors for concentrating solar applications</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Andraka, Charles E; Diver, Jr., Richard B</p> <p>2013-06-11</p> <p>Innovative tracking <span class="hlt">heat</span> <span class="hlt">flux</span> sensors located at or near the solar collector's focus for centering the concentrated image on a receiver assembly. With <span class="hlt">flux</span> sensors mounted near a receiver's aperture, the <span class="hlt">flux</span> gradient near the focus of a dish or trough collector can be used to precisely position the focused solar <span class="hlt">flux</span> on the receiver. The <span class="hlt">heat</span> <span class="hlt">flux</span> sensors comprise two closely-coupled thermocouple junctions with opposing electrical polarity that are separated by a thermal resistor. This arrangement creates an electrical signal proportional to <span class="hlt">heat</span> <span class="hlt">flux</span> intensity, and largely independent of temperature. The sensors are thermally grounded to allow a temperature difference to develop across the thermal resistor, and are cooled by a <span class="hlt">heat</span> sink to maintain an acceptable operating temperature.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_8 --> <div id="page_9" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="161"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..MARH25007F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..MARH25007F"><span>Phase-coherent engineering of <span class="hlt">electronic</span> <span class="hlt">heat</span> currents with a Josephson modulator</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fornieri, Antonio; Blanc, Christophe; Bosisio, Riccardo; D'Ambrosio, Sophie; Giazotto, Francesco</p> <p></p> <p>In this contribution we report the realization of the first balanced Josephson <span class="hlt">heat</span> modulator designed to offer full control at the nanoscale over the phase-coherent component of <span class="hlt">electronic</span> thermal currents. The ability to master the amount of <span class="hlt">heat</span> transferred through two tunnel-coupled superconductors by tuning their phase difference is the core of coherent caloritronics, and is expected to be a key tool in a number of nanoscience fields, including solid state cooling, thermal isolation, radiation detection, quantum information and thermal logic. Our device provides magnetic-<span class="hlt">flux</span>-dependent temperature modulations up to 40 mK in amplitude with a maximum of the <span class="hlt">flux</span>-to-temperature transfer coefficient reaching 200 mK per <span class="hlt">flux</span> quantum at a bath temperature of 25 mK. Foremost, it demonstrates the exact correspondence in the phase-engineering of charge and <span class="hlt">heat</span> currents, breaking ground for advanced caloritronic nanodevices such as thermal splitters, <span class="hlt">heat</span> pumps and time-dependent <span class="hlt">electronic</span> engines.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930022365','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930022365"><span>Thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensor for Space Shuttle Main Engine turbine environment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Will, Herbert</p> <p>1991-01-01</p> <p>The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design limits and beyond. The extremely <span class="hlt">high</span> temperatures and rapid temperature cycling can easily cause parts to fail if they are not properly designed. Thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensors can provide <span class="hlt">heat</span> loading information with almost no disturbance of gas flows or of the blade. These sensors can provide steady state and transient <span class="hlt">heat</span> <span class="hlt">flux</span> information. A thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensor is described which makes it easier to measure small temperature differences across very thin insulating layers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhST..170a4022R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhST..170a4022R"><span>Realization of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> tungsten monoblock type target with graded interlayer for application to DEMO divertor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Richou, M.; Gallay, F.; Böswirth, B.; Chu, I.; Lenci, M.; Loewenhoff, Th; Quet, A.; Greuner, H.; Kermouche, G.; Meillot, E.; Pintsuk, G.; Visca, E.; You, J. H.</p> <p>2017-12-01</p> <p>The divertor is the key in-vessel plasma-facing component being in charge of power exhaust and removal of impurity particles. In DEMO, divertor targets must survive an environment of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> (˜up to 20 MW m-2 during slow transients) and neutron irradiation. One advanced concept for components in monoblock configuration concerns the insertion of a compositionally graded layer between tungsten and CuCrZr instead of the soft copper interlayer. As a first step, a thin graded layer (˜25 μm) was developed. As a second step, a thicker graded layer (˜500 μm), which is actually being developed, will also be inserted to study the compliant role of a macroscopic graded layer. This paper reports the results of cyclic <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> loading tests up to 20 MW m-2 and to <span class="hlt">heat</span> <span class="hlt">flux</span> higher than 25 MW m-2 that mock-ups equipped with thin graded layer survived without visible damage. First feedback on manufacturing steps is also presented. Moreover, the first results obtained on the development of the thick graded layer and its integration in a monoblock configuration are shown.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70190499','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70190499"><span>Viscous relaxation of Ganymede's impact craters: Constraints on <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Bland, Michael T.; Singer, Kelsi N.; McKinnon, William B.; Schenk, Paul M.</p> <p>2017-01-01</p> <p>Measurement of crater depths in Ganymede’s dark terrain have revealed substantial numbers of unusually shallow craters indicative of viscous relaxation [see companion paper: Singer, K.N., Schenk, P. M., Bland, M.T., McKinnon, W.B., (2017). Relaxed impact craters on Ganymede: Regional variations and <span class="hlt">high</span> <span class="hlt">heat</span> flow. Icarus, submitted]. These viscously relaxed craters provide insight into the thermal history of the dark terrain: the rate of relaxation depends on the size of the crater and the thermal structure of the lithosphere. Here we use finite element simulations of crater relaxation to constrain the <span class="hlt">heat</span> <span class="hlt">flux</span> within the dark terrain when relaxation occurred. We show that the degree of viscous relaxation observed cannot be achieved through radiogenic <span class="hlt">heating</span> alone, even if all of the relaxed craters are ancient and experienced the <span class="hlt">high</span> radiogenic <span class="hlt">fluxes</span> present early in the satellite’s history. For craters with diameter ≥ 10 km, <span class="hlt">heat</span> <span class="hlt">fluxes</span> of 40–50 mW m-2−2"> can reproduce the observed crater depths, but only if the <span class="hlt">fluxes</span> are sustained for ∼1 Gyr. These craters can also be explained by shorter-lived “<span class="hlt">heat</span> pulses” with magnitudes of ∼100 mW m-2−2"> and timescales of 10–100 Myr. At small crater diameters (4 km) the observed shallow depths are difficult to achieve even when <span class="hlt">heat</span> <span class="hlt">fluxes</span> as <span class="hlt">high</span> as 150 mW m-2−2"> are sustained for 1 Gyr. The extreme thermal conditions required to viscously relax small craters may indicate that mechanisms other than viscous relaxation, such as topographic degradation, are also in play at small crater diameters. The timing of the relaxation event(s) is poorly constrained due to the sparsity of adequate topographic information, though it likely occurred in Ganymede’s middle history (neither recently, nor shortly after satellite formation). The consistency between the timing and magnitude of the <span class="hlt">heat</span> <span class="hlt">fluxes</span> derived here and those inferred from other tectonic features suggests that a single event</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017Icar..296..275B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017Icar..296..275B"><span>Viscous relaxation of Ganymede's impact craters: Constraints on <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bland, Michael T.; Singer, Kelsi N.; McKinnon, William B.; Schenk, Paul M.</p> <p>2017-11-01</p> <p>Measurement of crater depths in Ganymede's dark terrain have revealed substantial numbers of unusually shallow craters indicative of viscous relaxation [see companion paper: Singer, K.N., Schenk, P. M., Bland, M.T., McKinnon, W.B., (2017). Relaxed impact craters on Ganymede: Regional variations and <span class="hlt">high</span> <span class="hlt">heat</span> flow. Icarus, submitted]. These viscously relaxed craters provide insight into the thermal history of the dark terrain: the rate of relaxation depends on the size of the crater and the thermal structure of the lithosphere. Here we use finite element simulations of crater relaxation to constrain the <span class="hlt">heat</span> <span class="hlt">flux</span> within the dark terrain when relaxation occurred. We show that the degree of viscous relaxation observed cannot be achieved through radiogenic <span class="hlt">heating</span> alone, even if all of the relaxed craters are ancient and experienced the <span class="hlt">high</span> radiogenic <span class="hlt">fluxes</span> present early in the satellite's history. For craters with diameter ≥ 10 km, <span class="hlt">heat</span> <span class="hlt">fluxes</span> of 40-50 mW m-2 can reproduce the observed crater depths, but only if the <span class="hlt">fluxes</span> are sustained for ∼1 Gyr. These craters can also be explained by shorter-lived "<span class="hlt">heat</span> pulses" with magnitudes of ∼100 mW m-2 and timescales of 10-100 Myr. At small crater diameters (4 km) the observed shallow depths are difficult to achieve even when <span class="hlt">heat</span> <span class="hlt">fluxes</span> as <span class="hlt">high</span> as 150 mW m-2 are sustained for 1 Gyr. The extreme thermal conditions required to viscously relax small craters may indicate that mechanisms other than viscous relaxation, such as topographic degradation, are also in play at small crater diameters. The timing of the relaxation event(s) is poorly constrained due to the sparsity of adequate topographic information, though it likely occurred in Ganymede's middle history (neither recently, nor shortly after satellite formation). The consistency between the timing and magnitude of the <span class="hlt">heat</span> <span class="hlt">fluxes</span> derived here and those inferred from other tectonic features suggests that a single event caused both Ganymede's tectonic deformation and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950057072&hterms=coverage&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcoverage','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950057072&hterms=coverage&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcoverage"><span>Relativistic <span class="hlt">electron</span> <span class="hlt">flux</span> comparisons at low and <span class="hlt">high</span> altitudes with fast time resolution and broad spatial coverage</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Imhof, W. L.; Gaines, E. E.; Mcglennon, J. P.; Baker, D. N.; Reeves, G. D.; Belian, R. D.</p> <p>1994-01-01</p> <p>Analyses are presented for the first <span class="hlt">high</span>-time resolution multisatellite study of the spatial and temporal characteristics of a relativistic <span class="hlt">electron</span> enhancement event with a rapid onset. Measurements of MeV <span class="hlt">electrons</span> were made from two low-altitude polar orbiting satellites and three spacecraft at synchronous altitude. The <span class="hlt">electron</span> <span class="hlt">fluxes</span> observed by the low-altitude satellites include precipitating <span class="hlt">electrons</span> in both the bounce and drift loss cones as well as <span class="hlt">electrons</span> that are stably trapped, whereas the observations at geosynchronous altitude are dominated by the trapped population. The <span class="hlt">fluxes</span> of greater than 1 MeV <span class="hlt">electrons</span> at low-satellite altitude over a wide range of L shells tracked very well the <span class="hlt">fluxes</span> greater than 0.93 MeV at synchronous altitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1917050Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1917050Z"><span>Mesoscale eddies control meridional <span class="hlt">heat</span> <span class="hlt">flux</span> variability in the subpolar North Atlantic</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhao, Jian; Bower, Amy; Yang, Jiayan; Lin, Xiaopei; Zhou, Chun</p> <p>2017-04-01</p> <p>The meridional <span class="hlt">heat</span> <span class="hlt">flux</span> in the subpolar North Atlantic is vital to the climate of the <span class="hlt">high</span>-latitude North Atlantic. For the basinwide <span class="hlt">heat</span> <span class="hlt">flux</span> across a section between Greenland and Scotland, much of the variability occurs in the Iceland basin, where the North Atlantic Current (NAC) carries relatively warm and salty water northward. As a component of the Overturning in the Subpolar North Atlantic Program (OSNAP), WHOI and OUC are jointly operating gliders in the Iceland Basin to continuously monitor the circulation and corresponding <span class="hlt">heat</span> <span class="hlt">flux</span> in this eddy-rich region. Based on one year of observations, two circulation regimes in the Iceland basin have been identified: a mesoscale eddy like circulation pattern and northward NAC circulation pattern. When a mesoscale eddy is generated, the rotational currents associated with the eddy lead to both northward and southward flow in the Iceland basin. This is quite different from the broad northward flow associated with the NAC when there is no eddy. The transition between the two regimes coupled with the strong temperature front in the Iceland basin can modify the meridional <span class="hlt">heat</span> <span class="hlt">flux</span> on the order of 0.3PW, which is the dominant source for the <span class="hlt">heat</span> <span class="hlt">flux</span> change the Iceland Basin. According to <span class="hlt">high</span>-resolution numerical model results, the Iceland Basin has the largest contribution to the meridional <span class="hlt">heat</span> <span class="hlt">flux</span> variability along the section between Greenland and Scotland. Therefore, mesoscale eddies in the Iceland Basin provide important dynamics to control the meridional <span class="hlt">heat</span> <span class="hlt">flux</span> variability in the subpolar North Atlantic.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015MicST..27..369W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015MicST..27..369W"><span>Experiments of Transient Condensation <span class="hlt">Heat</span> Transfer on the <span class="hlt">Heat</span> <span class="hlt">Flux</span> Senor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Xuwen; Liu, Qiusheng; Zhu, Zhiqiang; Chen, Xue</p> <p>2015-09-01</p> <p>The influence of transient <span class="hlt">heat</span> transfer in different condensation condition was investigated experimentally in the present paper. Getting condensation <span class="hlt">heat</span> and mass transfer regularity and characteristics in space can provide theoretical basis for thermodynamic device such as <span class="hlt">heat</span> pipes, loop <span class="hlt">heat</span> pipes and capillary pumped loops as well as other fluid management engineering designing. In order to study the condensation process in space, an experimental study has been carried out on the ground for space experiment. The results show that transit <span class="hlt">heat</span> transfer coefficient of film condensation is related to the condensation film width, the flow condition near the two phase interface and the pressure of the vapor and non-condensable gas in chamber. On the ground, the condensation <span class="hlt">heat</span> <span class="hlt">flux</span> on vertical surface is higher than it on horizontal surface. The transit <span class="hlt">heat</span> <span class="hlt">flux</span> of film condensation is affected by the temperature of superheated vapor, the temperature of condensation surface and non-condensable gas pressure. Condensation <span class="hlt">heat</span> <span class="hlt">flux</span> with vapor forced convection is many times more than it with natural convection. All of <span class="hlt">heat</span> <span class="hlt">flux</span> for both vapor forced convection and natural convection condensation in limited chamber declines dramatically over time. The present experiment is preliminary work for our future space experiments of the condensation and <span class="hlt">heat</span> transfer process onboard the Chinese Spacecraft "TZ-1" to be launched in 2016.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1223069-evaluation-cooling-conditions-high-heat-flux-testing-facility-based-plasma-arc-lamps','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1223069-evaluation-cooling-conditions-high-heat-flux-testing-facility-based-plasma-arc-lamps"><span>Evaluation of Cooling Conditions for a <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Testing Facility Based on Plasma-Arc Lamps</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Charry, Carlos H.; Abdel-khalik, Said I.; Yoda, Minami; ...</p> <p>2015-07-31</p> <p>The new Irradiated Material Target Station (IMTS) facility for fusion materials at Oak Ridge National Laboratory (ORNL) uses an infrared plasma-arc lamp (PAL) to deliver incident <span class="hlt">heat</span> <span class="hlt">fluxes</span> as <span class="hlt">high</span> as 27 MW/m 2. The facility is being used to test irradiated plasma-facing component materials as part of the joint US-Japan PHENIX program. The irradiated samples are to be mounted on molybdenum sample holders attached to a water-cooled copper rod. Depending on the size and geometry of samples, several sample holders and copper rod configurations have been fabricated and tested. As a part of the effort to design sample holdersmore » compatible with the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> (HHF) testing to be conducted at the IMTS facility, numerical simulations have been performed for two different water-cooled sample holder designs using the ANSYS FLUENT 14.0 commercial computational fluid dynamics (CFD) software package. The primary objective of this work is to evaluate the cooling capability of different sample holder designs, i.e. to estimate their maximum allowable incident <span class="hlt">heat</span> <span class="hlt">flux</span> values. 2D axisymmetric numerical simulations are performed using the realizable k-ε turbulence model and the RPI nucleate boiling model within ANSYS FLUENT 14.0. The results of the numerical model were compared against the experimental data for two sample holder designs tested in the IMTS facility. The model has been used to parametrically evaluate the effect of various operational parameters on the predicted temperature distributions. The results were used to identify the limiting parameter for safe operation of the two sample holders and the associated peak <span class="hlt">heat</span> <span class="hlt">flux</span> limits. The results of this investigation will help guide the development of new sample holder designs.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/867765','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/867765"><span>Optical <span class="hlt">heat</span> <span class="hlt">flux</span> gauge</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Noel, Bruce W.; Borella, Henry M.; Cates, Michael R.; Turley, W. Dale; MacArthur, Charles D.; Cala, Gregory C.</p> <p>1991-01-01</p> <p>A <span class="hlt">heat</span> <span class="hlt">flux</span> gauge comprising first and second thermographic phosphor layers separated by a layer of a thermal insulator, wherein each thermographic layer comprises a plurality of respective thermographic sensors in a juxtaposed relationship with respect to each other. The gauge may be mounted on a surface with the first thermographic phosphor in contact with the surface. A light source is directed at the gauge, causing the phosphors to luminesce. The luminescence produced by the phosphors is collected and its spectra analyzed in order to determine the <span class="hlt">heat</span> <span class="hlt">flux</span> on the surface. First and second phosphor layers must be different materials to assure that the spectral lines collected will be distinguishable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC21G1021K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC21G1021K"><span>Causes of Potential Urban <span class="hlt">Heat</span> Island Space Using <span class="hlt">Heat</span> <span class="hlt">flux</span> Budget Under Urban Canopy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwon, Y. J.; Lee, D. K.</p> <p>2017-12-01</p> <p>Raised concerns about possible contribution from urban <span class="hlt">heat</span> island to global warming is about 30 percent. Therefore, mitigating urban <span class="hlt">heat</span> island became one of major issues to solve among urban planners, urban designers, landscape architects, urban affair decision makers and etc. Urban <span class="hlt">heat</span> island effect on a micro-scale is influenced by factors such as wind, water vapor and solar radiation. Urban <span class="hlt">heat</span> island effect on a microscale is influenced by factors like wind, water vapor and solar radiation. These microscopic climates are also altered by factors affecting the <span class="hlt">heat</span> content in space, like SVF and aspect ratio depending on the structural characteristics of various urban canyon components. Indicators of <span class="hlt">heat</span> mitigation in urban design stage allows us to create a spatial structure considering the <span class="hlt">heat</span> balance budget. The spatial characteristics affect thermal change by varying <span class="hlt">heat</span> storage, emitting or absorbing the <span class="hlt">heat</span>. The research defines characteristics of the space composed of the factors affecting the <span class="hlt">heat</span> <span class="hlt">flux</span> change as the potential urban <span class="hlt">heat</span> island space. Potential urban <span class="hlt">heat</span> island spaces are that having higher <span class="hlt">heat</span> <span class="hlt">flux</span> than periphery space. The study is to know the spatial characteristics that affects the subsequent temperature rise by the <span class="hlt">heat</span> <span class="hlt">flux</span>. As a research method, four types of potential <span class="hlt">heat</span> island space regions were analyzed. I categorized the spatial types by comparing parameters' value of energy balance in day and night: 1) day severe areas, 2) day comfort areas, 3) night severe areas, 4) night comfort areas. I have looked at these four types of potential urban <span class="hlt">heat</span> island areas from a microscopic perspective and investigated how various forms of <span class="hlt">heat</span> influences on higher <span class="hlt">heat</span> <span class="hlt">flux</span> areas. This research was designed to investigate the <span class="hlt">heat</span> indicators to be reflected in the design of urban canyon for <span class="hlt">heat</span> mitigation. As a result, severe areas in daytime have <span class="hlt">high</span> SVF rate, sensible <span class="hlt">heat</span> is generated. Day comfort areas have shadow effect</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1030872','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1030872"><span>Effects of Mixed Layer Shear on Vertical <span class="hlt">Heat</span> <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2016-12-01</p> <p>correlation of ice speed to <span class="hlt">heat</span> <span class="hlt">flux</span> (r = .312, p < .001). Relationships between ice speed and shear (r = .107, p < .001), ice speed and inverse ...Richardson number (r = .035, p = .256), inverse Richardson number and <span class="hlt">heat</span> <span class="hlt">flux</span> (r = .3, p < .001), <span class="hlt">heat</span> content and <span class="hlt">heat</span> <span class="hlt">flux</span> (r = .084, p < .001) were...correlation of ice speed to <span class="hlt">heat</span> <span class="hlt">flux</span> (r = .312, p < .001). Relationships between ice speed and shear (r = .107, p < .001), ice speed and inverse Richardson</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013AGUFMSM33A2171P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013AGUFMSM33A2171P"><span>Prediction of <span class="hlt">high</span>-energy radiation belt <span class="hlt">electron</span> <span class="hlt">fluxes</span> using a combined VERB-NARMAX model</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pakhotin, I. P.; Balikhin, M. A.; Shprits, Y.; Subbotin, D.; Boynton, R.</p> <p>2013-12-01</p> <p>This study is concerned with the modelling and forecasting of energetic <span class="hlt">electron</span> <span class="hlt">fluxes</span> that endanger satellites in space. By combining data-driven predictions from the NARMAX methodology with the physics-based VERB code, it becomes possible to predict <span class="hlt">electron</span> <span class="hlt">fluxes</span> with a <span class="hlt">high</span> level of accuracy and across a radial distance from inside the local acceleration region to out beyond geosynchronous orbit. The model coupling also makes is possible to avoid accounting for seed <span class="hlt">electron</span> variations at the outer boundary. Conversely, combining a convection code with the VERB and NARMAX models has the potential to provide even greater accuracy in forecasting that is not limited to geostationary orbit but makes predictions across the entire outer radiation belt region.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/21612531-operation-ornl-high-particle-flux-helicon-plasma-source','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/21612531-operation-ornl-high-particle-flux-helicon-plasma-source"><span>Operation of the ORNL <span class="hlt">High</span> Particle <span class="hlt">Flux</span> Helicon Plasma Source</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Goulding, R. H.; Biewer, T. M.; Caughman, J. B. O.</p> <p>2011-12-23</p> <p>A <span class="hlt">high</span> power, <span class="hlt">high</span> particle <span class="hlt">flux</span> rf-based helicon plasma source has been constructed at ORNL and operated at power levels up to 30 kW. <span class="hlt">High</span>-density hydrogen and helium plasmas have been produced. The source has been designed as the basis for a linear plasma materials interaction (PMI) test facility that will generate particle <span class="hlt">fluxes</span> {Gamma}{sub p}10{sup 23} m{sup -3} s{sup -1}, and utilize additional ion and <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> to produce <span class="hlt">high</span> parallel (to the magnetic field) <span class="hlt">heat</span> <span class="hlt">fluxes</span> of {approx}10 MW/m{sup 2}. An rf-based source for PMI research is of interest because <span class="hlt">high</span> plasma densities are generated with nomore » internal electrodes, allowing true steady state operation with minimal impurity generation. The ORNL helicon source has a diameter of 15 cm and to-date has operated at a frequency f = 13.56 MHz, with magnetic field strength |B| in the antenna region up to {approx}0.15 T. Maximum densities of 3x10{sup 19} m{sup -3} in He and 2.5x10{sup 19} m{sup -3} in H have been achieved. Radial density profiles have been seen to be dependent on the axial |B| profile.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1048174-operation-ornl-high-particle-flux-helicon-plasma-source','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1048174-operation-ornl-high-particle-flux-helicon-plasma-source"><span>Operation of the ORNL <span class="hlt">High</span> Particle <span class="hlt">Flux</span> Helicon Plasma Source</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Goulding, Richard Howell; Biewer, Theodore M; Caughman, John B</p> <p>2011-01-01</p> <p>A <span class="hlt">high</span> power, <span class="hlt">high</span> particle <span class="hlt">flux</span> rf-based helicon plasma source has been constructed at ORNL and operated at power levels up to 30 kW. <span class="hlt">High</span>-density hydrogen and helium plasmas have been produced. The source has been designed as the basis for a linear plasma materials interaction (PMI) test facility that will generate particle <span class="hlt">fluxes</span> Gamma(p) > 10(23) M-3 s(-1), and utilize additional ion and <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> to produce <span class="hlt">high</span> parallel (to the magnetic field) <span class="hlt">heat</span> <span class="hlt">fluxes</span> of similar to 10 MW/m(2). An rf-based source for PMI research is of interest because <span class="hlt">high</span> plasma densities are generated with no internalmore » electrodes, allowing true steady state operation with minimal impurity generation. The ORNL helicon source has a diameter of 15 cm and to-date has operated at a frequency f = 13.56 MHz, with magnetic field strength vertical bar B vertical bar in the antenna region up to similar to 0.15 T. Maximum densities of 3 x 10(19) M-3 in He and 2.5 x 10(19) m(-3) in H have been achieved. Radial density profiles have been seen to be dependent on the axial vertical bar B vertical bar profile.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010ApPhL..97h1502D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010ApPhL..97h1502D"><span>Production of <span class="hlt">high</span> transient <span class="hlt">heat</span> and particle <span class="hlt">fluxes</span> in a linear plasma device</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>De Temmerman, G.; Zielinski, J. J.; van der Meiden, H.; Melissen, W.; Rapp, J.</p> <p>2010-08-01</p> <p>We report on the generation of <span class="hlt">high</span> transient <span class="hlt">heat</span> and particle <span class="hlt">fluxes</span> in a linear plasma device by pulsed operation of the plasma source. A capacitor bank is discharged into the source to transiently increase the discharge current up to 1.7 kA, allowing peak densities and temperature of 70×1020 m-3 and 6 eV corresponding to a surface power density of about 400 MW m-2.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhST..170a4007B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhST..170a4007B"><span>Comparison of <span class="hlt">heat</span> <span class="hlt">flux</span> measurement techniques during the DIII-D metal ring campaign</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Barton, J. L.; Nygren, R. E.; Unterberg, E. A.; Watkins, J. G.; Makowski, M. A.; Moser, A.; Rudakov, D. L.; Buchenauer, D.</p> <p>2017-12-01</p> <p>The <span class="hlt">heat</span> <span class="hlt">fluxes</span> expected in the ITER divertor raise concerns about the damage tolerances of tungsten, especially due to thermal transients caused by edge localized modes (ELMs) as well as frequent temperature cycling from <span class="hlt">high</span> to low extremes. Therefore we are motivated to understand the <span class="hlt">heat</span> <span class="hlt">flux</span> conditions that can cause not only enhanced erosion but also bulk thermo-mechanical damage to a tungsten divertor. For the metal ring campaign in DIII-D, tungsten-coated TZM tile inserts were installed making two toroidal arrays of metal tile inserts in the lower divertor. This study examines the deposited <span class="hlt">heat</span> <span class="hlt">flux</span> on these rings with embedded thermocouples (TCs) sampling at 10 kHz and compares them to Langmuir probe (LP) and infrared thermography (IRTV) <span class="hlt">heat</span> <span class="hlt">flux</span> measurements. We see agreement of the TC, LP, and IRTV data within 20% of the <span class="hlt">heat</span> <span class="hlt">flux</span> averaged over the entire discharge, and that all three diagnostics suggest parallel <span class="hlt">heat</span> <span class="hlt">flux</span> at the OSP location increases linearly with input <span class="hlt">heating</span> power. The TC and LP <span class="hlt">heat</span> <span class="hlt">flux</span> time traces during the discharge trend together during large changes to the average <span class="hlt">heat</span> <span class="hlt">flux</span>. By subtracting the LP measured inter-ELM <span class="hlt">heat</span> <span class="hlt">flux</span> from TC data, using a rectangular ELM energy pulse shape, and taking the relative size and duration of each ELM from {{D}}α measurements, we extract the ELM <span class="hlt">heat</span> <span class="hlt">fluxes</span> from TC data. This over-estimates the IRTV measured ELM <span class="hlt">heat</span> <span class="hlt">fluxes</span> by a factor of 1.9, and could be due to the simplicity of the TC <span class="hlt">heat</span> <span class="hlt">flux</span> model and the assumed ELM energy pulse shape. ELM <span class="hlt">heat</span> <span class="hlt">fluxes</span> deposited on the inserts are used to model tungsten erosion in this campaign. These TC ELM <span class="hlt">heat</span> <span class="hlt">flux</span> estimates are used in addition to IRTV, especially in cases where the IRTV view to the metal ring is obstructed. We observe that some metal inserts were deformed due to exposed leading edges. The thermal conditions on these inserts are investigated with the thermal modeling code ABAQUS using our <span class="hlt">heat</span> <span class="hlt">flux</span> measurements when these edges</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EGUGA..1615572B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EGUGA..1615572B"><span>Towards Improved Estimates of Ocean <span class="hlt">Heat</span> <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bentamy, Abderrahim; Hollman, Rainer; Kent, Elisabeth; Haines, Keith</p> <p>2014-05-01</p> <p>Recommendations and priorities for ocean <span class="hlt">heat</span> <span class="hlt">flux</span> research are for instance outlined in recent CLIVAR and WCRP reports, eg. Yu et al (2013). Among these is the need for improving the accuracy, the consistency, and the spatial and temporal resolution of air-sea <span class="hlt">fluxes</span> over global as well as at region scales. To meet the main air-sea <span class="hlt">flux</span> requirements, this study is aimed at obtaining and analyzing all the <span class="hlt">heat</span> <span class="hlt">flux</span> components (latent, sensible and radiative) at the ocean surface over global oceans using multiple satellite sensor observations in combination with in-situ measurements and numerical model analyses. The <span class="hlt">fluxes</span> will be generated daily and monthly for the 20-year (1992-2011) period, between 80N and 80S and at 0.25deg resolution. Simultaneous estimates of all surface <span class="hlt">heat</span> <span class="hlt">flux</span> terms have not yet been calculated at such large scale and long time period. Such an effort requires a wide range of expertise and data sources that only recently are becoming available. Needed are methods for integrating many data sources to calculate energy <span class="hlt">fluxes</span> (short-wave, long wave, sensible and latent <span class="hlt">heat</span>) across the air-sea interface. We have access to all the relevant, recently available satellite data to perform such computations. Yu, L., K. Haines, M. Bourassa, M. Cronin, S. Gulev, S. Josey, S. Kato, A. Kumar, T. Lee, D. Roemmich: Towards achieving global closure of ocean <span class="hlt">heat</span> and freshwater budgets: Recommendations for advancing research in air-sea <span class="hlt">fluxes</span> through collaborative activities. INTERNATIONAL CLIVAR PROJECT OFFICE, 2013: International CLIVAR Publication Series No 189. http://www.clivar.org/sites/default/files/ICPO189_WHOI_<span class="hlt">fluxes</span>_workshop.pdf</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MMTB...48.1951Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MMTB...48.1951Y"><span>Controlling Radiative <span class="hlt">Heat</span> Transfer Across the Mold <span class="hlt">Flux</span> Layer by the Scattering Effect of the Borosilicate Mold <span class="hlt">Flux</span> System with Metallic Iron</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yoon, Dae-Woo; Cho, Jung-Wook; Kim, Seon-Hyo</p> <p>2017-08-01</p> <p>The present study proposes a countermeasure for regulating total <span class="hlt">heat</span> <span class="hlt">flux</span> through the mold <span class="hlt">flux</span> layer by designed mold <span class="hlt">flux</span> with additive metallic iron particles. The <span class="hlt">heat</span> <span class="hlt">flux</span> through the B2O3-CaO-SiO2-Na2O-CaF2-Fe system was investigated using the infrared emitter technique to evaluate total <span class="hlt">flux</span> density across the mold <span class="hlt">flux</span> film. Both scanning <span class="hlt">electron</span> microscope (SEM) and X-ray diffraction analysis were employed in order to identify the morphological and compositional changes of the crystalline phase, according to increasing iron contents in the mold <span class="hlt">flux</span>. It was confirmed that the crystalline layer of studied mold <span class="hlt">fluxes</span> does not have a meaningful effect on the total <span class="hlt">heat</span> <span class="hlt">flux</span> density due to the similar structure and fraction of the crystalline phase. The extinction coefficient was measured for glassy mold <span class="hlt">fluxes</span> using an ultraviolet/visible and a Fourier transformation-infrared ray spectrometer in the range of 0.5 to 5 μm. For analyzing the scattering behavior of iron particles on the extinction coefficient, the number density and diameter of particles were observed by an automated SEM (auto-SEM). With these data, Mie scattering theory is adopted to define the scattering behavior of dispersed iron droplets in glassy matrix. It was found that the theoretical scattering coefficient demonstrated about 1623 to 3295 m-1, which is in accordance with the experimental results. In doing so, this study successfully achieves the strong scattering behavior that would contribute greatly to the optimization of overall <span class="hlt">heat</span> <span class="hlt">flux</span> through the mold <span class="hlt">flux</span> film during the casting process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUOSPO54F3320B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUOSPO54F3320B"><span>Satellite-based Calibration of <span class="hlt">Heat</span> <span class="hlt">Flux</span> at the Ocean Surface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Barron, C. N.; Dastugue, J. M.; May, J. C.; Rowley, C. D.; Smith, S. R.; Spence, P. L.; Gremes-Cordero, S.</p> <p>2016-02-01</p> <p>Model forecasts of upper ocean <span class="hlt">heat</span> content and variability on diurnal to daily scales are <span class="hlt">highly</span> dependent on estimates of <span class="hlt">heat</span> <span class="hlt">flux</span> through the air-sea interface. Satellite remote sensing is applied to not only inform the initial ocean state but also to mitigate errors in surface <span class="hlt">heat</span> <span class="hlt">flux</span> and model representations affecting the distribution of <span class="hlt">heat</span> in the upper ocean. Traditional assimilation of sea surface temperature (SST) observations re-centers ocean models at the start of each forecast cycle. Subsequent evolution depends on estimates of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> and upper-ocean processes over the forecast period. The COFFEE project (Calibration of Ocean Forcing with satellite <span class="hlt">Flux</span> Estimates) endeavors to correct ocean forecast bias through a responsive error partition among surface <span class="hlt">heat</span> <span class="hlt">flux</span> and ocean dynamics sources. A suite of experiments in the southern California Current demonstrates a range of COFFEE capabilities, showing the impact on forecast error relative to a baseline three-dimensional variational (3DVAR) assimilation using Navy operational global or regional atmospheric forcing. COFFEE addresses satellite-calibration of surface <span class="hlt">fluxes</span> to estimate surface error covariances and links these to the ocean interior. Experiment cases combine different levels of <span class="hlt">flux</span> calibration with different assimilation alternatives. The cases may use the original <span class="hlt">fluxes</span>, apply full satellite corrections during the forecast period, or extend hindcast corrections into the forecast period. Assimilation is either baseline 3DVAR or standard strong-constraint 4DVAR, with work proceeding to add a 4DVAR expanded to include a weak constraint treatment of the surface <span class="hlt">flux</span> errors. Covariance of <span class="hlt">flux</span> errors is estimated from the recent time series of forecast and calibrated <span class="hlt">flux</span> terms. While the California Current examples are shown, the approach is equally applicable to other regions. These approaches within a 3DVAR application are anticipated to be useful for global and larger</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_9 --> <div id="page_10" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="181"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HEDP...27...12L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HEDP...27...12L"><span>Laser ablation under different <span class="hlt">electron</span> <span class="hlt">heat</span> conduction models in inertial confinement fusion</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Shuanggui; Ren, Guoli; Huo, Wen Yi</p> <p>2018-06-01</p> <p>In this paper, we study the influence of three different <span class="hlt">electron</span> <span class="hlt">heat</span> conduction models on the laser ablation of gold plane target. Different from previous studies, we concentrate on the plasma conditions, the conversion efficiency from laser into soft x rays and the scaling relation of mass ablation, which are relevant to hohlraum physics study in indirect drive inertial confinement fusion. We find that the simulated <span class="hlt">electron</span> temperature in corona region is sensitive to the <span class="hlt">electron</span> <span class="hlt">heat</span> conduction models. For different <span class="hlt">electron</span> <span class="hlt">heat</span> conduction models, there are obvious differences in magnitude and spatial profile of <span class="hlt">electron</span> temperature. For the <span class="hlt">flux</span> limit model, the calculated conversion efficiency is sensitive to <span class="hlt">flux</span> limiters. In the laser ablation of gold, most of the laser energies are converted into x rays. So the scaling relation of mass ablation rate is quite different from that of low Z materials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1373840-novel-approach-evaluate-soil-heat-flux-calculation-analytical-review-nine-methods-soil-heat-flux-calculation','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1373840-novel-approach-evaluate-soil-heat-flux-calculation-analytical-review-nine-methods-soil-heat-flux-calculation"><span>A novel approach to evaluate soil <span class="hlt">heat</span> <span class="hlt">flux</span> calculation: An analytical review of nine methods: Soil <span class="hlt">Heat</span> <span class="hlt">Flux</span> Calculation</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Gao, Zhongming; Russell, Eric S.; Missik, Justine E. C.</p> <p></p> <p>We evaluated nine methods of soil <span class="hlt">heat</span> <span class="hlt">flux</span> calculation using field observations. All nine methods underestimated the soil <span class="hlt">heat</span> <span class="hlt">flux</span> by at least 19%. This large underestimation is mainly caused by uncertainties in soil thermal properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1914268F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1914268F"><span>Millisecond resolution <span class="hlt">electron</span> <span class="hlt">fluxes</span> from the Cluster satellites: Calibrated EDI ambient <span class="hlt">electron</span> data</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Förster, Matthias; Rashev, Mikhail; Haaland, Stein</p> <p>2017-04-01</p> <p>The <span class="hlt">Electron</span> Drift Instrument (EDI) onboard Cluster can measure 500 eV and 1 keV <span class="hlt">electron</span> <span class="hlt">fluxes</span> with <span class="hlt">high</span> time resolution during passive operation phases in its Ambient <span class="hlt">Electron</span> (AE) mode. Data from this mode is available in the Cluster Science Archive since October 2004 with a cadence of 16 Hz in the normal mode or 128 Hz for burst mode telemetry intervals. The <span class="hlt">fluxes</span> are recorded at pitch angles of 0, 90, and 180 degrees. This paper describes the calibration and validation of these measurements. The <span class="hlt">high</span> resolution AE data allow precise temporal and spatial diagnostics of magnetospheric boundaries and will be used for case studies and statistical studies of low energy <span class="hlt">electron</span> <span class="hlt">fluxes</span> in the near-Earth space. We show examples of applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.T13B0517B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.T13B0517B"><span>A new <span class="hlt">heat</span> <span class="hlt">flux</span> model for the Antarctic Peninsula incorporating spatially variable upper crustal radiogenic <span class="hlt">heat</span> production</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Burton-Johnson, A.; Halpin, J.; Whittaker, J. M.; Graham, F. S.; Watson, S. J.</p> <p>2017-12-01</p> <p>We present recently published findings (Burton-Johnson et al., 2017) on the variability of Antarctic sub-glacial <span class="hlt">heat</span> <span class="hlt">flux</span> and the impact from upper crustal geology. Our new method reveals that the upper crust contributes up to 70% of the Antarctic Peninsula's subglacial <span class="hlt">heat</span> <span class="hlt">flux</span>, and that <span class="hlt">heat</span> <span class="hlt">flux</span> values are more variable at smaller spatial resolutions than geophysical methods can resolve. Results indicate a higher <span class="hlt">heat</span> <span class="hlt">flux</span> on the east and south of the Peninsula (mean 81 mWm-2) where silicic rocks predominate, than on the west and north (mean 67 mWm-2) where volcanic arc and quartzose sediments are dominant. Whilst the data supports the contribution of HPE-enriched granitic rocks to <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> values, sedimentary rocks can be of comparative importance dependent on their provenance and petrography. Models of subglacial <span class="hlt">heat</span> <span class="hlt">flux</span> must utilize a heterogeneous upper crust with variable radioactive <span class="hlt">heat</span> production if they are to accurately predict basal conditions of the ice sheet. Our new methodology and dataset facilitate improved numerical model simulations of ice sheet dynamics. The most significant challenge faced remains accurate determination of crustal structure, particularly the depths of the HPE-enriched sedimentary basins and the sub-glacial geology away from exposed outcrops. Continuing research (particularly detailed geophysical interpretation) will better constrain these unknowns and the effect of upper crustal geology on the Antarctic ice sheet. Burton-Johnson, A., Halpin, J.A., Whittaker, J.M., Graham, F.S., and Watson, S.J., 2017, A new <span class="hlt">heat</span> <span class="hlt">flux</span> model for the Antarctic Peninsula incorporating spatially variable upper crustal radiogenic <span class="hlt">heat</span> production: Geophysical Research Letters, v. 44, doi: 10.1002/2017GL073596.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010JSASS..58...68O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010JSASS..58...68O"><span>Effects of Crack on <span class="hlt">Heat</span> <span class="hlt">Flux</span> in Hypersonic Shock/Boundary-Layer Interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ozawa, Hiroshi; Hanai, Katsuhisa; Kitamura, Keiichi; Mori, Koichi; Nakamura, Yoshiaki</p> <p></p> <p>A small crack on body surface led to a tragic accident in 2003, which is the Columbia accident. During the shuttle's re-entry, <span class="hlt">high</span> temperature gas penetrated crack on leading-edge of the left wing and melted the aluminum structure, finally the Columbia blew up. Since early times, there are many fundamental studies about simple cavity-flow formed on body surface in hypersonic speeds. However, an investigation of Shock/Boundary-Layer Interaction (SBLI) on crack has not been researched. For multistage space transportation vehicle such as TSTO, SBLI is an inevitable problem, and then SBLI on crack becomes a critical issue for TSTO development. In this study, the effects of crack, where SBLI occurs, were investigated for TSTO hypersonic speed (M∞ = 8.1). A square crack locates at SBLI point on the TSTO booster. Results show that a crack and its depth strongly effect on peak <span class="hlt">heat</span> <span class="hlt">flux</span> and aerodynamic interaction flow-field. In the cases of shallow crack (d/C ≤ 0.10), there exist two <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> regions on crack floor, which locates at a flow reattachment region and a back end wall of crack. In this case, a peak <span class="hlt">heat</span> <span class="hlt">flux</span> at flow reattachment region becomes about 2 times as large as the stagnation point <span class="hlt">heat</span> <span class="hlt">flux</span>, which value becomes larger compared with a peak <span class="hlt">heat</span> <span class="hlt">flux</span> in the case of No-Crack TSTO. While in the case of deep crack (d/C = 0.20), overall <span class="hlt">heat</span> <span class="hlt">flux</span> on crack floor decreases to below the stagnation point <span class="hlt">heat</span> <span class="hlt">flux</span>. These results provide useful data for a development of TSTO thermal protection system (TPS) such as thermal protection tile.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005APS..DPPBO1003L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005APS..DPPBO1003L"><span>Effect of Ponderomotive Terms on <span class="hlt">Heat</span> <span class="hlt">Flux</span> in Laser-Produced Plasmas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, G.</p> <p>2005-10-01</p> <p>A laser electromagnetic field introduces ponderomotive termsootnotetextV. N. Goncharov and G. Li, Phys. Plasmas 11, 5680 (2004). in the <span class="hlt">heat</span> <span class="hlt">flux</span> in a plasma. To account for the nonlocal effects in the ponderomotive terms, first, the kinetic equation coupled with the Maxwell equations is numerically solved for the isotropic part of the <span class="hlt">electron</span> distribution function. Such an equation includes self-consistent electromagnetic fields and laser absorption through the inverse bremsstrahlung. Then, the anisotropic part is found by solving a simplified Fokker--Planck equation. Using the distribution function, the electric current and <span class="hlt">heat</span> <span class="hlt">flux</span> are obtained and substituted into the hydrocode LILAC to simulate ICF implosions. The simulation results are compared against the existing nonlocal <span class="hlt">electron</span> conduction modelsootnotetextG. P. Schurtz, P. D. Nicola"i, and M. Busquet, Phys. Plasmas 9, 4238 (2000). and Fokker--Planck simulations. This work was supported by the U.S. Department of Energy Office of Inertial Confinement Fusion under Cooperative Agreement No. DE-FC52-92SF19460.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/7274828','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/7274828"><span>Optical <span class="hlt">heat</span> <span class="hlt">flux</span> gauge</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Noel, B.W.; Borella, H.M.; Cates, M.R.; Turley, W.D.; MacArthur, C.D.; Cala, G.C.</p> <p>1991-04-09</p> <p>A <span class="hlt">heat</span> <span class="hlt">flux</span> gauge is disclosed comprising first and second thermographic phosphor layers separated by a layer of a thermal insulator, wherein each thermographic layer comprises a plurality of respective thermographic sensors in a juxtaposed relationship with respect to each other. The gauge may be mounted on a surface with the first thermographic phosphor in contact with the surface. A light source is directed at the gauge, causing the phosphors to luminesce. The luminescence produced by the phosphors is collected and its spectra analyzed in order to determine the <span class="hlt">heat</span> <span class="hlt">flux</span> on the surface. First and second phosphor layers must be different materials to assure that the spectral lines collected will be distinguishable. 9 figures.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110023417','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110023417"><span>On the Relationship Between <span class="hlt">High</span> Speed Solar Wind Streams and Radiation Belt <span class="hlt">Electron</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zheng, Yihua</p> <p>2011-01-01</p> <p>Both past and recent research results indicate that solar wind speed has a close connection to radiation belt <span class="hlt">electron</span> <span class="hlt">fluxes</span> [e.g., Paulikas and Blake, 1979; Reeves et aI., 2011]: a higher solar wind speed is often associated with a higher level of radiation <span class="hlt">electron</span> <span class="hlt">fluxes</span>. But the relationship can be very complex [Reeves et aI., 2011]. The study presented here provides further corroboration of this viewpoint by emphasizing the importance of a global perspective and time history. We find that all the events during years 2010 and 2011 where the >0.8 MeV integral <span class="hlt">electron</span> <span class="hlt">flux</span> exceeds 10(exp 5) particles/sq cm/sr/s (pfu) at GEO orbit are associated with the <span class="hlt">high</span> speed streams (HSS) following the onset of the Stream Interaction Region (SIR), with most of them belonging to the long-lasting Corotating Interaction Region (CIR). Our preliminary results indicate that during HSS events, a maximum speed of 700 km/s and above is a sufficient but not necessary condition for the > 0.8 MeV <span class="hlt">electron</span> <span class="hlt">flux</span> to reach 10(exp 5) pfu. But in the exception cases of HSS events where the <span class="hlt">electron</span> <span class="hlt">flux</span> level exceeds the 10(exp 5) pfu value but the maximum solar wind speed is less than 700 km/s, a prior impact can be noted either from a CME or a transient SIR within 3-4 days before the arrival of the HSS - stressing the importance of time history. Through superposed epoch analysis and studies providing comparisons with the CME events and the HSS events where the <span class="hlt">flux</span> level fails to reach the 10(exp 5) pfu, we will present the quantitative assessment of behaviors and relationships of various quantities, such as the time it takes to reach the <span class="hlt">flux</span> threshold value from the stream interface and its dependence on different physical parameters (e.g., duration of the HSS event, its maximum or average of the solar wind speed, IMF Bz, Kp). The ultimate goal is to apply what is derived to space weather forecasting.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950014379','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950014379"><span>An augmented Young-Laplace model of an evaporating meniscus in a micro-channel with <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wayner, P. C., Jr.; Plawsky, J.; Schonberg, J. A.; Dasgupta, S.</p> <p>1993-01-01</p> <p><span class="hlt">High</span> <span class="hlt">flux</span> evaporations from a steady meniscus formed in a 2 micron channel is modeled using the augmented Young-Laplace equation. The <span class="hlt">heat</span> <span class="hlt">flux</span> is found to be a function of the long range van der Waals dispersion force which represents interfacial conditions between heptane and various substrates. <span class="hlt">Heat</span> <span class="hlt">fluxes</span> of (1.3-1.6) x 10(exp 6) W/m(exp 2) based on the width of the channel are obtained for heptane completely wetting the substrate at 100 C. Small channels are used to obtain these large <span class="hlt">fluxes</span>. Even though the real contact angle is 0 deg, the apparent contact angle is found to vary between 24.8 deg and 25.6 deg. The apparent contact angle, which represents viscous losses near the contact line, has a large effect on the <span class="hlt">heat</span> flow rate because of its effect on capillary suction and the area of the meniscus. The interfacial <span class="hlt">heat</span> <span class="hlt">flux</span> is modeled using kinetic theory for the evaporation rate. The superheated state depends on the temperature and the pressure of the liquid phase. The liquid pressure differs from the pressure of the vapor phase due to capillarity and long range van der Waals dispersion forces which are relevant in the ultra think film formed at the leading edge of the meniscus. Important pressure gradients in the thin film cause a substantial apparent contact angle for a complete wetting system. The temperature of the liquid is related to the evaporation rate and to the substrate temperature through the steady <span class="hlt">heat</span> conduction equation. Conduction in the liquid phase is calculated using finite element analysis except in the vicinity of the thin film. A lubrication theory solution for the thin film is combined with the finite element analysis by the method of matched asymptotic expansions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890000356&hterms=Rhodium&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DRhodium','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890000356&hterms=Rhodium&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DRhodium"><span><span class="hlt">Heat-Flux</span> Sensor For Hot Engine Cylinders</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kim, Walter S.; Barrows, Richard F.; Smith, Floyd A.; Koch, John</p> <p>1989-01-01</p> <p><span class="hlt">Heat-flux</span> sensor includes buried wire thermocouple and thin-film surface thermocouple, made of platinum and platinum with 13 percent rhodium. Sensor intended for use in ceramic-insulated, low-<span class="hlt">heat</span>-rejection diesel engine at temperatures of about 1,000 K. Thermocouple junction resists environment in cylinder of advanced <span class="hlt">high</span>-temperature diesel engine created by depositing overlapping films of Pt and 0.87 Pt/0.13 Rh on iron plug. Plug also contains internal thermocouple.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980017166','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980017166"><span>Forced Convection Boiling and Critical <span class="hlt">Heat</span> <span class="hlt">Flux</span> of Ethanol in Electrically <span class="hlt">Heated</span> Tube Tests</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Meyer, Michael L.; Linne, Diane L.; Rousar, Donald C.</p> <p>1998-01-01</p> <p>Electrically <span class="hlt">heated</span> tube tests were conducted to characterize the critical <span class="hlt">heat</span> <span class="hlt">flux</span> (transition from nucleate to film boiling) of subcritical ethanol flowing at conditions relevant to the design of a regeneratively cooled rocket engine thrust chamber. The coolant was SDA-3C alcohol (95% ethyl alcohol, 5% isopropyl alcohol by weight), and tests were conducted over the following ranges of conditions: pressure from 144 to 703 psia, flow velocities from 9.7 to 77 ft/s, coolant subcooling from 33 to 362 F, and critical <span class="hlt">heat</span> <span class="hlt">fluxes</span> up to 8.7 BTU/in(exp 2)/sec. For the data taken near 200 psia, critical <span class="hlt">heat</span> <span class="hlt">flux</span> was correlated as a function of the product of velocity and fluid subcooling to within +/- 20%. For data taken at higher pressures, an additional pressure term is needed to correlate the critical <span class="hlt">heat</span> <span class="hlt">flux</span>. It was also shown that at the higher test pressures and/or flow rates, exceeding the critical <span class="hlt">heat</span> <span class="hlt">flux</span> did not result in wall burnout. This result may significantly increase the engine <span class="hlt">heat</span> <span class="hlt">flux</span> design envelope for higher pressure conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5407354','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5407354"><span>Estimating spatially distributed turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> from <span class="hlt">high</span>-resolution thermal imagery acquired with a UAV system</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Brenner, Claire; Thiem, Christina Elisabeth; Wizemann, Hans-Dieter; Bernhardt, Matthias; Schulz, Karsten</p> <p>2017-01-01</p> <p>ABSTRACT In this study, <span class="hlt">high</span>-resolution thermal imagery acquired with a small unmanned aerial vehicle (UAV) is used to map evapotranspiration (ET) at a grassland site in Luxembourg. The land surface temperature (LST) information from the thermal imagery is the key input to a one-source and two-source energy balance model. While the one-source model treats the surface as a single uniform layer, the two-source model partitions the surface temperature and <span class="hlt">fluxes</span> into soil and vegetation components. It thus explicitly accounts for the different contributions of both components to surface temperature as well as turbulent <span class="hlt">flux</span> exchange with the atmosphere. Contrary to the two-source model, the one-source model requires an empirical adjustment parameter in order to account for the effect of the two components. Turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> estimates of both modelling approaches are compared to eddy covariance (EC) measurements using the <span class="hlt">high</span>-resolution input imagery UAVs provide. In this comparison, the effect of different methods for energy balance closure of the EC data on the agreement between modelled and measured <span class="hlt">fluxes</span> is also analysed. Additionally, the sensitivity of the one-source model to the derivation of the empirical adjustment parameter is tested. Due to the very dry and hot conditions during the experiment, pronounced thermal patterns developed over the grassland site. These patterns result in spatially variable turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. The model comparison indicates that both models are able to derive ET estimates that compare well with EC measurements under these conditions. However, the two-source model, with a more complex treatment of the energy and surface temperature partitioning between the soil and vegetation, outperformed the simpler one-source model in estimating sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. This is consistent with findings from prior studies. For the one-source model, a time-variant expression of the adjustment parameter (to account for the difference</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28515537','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28515537"><span>Estimating spatially distributed turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> from <span class="hlt">high</span>-resolution thermal imagery acquired with a UAV system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Brenner, Claire; Thiem, Christina Elisabeth; Wizemann, Hans-Dieter; Bernhardt, Matthias; Schulz, Karsten</p> <p>2017-05-19</p> <p>In this study, <span class="hlt">high</span>-resolution thermal imagery acquired with a small unmanned aerial vehicle (UAV) is used to map evapotranspiration (ET) at a grassland site in Luxembourg. The land surface temperature (LST) information from the thermal imagery is the key input to a one-source and two-source energy balance model. While the one-source model treats the surface as a single uniform layer, the two-source model partitions the surface temperature and <span class="hlt">fluxes</span> into soil and vegetation components. It thus explicitly accounts for the different contributions of both components to surface temperature as well as turbulent <span class="hlt">flux</span> exchange with the atmosphere. Contrary to the two-source model, the one-source model requires an empirical adjustment parameter in order to account for the effect of the two components. Turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> estimates of both modelling approaches are compared to eddy covariance (EC) measurements using the <span class="hlt">high</span>-resolution input imagery UAVs provide. In this comparison, the effect of different methods for energy balance closure of the EC data on the agreement between modelled and measured <span class="hlt">fluxes</span> is also analysed. Additionally, the sensitivity of the one-source model to the derivation of the empirical adjustment parameter is tested. Due to the very dry and hot conditions during the experiment, pronounced thermal patterns developed over the grassland site. These patterns result in spatially variable turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. The model comparison indicates that both models are able to derive ET estimates that compare well with EC measurements under these conditions. However, the two-source model, with a more complex treatment of the energy and surface temperature partitioning between the soil and vegetation, outperformed the simpler one-source model in estimating sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. This is consistent with findings from prior studies. For the one-source model, a time-variant expression of the adjustment parameter (to account for the difference between</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22597986-design-calibration-novel-transient-radiative-heat-flux-meter-spacecraft-thermal-test','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22597986-design-calibration-novel-transient-radiative-heat-flux-meter-spacecraft-thermal-test"><span>Design and calibration of a novel transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> meter for a spacecraft thermal test</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sheng, Chunchen; Hu, Peng, E-mail: hupeng@ustc.edu.cn; Cheng, Xiaofang</p> <p>2016-06-15</p> <p>Radiative <span class="hlt">heat</span> <span class="hlt">flux</span> measurement is significantly important for a spacecraft thermal test. To satisfy the requirements of both <span class="hlt">high</span> accuracy and fast response, a novel transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> meter was developed. Its thermal receiver consists of a central thermal receiver and two thermal guarded annular plates, which ensure the temperature distribution of the central thermal receiver to be uniform enough for reasonably applying lumped <span class="hlt">heat</span> capacity method in a transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> measurement. This novel transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> meter design can also take accurate measurements regardless of spacecraft surface temperature and incident radiation spectrum. The measurement principlemore » was elaborated and the coefficients were calibrated. Experimental results from testing a blackbody furnace and an Xenon lamp show that this novel transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> meter can be used to measure transient radiative <span class="hlt">heat</span> <span class="hlt">flux</span> up to 1400 W/m{sup 2} with <span class="hlt">high</span> accuracy and the response time of less than 10 s.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950007885','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950007885"><span>Hypersonic Engine Leading Edge Experiments in a <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span>, Supersonic Flow Environment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gladden, Herbert J.; Melis, Matthew E.</p> <p>1994-01-01</p> <p>A major concern in advancing the state-of-the-art technologies for hypersonic vehicles is the development of an aeropropulsion system capable of withstanding the sustained <span class="hlt">high</span> thermal loads expected during hypersonic flight. Three aerothermal load related concerns are the boundary layer transition from laminar to turbulent flow, articulating panel seals in <span class="hlt">high</span> temperature environments, and strut (or cowl) leading edges with shock-on-shock interactions. A multidisciplinary approach is required to address these technical concerns. A hydrogen/oxygen rocket engine <span class="hlt">heat</span> source has been developed at the NASA Lewis Research Center as one element in a series of facilities at national laboratories designed to experimentally evaluate the <span class="hlt">heat</span> transfer and structural response of the strut (or cowl) leading edge. A recent experimental program conducted in this facility is discussed and related to cooling technology capability. The specific objective of the experiment discussed is to evaluate the erosion and oxidation characteristics of a coating on a cowl leading edge (or strut leading edge) in a supersonic, <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> environment. <span class="hlt">Heat</span> transfer analyses of a similar leading edge concept cooled with gaseous hydrogen is included to demonstrate the complexity of the problem resulting from plastic deformation of the structures. Macro-photographic data from a coated leading edge model show progressive degradation over several thermal cycles at aerothermal conditions representative of <span class="hlt">high</span> Mach number flight.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22600082-electron-holes-inhomogeneous-magnetic-field-electron-heating-electron-hole-evolution','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22600082-electron-holes-inhomogeneous-magnetic-field-electron-heating-electron-hole-evolution"><span><span class="hlt">Electron</span> holes in inhomogeneous magnetic field: <span class="hlt">Electron</span> <span class="hlt">heating</span> and <span class="hlt">electron</span> hole evolution</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Vasko, I. Y.; Space Research Institute of Russian Academy of Science, Moscow; Agapitov, O. V.</p> <p></p> <p><span class="hlt">Electron</span> holes are electrostatic non-linear structures widely observed in the space plasma. In the present paper, we analyze the process of energy exchange between <span class="hlt">electrons</span> trapped within <span class="hlt">electron</span> hole, untrapped <span class="hlt">electrons</span>, and an <span class="hlt">electron</span> hole propagating in a weakly inhomogeneous magnetic field. We show that as the <span class="hlt">electron</span> hole propagates into the region with stronger magnetic field, trapped <span class="hlt">electrons</span> are <span class="hlt">heated</span> due to the conservation of the first adiabatic invariant. At the same time, the <span class="hlt">electron</span> hole amplitude may increase or decrease in dependence on properties of distribution functions of trapped and untrapped resonant <span class="hlt">electrons</span>. The energy gain of trappedmore » <span class="hlt">electrons</span> is due to the energy losses of untrapped <span class="hlt">electrons</span> and/or decrease of the <span class="hlt">electron</span> hole energy. We stress that taking into account the energy exchange with untrapped <span class="hlt">electrons</span> increases the lifetime of <span class="hlt">electron</span> holes in inhomogeneous magnetic field. We illustrate the suggested mechanism for small-amplitude Schamel's [Phys. Scr. T2, 228–237 (1982)] <span class="hlt">electron</span> holes and show that during propagation along a positive magnetic field gradient their amplitude should grow. Neglect of the energy exchange with untrapped <span class="hlt">electrons</span> would result in the <span class="hlt">electron</span> hole dissipation with only modest <span class="hlt">heating</span> factor of trapped <span class="hlt">electrons</span>. The suggested mechanism may contribute to generation of suprathermal <span class="hlt">electron</span> <span class="hlt">fluxes</span> in the space plasma.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4279525','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4279525"><span><span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensors for Infrared Thermography in Convective <span class="hlt">Heat</span> Transfer</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Carlomagno, Giovanni Maria; de Luca, Luigi; Cardone, Gennaro; Astarita, Tommaso</p> <p>2014-01-01</p> <p>This paper reviews the most dependable <span class="hlt">heat</span> <span class="hlt">flux</span> sensors, which can be used with InfraRed (IR) thermography to measure convective <span class="hlt">heat</span> transfer coefficient distributions, and some of their applications performed by the authors' research group at the University of Naples Federico II. After recalling the basic principles that make IR thermography work, the various <span class="hlt">heat</span> <span class="hlt">flux</span> sensors to be used with it are presented and discussed, describing their capability to investigate complex thermo-fluid-dynamic flows. Several applications to streams, which range from natural convection to hypersonic flows, are also described. PMID:25386758</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160009728','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160009728"><span>Hybrid <span class="hlt">Heat</span> Pipes for Lunar and Martian Surface and <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Space Applications</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ababneh, Mohammed T.; Tarau, Calin; Anderson, William G.; Farmer, Jeffery T.; Alvarez-Hernandez, Angel R.</p> <p>2016-01-01</p> <p>Novel hybrid wick <span class="hlt">heat</span> pipes are developed to operate against gravity on planetary surfaces, operate in space carrying power over long distances and act as thermosyphons on the planetary surface for Lunar and Martian landers and rovers. These hybrid <span class="hlt">heat</span> pipes will be capable of operating at the higher <span class="hlt">heat</span> <span class="hlt">flux</span> requirements expected in NASA's future spacecraft and on the next generation of polar rovers and equatorial landers. In addition, the sintered evaporator wicks mitigate the start-up problems in vertical gravity aided <span class="hlt">heat</span> pipes because of large number of nucleation sites in wicks which will allow easy boiling initiation. ACT, NASA Marshall Space Flight Center, and NASA Johnson Space Center, are working together on the Advanced Passive Thermal experiment (APTx) to test and validate the operation of a hybrid wick VCHP with warm reservoir and HiK"TM" plates in microgravity environment on the ISS.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4497480','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4497480"><span>Simulation of <span class="hlt">high</span>-energy radiation belt <span class="hlt">electron</span> <span class="hlt">fluxes</span> using NARMAX-VERB coupled codes</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Pakhotin, I P; Drozdov, A Y; Shprits, Y Y; Boynton, R J; Subbotin, D A; Balikhin, M A</p> <p>2014-01-01</p> <p>This study presents a fusion of data-driven and physics-driven methodologies of energetic <span class="hlt">electron</span> <span class="hlt">flux</span> forecasting in the outer radiation belt. Data-driven NARMAX (Nonlinear AutoRegressive Moving Averages with eXogenous inputs) model predictions for geosynchronous orbit <span class="hlt">fluxes</span> have been used as an outer boundary condition to drive the physics-based Versatile <span class="hlt">Electron</span> Radiation Belt (VERB) code, to simulate energetic <span class="hlt">electron</span> <span class="hlt">fluxes</span> in the outer radiation belt environment. The coupled system has been tested for three extended time periods totalling several weeks of observations. The time periods involved periods of quiet, moderate, and strong geomagnetic activity and captured a range of dynamics typical of the radiation belts. The model has successfully simulated energetic <span class="hlt">electron</span> <span class="hlt">fluxes</span> for various magnetospheric conditions. Physical mechanisms that may be responsible for the discrepancies between the model results and observations are discussed. PMID:26167432</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030000755','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030000755"><span>Corrections of <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements on Launch Vehicles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Reinarts, Thomas R.; Matson, Monique L.; Walls, Laurie K.</p> <p>2002-01-01</p> <p>Knowledge of aerothermally induced convective <span class="hlt">heat</span> transfer is important in the design of thermal protection systems for launch vehicles. Aerothermal models are typically calibrated via the data from circular, in-flight, flush-mounted surface <span class="hlt">heat</span> <span class="hlt">flux</span> gauges exposed to the thermal and velocity boundary layers of the external flow. Typically, copper or aluminum Schmidt- Boelter gauges, which take advantage of the one-dimensional Fourier's law of <span class="hlt">heat</span> conduction, are used to measure the incident <span class="hlt">heat</span> <span class="hlt">flux</span>. This instrumentation, when surrounded by low-conductivity insulation, has a wall temperature significantly lower than the insulation. As a result of this substantial disturbance to the thermal boundary layer, the <span class="hlt">heat</span> <span class="hlt">flux</span> incident on the gauge tends to be considerably higher than it would have been on the insulation had the calorimeter not been there. In addition, radial conductive <span class="hlt">heat</span> transfer from the hotter insulation can cause the calorimeter to indicate <span class="hlt">heat</span> <span class="hlt">fluxes</span> higher than actual. An overview of an effort to develop and calibrate gauge correction techniques for both of these effects will be presented.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_10 --> <div id="page_11" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="201"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2001AGUFM.H32G..07O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2001AGUFM.H32G..07O"><span>Measuring Subsurface Water <span class="hlt">Fluxes</span> Using a <span class="hlt">Heat</span> Pulse Sensor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ochsner, T. E.; Wang, Q.; Horton, R.</p> <p>2001-12-01</p> <p>Subsurface water <span class="hlt">flux</span> is an important parameter in studies of runoff, infiltration, groundwater recharge, and subsurface chemical transport. <span class="hlt">Heat</span> pulse sensors have been proposed as promising tools for measuring subsurface water <span class="hlt">fluxes</span>. Our <span class="hlt">heat</span> pulse probe consists of three 4-cm stainless-steel needles embedded in a waterproof epoxy body. The needles contain resistance heaters and thermocouples. The probes are connected to an external datalogger and power supply and then installed in soil. To measure the water <span class="hlt">flux</span>, a 15-s <span class="hlt">heat</span> pulse is generated at the middle needle using the power supply and the resistance heater, and the temperature increases at the needles 6-mm upstream and downstream from the heater are recorded using the thermocouples and datalogger. To date, <span class="hlt">heat</span> pulse methods have required cumbersome mathematical analysis to calculate soil water <span class="hlt">flux</span> from this measured data. We present a new mathematical analysis showing that a simple relationship exists between water <span class="hlt">flux</span> and the ratio of the temperature increase downstream from the line <span class="hlt">heat</span> source to the temperature increase upstream from the line <span class="hlt">heat</span> source. The simplicity of this relationship makes <span class="hlt">heat</span> pulse sensors a more attractive option for measuring subsurface water <span class="hlt">fluxes</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JAP...122f3302G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JAP...122f3302G"><span>Material impacts and <span class="hlt">heat</span> <span class="hlt">flux</span> characterization of an electrothermal plasma source with an applied magnetic field</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gebhart, T. E.; Martinez-Rodriguez, R. A.; Baylor, L. R.; Rapp, J.; Winfrey, A. L.</p> <p>2017-08-01</p> <p>To produce a realistic tokamak-like plasma environment in linear plasma device, a transient source is needed to deliver <span class="hlt">heat</span> and particle <span class="hlt">fluxes</span> similar to those seen in an edge localized mode (ELM). ELMs in future large tokamaks will deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of ˜1 GW/m2 to the divertor plasma facing components at a few Hz. An electrothermal plasma source can deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of this magnitude. These sources operate in an ablative arc regime which is driven by a DC capacitive discharge. An electrothermal source was configured with two pulse lengths and tested under a solenoidal magnetic field to determine the resulting impact on liner ablation, plasma parameters, and delivered <span class="hlt">heat</span> <span class="hlt">flux</span>. The arc travels through and ablates a boron nitride liner and strikes a tungsten plate. The tungsten target plate is analyzed for surface damage using a scanning <span class="hlt">electron</span> microscope.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730019076','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730019076"><span>Extended hydrodynamic theory of the peak and minimum pool boiling <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Linehard, J. H.; Dhir, V. K.</p> <p>1973-01-01</p> <p>The hydrodynamic theory of the extreme pool boiling <span class="hlt">heat</span> <span class="hlt">fluxes</span> is expanded to embrace a variety of problems that have not previously been analyzed. These problems include the prediction of the peak <span class="hlt">heat</span> <span class="hlt">flux</span> on a variety of finite heaters, the influence of viscosity on the Taylor and Helmoltz instability mechanisms with application to film boiling and to the peak <span class="hlt">heat</span> <span class="hlt">flux</span> in viscous liquids, the formalization of the analogy between <span class="hlt">high</span>-current-density electrolysis and boiling, and the description of boiling in the low-gravity limit. The predictions are verified with a large number of new data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1345540-models-sol-transport-relation-scaling-divertor-heat-flux-width-diii','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1345540-models-sol-transport-relation-scaling-divertor-heat-flux-width-diii"><span>Models of SOL transport and their relation to scaling of the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> width in DIII-D</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Makowski, M. A.; Lasnier, C. J.; Leonard, A. W.; ...</p> <p>2014-10-06</p> <p>Strong support for the critical pressure gradient model for the <span class="hlt">heat</span> <span class="hlt">flux</span> width has been obtained, in that the measured separatrix pressure gradient lies below and scales similarly to the pressure gradient limit obtained from the ideal, infinite-n stability codes, BALOO and 2DX, in all cases that have been examined. Predictions of a heuristic drift model for the <span class="hlt">heat</span> <span class="hlt">flux</span> width are also in qualitative agreement with the measurements. We obtained these results by using an improved <span class="hlt">high</span> rep-rate and higher edge spatial resolution Thomson scattering system on DIII-D to measure the upstream <span class="hlt">electron</span> temperature and density profiles. In ordermore » to compare theory and experiment, profiles of density, temperature, and pressure for both <span class="hlt">electrons</span> and ions are needed as well values of these quantitities at the separatrix. We also developed a simple method to identify a proxy for the separatrix.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1394578-prototyping-phase-high-heat-flux-scraper-element-wendelstein','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1394578-prototyping-phase-high-heat-flux-scraper-element-wendelstein"><span>Prototyping phase of the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> scraper element of Wendelstein 7-X</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Boscary, Jean; Greuner, Henri; Ehrke, G.; ...</p> <p>2016-03-24</p> <p>The water-cooled <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> scraper element aims to reduce excessive <span class="hlt">heat</span> loads on the target element ends of the actively cooled divertor of Wendelstein 7-X. Its purpose is to intercept some of the plasma <span class="hlt">fluxes</span> both upstream and downstream before they reach the divertor surface. The scraper element has 24 identical plasma facing components (PFCs) divided into 6 modules. One module has 4 PFCs hydraulically connected in series by 2 water boxes. A PFC, 247 mm long and 28 mm wide, has 13 monoblocks made of CFC NB31 bonded by hot isostatic pressing onto a CuCrZr cooling tube equippedmore » with a copper twisted tape. 4 full-scale prototypes of PFCs have been successfully tested in the GLADIS facility up to 20 MW/m 2. The difference observed between measured and calculated surface temperatures is probably due to the inhomogeneity of CFC properties. The design of the water box prototypes has been detailed to allow the junction between the cooling pipe of the PFCs and the water boxes by internal orbital welding. In conclusion, the prototypes are presently under fabrication.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999JPFR...75..594K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999JPFR...75..594K"><span>Development of <span class="hlt">High</span>-Z Materials with Improved Toughness for <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Components</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kurishita, Hiroaki; Kitsunai, Yuji; Kuwabara, Tetsuya; Hasegawa, Masayuki; Hiraoka, Yutaka; Takida, Tomohiro; Igarashi, Tadashi</p> <p></p> <p>Tungsten is superior to other materials in physical and mechanical properties for use as <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> components in future fusion reactors. The key issue of the metal is to improve the low temperature embrittlement, the recrystallization embrittlement and the irradiation embrittlement. An alloy design and microstructure control for achieving simultaneous and significant improvements in those embrittlements are described and are applied to tungsten and molybdenum which has quite similar properties as tungsten. The result of the application is presented for each of the embrittlement, with considerable success. Emphasis is placed on the occurrence of RIDU (Radiation Induced Ductilization) because RIDU is expected to provide the scenario to overcome severe irradiation embrittlement that is the most crucial problem for structure materials exposed in fusion environment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930036989&hterms=coulomb&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcoulomb','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930036989&hterms=coulomb&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcoulomb"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> dropouts in the solar wind and Coulomb scattering effects</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fitzenreiter, R. J.; Ogilvie, K. W.</p> <p>1992-01-01</p> <p>Data on solar wind <span class="hlt">electrons</span> at the ISEE 3 spacecraft located 0.01 AU upstream from the earth (McComas et al., 1989) showed periods of time when the <span class="hlt">flux</span> of antisunward suprathermal <span class="hlt">electrons</span> would decrease suddenly, leading to <span class="hlt">heat</span> <span class="hlt">flux</span> dropouts (HFDs). This paper examines data from ISEE 1 at the 1.5 x 10 exp 6 km downstream location to determine whether HFDs identified at ISEE 3 by McComas et al. can be detected at this location and whether the ISEE 1 observations can provide information to one or the other possible interpretations of HFDs: that HFDs are due to enhanced Coulomb scattering, or to disconnection from the sun of the magnetic <span class="hlt">flux</span> tube. The results of the examination identified the presence of HFD events in the ISEE 1 data, and the findings indicate that Coulomb scattering plays a substantial role in at least some HFD events.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JGRC..122.4569M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JGRC..122.4569M"><span>Mixing rates and vertical <span class="hlt">heat</span> <span class="hlt">fluxes</span> north of Svalbard from Arctic winter to spring</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Meyer, Amelie; Fer, Ilker; Sundfjord, Arild; Peterson, Algot K.</p> <p>2017-06-01</p> <p>Mixing and <span class="hlt">heat</span> <span class="hlt">flux</span> rates collected in the Eurasian Basin north of Svalbard during the N-ICE2015 drift expedition are presented. The observations cover the deep Nansen Basin, the Svalbard continental slope, and the shallow Yermak Plateau from winter to summer. Mean quiescent winter <span class="hlt">heat</span> <span class="hlt">flux</span> values in the Nansen Basin are 2 W m-2 at the ice-ocean interface, 3 W m-2 in the pycnocline, and 1 W m-2 below the pycnocline. Large <span class="hlt">heat</span> <span class="hlt">fluxes</span> exceeding 300 W m-2 are observed in the late spring close to the surface over the Yermak Plateau. The data consisting of 588 microstructure profiles and 50 days of <span class="hlt">high</span>-resolution under-ice turbulence measurements are used to quantify the impact of several forcing factors on turbulent dissipation and <span class="hlt">heat</span> <span class="hlt">flux</span> rates. Wind forcing increases turbulent dissipation seven times in the upper 50 m, and doubles <span class="hlt">heat</span> <span class="hlt">fluxes</span> at the ice-ocean interface. The presence of warm Atlantic Water close to the surface increases the temperature gradient in the water column, leading to enhanced <span class="hlt">heat</span> <span class="hlt">flux</span> rates within the pycnocline. Steep topography consistently enhances dissipation rates by a factor of four and episodically increases <span class="hlt">heat</span> <span class="hlt">flux</span> at depth. It is, however, the combination of storms and shallow Atlantic Water that leads to the highest <span class="hlt">heat</span> <span class="hlt">flux</span> rates observed: ice-ocean interface <span class="hlt">heat</span> <span class="hlt">fluxes</span> average 100 W m-2 during peak events and are associated with rapid basal sea ice melt, reaching 25 cm/d.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20150023376&hterms=love&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dlove','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20150023376&hterms=love&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dlove"><span>Tropical Gravity Wave Momentum <span class="hlt">Fluxes</span> and Latent <span class="hlt">Heating</span> Distributions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Geller, Marvin A.; Zhou, Tiehan; Love, Peter T.</p> <p>2015-01-01</p> <p>Recent satellite determinations of global distributions of absolute gravity wave (GW) momentum <span class="hlt">fluxes</span> in the lower stratosphere show maxima over the summer subtropical continents and little evidence of GW momentum <span class="hlt">fluxes</span> associated with the intertropical convergence zone (ITCZ). This seems to be at odds with parameterizations forGWmomentum <span class="hlt">fluxes</span>, where the source is a function of latent <span class="hlt">heating</span> rates, which are largest in the region of the ITCZ in terms of monthly averages. The authors have examined global distributions of atmospheric latent <span class="hlt">heating</span>, cloud-top-pressure altitudes, and lower-stratosphere absolute GW momentum <span class="hlt">fluxes</span> and have found that monthly averages of the lower-stratosphere GW momentum <span class="hlt">fluxes</span> more closely resemble the monthly mean cloud-top altitudes rather than the monthly mean rates of latent <span class="hlt">heating</span>. These regions of highest cloud-top altitudes occur when rates of latent <span class="hlt">heating</span> are largest on the time scale of cloud growth. This, plus previously published studies, suggests that convective sources for stratospheric GW momentum <span class="hlt">fluxes</span>, being a function of the rate of latent <span class="hlt">heating</span>, will require either a climate model to correctly model this rate of latent <span class="hlt">heating</span> or some ad hoc adjustments to account for shortcomings in a climate model's land-sea differences in convective latent <span class="hlt">heating</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20160003590&hterms=strengthening&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dstrengthening','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20160003590&hterms=strengthening&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dstrengthening"><span>The Impact of Trends in the Large Scale Atmospheric Circulation on Mediterranean Surface Turbulent <span class="hlt">Heat</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Romanski, Joy; Hameed, Sultan</p> <p>2015-01-01</p> <p>Interannual variations of latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> (LHF) and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> (SHF) over the Mediterranean for the boreal winter season (DJF) show positive trends during 1958-2011. Using reanalysis and satellite-based products, the variability and trends in the <span class="hlt">heat</span> <span class="hlt">fluxes</span> are compared with variations in three atmospheric teleconnection patterns: the North Atlantic Oscillation (NAO), the pressure and position of the Azores <span class="hlt">High</span> (AH), and the East Atlantic-West Russia teleconnection pattern (EAWR). Comparison of correlations between the <span class="hlt">heat</span> <span class="hlt">fluxes</span> and teleconnections, along with analysis of composites of surface temperature, humidity, and wind fields for different teleconnection states, demonstrates that the AH explains the <span class="hlt">heat</span> <span class="hlt">flux</span> changes more successfully than NAO and EAWR. Trends in pressure and longitude of the Azores <span class="hlt">High</span> show a strengthening and an eastward shift. Variations of the Azores <span class="hlt">High</span> occur along an axis defined by lower pressure and westward location at one extreme and higher pressure and eastward location at the other extreme. The shift of the AH from predominance of the low/west state to the <span class="hlt">high</span>/east state induces trends in Mediterranean Sea surface winds, temperature, and moisture. These, combined with sea surface warming trends, produce trends in wintertime sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PhPl...22a2901K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PhPl...22a2901K"><span>Ionospheric modifications in <span class="hlt">high</span> frequency <span class="hlt">heating</span> experiments</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kuo, Spencer P.</p> <p>2015-01-01</p> <p>Featured observations in <span class="hlt">high</span>-frequency (HF) <span class="hlt">heating</span> experiments conducted at Arecibo, EISCAT, and <span class="hlt">high</span> frequency active auroral research program are discussed. These phenomena appearing in the F region of the ionosphere include <span class="hlt">high</span>-frequency heater enhanced plasma lines, airglow enhancement, energetic <span class="hlt">electron</span> <span class="hlt">flux</span>, artificial ionization layers, artificial spread-F, ionization enhancement, artificial cusp, wideband absorption, short-scale (meters) density irregularities, and stimulated electromagnetic emissions, which were observed when the O-mode HF heater waves with frequencies below foF2 were applied. The implication and associated physical mechanism of each observation are discussed and explained. It is shown that these phenomena caused by the HF <span class="hlt">heating</span> are all ascribed directly or indirectly to the excitation of parametric instabilities which instigate anomalous <span class="hlt">heating</span>. Formulation and analysis of parametric instabilities are presented. The results show that oscillating two stream instability and parametric decay instability can be excited by the O-mode HF heater waves, transmitted from all three <span class="hlt">heating</span> facilities, in the regions near the HF reflection height and near the upper hybrid resonance layer. The excited Langmuir waves, upper hybrid waves, ion acoustic waves, lower hybrid waves, and field-aligned density irregularities set off subsequent wave-wave and wave-<span class="hlt">electron</span> interactions, giving rise to the observed phenomena.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000JNuM..283.1121T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000JNuM..283.1121T"><span>Changes of composition and microstructure of joint interface of tungsten coated carbon by <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tokunaga, K.; Matsubara, T.; Miyamoto, Y.; Takao, Y.; Yoshida, N.; Noda, N.; Kubota, Y.; Sogabe, T.; Kato, T.; Plöchl, L.</p> <p>2000-12-01</p> <p>Tungsten coatings of 0.5 and 1 mm thickness were successfully deposited by the vacuum plasma spraying (VPS) technique on carbon/carbon fiber composite (CFC), CX-2002U and isotropic fine grained graphite, IG-430U. <span class="hlt">High</span> <span class="hlt">heat</span> <span class="hlt">flux</span> experiments by irradiation of <span class="hlt">electron</span> beam with uniform profile were performed on the coated samples in order to prove the suitability and load limit of such coating materials. The cross-sectional composition and structure of the interface of VPS-W and carbon material samples were investigated. Compositional analyses showed that the Re/W multi-layer acts as diffusion barrier for carbon and suppresses tungsten carbide formation in the VPS-W layer at <span class="hlt">high</span> temperature about 1300°C. Microstructure of the joint interface of the sample changed in the case of a peak temperature of about 2800°C. The multi-layer structure completely disappeared and compositional distribution was almost uniform in the interface of the sample after melting and resolidification. The diffusion barrier for carbon is not expected to act in this stage.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007APS..DPPBI1005S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007APS..DPPBI1005S"><span>Divertor <span class="hlt">Heat</span> <span class="hlt">Flux</span> Reduction and Detachment in the National Spherical Torus eXperiment.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Soukhanovskii, Vsevolod</p> <p>2007-11-01</p> <p>Steady-state handling of the <span class="hlt">heat</span> <span class="hlt">flux</span> is a critical divertor issue for both the International Thermonuclear Experimental Reactor and spherical torus (ST) devices. Because of an inherently compact divertor, it was thought that ST-based devices might not be able to fully utilize radiative and dissipative divertor techniques based on induced power and momentum loss. However, initial experiments conducted in the National Spherical Torus Experiment in an open geometry horizontal carbon plate divertor using 0.8 MA 2-6 MW NBI-<span class="hlt">heated</span> lower single null H-mode plasmas at the lower end of elongations κ=1.8-2.4 and triangularities δ=0.45-0.75 demonstrated that <span class="hlt">high</span> divertor peak <span class="hlt">heat</span> <span class="hlt">fluxes</span>, up to 6-10 MW/ m^2, could be reduced by 50-75% using a <span class="hlt">high</span>-recycling radiative divertor regime with D2 injection. Furthermore, similar reduction was obtained with a partially detached divertor (PDD) at <span class="hlt">high</span> D2 injection rates, however, it was accompanied by an X-point MARFE that quickly led to confinement degradation. Another approach takes advantage of the ST relation between strong shaping and <span class="hlt">high</span> performance, and utilizes the poloidal magnetic <span class="hlt">flux</span> expansion in the divertor region. Up to 60 % reduction in divertor peak <span class="hlt">heat</span> <span class="hlt">flux</span> was achieved at similar levels of scrape-off layer power by varying plasma shaping and thereby increasing the outer strike point (OSP) poloidal <span class="hlt">flux</span> expansion from 4-6 to 18-22. In recent experiments conducted in <span class="hlt">highly</span>-shaped 1.0-1.2 MA 6 MW NBI <span class="hlt">heated</span> H-mode plasmas with divertor D2 injection at rates up to 10^22 s-1, a PDD regime with OSP peak <span class="hlt">heat</span> <span class="hlt">flux</span> 0.5-1.5 MW/m^2 was obtained without noticeable confinement degradation. Calculations based on a two point scrape-off layer model with parameterized power and momentum losses show that the short parallel connection length at the OSP sets the upper limit on the radiative exhaust channel, and both the impurity radiation and large momentum sink achievable only at <span class="hlt">high</span> divertor neutral pressures are required</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1376436-material-impacts-heat-flux-characterization-electrothermal-plasma-source-applied-magnetic-field','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1376436-material-impacts-heat-flux-characterization-electrothermal-plasma-source-applied-magnetic-field"><span>Material impacts and <span class="hlt">heat</span> <span class="hlt">flux</span> characterization of an electrothermal plasma source with an applied magnetic field</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Gebhart, T. E.; Martinez-Rodriguez, R. A.; Baylor, L. R.; ...</p> <p>2017-08-11</p> <p>To produce a realistic tokamak-like plasma environment in linear plasma device, a transient source is needed to deliver <span class="hlt">heat</span> and particle <span class="hlt">fluxes</span> similar to those seen in an edge localized mode (ELM). ELMs in future large tokamaks will deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of ~1 GW/m 2 to the divertor plasma facing components at a few Hz. An electrothermal plasma source can deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of this magnitude. These sources operate in an ablative arc regime which is driven by a DC capacitive discharge. An electrothermal source was configured in this paper with two pulse lengths and tested under a solenoidal magneticmore » field to determine the resulting impact on liner ablation, plasma parameters, and delivered <span class="hlt">heat</span> <span class="hlt">flux</span>. The arc travels through and ablates a boron nitride liner and strikes a tungsten plate. Finally, the tungsten target plate is analyzed for surface damage using a scanning <span class="hlt">electron</span> microscope.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1376436-material-impacts-heat-flux-characterization-electrothermal-plasma-source-applied-magnetic-field','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1376436-material-impacts-heat-flux-characterization-electrothermal-plasma-source-applied-magnetic-field"><span>Material impacts and <span class="hlt">heat</span> <span class="hlt">flux</span> characterization of an electrothermal plasma source with an applied magnetic field</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Gebhart, T. E.; Martinez-Rodriguez, R. A.; Baylor, L. R.</p> <p></p> <p>To produce a realistic tokamak-like plasma environment in linear plasma device, a transient source is needed to deliver <span class="hlt">heat</span> and particle <span class="hlt">fluxes</span> similar to those seen in an edge localized mode (ELM). ELMs in future large tokamaks will deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of ~1 GW/m 2 to the divertor plasma facing components at a few Hz. An electrothermal plasma source can deliver <span class="hlt">heat</span> <span class="hlt">fluxes</span> of this magnitude. These sources operate in an ablative arc regime which is driven by a DC capacitive discharge. An electrothermal source was configured in this paper with two pulse lengths and tested under a solenoidal magneticmore » field to determine the resulting impact on liner ablation, plasma parameters, and delivered <span class="hlt">heat</span> <span class="hlt">flux</span>. The arc travels through and ablates a boron nitride liner and strikes a tungsten plate. Finally, the tungsten target plate is analyzed for surface damage using a scanning <span class="hlt">electron</span> microscope.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012PhDT........17F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012PhDT........17F"><span>Evaluation of bulk <span class="hlt">heat</span> <span class="hlt">fluxes</span> from atmospheric datasets</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Farmer, Benton</p> <p></p> <p><span class="hlt">Heat</span> <span class="hlt">fluxes</span> at the air-sea interface are an important component of the Earth's <span class="hlt">heat</span> budget. In addition, they are an integral factor in determining the sea surface temperature (SST) evolution of the oceans. Different representations of these <span class="hlt">fluxes</span> are used in both the atmospheric and oceanic communities for the purpose of <span class="hlt">heat</span> budget studies and, in particular, for forcing oceanic models. It is currently difficult to quantify the potential impact varying <span class="hlt">heat</span> <span class="hlt">flux</span> representations have on the ocean response. In this study, a diagnostic tool is presented that allows for a straightforward comparison of surface <span class="hlt">heat</span> <span class="hlt">flux</span> formulations and atmospheric data sets. Two variables, relaxation time (RT) and the apparent temperature (T*), are derived from the linearization of the bulk formulas. They are then calculated to compare three bulk formulae and five atmospheric datasets. Additionally, the linearization is expanded to the second order to compare the amount of residual <span class="hlt">flux</span> present. It is found that the use of a bulk formula employing a constant <span class="hlt">heat</span> transfer coefficient produces longer relaxation times and contains a greater amount of residual <span class="hlt">flux</span> in the higher order terms of the linearization. Depending on the temperature difference, the residual <span class="hlt">flux</span> remaining in the second order and above terms can reach as much as 40--50% of the total residual on a monthly time scale. This is certainly a non-negligible residual <span class="hlt">flux</span>. In contrast, a bulk formula using a stability and wind dependent transfer coefficient retains much of the total <span class="hlt">flux</span> in the first order term, as only a few percent remain in the residual <span class="hlt">flux</span>. Most of the difference displayed among the bulk formulas stems from the sensitivity to wind speed and the choice of a constant or spatially varying transfer coefficient. Comparing the representation of RT and T* provides insight into the differences among various atmospheric datasets. In particular, the representations of the western boundary current, upwelling</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040171624','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040171624"><span>Thermal Control Utilizing an Thermal Control Utilizing an Two-Phase Loop with <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Source</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jeong, Seong-Il; Didion, Jeffrey</p> <p>2004-01-01</p> <p>The electric field applied in dielectric fluids causes an imbalance in the dissociation-recombination reaction generated free space charges. The generated charges are redistributed by the applied electric field resulting in the heterocharge layers in the Vicinity of the electrodes. Proper design of the electrodes generates net axial flow motion pumping the fluid. The electrohydrodynamic (EHD) conduction pump is a new device that pumps dielectric fluids utilizing heterocharge layers formed by imposition of electrostatic fields. This paper evaluates the experimental performance of a two-phase breadboard thermal control loop consisting of an EHD conduction pump, condenser, pre-heater, <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> evaporator (HE), transport lines, and reservoir (accumulator). The generated pressure head and the maximum applicable <span class="hlt">heat</span> <span class="hlt">flux</span> are experimentally determined at various applied voltages and sink temperatures. Recovery from dryout condition by increasing the applied voltage to the pump is also demonstrated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16118893','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16118893"><span>Finger <span class="hlt">heat</span> <span class="hlt">flux</span>/temperature as an indicator of thermal imbalance with application for extravehicular activity.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Koscheyev, Victor S; Leon, Gloria R; Coca, Aitor</p> <p>2005-11-01</p> <p>The designation of a simple, non-invasive, and <span class="hlt">highly</span> precise method to monitor the thermal status of astronauts is important to enhance safety during extravehicular activities (EVA) and onboard emergencies. Finger temperature (Tfing), finger <span class="hlt">heat</span> <span class="hlt">flux</span>, and indices of core temperature (Tc) [rectal (Tre), ear canal (Tec)] were assessed in 3 studies involving different patterns of <span class="hlt">heat</span> removal/insertion from/to the body by a multi-compartment liquid cooling/warming garment (LCWG). Under both uniform and nonuniform temperature conditions on the body surface, Tfing and finger <span class="hlt">heat</span> <span class="hlt">flux</span> were <span class="hlt">highly</span> correlated with garment <span class="hlt">heat</span> <span class="hlt">flux</span>, and also <span class="hlt">highly</span> correlated with each other. Tc responses did not adequately reflect changes in thermal balance during the ongoing process of <span class="hlt">heat</span> insertion/removal from the body. Overall, Tfing/finger <span class="hlt">heat</span> <span class="hlt">flux</span> adequately reflected the initial destabilization of thermal balance, and therefore appears to have significant potential as a useful index for monitoring and maintaining thermal balance and comfort in extreme conditions in space as well as on Earth. c2005 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70159970','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70159970"><span>Automated calculation of surface energy <span class="hlt">fluxes</span> with <span class="hlt">high</span>-frequency lake buoy data</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Woolway, R. Iestyn; Jones, Ian D; Hamilton, David P.; Maberly, Stephen C; Muroaka, Kohji; Read, Jordan S.; Smyth, Robyn L; Winslow, Luke A.</p> <p>2015-01-01</p> <p>Lake <span class="hlt">Heat</span> <span class="hlt">Flux</span> Analyzer is a program used for calculating the surface energy <span class="hlt">fluxes</span> in lakes according to established literature methodologies. The program was developed in MATLAB for the rapid analysis of <span class="hlt">high</span>-frequency data from instrumented lake buoys in support of the emerging field of aquatic sensor network science. To calculate the surface energy <span class="hlt">fluxes</span>, the program requires a number of input variables, such as air and water temperature, relative humidity, wind speed, and short-wave radiation. Available outputs for Lake <span class="hlt">Heat</span> <span class="hlt">Flux</span> Analyzer include the surface <span class="hlt">fluxes</span> of momentum, sensible <span class="hlt">heat</span> and latent <span class="hlt">heat</span> and their corresponding transfer coefficients, incoming and outgoing long-wave radiation. Lake <span class="hlt">Heat</span> <span class="hlt">Flux</span> Analyzer is open source and can be used to process data from multiple lakes rapidly. It provides a means of calculating the surface <span class="hlt">fluxes</span> using a consistent method, thereby facilitating global comparisons of <span class="hlt">high</span>-frequency data from lake buoys.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2002cosp...34E.520X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2002cosp...34E.520X"><span>Forecast the energetic <span class="hlt">electron</span> <span class="hlt">flux</span> on geosynchronous orbit with interplanetary parameters</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xue, B.; Ye, Z.</p> <p></p> <p>The <span class="hlt">high</span> <span class="hlt">flux</span> of energetic <span class="hlt">electron</span> on geo-synchronous orbit can cause many kinds of malfunction of the satellite there, within which the bulk charging is the most significant that several broadcast satellite failures were confirmed to be due to this effect. The <span class="hlt">electron</span> <span class="hlt">flux</span> on geo-synchronous orbit varies in a large range even up to three orders accompanied the passage of interplanetary magnetic cloud and the following geomagnetic disturbances. Upon investigating <span class="hlt">electron</span> <span class="hlt">flux</span>, interplanetary solar wind data, and geomagnetic data as well, we found that: (1) The enhancement of energetic <span class="hlt">flux</span> on the geo-synchronous orbit exhibits periodic recurrence of 27days. (2)Significant increase of <span class="hlt">electron</span> <span class="hlt">flux</span> relates to interplanetary index and characters of their distribution. (3)The <span class="hlt">electron</span> <span class="hlt">flux</span> also has relation to solar activity index. In our research work, artificial neural network was employed and constructed according to the job. The neural network, we call it full connecting network, was proved to be a sufficient tool to analyze the character of the evolving parameters, remember the omen of "<span class="hlt">electron</span> storm", and establish the relationship between interplanetary parameters etc., and the fluence of <span class="hlt">high</span> energetic <span class="hlt">electrons</span>. The neural network was carefully constructed and trained to do the job mentioned above. Preliminary result showed that the accuracy forecast of <span class="hlt">electron</span> <span class="hlt">flux</span> 1 day ahead can reach 80%, and 70% for 2 days ahead.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_11 --> <div id="page_12" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="221"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24745228','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24745228"><span>Thermal performance of ethylene glycol based nanofluids in an <span class="hlt">electronic</span> <span class="hlt">heat</span> sink.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Selvakumar, P; Suresh, S</p> <p>2014-03-01</p> <p><span class="hlt">Heat</span> transfer in <span class="hlt">electronic</span> devices such as micro processors and power converters is much essential to keep these devices cool for the better functioning of the systems. Air cooled <span class="hlt">heat</span> sinks are not able to remove the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> produced by the today's <span class="hlt">electronic</span> components. Liquids work better than air in removing <span class="hlt">heat</span>. Thermal conductivity which is the most essential property of any <span class="hlt">heat</span> transfer fluid can be enhanced by adding nano scale solid particles which possess higher thermal conductivity than the liquids. In this work the convective <span class="hlt">heat</span> transfer and pressure drop characteristics of the water/ethylene glycol mixture based nanofluids consisting of Al2O3, CuO nanoparticles with a volume concentration of 0.1% are studied experimentally in a rectangular channel <span class="hlt">heat</span> sink. The nano particles are characterized using Scanning <span class="hlt">Electron</span> Microscope and the nannofluids are prepared by using an ultrasonic vibrator and Sodium Lauryl Salt surfactant. The experimental results showed that nanofluids of 0.1% volume concentration give higher convective <span class="hlt">heat</span> transfer coefficient values than the plain water/ethylene glycol mixture which is prepared in the volume ratio of 70:30. There is no much penalty in the pressure drop values due to the inclusion of nano particles in the water/ethylene glycol mixture.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1305850-broadening-divertor-heat-flux-profile-increasing-number-elm-filaments-nstx','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1305850-broadening-divertor-heat-flux-profile-increasing-number-elm-filaments-nstx"><span>Broadening of divertor <span class="hlt">heat</span> <span class="hlt">flux</span> profile with increasing number of ELM filaments in NSTX</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Ahn, J. -W.; Maingi, R.; Canik, J. M.; ...</p> <p>2014-11-13</p> <p>Edge localized modes (ELMs) represent a challenge to future fusion devices, owing to cyclical <span class="hlt">high</span> peak <span class="hlt">heat</span> <span class="hlt">fluxes</span> on divertor plasma facing surfaces. One ameliorating factor has been that the <span class="hlt">heat</span> <span class="hlt">flux</span> characteristic profile width has been observed to broaden with the size of the ELM, as compared with the inter-ELM <span class="hlt">heat</span> <span class="hlt">flux</span> profile. In contrast, the <span class="hlt">heat</span> <span class="hlt">flux</span> profile has been observed to narrow during ELMs under certain conditions in NSTX. Here we show that the ELM <span class="hlt">heat</span> <span class="hlt">flux</span> profile width increases with the number of filamentary striations observed, i.e., profile narrowing is observed with zero or very fewmore » striations. Because NSTX often lies on the long wavelength current-driven mode side of ideal MHD instabilities, few filamentary structures can be expected under many conditions. Lastly, ITER is also projected to lie on the current driven low-n stability boundary, and therefore detailed projections of the unstable modes expected in ITER and the <span class="hlt">heat</span> <span class="hlt">flux</span> driven in ensuing filamentary structures is needed.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DPPB10035H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DPPB10035H"><span><span class="hlt">Electron</span> Temperature Gradient Scale Measurements in ICRF <span class="hlt">Heated</span> Plasmas at Alcator C-Mod</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Houshmandyar, Saeid; Phillips, Perry E.; Rowan, William L.; Howard, Nathaniel T.; Greenwald, Martin</p> <p>2016-10-01</p> <p>It is generally believed that the temperature gradient is a driving mechanism for the turbulent transport in hot and magnetically confined plasmas. A feature of many anomalous transport models is the critical threshold value (LC) for the gradient scale length, above which both the turbulence and the <span class="hlt">heat</span> transport increases. This threshold is also predicted by the recent multi-scale gyrokinetic simulations, which are focused on addressing the <span class="hlt">electron</span> (and ion) <span class="hlt">heat</span> transport in tokamaks. Recently, we have established an accurate technique (BT-jog) to directly measure the <span class="hlt">electron</span> temperature gradient scale length (LTe =Te / ∇T) profile, using a <span class="hlt">high</span>-spatial resolution radiometer-based <span class="hlt">electron</span> cyclotron emission (ECE) diagnostic. For the work presented here, <span class="hlt">electrons</span> are <span class="hlt">heated</span> by ion cyclotron range of frequencies (ICRF) through minority <span class="hlt">heating</span> in L-mode plasmas at different power levels, TRANSP runs determine the <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> and the scale lengths are measured through the BT-jog technique. Furthermore, the experiment is extended for different plasma current and <span class="hlt">electron</span> densities by which the parametric dependence of LC on magnetic shear, safety factor and density will be investigated. This work is supported by U.S. DoE OFES, under Award No. DE-FG03-96ER-54373.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1985tehs.nasa...51A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1985tehs.nasa...51A"><span>Development of <span class="hlt">heat</span> <span class="hlt">flux</span> sensors for turbine airfoils</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Atkinson, William H.; Cyr, Marcia A.; Strange, Richard R.</p> <p>1985-10-01</p> <p>The objectives of this program are to develop <span class="hlt">heat</span> <span class="hlt">flux</span> sensors suitable for installation in hot section airfoils of advanced aircraft turbine engines and to experimentally verify the operation of these <span class="hlt">heat</span> <span class="hlt">flux</span> sensors in a cylinder in a cross flow experiment. Embedded thermocouple and Gardon gauge sensors were developed and fabricated into both blades and vanes. These were then calibrated using a quartz lamp bank <span class="hlt">heat</span> source and finally subjected to thermal cycle and thermal soak testing. These sensors were also fabricated into cylindrical test pieces and tested in a burner exhaust to verify <span class="hlt">heat</span> <span class="hlt">flux</span> measurements produced by these sensors. The results of the cylinder in cross flow tests are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880001761','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880001761"><span>Development of <span class="hlt">heat</span> <span class="hlt">flux</span> sensors for turbine airfoils</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Atkinson, William H.; Cyr, Marcia A.; Strange, Richard R.</p> <p>1985-01-01</p> <p>The objectives of this program are to develop <span class="hlt">heat</span> <span class="hlt">flux</span> sensors suitable for installation in hot section airfoils of advanced aircraft turbine engines and to experimentally verify the operation of these <span class="hlt">heat</span> <span class="hlt">flux</span> sensors in a cylinder in a cross flow experiment. Embedded thermocouple and Gardon gauge sensors were developed and fabricated into both blades and vanes. These were then calibrated using a quartz lamp bank <span class="hlt">heat</span> source and finally subjected to thermal cycle and thermal soak testing. These sensors were also fabricated into cylindrical test pieces and tested in a burner exhaust to verify <span class="hlt">heat</span> <span class="hlt">flux</span> measurements produced by these sensors. The results of the cylinder in cross flow tests are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.nrel.gov/csp/facility-hfsf.html','SCIGOVWS'); return false;" href="https://www.nrel.gov/csp/facility-hfsf.html"><span><span class="hlt">High-Flux</span> Solar Furnace Facility | Concentrating Solar Power | NREL</span></a></p> <p><a target="_blank" href="http://www.science.gov/aboutsearch.html">Science.gov Websites</a></p> <p></p> <p></p> <p><em><span class="hlt">High</em>-Flux</span> Solar Furnace Facility <em><span class="hlt">High</em>-Flux</span> Solar Furnace Facility NREL's <em><span class="hlt">High</em>-Flux</span> Solar Furnace (HFSF) is a 10-kW optical furnace for testing <em><span class="hlt">high</span></em>-temperature processes or applications requiring <em><span class="hlt">high</span></em> range of technologies with a diverse set of experimental requirements. The <em><span class="hlt">high</span></em> <span class="hlt">heating</span> rates create the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880001849','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880001849"><span>Enhancement of surface-atmosphere <span class="hlt">fluxes</span> by desert-fringe vegetation through reduction of surface albedo and of soil <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Otterman, J.</p> <p>1987-01-01</p> <p>Under the arid conditions prevailing at the end of the dry season in the western Negev/northern Sinai region, vegetation causes a sharp increase relative to bare soil in the daytime sensible <span class="hlt">heat</span> <span class="hlt">flux</span> from the surface to the atmosphere. Two mechanisms are involved: the increase in the surface absorptivity and a decrease in the surface <span class="hlt">heat</span> <span class="hlt">flux</span>. By increasing the sensible <span class="hlt">heat</span> <span class="hlt">flux</span> to the atmosphere through the albedo and the soil <span class="hlt">heat</span> <span class="hlt">flux</span> reductions, the desert-fringe vegetation increases the daytime convection and the growth of the planetary boundary layer. Removal of vegetation by overgrazing, by reducing the sensible <span class="hlt">heat</span> <span class="hlt">flux</span>, tends to reduce daytime convective precipitation, producing higher probabilities of drought conditions. This assessment of overgrazing is based on observations in the Sinai/Negev, where the soil albedo is <span class="hlt">high</span> and where overgrazing produces an essential bare soil. Even if the assessment for the Sinai/Negev does not quantitatively apply throughout Africa, the current practice in many African countries of maintaining a large population of grazing animals, can contribute through the mesoscale mechanisms described to reduce daytime convective precipitation, perpetuating higher probabilities of drought. Time-of-day analysis of precipitation in Africa appears worthwhile, to better assess the role of the surface conditions in contributing to drought.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUOSHE12A..03H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUOSHE12A..03H"><span>Energy and variance budgets of a diffusive staircase with implications for <span class="hlt">heat</span> <span class="hlt">flux</span> scaling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hieronymus, M.; Carpenter, J. R.</p> <p>2016-02-01</p> <p>Diffusive convection, the mode of double-diffusive convection that occur when both temperature and salinity increase with increasing depth, is commonplace throughout the <span class="hlt">high</span> latitude oceans and diffusive staircases constitute an important <span class="hlt">heat</span> transport process in the Arctic Ocean. <span class="hlt">Heat</span> and buoyancy <span class="hlt">fluxes</span> through these staircases are often estimated using <span class="hlt">flux</span> laws deduced either from laboratory experiments, or from simplified energy or variance budgets. We have done direct numerical simulations of double-diffusive convection at a range of Rayleigh numbers and quantified the energy and variance budgets in detail. This allows us to compare the <span class="hlt">fluxes</span> in our simulations to those derived using known <span class="hlt">flux</span> laws and to quantify how well the simplified energy and variance budgets approximate the full budgets. The <span class="hlt">fluxes</span> are found to agree well with earlier estimates at <span class="hlt">high</span> Rayleigh numbers, but we find large deviations at low Rayleigh numbers. The close ties between the <span class="hlt">heat</span> and buoyancy <span class="hlt">fluxes</span> and the budgets of thermal variance and energy have been utilized to derive <span class="hlt">heat</span> <span class="hlt">flux</span> scaling laws in the field of thermal convection. The result is the so called GL-theory, which has been found to give accurate <span class="hlt">heat</span> <span class="hlt">flux</span> scaling laws in a very wide parameter range. Diffusive convection has many similarities to thermal convection and an extension of the GL-theory to diffusive convection is also presented and its predictions are compared to the results from our numerical simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940024321','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940024321"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> instrumentation for Hyflite thermal protection system</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Diller, T. E.</p> <p>1994-01-01</p> <p>Using Thermal Protection Tile core samples supplied by NASA, the surface characteristics of the FRCI, TUFI, and RCG coatings were evaluated. Based on these results, appropriate methods of surface preparation were determined and tested for the required sputtering processes. Sample sensors were fabricated on the RCG coating and adhesion was acceptable. Based on these encouraging results, complete <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensors were fabricated on the RCG coating. The issue of lead attachment was addressed with the annnealing and welding methods developed at NASA Lewis. Parallel gap welding appears to be the best method of lead attachment with prior <span class="hlt">heat</span> treatment of the sputtered pads. Sample <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensors were submitted for testing in the NASA Ames arc jet facility. Details of the project are contained in two attached reports. One additional item of interest is contained in the attached AIAA paper, which gives details of the transient response of a <span class="hlt">Heat</span> <span class="hlt">Flux</span> Microsensors in a shock tube facility at Virginia Tech. The response of the <span class="hlt">heat</span> <span class="hlt">flux</span> sensor was measured to be faster than 10 micro-s.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70032127','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70032127"><span>Using <span class="hlt">heat</span> to characterize streambed water <span class="hlt">flux</span> variability in four stream reaches</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Essaid, H.I.; Zamora, C.M.; McCarthy, K.A.; Vogel, J.R.; Wilson, J.T.</p> <p>2008-01-01</p> <p>Estimates of streambed water <span class="hlt">flux</span> are needed for the interpretation of streambed chemistry and reactions. Continuous temperature and head monitoring in stream reaches within four agricultural watersheds (Leary Weber Ditch, IN; Maple Creek, NE; DR2 Drain, WA; and Merced River, CA) allowed <span class="hlt">heat</span> to be used as a tracer to study the temporal and spatial variability of <span class="hlt">fluxes</span> through the streambed. Synoptic methods (seepage meter and differential discharge measurements) were compared with estimates obtained by using <span class="hlt">heat</span> as a tracer. Water <span class="hlt">flux</span> was estimated by modeling one-dimensional vertical flow of water and <span class="hlt">heat</span> using the model VS2DH. <span class="hlt">Flux</span> was influenced by physical heterogeneity of the stream channel and temporal variability in stream and ground-water levels. During most of the study period (April-December 2004), <span class="hlt">flux</span> was upward through the streambeds. At the IN, NE, and CA sites, <span class="hlt">high</span>-stage events resulted in rapid reversal of flow direction inducing short-term surface-water flow into the streambed. During late summer at the IN site, regional ground-water levels dropped, leading to surface-water loss to ground water that resulted in drying of the ditch. Synoptic measurements of <span class="hlt">flux</span> generally supported the model <span class="hlt">flux</span> estimates. Water flow through the streambed was roughly an order of magnitude larger in the humid basins (IN and NE) than in the arid basins (WA and CA). Downward <span class="hlt">flux</span>, in response to sudden <span class="hlt">high</span> streamflows, and seasonal variability in <span class="hlt">flux</span> was most pronounced in the humid basins and in <span class="hlt">high</span> conductivity zones in the streambed. Copyright ?? 2008 by the American Society of Agronomy, Crop Science Society of America, and Soil Science Society of America. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5114644','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5114644"><span><span class="hlt">High</span> <span class="hlt">flux</span> circularly polarized gamma beam factory: coupling a Fabry-Perot optical cavity with an <span class="hlt">electron</span> storage ring</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chaikovska, I.; Cassou, K.; Chiche, R.; Cizeron, R.; Cornebise, P.; Delerue, N.; Jehanno, D.; Labaye, F.; Marie, R.; Martens, A.; Peinaud, Y.; Soskov, V.; Variola, A.; Zomer, F.; Cormier, E.; Lhermite, J.; Dolique, V.; Flaminio, R.; Michel, C.; Pinard, L.; Sassolas, B.; Akagi, T.; Araki, S.; Honda, Y.; Omori, T.; Terunuma, N.; Urakawa, J.; Miyoshi, S.; Takahashi, T.; Yoshitama, H.</p> <p>2016-01-01</p> <p>We report and discuss <span class="hlt">high-flux</span> generation of circularly polarized γ-rays by means of Compton scattering. The γ-ray beam results from the collision of an external-cavity-enhanced infrared laser beam and a low emittance relativistic <span class="hlt">electron</span> beam. By operating a non-planar bow-tie <span class="hlt">high</span>-finesse optical Fabry-Perot cavity coupled to a storage ring, we have recorded a <span class="hlt">flux</span> of up to (3.5 ± 0.3) × 108 photons per second with a mean measured energy of 24 MeV. The γ-ray <span class="hlt">flux</span> has been sustained for several hours. In particular, we were able to measure a record value of up to 400 γ-rays per collision in a full bandwidth. Moreover, the impact of Compton scattering on the <span class="hlt">electron</span> beam dynamics could be observed resulting in a reduction of the <span class="hlt">electron</span> beam lifetime correlated to the laser power stored in the Fabry-Perot cavity. We demonstrate that the <span class="hlt">electron</span> beam lifetime provides an independent and consistent determination of the γ-ray <span class="hlt">flux</span>. Furthermore, a reduction of the γ-ray <span class="hlt">flux</span> due to intrabeam scattering has clearly been identified. These results, obtained on an accelerator test facility, warrant potential scaling and revealed both expected and yet unobserved effects. They set the baseline for further scaling of the future Compton sources under development around the world. PMID:27857146</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22612575-results-high-heat-flux-tests-tungsten-divertor-targets-under-plasma-heat-loads-expected-iter-tokamaks-review','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22612575-results-high-heat-flux-tests-tungsten-divertor-targets-under-plasma-heat-loads-expected-iter-tokamaks-review"><span>Results of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> tests of tungsten divertor targets under plasma <span class="hlt">heat</span> loads expected in ITER and tokamaks (review)</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Budaev, V. P., E-mail: budaev@mail.ru</p> <p>2016-12-15</p> <p><span class="hlt">Heat</span> loads on the tungsten divertor targets in the ITER and the tokamak power reactors reach ~10MW m{sup −2} in the steady state of DT discharges, increasing to ~0.6–3.5 GW m{sup −2} under disruptions and ELMs. The results of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> tests (HHFTs) of tungsten under such transient plasma <span class="hlt">heat</span> loads are reviewed in the paper. The main attention is paid to description of the surface microstructure, recrystallization, and the morphology of the cracks on the target. Effects of melting, cracking of tungsten, drop erosion of the surface, and formation of corrugated and porous layers are observed. Production ofmore » submicron-sized tungsten dust and the effects of the inhomogeneous surface of tungsten on the plasma–wall interaction are discussed. In conclusion, the necessity of further HHFTs and investigations of the durability of tungsten under <span class="hlt">high</span> pulsed plasma loads on the ITER divertor plates, including disruptions and ELMs, is stressed.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JGRD..12011957A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JGRD..12011957A"><span>Recent trends (2003-2013) of land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> on the southern side of the central Himalayas, Nepal</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Amatya, Pukar Man; Ma, Yaoming; Han, Cunbo; Wang, Binbin; Devkota, Lochan Prasad</p> <p>2015-12-01</p> <p>Novice efforts have been made in order to study the regional distribution of land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> on the southern side of the central Himalayas utilizing <span class="hlt">high</span>-resolution remotely sensed products, but these have been on instantaneous scale. In this study the Surface Energy Balance System model is used to obtain annual averaged maps of the land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> for 11 years (2003-2013) and study their annual trends on the central Himalayan region. The maps were derived at 5 km resolution using monthly input products ranging from satellite derived to Global Land Data Assimilation System meteorological data. It was found that the net radiation <span class="hlt">flux</span> is increasing as a result of decreasing precipitation (drier environment). The sensible <span class="hlt">heat</span> <span class="hlt">flux</span> did not change much except for the northwestern <span class="hlt">High</span> Himalaya and <span class="hlt">High</span> Mountains. In northwestern <span class="hlt">High</span> Himalaya sensible <span class="hlt">heat</span> <span class="hlt">flux</span> is decreasing because of decrease in wind speed, ground-air temperature difference, and increase in winter precipitation, whereas in <span class="hlt">High</span> Mountains it is increasing due to increase in ground-air temperature difference and <span class="hlt">high</span> rate of deforestation. The latent <span class="hlt">heat</span> <span class="hlt">flux</span> has an overall increasing trend with increase more pronounced in the lower regions compared to <span class="hlt">high</span> elevated regions. It has been reported that precipitation is decreasing with altitude in this region. Therefore, the increasing trend in latent <span class="hlt">heat</span> <span class="hlt">flux</span> can be attributed to increase in net radiation <span class="hlt">flux</span> under persistent forest cover and irrigation land used for agriculture.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JIEIC.tmp..264S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JIEIC.tmp..264S"><span>Prediction of Experimental Surface <span class="hlt">Heat</span> <span class="hlt">Flux</span> of Thin Film Gauges using ANFIS</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sarma, Shrutidhara; Sahoo, Niranjan; Unal, Aynur</p> <p>2018-05-01</p> <p>Precise quantification of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> in <span class="hlt">highly</span> transient environment is of paramount importance from the design point of view of several engineering equipment like thermal protection or cooling systems. Such environments are simulated in experimental facilities by exposing the surface with transient <span class="hlt">heat</span> loads typically step/impulsive in nature. The surface <span class="hlt">heating</span> rates are then determined from <span class="hlt">highly</span> transient temperature history captured by efficient surface temperature sensors. The classical approach is to use thin film gauges (TFGs) in which temperature variations are acquired within milliseconds, thereby allowing calculation of surface <span class="hlt">heat</span> <span class="hlt">flux</span>, based on the theory of one-dimensional <span class="hlt">heat</span> conduction on a semi-infinite body. With recent developments in the soft computing methods, the present study is an attempt for the application of intelligent system technique, called adaptive neuro fuzzy inference system (ANFIS) to recover surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> from a given temperature history recorded by TFGs without having the need to solve lengthy analytical equations. Experiments have been carried out by applying known quantity of `impulse <span class="hlt">heat</span> load' through laser beam on TFGs. The corresponding voltage signals have been acquired and surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> are estimated through classical analytical approach. These signals are then used to `train' the ANFIS model, which later predicts output for `test' values. Results from both methods have been compared and these surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> are used to predict the non-linear relationship between thermal and electrical properties of the gauges that are exceedingly pertinent to the design of efficient TFGs. Further, surface plots have been created to give an insight about dimensionality effect of the non-linear dependence of thermal/electrical parameters on each other. Later, it is observed that a properly optimized ANFIS model can predict the impulsive <span class="hlt">heat</span> profiles with significant accuracy. This paper thus shows the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150023475','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150023475"><span>The Impact of Trends in the Large Scale Atmospheric Circulation on Mediterranean Surface Turbulent <span class="hlt">Heat</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Romanski, Joy; Hameed, Sultan</p> <p>2015-01-01</p> <p>Interannual variations of latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> (LHF) and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> (SHF) over the Mediterranean for the boreal winter season (DJF) show positive trends during 1958-2011. Comparison of correlations between the <span class="hlt">heat</span> <span class="hlt">fluxes</span> and the intensity and location of the Azores <span class="hlt">High</span> (AH), and the NAO and East Atlantic-West Russia (EAWR) teleconnections, along with analysis of composites of surface temperature, humidity and wind fields for different teleconnection states, demonstrates that variations of the AH are found to explain the <span class="hlt">heat</span> <span class="hlt">flux</span> changes more successfully than the NAO and the EAWR. Trends in sea level pressure and longitude of the Azores <span class="hlt">High</span> during DJF show a strengthening, and an eastward shift. DJF Azores <span class="hlt">High</span> pressure and longitude are shown to co-vary such that variability of the Azores <span class="hlt">High</span> occurs along an axis defined by lower pressure and westward location at one extreme, and higher pressure and eastward location at the other extreme. The shift of the Azores <span class="hlt">High</span> from predominance of the low/west state to the <span class="hlt">high</span>/east state induces trends in Mediterranean Sea surface winds, temperature and moisture. These, combined with sea surface warming trends, produce trends in wintertime Mediterranean Sea sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120002841','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120002841"><span>Analysis of Voyager Observed <span class="hlt">High</span>-Energy <span class="hlt">Electron</span> <span class="hlt">Fluxes</span> in the Heliosheath Using MHD Simulations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Washimi, Haruichi; Webber, W. R.; Zank, Gary P.; Hu, Qiang; Florinski, Vladimir; Adams, James; Kubo, Yuki</p> <p>2011-01-01</p> <p>The Voyager spacecraft (V1 and V2) observed <span class="hlt">electrons</span> of 6-14 MeV in the heliosheath which showed several incidences of <span class="hlt">flux</span> variation relative to a background of gradually increasing <span class="hlt">flux</span> with distance from the Sun. The increasing <span class="hlt">flux</span> of background <span class="hlt">electrons</span> is thought to result from inward radial diffusion. We compare the temporal <span class="hlt">electron</span> <span class="hlt">flux</span> variation with dynamical phenomena in the heliosheath that are obtained from our MHD simulations. Because our simulation is based on V2 observed plasma data before V2 crossed the termination shock, this analysis is effective up to late 2008, i.e., about a year after the V2-crossing, during which disturbances, driven prior to the crossing time, survived in the heliosheath. Several <span class="hlt">electron</span> <span class="hlt">flux</span> variations correspond to times directly associated with interplanetary shock events. One noteworthy example corresponds to various times associated with the March 2006 interplanetary shock, these being the collision with the termination shock, the passage past the V1 spacecraft, and the collision with the region near the heliopause, as identified by W.R. Webber et al. for proton/helium of 7-200 MeV. Our simulations indicate that all other <span class="hlt">electron</span> <span class="hlt">flux</span> variations, except one, correspond well to the times when a shock-driven magneto-sonic pulse and its reflection in the heliosheath either passed across V1/V2, or collided with the termination shock or with the plasma sheet near the heliopause. This result suggests that variation in the <span class="hlt">electron</span> <span class="hlt">flux</span> should be due to either direct or indirect effects of magnetosonic pulses in the heliosheath driven by interplanetary shocks</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990014321','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990014321"><span>Conditions for Aeronomic Applicability of the Classical <span class="hlt">Electron</span> <span class="hlt">Heat</span> Conduction Formula</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cole, K. D.; Hoegy, W. R.</p> <p>1998-01-01</p> <p>Conditions for the applicability of the classical formula for <span class="hlt">heat</span> conduction in the <span class="hlt">electrons</span> in ionized gas are investigated. In a fully ionised gas ( V(sub en) much greater than V(sub ei)), when the mean free path for <span class="hlt">electron-electron</span> (or <span class="hlt">electron</span>-ion) collisions is much larger than the characteristic thermal scale length of the observed system, the conditions for applicability break down. In the case of the Venus ionosphere this breakdown is indicated for a large fraction of the <span class="hlt">electron</span> temperature data from altitudes greater than 180 km, for <span class="hlt">electron</span> densities less than 10(exp 4)/cc cm. In a partially ionised gas such that V(sub en) much greater than V(sub ei) there is breakdown of the formula not only when the mean free path of <span class="hlt">electrons</span> greatly exceeds the thermal scale length, but also when the gradient of neutral particle density exceeds the <span class="hlt">electron</span> thermal gradient. It is shown that <span class="hlt">electron</span> <span class="hlt">heat</span> conduction may be neglected in estimating the temperature of joule <span class="hlt">heated</span> <span class="hlt">electrons</span> by observed strong 100 Hz electric fields when the conduction <span class="hlt">flux</span> is limited by the saturation <span class="hlt">flux</span>. The results of this paper support our earlier aeronomical arguments against the hypothesis of planetary scale whistlers for the 100 Hz electric field signal. In turn this means that data from the 100 Hz signal may not be used to support the case for lightning on Venus.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PhPl...22d2516M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PhPl...22d2516M"><span>Turbulent transport regimes and the scrape-off layer <span class="hlt">heat</span> <span class="hlt">flux</span> width</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Myra, J. R.; D'Ippolito, D. A.; Russell, D. A.</p> <p>2015-04-01</p> <p>Understanding the responsible mechanisms and resulting scaling of the scrape-off layer (SOL) <span class="hlt">heat</span> <span class="hlt">flux</span> width is important for predicting viable operating regimes in future tokamaks and for seeking possible mitigation schemes. In this paper, we present a qualitative and conceptual framework for understanding various regimes of edge/SOL turbulence and the role of turbulent transport as the mechanism for establishing the SOL <span class="hlt">heat</span> <span class="hlt">flux</span> width. Relevant considerations include the type and spectral characteristics of underlying instabilities, the location of the gradient drive relative to the SOL, the nonlinear saturation mechanism, and the parallel <span class="hlt">heat</span> transport regime. We find a <span class="hlt">heat</span> <span class="hlt">flux</span> width scaling with major radius R that is generally positive, consistent with the previous findings [Connor et al., Nucl. Fusion 39, 169 (1999)]. The possible relationship of turbulence mechanisms to the neoclassical orbit width or heuristic drift mechanism in core energy confinement regimes known as low (L) mode and <span class="hlt">high</span> (H) mode is considered, together with implications for the future experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970000386','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970000386"><span>The Development of Novel, <span class="hlt">High-Flux</span>, <span class="hlt">Heat</span> Transfer Cells for Thermal Control in Microgravity</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Smith, Marc K.; Glezer, Ari</p> <p>1996-01-01</p> <p>In order to meet the future needs of thermal management and control in space applications such as the Space Lab, new <span class="hlt">heat</span>-transfer technology capable of much larger <span class="hlt">heat</span> <span class="hlt">fluxes</span> must be developed. To this end, we describe complementary numerical and experimental investigations into the fundamental fluid mechanics and <span class="hlt">heat</span>-transfer processes involved in a radically new, self contained, <span class="hlt">heat</span> transfer cell for microgravity applications. In contrast to conventional <span class="hlt">heat</span> pipes, the <span class="hlt">heat</span> transfer in this cell is based on a forced droplet evaporation process using a fine spray. The spray is produced by a novel fluidic technology recently developed at Georgia Tech. This technology is based on a vibration induced droplet atomization process. In this technique, a liquid droplet is placed on a flexible membrane and is vibrated normal to itself. When the proper drop size is attained, the droplet resonates with the surface motion of the membrane and almost immediately bursts into a shower of very fine secondary droplets. The small droplets travel to the opposite end of the cell where they impact a <span class="hlt">heated</span> surface and are evaporated. The vapor returns to the cold end of the cell and condenses to form the large droplets that are fragmented to form the spray. Preliminary estimates show that a <span class="hlt">heat</span> transfer cell based on this technology would have a <span class="hlt">heat-flux</span> capacity that is an order of magnitude higher than those of current <span class="hlt">heat</span> pipes designs used in microgravity applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950037243&hterms=impact+art&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dimpact%2Bart','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950037243&hterms=impact+art&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dimpact%2Bart"><span>The impact of land-surface wetness heterogeneity on mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chen, Fei; Avissar, Roni</p> <p>1994-01-01</p> <p>Vertical <span class="hlt">heat</span> <span class="hlt">fluxes</span> associated with mesoscale circulations generated by land-surface wetness discontinuities are often stronger than turbulent <span class="hlt">fluxes</span>, especially in the upper part of the atmospheric planetary boundary layer. As a result, they contribute significantly to the subgrid-scale <span class="hlt">fluxes</span> in large-scale atmospheric models. Yet they are not considered in these models. To provide some insights into the possible parameterization of these <span class="hlt">fluxes</span> in large-scale models, a state-of-the-art mesoscale numerical model was used to investigate the relationships between mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span> and atmospheric and land-surface characteristics that play a key role in the generation of mesoscale circulations. The distribution of land-surface wetness, the wavenumber and the wavelength of the land-surface discontinuities, and the large-scale wind speed have a significant impact on the mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Empirical functions were derived to characterize the relationships between mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span> and the spatial distribution of land-surface wetness. The strongest mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span> were obtained for a wavelength of forcing corresponding approximately to the local Rossby deformation radius. The mesoscale <span class="hlt">heat</span> <span class="hlt">fluxes</span> are weakened by large-scale background winds but remain significant even with moderate winds.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_12 --> <div id="page_13" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="241"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/5272193','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/5272193"><span>Device and method for <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span> density plasma</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Thode, L.E.</p> <p></p> <p>A device and method for relativistic <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span> density plasma in a small localized region are described. A relativistic <span class="hlt">electron</span> beam generator produces a <span class="hlt">high</span> voltage <span class="hlt">electron</span> beam which propagates along a vacuum drift tube and is modulated to initiate <span class="hlt">electron</span> bunching within the beam. The beam is then directed through a low density gas chamber which provides isolation between the vacuum modulator and the relativistic <span class="hlt">electron</span> beam target. The relativistic beam is then applied to a <span class="hlt">high</span> density target plasma which typically comprises DT, DD, hydrogen boron or similar thermonuclear gas at a density of 10/sup 17/ to 10/sup 20/.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhPl...25b2509G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhPl...25b2509G"><span>Multi-scale transport in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span> and projection to ITER</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Grierson, B. A.; Staebler, G. M.; Solomon, W. M.; McKee, G. R.; Holland, C.; Austin, M.; Marinoni, A.; Schmitz, L.; Pinsker, R. I.; DIII-D Team</p> <p>2018-02-01</p> <p>Multi-scale fluctuations measured by turbulence diagnostics spanning long and short wavelength spatial scales impact energy confinement and the scale-lengths of plasma kinetic profiles in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span>. Contrasting discharge phases with ECH + neutral beam injection (NBI) and NBI only at similar rotation reveal higher energy confinement and lower fluctuations when only NBI <span class="hlt">heating</span> is used. Modeling of the core transport with TGYRO using the TGLF turbulent transport model and NEO neoclassical transport reproduces the experimental profile changes upon application of direct <span class="hlt">electron</span> <span class="hlt">heating</span> and indicates that multi-scale transport mechanisms are responsible for changes in the temperature and density profiles. Intermediate and <span class="hlt">high</span>-k fluctuations appear responsible for the enhanced <span class="hlt">electron</span> thermal <span class="hlt">flux</span>, and intermediate-k <span class="hlt">electron</span> modes produce an inward particle pinch that increases the inverse density scale length. Projection to ITER is performed with TGLF and indicates a density profile that has a finite scale length due to intermediate-k <span class="hlt">electron</span> modes at low collisionality and increases the fusion gain. For a range of E × B shear, the dominant mechanism that increases fusion performance is suppression of outward low-k particle <span class="hlt">flux</span> and increased density peaking.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22390828-magnetic-flux-heat-losses-diffusive-advective-nernst-effects-maglif-like-plasma','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22390828-magnetic-flux-heat-losses-diffusive-advective-nernst-effects-maglif-like-plasma"><span>Magnetic <span class="hlt">flux</span> and <span class="hlt">heat</span> losses by diffusive, advective, and Nernst effects in MagLIF-like plasma</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Velikovich, A. L., E-mail: sasha.velikovich@nrl.navy.mil; Giuliani, J. L., E-mail: sasha.velikovich@nrl.navy.mil; Zalesak, S. T.</p> <p>2014-12-15</p> <p>The MagLIF approach to inertial confinement fusion involves subsonic/isobaric compression and <span class="hlt">heating</span> of a DT plasma with frozen-in magnetic <span class="hlt">flux</span> by a heavy cylindrical liner. The losses of <span class="hlt">heat</span> and magnetic <span class="hlt">flux</span> from the plasma to the liner are thereby determined by plasma advection and gradient-driven transport processes, such as thermal conductivity, magnetic field diffusion and thermomagnetic effects. Theoretical analysis based on obtaining exact self-similar solutions of the classical collisional Braginskii's plasma transport equations in one dimension demonstrates that the <span class="hlt">heat</span> loss from the hot plasma to the cold liner is dominated by the transverse <span class="hlt">heat</span> conduction and advection, andmore » the corresponding loss of magnetic <span class="hlt">flux</span> is dominated by advection and the Nernst effect. For a large <span class="hlt">electron</span> Hall parameter ω{sub e}τ{sub e} effective diffusion coefficients determining the losses of <span class="hlt">heat</span> and magnetic <span class="hlt">flux</span> are both shown to decrease with ω{sub e}τ{sub e} as does the Bohm diffusion coefficient, which is commonly associated with low collisionality and two-dimensional transport. This family of exact solutions can be used for verification of codes that model the MagLIF plasma dynamics.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AIPC.1573.1099I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AIPC.1573.1099I"><span>Ultra-<span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> cooling characteristics of cryogenic micro-solid nitrogen particles and its application to semiconductor wafer cleaning technology</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ishimoto, Jun; Oh, U.; Guanghan, Zhao; Koike, Tomoki; Ochiai, Naoya</p> <p>2014-01-01</p> <p>The ultra-<span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> cooling characteristics and impingement behavior of cryogenic micro-solid nitrogen (SN2) particles in relation to a <span class="hlt">heated</span> wafer substrate were investigated for application to next generation semiconductor wafer cleaning technology. The fundamental characteristics of cooling <span class="hlt">heat</span> transfer and photoresist removal-cleaning performance using micro-solid nitrogen particulate spray impinging on a <span class="hlt">heated</span> substrate were numerically investigated and experimentally measured by a new type of integrated computational-experimental technique. This study contributes not only advanced cryogenic cooling technology for <span class="hlt">high</span> thermal emission devices, but also to the field of nano device engineering including the semiconductor wafer cleaning technology.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC24C..04C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC24C..04C"><span>Improving Global Net Surface <span class="hlt">Heat</span> <span class="hlt">Flux</span> with Ocean Reanalysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Carton, J.; Chepurin, G. A.; Chen, L.; Grodsky, S.</p> <p>2017-12-01</p> <p>This project addresses the current level of uncertainty in surface <span class="hlt">heat</span> <span class="hlt">flux</span> estimates. Time mean surface <span class="hlt">heat</span> <span class="hlt">flux</span> estimates provided by atmospheric reanalyses differ by 10-30W/m2. They are generally unbalanced globally, and have been shown by ocean simulation studies to be incompatible with ocean temperature and velocity measurements. Here a method is presented 1) to identify the spatial and temporal structure of the underlying errors and 2) to reduce them by exploiting hydrographic observations and the analysis increments produced by an ocean reanalysis using sequential data assimilation. The method is applied to <span class="hlt">fluxes</span> computed from daily state variables obtained from three widely used reanalyses: MERRA2, ERA-Interim, and JRA-55, during an eight year period 2007-2014. For each of these seasonal <span class="hlt">heat</span> <span class="hlt">flux</span> errors/corrections are obtained. In a second set of experiments the <span class="hlt">heat</span> <span class="hlt">fluxes</span> are corrected and the ocean reanalysis experiments are repeated. This second round of experiments shows that the time mean error in the corrected <span class="hlt">fluxes</span> is reduced to within ±5W/m2 over the interior subtropical and midlatitude oceans, with the most significant changes occuring over the Southern Ocean. The global <span class="hlt">heat</span> <span class="hlt">flux</span> imbalance of each reanalysis is reduced to within a few W/m2 with this single correction. Encouragingly, the corrected forms of the three sets of <span class="hlt">fluxes</span> are also shown to converge. In the final discussion we present experiments beginning with a modified form of the ERA-Int reanalysis, produced by the DAKKAR program, in which state variables have been individually corrected based on independent measurements. Finally, we discuss the separation of <span class="hlt">flux</span> error from model error.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3995107','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3995107"><span>Estimation of Surface <span class="hlt">Heat</span> <span class="hlt">Flux</span> and Surface Temperature during Inverse <span class="hlt">Heat</span> Conduction under Varying Spray Parameters and Sample Initial Temperature</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Aamir, Muhammad; Liao, Qiang; Zhu, Xun; Aqeel-ur-Rehman; Wang, Hong</p> <p>2014-01-01</p> <p>An experimental study was carried out to investigate the effects of inlet pressure, sample thickness, initial sample temperature, and temperature sensor location on the surface <span class="hlt">heat</span> <span class="hlt">flux</span>, surface temperature, and surface ultrafast cooling rate using stainless steel samples of diameter 27 mm and thickness (mm) 8.5, 13, 17.5, and 22, respectively. Inlet pressure was varied from 0.2 MPa to 1.8 MPa, while sample initial temperature varied from 600°C to 900°C. Beck's sequential function specification method was utilized to estimate surface <span class="hlt">heat</span> <span class="hlt">flux</span> and surface temperature. Inlet pressure has a positive effect on surface <span class="hlt">heat</span> <span class="hlt">flux</span> (SHF) within a critical value of pressure. Thickness of the sample affects the maximum achieved SHF negatively. Surface <span class="hlt">heat</span> <span class="hlt">flux</span> as <span class="hlt">high</span> as 0.4024 MW/m2 was estimated for a thickness of 8.5 mm. Insulation effects of vapor film become apparent in the sample initial temperature range of 900°C causing reduction in surface <span class="hlt">heat</span> <span class="hlt">flux</span> and cooling rate of the sample. A sensor location near to quenched surface is found to be a better choice to visualize the effects of spray parameters on surface <span class="hlt">heat</span> <span class="hlt">flux</span> and surface temperature. Cooling rate showed a profound increase for an inlet pressure of 0.8 MPa. PMID:24977219</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25725898','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25725898"><span>Note: design and development of improved indirectly <span class="hlt">heated</span> cathode based strip <span class="hlt">electron</span> gun.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Maiti, Namita; Bade, Abhijeet; Tembhare, G U; Patil, D S; Dasgupta, K</p> <p>2015-02-01</p> <p>An improved design of indirectly <span class="hlt">heated</span> solid cathode based <span class="hlt">electron</span> gun (200 kW, 45 kV, 270° bent strip type <span class="hlt">electron</span> gun) has been presented. The solid cathode is made of thoriated tungsten, which acts as an improved source of <span class="hlt">electron</span> at lower temperature. So, <span class="hlt">high</span> power operation is possible without affecting structural integrity of the <span class="hlt">electron</span> gun. The design issues are addressed based on the uniformity of temperature on the solid cathode and the single long filament based design. The design approach consists of simulation followed by extensive experimentation. In the design, the effort has been put to tailor the non-uniformity of the <span class="hlt">heat</span> <span class="hlt">flux</span> from the filament to the solid cathode to obtain better uniformity of temperature on the solid cathode. Trial beam experiments have been carried out and it is seen that the modified design achieves one to one correspondence of the solid cathode length and the <span class="hlt">electron</span> beam length.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22392390-note-design-development-improved-indirectly-heated-cathode-based-strip-electron-gun','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22392390-note-design-development-improved-indirectly-heated-cathode-based-strip-electron-gun"><span>Note: Design and development of improved indirectly <span class="hlt">heated</span> cathode based strip <span class="hlt">electron</span> gun</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Maiti, Namita; Patil, D. S.; Dasgupta, K.</p> <p></p> <p>An improved design of indirectly <span class="hlt">heated</span> solid cathode based <span class="hlt">electron</span> gun (200 kW, 45 kV, 270° bent strip type <span class="hlt">electron</span> gun) has been presented. The solid cathode is made of thoriated tungsten, which acts as an improved source of <span class="hlt">electron</span> at lower temperature. So, <span class="hlt">high</span> power operation is possible without affecting structural integrity of the <span class="hlt">electron</span> gun. The design issues are addressed based on the uniformity of temperature on the solid cathode and the single long filament based design. The design approach consists of simulation followed by extensive experimentation. In the design, the effort has been put to tailor themore » non-uniformity of the <span class="hlt">heat</span> <span class="hlt">flux</span> from the filament to the solid cathode to obtain better uniformity of temperature on the solid cathode. Trial beam experiments have been carried out and it is seen that the modified design achieves one to one correspondence of the solid cathode length and the <span class="hlt">electron</span> beam length.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1429196-observations-electron-heating-during-ghz-microwave-power-application-proto-mpex','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1429196-observations-electron-heating-during-ghz-microwave-power-application-proto-mpex"><span>Observations of <span class="hlt">electron</span> <span class="hlt">heating</span> during 28 GHz microwave power application in proto-MPEX</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Biewer, Theodore M.; Bigelow, Tim S.; Caneses Marin, Juan F.; ...</p> <p>2018-02-01</p> <p>The Prototype Material Plasma Exposure Experiment at the Oak Ridge National Laboratory utilizes a variety of power systems to generate and deliver a <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> plasma onto the surface of material targets. In the experiments described here, a deuterium plasma is produced via a ~100 kW, 13.56 MHz RF helicon source, to which ~20 kW of 28 GHz microwave power is applied. The <span class="hlt">electron</span> density and temperature profiles are measured using a Thomson scattering (TS) diagnostic, and indicate that the <span class="hlt">electron</span> density is centrally peaked. In the core of the plasma column, the <span class="hlt">electron</span> density is higher than themore » cut-off density (~0.9 × 1019 m -3) for the launched mixture of X- and O-mode <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> waves to propagate. TS measurements indicate <span class="hlt">electron</span> temperature increases from ~5 eV to ~20 eV during 28 GHz power application when the neutral deuterium pressure is reduced below 0.13 Pa (~1 mTorr.).« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhPl...25b4501B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhPl...25b4501B"><span>Observations of <span class="hlt">electron</span> <span class="hlt">heating</span> during 28 GHz microwave power application in proto-MPEX</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Biewer, T. M.; Bigelow, T. S.; Caneses, J. F.; Diem, S. J.; Green, D. L.; Kafle, N.; Rapp, J.; Proto-MPEX Team</p> <p>2018-02-01</p> <p>The Prototype Material Plasma Exposure Experiment at the Oak Ridge National Laboratory utilizes a variety of power systems to generate and deliver a <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> plasma onto the surface of material targets. In the experiments described here, a deuterium plasma is produced via a ˜100 kW, 13.56 MHz RF helicon source, to which ˜20 kW of 28 GHz microwave power is applied. The <span class="hlt">electron</span> density and temperature profiles are measured using a Thomson scattering (TS) diagnostic, and indicate that the <span class="hlt">electron</span> density is centrally peaked. In the core of the plasma column, the <span class="hlt">electron</span> density is higher than the cut-off density (˜0.9 × 1019 m-3) for the launched mixture of X- and O-mode <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> waves to propagate. TS measurements indicate <span class="hlt">electron</span> temperature increases from ˜5 eV to ˜20 eV during 28 GHz power application when the neutral deuterium pressure is reduced below 0.13 Pa (˜1 mTorr.).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008RScI...79jF125W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008RScI...79jF125W"><span><span class="hlt">High</span> <span class="hlt">heat</span> <span class="hlt">flux</span> Langmuir probe array for the DIII-D divertor platesa)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Watkins, J. G.; Taussig, D.; Boivin, R. L.; Mahdavi, M. A.; Nygren, R. E.</p> <p>2008-10-01</p> <p>Two modular arrays of Langmuir probes designed to handle a <span class="hlt">heat</span> <span class="hlt">flux</span> of up to 25 MW/m2 for 10 s exposures have been installed in the lower divertor target plates of the DIII-D tokamak. The 20 pyrolytic graphite probe tips have more than three times higher thermal conductivity and 16 times larger mass than the original DIII-D isotropic graphite probes. The probe tips have a fixed 12.5° surface angle to distribute the <span class="hlt">heat</span> <span class="hlt">flux</span> more uniformly than the previous 6 mm diameter domed collectors and a symmetric "rooftop" design to allow operation with reversed toroidal magnetic field. A large spring-loaded contact area improves <span class="hlt">heat</span> conduction from each probe tip through a ceramic insulator into a cooled graphite divertor floor tile. The probe tips, brazed to molybdenum foil to ensure good electrical contact, are mounted in a ceramic tray for electrical isolation and reliable cable connections. The new probes are located 1.5 cm radially apart in a staggered arrangement near the entrance to the lower divertor pumping baffle and are linearly spaced 3 cm apart on the shelf above the in-vessel cryopump. Typical target plate profiles of Jsat, Te, and Vf with 4 mm spatial resolution are shown.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016HMT....52.1541L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016HMT....52.1541L"><span>A thermosyphon <span class="hlt">heat</span> pipe cooler for <span class="hlt">high</span> power LEDs cooling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Ji; Tian, Wenkai; Lv, Lucang</p> <p>2016-08-01</p> <p>Light emitting diode (LED) cooling is facing the challenge of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> more seriously with the increase of input power and diode density. The proposed unique thermosyphon <span class="hlt">heat</span> pipe <span class="hlt">heat</span> sink is particularly suitable for cooling of <span class="hlt">high</span> power density LED chips and other <span class="hlt">electronics</span>, which has a <span class="hlt">heat</span> dissipation potential of up to 280 W within an area of 20 mm × 22 mm (>60 W/cm2) under natural air convection. Meanwhile, a thorough visualization investigation was carried out to explore the two phase flow characteristics in the proposed thermosyphon <span class="hlt">heat</span> pipe. Implementing this novel thermosyphon <span class="hlt">heat</span> pipe <span class="hlt">heat</span> sink in the cooling of a commercial 100 W LED integrated chip, a very low apparent thermal resistance of 0.34 K/W was obtained under natural air convection with the aid of the enhanced boiling <span class="hlt">heat</span> transfer at the evaporation side and the enhanced natural air convection at the condensation side.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000APS..DPPGI3005S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000APS..DPPGI3005S"><span>A Non Local <span class="hlt">Electron</span> <span class="hlt">Heat</span> Transport Model for Multi-Dimensional Fluid Codes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schurtz, Guy</p> <p>2000-10-01</p> <p>Apparent inhibition of thermal <span class="hlt">heat</span> flow is one of the most ancient problems in computational Inertial Fusion and <span class="hlt">flux</span>-limited Spitzer-Harm conduction has been a mainstay in multi-dimensional hydrodynamic codes for more than 25 years. Theoretical investigation of the problem indicates that <span class="hlt">heat</span> transport in laser produced plasmas has to be considered as a non local process. Various authors contributed to the non local theory and proposed convolution formulas designed for practical implementation in one-dimensional fluid codes. Though the theory, confirmed by kinetic calculations, actually predicts a reduced <span class="hlt">heat</span> <span class="hlt">flux</span>, it fails to explain the very small limiters required in two-dimensional simulations. Fokker-Planck simulations by Epperlein, Rickard and Bell [PRL 61, 2453 (1988)] demonstrated that non local effects could lead to a strong reduction of <span class="hlt">heat</span> flow in two dimensions, even in situations where a one-dimensional analysis suggests that the <span class="hlt">heat</span> flow is nearly classical. We developed at CEA/DAM a non local <span class="hlt">electron</span> <span class="hlt">heat</span> transport model suitable for implementation in our two-dimensional radiation hydrodynamic code FCI2. This model may be envisionned as the first step of an iterative solution of the Fokker-Planck equations; it takes the mathematical form of multigroup diffusion equations, the solution of which yields both the <span class="hlt">heat</span> <span class="hlt">flux</span> and the departure of the <span class="hlt">electron</span> distribution function to the Maxwellian. Although direct implementation of the model is straightforward, formal solutions of it can be expressed in convolution form, exhibiting a three-dimensional tensor propagator. Reduction to one dimension retrieves the original formula of Luciani, Mora and Virmont [PRL 51, 1664 (1983)]. Intense magnetic fields may be generated by thermal effects in laser targets; these fields, as well as non local effects, will inhibit <span class="hlt">electron</span> conduction. We present simulations where both effects are taken into account and shortly discuss the coupling strategy between them.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvE..97b2122S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvE..97b2122S"><span>Hyperbolic <span class="hlt">heat</span> conduction, effective temperature, and third law for nonequilibrium systems with <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sobolev, S. L.</p> <p>2018-02-01</p> <p>Some analogies between different nonequilibrium <span class="hlt">heat</span> conduction models, particularly random walk, the discrete variable model, and the Boltzmann transport equation with the single relaxation time approximation, have been discussed. We show that, under an assumption of a finite value of the <span class="hlt">heat</span> carrier velocity, these models lead to the hyperbolic <span class="hlt">heat</span> conduction equation and the modified Fourier law with relaxation term. Corresponding effective temperature and entropy have been introduced and analyzed. It has been demonstrated that the effective temperature, defined as a geometric mean of the kinetic temperatures of the <span class="hlt">heat</span> carriers moving in opposite directions, acts as a criterion for thermalization and is a nonlinear function of the kinetic temperature and <span class="hlt">heat</span> <span class="hlt">flux</span>. It is shown that, under <span class="hlt">highly</span> nonequilibrium conditions when the <span class="hlt">heat</span> <span class="hlt">flux</span> tends to its maximum possible value, the effective temperature, <span class="hlt">heat</span> capacity, and local entropy go to zero even at a nonzero equilibrium temperature. This provides a possible generalization of the third law to nonequilibrium situations. Analogies and differences between the proposed effective temperature and some other definitions of a temperature in nonequilibrium state, particularly for active systems, disordered semiconductors under electric field, and adiabatic gas flow, have been shown and discussed. Illustrative examples of the behavior of the effective temperature and entropy during nonequilibrium <span class="hlt">heat</span> conduction in a monatomic gas and a strong shockwave have been analyzed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/111419','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/111419"><span>A comparison of critical <span class="hlt">heat</span> <span class="hlt">flux</span> in tubes and bilaterally <span class="hlt">heated</span> annuli</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Doerffer, S.; Groeneveld, D.C.; Cheng, S.C.</p> <p>1995-09-01</p> <p>This paper examines the critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) behaviour for annular flow in bilaterally <span class="hlt">heated</span> annuli and compares it to that in tubes and unilaterally <span class="hlt">heated</span> annuli. It was found that the differences in CHF between bilaterally and unilaterally <span class="hlt">heated</span> annuli or tubes strongly depend on pressure and quality. the CHF in bilaterally <span class="hlt">heated</span> annuli can be predicted by tube CHF prediction methods for the simultaneous CHF occurrence at both surfaces, and the following flow conditions: pressure 7-10 MPa, mass <span class="hlt">flux</span> 0.5-4.0 Mg/m{sup 2}s and critical quality 0.23-0.9. The effect on CHF of the outer-to-inner surface <span class="hlt">heat</span> <span class="hlt">flux</span> ratio, wasmore » also examined. The prediction of CHF for bilaterally <span class="hlt">heated</span> annuli was based on the droplet-diffusion model proposed by Kirillov and Smogalev. While their model refers only to CHF occurrence at the inner surface, we extended it to cases where CHF occurs at the outer surface, and simultaneously at both surfaces, thus covering all cases of CHF occurrence in bilaterally <span class="hlt">heated</span> annuli. From the annuli CHF data of Becker and Letzter, we derived empirical functions required by the model. the proposed equations provide good accuracy for the CHF data used in this study. Moreover, the equations can predict conditions at which CHF occurs simultaneously at both surfaces. Also, this method can be used for cases with only one <span class="hlt">heated</span> surface.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhLA..381.3621L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhLA..381.3621L"><span>Size effects in non-linear <span class="hlt">heat</span> conduction with <span class="hlt">flux</span>-limited behaviors</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Shu-Nan; Cao, Bing-Yang</p> <p>2017-11-01</p> <p>Size effects are discussed for several non-linear <span class="hlt">heat</span> conduction models with <span class="hlt">flux</span>-limited behaviors, including the phonon hydrodynamic, Lagrange multiplier, hierarchy moment, nonlinear phonon hydrodynamic, tempered diffusion, thermon gas and generalized nonlinear models. For the phonon hydrodynamic, Lagrange multiplier and tempered diffusion models, <span class="hlt">heat</span> <span class="hlt">flux</span> will not exist in problems with sufficiently small scale. The existence of <span class="hlt">heat</span> <span class="hlt">flux</span> needs the sizes of <span class="hlt">heat</span> conduction larger than their corresponding critical sizes, which are determined by the physical properties and boundary temperatures. The critical sizes can be regarded as the theoretical limits of the applicable ranges for these non-linear <span class="hlt">heat</span> conduction models with <span class="hlt">flux</span>-limited behaviors. For sufficiently small scale <span class="hlt">heat</span> conduction, the phonon hydrodynamic and Lagrange multiplier models can also predict the theoretical possibility of violating the second law and multiplicity. Comparisons are also made between these non-Fourier models and non-linear Fourier <span class="hlt">heat</span> conduction in the type of fast diffusion, which can also predict <span class="hlt">flux</span>-limited behaviors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013IJTP...52.3598A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013IJTP...52.3598A"><span>Gravitational Collapse with <span class="hlt">Heat</span> <span class="hlt">Flux</span> and Gravitational Waves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ahmad, Zahid; Ahmed, Qazi Zahoor; Awan, Abdul Sami</p> <p>2013-10-01</p> <p>In this paper, we investigated the cylindrical gravitational collapse with <span class="hlt">heat</span> <span class="hlt">flux</span> by considering the appropriate geometry of the interior and exterior spacetimes. For this purpose, we matched collapsing fluid to an exterior containing gravitational waves.The effects of <span class="hlt">heat</span> <span class="hlt">flux</span> on gravitational collapse are investigated and matched with the results obtained by Herrera and Santos (Class. Quantum Gravity 22:2407, 2005).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20050203797&hterms=temperature+dog&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dtemperature%2Bdog','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20050203797&hterms=temperature+dog&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dtemperature%2Bdog"><span>Microsample Characterization of Coatings for GRCop-84 for <span class="hlt">High</span> Temperature <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Application</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jain, Piyush; Hemker, Kevin J.; Raj, Sai V.</p> <p>2004-01-01</p> <p>NASA's Glenn Research Center has developed GRCop-84 (Cu-8at.%Cr-4% Nb), a <span class="hlt">high</span> conductivity, <span class="hlt">high</span> strength copper alloy for use as liners in rocket engine combustion chambers, nozzle ramps and other actively-cooled components subject to <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Two metallic coatings, NiCrAlY and Cu-26%Cr, are being considered for preventing blanching, reducing 'dog- house' failures and providing better environmental resistance to the GRCop-84 liners. This presentation will outline a study of coating-substrate interactions that occur as a result of thermal cycling and coating specific properties at different temperatures. A furnace has been built to thermally cycle the samples under argon. The microsample testing approach is being used to measure the coating-substrate interfacial strength. Cu-26Cr/GRCop-84 samples did not show any obvious interdiffusion after 300 thermal cycles. Interfacial strength tests of these samples were affected by porosity present in the samples. A complete set of observations and results for Cu-26Cr and NiCrAlY coatings will be presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013JNuM..433..523Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013JNuM..433..523Y"><span>Recrystallization and grain growth behavior of rolled tungsten under VDE-like short pulse <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> loads</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yuan, Y.; Greuner, H.; Böswirth, B.; Krieger, K.; Luo, G.-N.; Xu, H. Y.; Fu, B. Q.; Li, M.; Liu, W.</p> <p>2013-02-01</p> <p>Short pulse <span class="hlt">heat</span> loads expected for vertical displacement events (VDEs) in ITER were applied in the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> (HHF) test facility GLADIS at IPP-Garching onto samples of rolled W. Pulsed neutral beams with the central <span class="hlt">heat</span> <span class="hlt">flux</span> of 23 MW/m2 were applied for 0.5, 1.0 and 1.5 s, respectively. Rapid recrystallization of the adiabatically loaded 3 mm thick samples was observed when the pulse duration was up to 1.0 s. Grains grew markedly following recrystallization with increasing pulse length. The recrystallization temperature and temperature dependence of the recrystallized grain size were also investigated. The results showed that the recrystallization temperature of the W grade was around 2480 °C under the applied <span class="hlt">heat</span> loading condition, which was nearly 1150 °C higher than the conventional recrystallization temperature, and the grains were much finer. A linear relationship between the logarithm of average grain size (ln d) and the inverse of maximum surface temperature (1/Tmax) was found and accordingly the activation energy for grain growth in temperature evolution up to Tmax in 1.5 s of the short pulse HHF load was deduced to be 4.1 eV. This provided an effective clue to predict the structure evolution under short pulse HHF loads.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013BoLMe.147..569A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013BoLMe.147..569A"><span>Improvements in Sensible <span class="hlt">Heat-Flux</span> Parametrization in the <span class="hlt">High</span>-Resolution Regional Model (HRM) Through the Modified Treatment of the Roughness Length for <span class="hlt">Heat</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Anurose, T. J.; Subrahamanyam, D. Bala</p> <p>2013-06-01</p> <p>We discuss the impact of the differential treatment of the roughness lengths for momentum and <span class="hlt">heat</span> (z_{0m} and z_{0h}) in the <span class="hlt">flux</span> parametrization scheme of the <span class="hlt">high</span>-resolution regional model (HRM) for a heterogeneous terrain centred around Thiruvananthapuram, India (8.5°N, 76.9°E). The magnitudes of sensible <span class="hlt">heat</span> <span class="hlt">flux</span> ( H) obtained from HRM simulations using the original parametrization scheme differed drastically from the concurrent in situ observations. With a view to improving the performance of this parametrization scheme, two distinct modifications are incorporated: (1) In the first method, a constant value of 100 is assigned to the z_{0m}/z_{0h} ratio; (2) and in the second approach, this ratio is treated as a function of time. Both these modifications in the HRM model showed significant improvements in the H simulations for Thiruvananthapuram and its adjoining regions. Results obtained from the present study provide a first-ever comparison of H simulations using the modified parametrization scheme in the HRM model with in situ observations for the Indian coastal region, and suggest a differential treatment of z_{0m} and z_{0h} in the <span class="hlt">flux</span> parametrization scheme.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_13 --> <div id="page_14" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="261"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGP41A0954M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGP41A0954M"><span>New geothermal <span class="hlt">heat</span> <span class="hlt">flux</span> map of Greenland and the Iceland hotspot track</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Martos, Y. M.; Jordan, T. A.; Catalan, M.; Jordan, T. M.; Bamber, J. L.; Vaughan, D. G.</p> <p>2017-12-01</p> <p>Greenland is the second largest reservoir of water on Earth and about 80% of its surface is covered by ice. It is mainly composed of Archean blocks that collided during the Early Proterozoic. Indirect methods have been used to study its subglacial thermal conditions, geology and lithospheric structure. Numerous regions of basal melting are identified in the central and north Greenland but their relationship with geothermal <span class="hlt">heat</span> <span class="hlt">flux</span> is not yet clear. Crustal thickness derived by seismology and gravity data are consistent, showing no significant lateral variations, and providing average values of about 40 and 36 km respectively. Even though Greenland is considered a craton its crust has been affected by the presume passage of the Iceland hotspot since at least 100 Ma. Here we present the newest and highest resolution Curie Depth and geothermal <span class="hlt">heat</span> <span class="hlt">flux</span> maps for Greenland as well as their associated uncertainties. For estimating the Curie Depths we applied spectral methods to aeromagnetic data from the World Digital Magnetic Anomaly Map WDMAM2.0. Calculated Curie Depths vary from 25 to 50 km with shallower values located to the east. A thermal model is built based on the 1D <span class="hlt">heat</span> conduction equation and considering steady state conditions. The thermal parameters are then optimized using local values derived from direct measurements, temperature profiles and more indirect methods such as radar imaging. The <span class="hlt">heat</span> <span class="hlt">flux</span> distribution shows higher spatial variability and a very different pattern than previously proposed and with values of 50-80 mW/m2. We identify a NW-SE <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> feature crossing Greenland which we correlate with the Iceland hotspot track. Additionally, to evaluate the lithospheric structure we calculate the Bouguer anomaly from GOCO5s satellite free air data and construct several gravity models across the proposed hotspot track. We show that a dense lower crust body in the same location the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> trend is permissible from a gravimetric</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1914314B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1914314B"><span>The forgotten component of sub-glacial <span class="hlt">heat</span> flow: Upper crustal <span class="hlt">heat</span> production and resultant total <span class="hlt">heat</span> <span class="hlt">flux</span> on the Antarctic Peninsula</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Burton-Johnson, Alex; Halpin, Jacqueline; Whittaker, Joanne; Watson, Sally</p> <p>2017-04-01</p> <p>Seismic and magnetic geophysical methods have both been employed to produce estimates of <span class="hlt">heat</span> <span class="hlt">flux</span> beneath the Antarctic ice sheet. However, both methods use a homogeneous upper crustal model despite the variable concentration of <span class="hlt">heat</span> producing elements within its composite lithologies. Using geological and geochemical datasets from the Antarctic Peninsula we have developed a new methodology for incorporating upper crustal <span class="hlt">heat</span> production in <span class="hlt">heat</span> <span class="hlt">flux</span> models and have shown the greater variability this introduces in to estimates of crustal <span class="hlt">heat</span> <span class="hlt">flux</span>, with implications for glaciological modelling.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/10163684','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/10163684"><span>US-Japan workshop Q-181 on <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> components and plasma-surface interactions for next devices: Proceedings</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>McGrath, R.T.; Yamashina, T.</p> <p></p> <p>This report contain viewgraphs of papers from the following sessions: plasma facing components issues for future machines; recent PMI results from several tokamaks; <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> technology; plasma facing components design and applications; plasma facing component materials and irradiation damage; boundary layer plasma; plasma disruptions; conditioning and tritium; and erosion/redeposition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JChPh.147x1101A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JChPh.147x1101A"><span>Communication: On the calculation of time-dependent <span class="hlt">electron</span> <span class="hlt">flux</span> within the Born-Oppenheimer approximation: A <span class="hlt">flux-flux</span> reflection principle</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Albert, Julian; Hader, Kilian; Engel, Volker</p> <p>2017-12-01</p> <p>It is commonly assumed that the time-dependent <span class="hlt">electron</span> <span class="hlt">flux</span> calculated within the Born-Oppenheimer (BO) approximation vanishes. This is not necessarily true if the <span class="hlt">flux</span> is directly determined from the continuity equation obeyed by the <span class="hlt">electron</span> density. This finding is illustrated for a one-dimensional model of coupled <span class="hlt">electronic</span>-nuclear dynamics. There, the BO <span class="hlt">flux</span> is in perfect agreement with the one calculated from a solution of the time-dependent Schrödinger equation for the coupled motion. A reflection principle is derived where the nuclear BO <span class="hlt">flux</span> is mapped onto the <span class="hlt">electronic</span> <span class="hlt">flux</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMOS22B..05M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMOS22B..05M"><span>Atmospheric responses to sensible and latent <span class="hlt">heating</span> <span class="hlt">fluxes</span> over the Gulf Stream</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Minobe, S.; Ida, T.; Takatama, K.</p> <p>2016-12-01</p> <p>Air-sea interaction over mid-latitude oceanic fronts such as the Gulf Stream attracted large attention in the last decade. Observational analyses and modelling studies revealed that atmospheric responses over the Gulf Stream including surface wind convergence, enhanced precipitation and updraft penetrating to middle-to-upper troposphere roughly on the Gulf Stream current axis or on the warmer flank of sea-surface temperature (SST) front of the Gulf Stream . For these atmospheric responses, oceanic information should be transmitted to the atmosphere via turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span>, and thus the mechanisms for atmospheric responses can be understood better by examining latent and sensible air-sea <span class="hlt">heat</span> <span class="hlt">fluxes</span> more closely. Thus, the roles of the sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> are examined by conducting a series of numerical experiments using the IPRC Regional Atmospheric Model over the Gulf Stream by applying SST smoothing for latent and sensible <span class="hlt">heating</span> separately. The results indicate that the sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> affect the atmosphere differently. Sensible <span class="hlt">heat</span> <span class="hlt">flux</span> intensifies surface wind convergence to produce sea-level pressure (SLP) anomaly. Latent <span class="hlt">heat</span> <span class="hlt">flux</span> supplies moistures and maintains enhanced precipitation. The different <span class="hlt">heat</span> <span class="hlt">flux</span> components cause upward wind velocity at different levels.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPJ11115S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPJ11115S"><span>Observation of <span class="hlt">Electron</span> Bernstein Wave <span class="hlt">Heating</span> in the RFP</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Seltzman, Andrew; Anderson, Jay; Goetz, John; Forest, Cary</p> <p>2017-10-01</p> <p>The first observation of RF <span class="hlt">heating</span> in a reversed field pinch (RFP) using the <span class="hlt">electron</span> Bernstein wave (EBW) has been demonstrated on MST. Efficient mode conversion of an outboard-launched X mode wave at 5.5 GHz leads to Doppler-shifted resonant absorption (ωrf = nωce-k||v||) for a broad range (n =1-7) of harmonics. The dynamics of EBW-<span class="hlt">heated</span> <span class="hlt">electrons</span> are measured using a spatial distribution of solid targets with diametrically opposed x-ray detectors. EBW <span class="hlt">heating</span> produces a clear supra-thermal <span class="hlt">electron</span> tail in MST. Radial deposition of the EBW is controlled with |B|and is measured using the HXR <span class="hlt">flux</span> emitted from an insertable probe. In the thick-shelled MST RFP, the radial accessibility of EBW is limited to r/a >0.8 ( 10cm) by magnetic field error induced by the porthole necessary for the antenna. Experimental measurements show EBW propagation inward through a stochastic magnetic field. EBW-<span class="hlt">heated</span> test <span class="hlt">electrons</span> are used as a direct probe of edge (r/a >0.9) radial transport, showing a modest transition from `standard' to reduced-tearing RFP operation. <span class="hlt">Electron</span> loss is too fast for collisional effects and implies a large non-collisional radial diffusivity. EBW <span class="hlt">heating</span> has been demonstrated in reduced magnetic stochasticity plasmas with β = 15-20%. Work supported by USDOE.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/111415','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/111415"><span>A formal approach for the prediction of the critical <span class="hlt">heat</span> <span class="hlt">flux</span> in subcooled water</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Lombardi, C.</p> <p>1995-09-01</p> <p>The critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) in subcooled water at <span class="hlt">high</span> mass <span class="hlt">fluxes</span> are not yet satisfactory correlated. For this scope a formal approach is here followed, which is based on an extension of the parameters and the correlation used for the dryout prediction for medium <span class="hlt">high</span> quality mixtures. The obtained correlation, in spite of its simplicity and its explicit form, yields satisfactory predictions, also when applied to more conventional CHF data at low-medium mass <span class="hlt">fluxes</span> and <span class="hlt">high</span> pressures. Further improvements are possible, if a more complete data bank will be available. The main and general open item is the definitionmore » of a criterion, depending only on independent parameters, such as mass <span class="hlt">flux</span>, pressure, inlet subcooling and geometry, to predict whether the <span class="hlt">heat</span> transfer crisis will result as a DNB or a dryout phenomenon.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1432047-multi-scale-transport-diii-iter-baseline-scenario-direct-electron-heating-projection-iter','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1432047-multi-scale-transport-diii-iter-baseline-scenario-direct-electron-heating-projection-iter"><span>Multi-scale transport in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span> and projection to ITER</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Grierson, B. A.; Staebler, G. M.; Solomon, W. M.</p> <p></p> <p>Multi-scale fluctuations measured by turbulence diagnostics spanning long and short wavelength spatial scales impact energy confinement and the scale-lengths of plasma kinetic profiles in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span>. Contrasting discharge phases with ECH + neutral beam injection (NBI) and NBI only at similar rotation reveal higher energy confinement and lower fluctuations when only NBI <span class="hlt">heating</span> is used. Modeling of the core transport with TGYRO using the TGLF turbulent transport model and NEO neoclassical transport reproduces the experimental profile changes upon application of direct <span class="hlt">electron</span> <span class="hlt">heating</span> and indicates that multi-scale transport mechanisms are responsible for changesmore » in the temperature and density profiles. Intermediate and <span class="hlt">high</span>-k fluctuations appear responsible for the enhanced <span class="hlt">electron</span> thermal <span class="hlt">flux</span>, and intermediate-k <span class="hlt">electron</span> modes produce an inward particle pinch that increases the inverse density scale length. Projection to ITER is performed with TGLF and indicates a density profile that has a finite scale length due to intermediate-k <span class="hlt">electron</span> modes at low collisionality and increases the fusion gain. Finally, for a range of E×B shear, the dominant mechanism that increases fusion performance is suppression of outward low-k particle <span class="hlt">flux</span> and increased density peaking.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1432047-multi-scale-transport-diii-iter-baseline-scenario-direct-electron-heating-projection-iter','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1432047-multi-scale-transport-diii-iter-baseline-scenario-direct-electron-heating-projection-iter"><span>Multi-scale transport in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span> and projection to ITER</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Grierson, B. A.; Staebler, G. M.; Solomon, W. M.; ...</p> <p>2018-02-01</p> <p>Multi-scale fluctuations measured by turbulence diagnostics spanning long and short wavelength spatial scales impact energy confinement and the scale-lengths of plasma kinetic profiles in the DIII-D ITER baseline scenario with direct <span class="hlt">electron</span> <span class="hlt">heating</span>. Contrasting discharge phases with ECH + neutral beam injection (NBI) and NBI only at similar rotation reveal higher energy confinement and lower fluctuations when only NBI <span class="hlt">heating</span> is used. Modeling of the core transport with TGYRO using the TGLF turbulent transport model and NEO neoclassical transport reproduces the experimental profile changes upon application of direct <span class="hlt">electron</span> <span class="hlt">heating</span> and indicates that multi-scale transport mechanisms are responsible for changesmore » in the temperature and density profiles. Intermediate and <span class="hlt">high</span>-k fluctuations appear responsible for the enhanced <span class="hlt">electron</span> thermal <span class="hlt">flux</span>, and intermediate-k <span class="hlt">electron</span> modes produce an inward particle pinch that increases the inverse density scale length. Projection to ITER is performed with TGLF and indicates a density profile that has a finite scale length due to intermediate-k <span class="hlt">electron</span> modes at low collisionality and increases the fusion gain. Finally, for a range of E×B shear, the dominant mechanism that increases fusion performance is suppression of outward low-k particle <span class="hlt">flux</span> and increased density peaking.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AAS...23221713M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AAS...23221713M"><span>X-ray <span class="hlt">Heating</span> and <span class="hlt">Electron</span> Temperature of Laboratory Photoionized Plasmas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mancini, Roberto; Lockard, Tom; Mayes, Daniel C.; Loisel, Guillaume; Bailey, James E.; Rochau, Gregory; Abdallah, J.; Golovkin, I.</p> <p>2018-06-01</p> <p>In separate experiments performed at the Z facility of Sandia National Laboratories two different samples were employed to produce and characterize photoionized plasmas. One was a gas cell filled with neon, and the other was a thin silicon layer coated with plastic. Both samples were driven by the broadband x-ray <span class="hlt">flux</span> produced at the collapse of a wire array z-pinch implosion. Transmission spectroscopy of a narrowband portion of the x-ray <span class="hlt">flux</span> was used to diagnose the charge state distribution, and the <span class="hlt">electron</span> temperature was extracted from a Li-like ion level population ratio. To interpret the temperature measurement, we performed Boltzmann kinetics and radiation-hydrodynamic simulations. We found that non-equilibrium atomic physics and the coupling of the radiation <span class="hlt">flux</span> to the atomic level population kinetics play a critical role in modeling the x-ray <span class="hlt">heating</span> of photoionized plasmas. In spite of being driven by similar x-ray drives, differences of ionization and charged state distributions in the neon and silicon plasmas are reflected in the plasma <span class="hlt">heating</span> and observed <span class="hlt">electron</span> temperatures.This work was sponsored in part by DOE Office of Science Grant DE-SC0014451, and the Z Facility Fundamental Science Program of SNL.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/864118','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/864118"><span>Method and apparatus for determining vertical <span class="hlt">heat</span> <span class="hlt">flux</span> of geothermal field</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Poppendiek, Heinz F.</p> <p>1982-01-01</p> <p>A method and apparatus for determining vertical <span class="hlt">heat</span> <span class="hlt">flux</span> of a geothermal field, and mapping the entire field, is based upon an elongated <span class="hlt">heat-flux</span> transducer (10) comprised of a length of tubing (12) of relatively low thermal conductivity with a thermopile (20) inside for measuring the thermal gradient between the ends of the transducer after it has been positioned in a borehole for a period sufficient for the tube to reach thermal equilibrium. The transducer is thermally coupled to the surrounding earth by a fluid annulus, preferably water or mud. A second transducer comprised of a length of tubing of relatively <span class="hlt">high</span> thermal conductivity is used for a second thermal gradient measurement. The ratio of the first measurement to the second is then used to determine the earth's thermal conductivity, k.sub..infin., from a precalculated graph, and using the value of thermal conductivity thus determined, then determining the vertical earth temperature gradient, b, from predetermined steady state <span class="hlt">heat</span> balance equations which relate the undisturbed vertical earth temperature distributions at some distance from the borehole and earth thermal conductivity to the temperature gradients in the transducers and their thermal conductivity. The product of the earth's thermal conductivity, k.sub..infin., and the earth's undisturbed vertical temperature gradient, b, then determines the earth's vertical <span class="hlt">heat</span> <span class="hlt">flux</span>. The process can be repeated many times for boreholes of a geothermal field to map vertical <span class="hlt">heat</span> <span class="hlt">flux</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100015631','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100015631"><span>Thin Film <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensor Development for Ceramic Matrix Composite (CMC) Systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wrbanek, John D.; Fralick, Gustave C.; Hunter, Gary W.; Zhu, Dongming; Laster, Kimala L.; Gonzalez, Jose M.; Gregory, Otto J.</p> <p>2010-01-01</p> <p>The NASA Glenn Research Center (GRC) has an on-going effort for developing <span class="hlt">high</span> temperature thin film sensors for advanced turbine engine components. Stable, <span class="hlt">high</span> temperature thin film ceramic thermocouples have been demonstrated in the lab, and novel methods of fabricating sensors have been developed. To fabricate thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensors for Ceramic Matrix Composite (CMC) systems, the rough and porous nature of the CMC system posed a significant challenge for patterning the fine features required. The status of the effort to develop thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensors specifically for use on silicon carbide (SiC) CMC systems with these new technologies is described.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920075515&hterms=Supercritical+fluid&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3DSupercritical%2Bfluid','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920075515&hterms=Supercritical+fluid&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3DSupercritical%2Bfluid"><span><span class="hlt">Electron</span> <span class="hlt">heating</span> in a Monte Carlo model of a <span class="hlt">high</span> Mach number, supercritical, collisionless shock</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ellison, Donald C.; Jones, Frank C.</p> <p>1987-01-01</p> <p>Preliminary work in the investigation of <span class="hlt">electron</span> injection and acceleration at parallel shocks is presented. A simple model of <span class="hlt">electron</span> <span class="hlt">heating</span> that is derived from a unified shock model which includes the effects of an electrostatic potential jump is described. The unified shock model provides a kinetic description of the injection and acceleration of ions and a fluid description of <span class="hlt">electron</span> <span class="hlt">heating</span> at <span class="hlt">high</span> Mach number, supercritical, and parallel shocks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/20770232-investigation-saturated-critical-heat-flux-single-uniformly-heated-microchannel','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/20770232-investigation-saturated-critical-heat-flux-single-uniformly-heated-microchannel"><span>Investigation of saturated critical <span class="hlt">heat</span> <span class="hlt">flux</span> in a single, uniformly <span class="hlt">heated</span> microchannel</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Wojtan, Leszek; Revellin, Remi; Thome, John R.</p> <p>2006-08-15</p> <p>A series of tests have been performed to determine the saturated critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) in 0.5 and 0.8mm internal diameter microchannel tubes as a function of refrigerant mass velocity, <span class="hlt">heated</span> length, saturation temperature and inlet liquid subcooling. The tested refrigerants were R-134a and R-245fa and the <span class="hlt">heated</span> length of microchannel was varied between 20 and 70mm. The results show a strong dependence of CHF on mass velocity, <span class="hlt">heated</span> length and microchannel diameter but no influence of liquid subcooling (2-15{sup o}C) was observed. The experimental results have been compared to the well-known CHF single-channel correlation of Y. Katto and H.more » Ohno [An improved version of the generalized correlation of critical <span class="hlt">heat</span> <span class="hlt">flux</span> for the forced convective boiling in uniformly <span class="hlt">heated</span> vertical tubes, Int. J. <span class="hlt">Heat</span> and Mass Transfer 27 (9) (1984) 1641-1648] and the multichannel correlation of W. Qu and I. Mudawar [Measurement and correlation of critical <span class="hlt">heat</span> <span class="hlt">flux</span> in two-phase microchannel <span class="hlt">heat</span> sinks, Int. J. <span class="hlt">Heat</span> and Mass Transfer 47 (2004) 2045-2059]. The comparison shows that the correlation of Katto-Ohno predicts microchannel data with a mean absolute error of 32.8% with only 41.2% of the data falling within a +/-15% error band. The correlation of Qu and Mudawar shows the same trends as the CHF data but significantly overpredicts them. Based on the present experimental data, a new microscale version of the Katto-Ohno correlation for the prediction of CHF during saturated boiling in microchannels has been proposed. (author)« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MeScT..28b5901L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MeScT..28b5901L"><span>Infrared thermography with non-uniform <span class="hlt">heat</span> <span class="hlt">flux</span> boundary conditions on the rotor endwall of an axial turbine</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lazzi Gazzini, S.; Schädler, R.; Kalfas, A. I.; Abhari, R. S.</p> <p>2017-02-01</p> <p>It is technically challenging to measure <span class="hlt">heat</span> <span class="hlt">fluxes</span> on the rotating components of gas turbines, yet accurate knowledge of local <span class="hlt">heat</span> loads under engine-representative conditions is crucial for ensuring the reliability of the designs. In this work, quantitative image processing tools were developed to perform fast and accurate infrared thermography measurements on 3D-shaped film-heaters directly deposited on the turbine endwalls. The newly developed image processing method and instrumentation were used to measure the <span class="hlt">heat</span> load on the rotor endwalls of an axial turbine. A step-transient <span class="hlt">heat</span> <span class="hlt">flux</span> calibration technique is applied to measure the <span class="hlt">heat</span> <span class="hlt">flux</span> generated locally by the film heater, thus eliminating the need for a rigorously iso-energetic boundary condition. On-board <span class="hlt">electronics</span> installed on the rotor record the temperature readings of RTDs installed in the substrate below the heaters in order to evaluate the conductive losses in the solid. Full maps of <span class="hlt">heat</span> transfer coefficient and adiabatic wall temperature are produced for two different operating conditions, demonstrating the sensitivity of the technique to local flow features and variations in <span class="hlt">heat</span> transfer due to Reynolds number effect.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFM.A33M..04H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFM.A33M..04H"><span>An Analysis of Inter-annual Variability and Uncertainty of Continental Surface <span class="hlt">Heat</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huang, S. Y.; Deng, Y.; Wang, J.</p> <p>2016-12-01</p> <p>The inter-annual variability and the corresponding uncertainty of land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> during the first decade of the 21st century are re-evaluated at continental scale based on the <span class="hlt">heat</span> <span class="hlt">fluxes</span> estimated by the maximum entropy production (MEP) model. The MEP model predicted <span class="hlt">heat</span> <span class="hlt">fluxes</span> are constrained by surface radiation <span class="hlt">fluxes</span>, automatically satisfy surface energy balance, and are independent of temperature/moisture gradient, wind speed, and roughness lengths. The surface radiation <span class="hlt">fluxes</span> and temperature data from Clouds and the Earth's Radiant Energy System and the surface specific humidity data from Modern-Era Retrospective analysis for Research and Applications were used to reproduce the global surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> with land-cover data from the NASA Energy and Water cycle Study (NEWS). Our analysis shows that the annual means of continental latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> have increasing trends associated with increasing trends in surface net radiative <span class="hlt">fluxes</span>. The sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> also have increasing trends over most continents except for South America. Ground <span class="hlt">heat</span> <span class="hlt">fluxes</span> have little trends. The continental-scale analysis of the MEP <span class="hlt">fluxes</span> are compared with other existing global surface <span class="hlt">fluxes</span> data products and the implications of the results for inter-annual to decadal variability of regional surface energy budget are discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.H54C..03L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.H54C..03L"><span>Mapping surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> by assimilating GOES land surface temperature and SMAP products</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lu, Y.; Steele-Dunne, S. C.; Van De Giesen, N.</p> <p>2017-12-01</p> <p>Surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> significantly affect the land-atmosphere interaction, but their modelling is often hindered by the lack of in-situ measurements and the <span class="hlt">high</span> spatial heterogeneity. Here, we propose a hybrid particle assimilation strategy to estimate surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> by assimilating GOES land surface temperature (LST) data and SMAP products into a simple dual-source surface energy balance model, in which the requirement for in-situ data is minimized. The study aims to estimate two key parameters: a neutral bulk <span class="hlt">heat</span> transfer coefficient (CHN) and an evaporative fraction (EF). CHN scales the sum of surface energy <span class="hlt">fluxes</span>, and EF represents the partitioning between <span class="hlt">flux</span> components. To bridge the huge resolution gap between GOES and SMAP data, SMAP data are assimilated using a particle filter to update soil moisture which constrains EF, and GOES data are assimilated with an adaptive particle batch smoother to update CHN. The methodology is applied to an area in the US Southern Great Plains with forcing data from NLDAS-2 and the GPM mission. Assessment against in-situ observations suggests that the sensible and latent <span class="hlt">heat</span> <span class="hlt">flux</span> estimates are greatly improved at both daytime and 30-min scale after assimilation, particularly for latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Comparison against an LST-only assimilation case demonstrates that despite the coarse resolution, assimilating SMAP data is not only beneficial but also crucial for successful and robust <span class="hlt">flux</span> estimation, particularly when the modelling uncertainties are large. Since the methodology is independent on in-situ data, it can be easily applied to other areas.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMSM53A..06R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMSM53A..06R"><span><span class="hlt">High</span> Latitude Precipitating Energy <span class="hlt">Flux</span> and Joule <span class="hlt">Heating</span> During Geomagnetic Storms Determined from AMPERE Field-aligned Currents</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Robinson, R. M.; Zanetti, L. J.; Anderson, B. J.; Korth, H.; Samara, M.; Michell, R.; Grubbs, G. A., II; Hampton, D. L.; Dropulic, A.</p> <p>2016-12-01</p> <p>A <span class="hlt">high</span> latitude conductivity model based on field-aligned currents measured by the Active Magnetosphere and Planetary Electrodynamics Response Experiment (AMPERE) provides the means for complete specification of electric fields and currents at <span class="hlt">high</span> latitudes. Based on coordinated measurements made by AMPERE and the Poker Flat Incoherent Scatter Radar, the model determines the most likely value of the ionospheric conductance from the direction, magnitude, and magnetic local time of the field-aligned current. A conductance model driven by field-aligned currents ensures spatial and temporal consistency between the calculated electrodynamic parameters. To validate the results, the Pedersen and Hall conductances were used to calculate the energy <span class="hlt">flux</span> associated with the energetic particle precipitation. When integrated over the entire hemisphere, the total energy <span class="hlt">flux</span> compares well with the Hemispheric Power Index derived from the OVATION-PRIME model. The conductances were also combined with the field-aligned currents to calculate the self-consistent electric field, which was then used to compute horizontal currents and Joule <span class="hlt">heating</span>. The magnetic perturbations derived from the currents replicate most of the variations observed in ground-based magnetograms. The model was used to study <span class="hlt">high</span> latitude particle precipitation, currents, and Joule <span class="hlt">heating</span> for 24 magnetic storms. In most cases, the total energy input from precipitating particles and Joule <span class="hlt">heating</span> exhibits a sharply-peaked maximum at the times of local minima in Dst, suggesting a close coupling between the ring current and the <span class="hlt">high</span> latitude currents driven by the Region 2 field-aligned currents. The rapid increase and decrease of the <span class="hlt">high</span> latitude energy deposition suggests an explosive transfer of energy from the magnetosphere to the ionosphere just prior to storm recovery.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JNuM..463..198D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JNuM..463..198D"><span>Effect of <span class="hlt">high-flux</span> H/He plasma exposure on tungsten damage due to transient <span class="hlt">heat</span> loads</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>De Temmerman, G.; Morgan, T. W.; van Eden, G. G.; de Kruif, T.; Wirtz, M.; Matejicek, J.; Chraska, T.; Pitts, R. A.; Wright, G. M.</p> <p>2015-08-01</p> <p>The thermal shock behaviour of tungsten exposed to <span class="hlt">high-flux</span> plasma is studied using a <span class="hlt">high</span>-power laser. The cases of laser-only, sequential laser and hydrogen (H) plasma and simultaneous laser plus H plasma exposure are studied. H plasma exposure leads to an embrittlement of the material and the appearance of a crack network originating from the centre of the laser spot. Under simultaneous loading, significant surface melting is observed. In general, H plasma exposure lowers the <span class="hlt">heat</span> <span class="hlt">flux</span> parameter (FHF) for the onset of surface melting by ∼25%. In the case of He-modified (fuzzy) surfaces, strong surface deformations are observed already after 1000 laser pulses at moderate FHF = 19 MJ m-2 s-1/2, and a dense network of fine cracks is observed. These results indicate that <span class="hlt">high</span>-fluence ITER-like plasma exposure influences the thermal shock properties of tungsten, lowering the permissible transient energy density beyond which macroscopic surface modifications begin to occur.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1992ThApC..46...53B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1992ThApC..46...53B"><span>Tests of a robust eddy correlation system for sensible <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Blanford, J. H.; Gay, L. W.</p> <p>1992-03-01</p> <p>Sensible <span class="hlt">heat</span> <span class="hlt">flux</span> estimates from a simple, one-propeller eddy correlation system (OPEC) were compared with those from a sonic anemometer eddy correlation system (SEC). In accordance with similarity theory, the performance of the OPEC system improved with increasing height of the sensor above the surface. <span class="hlt">Flux</span> totals from the two systems at sites with adequate fetch were in excellent agreement after frequency response corrections were applied. The propeller system appears suitable for long periods of unattended measurement. The sensible <span class="hlt">heat</span> <span class="hlt">flux</span> measurements can be combined with net radiation and soil <span class="hlt">heat</span> <span class="hlt">flux</span> measurements to estimate latent <span class="hlt">heat</span> as a residual in the surface energy balance.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_14 --> <div id="page_15" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="281"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/863908','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/863908"><span>Device and method for <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span> density plasma</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Thode, Lester E.</p> <p>1981-01-01</p> <p>A device and method for relativistic <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span> density plasma in a small localized region. A relativistic <span class="hlt">electron</span> beam generator produces a <span class="hlt">high</span> voltage <span class="hlt">electron</span> beam which propagates along a vacuum drift tube and is modulated to initiate <span class="hlt">electron</span> bunching within the beam. The beam is then directed through a low density gas chamber which provides isolation between the vacuum modulator and the relativistic <span class="hlt">electron</span> beam target. The relativistic beam is then applied to a <span class="hlt">high</span> density target plasma which typically comprises DT, DD, hydrogen boron or similar thermonuclear gas at a density of 10.sup.17 to 10.sup.20 <span class="hlt">electrons</span> per cubic centimeter. The target plasma is ionized prior to application of the <span class="hlt">electron</span> beam by means of a laser or other preionization source. Utilizing a relativistic <span class="hlt">electron</span> beam with an individual particle energy exceeding 3 MeV, classical scattering by relativistic <span class="hlt">electrons</span> passing through isolation foils is negligible. As a result, relativistic streaming instabilities are initiated within the <span class="hlt">high</span> density target plasma causing the relativistic <span class="hlt">electron</span> beam to efficiently deposit its energy into a small localized region within the <span class="hlt">high</span> density plasma target.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910011011','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910011011"><span>Self-pressurization of a flightweight liquid hydrogen storage tank subjected to low <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hasan, M. M.; Lin, C. S.; Vandresar, N. T.</p> <p>1991-01-01</p> <p>Results are presented for an experimental investigation of self-pressurization and thermal stratification of a 4.89 cu m liquid hydrogen (LH2) storage tank subjected to low <span class="hlt">heat</span> <span class="hlt">flux</span> (0.35, 2.0, and 3.5 W/sq m) under normal gravity conditions. Tests were performed at fill levels of 83 to 84 percent (by volume). The LH2 tank was representative of future spacecraft tankage, having a low mass-to-volume ratio and <span class="hlt">high</span> performance multilayer thermal insulation. Results show that the pressure rise rate and thermal stratification increase with increasing <span class="hlt">heat</span> <span class="hlt">flux</span>. At the lowest <span class="hlt">heat</span> <span class="hlt">flux</span>, the pressure rise rate is comparable to the homogenous rate, while at the highest <span class="hlt">heat</span> <span class="hlt">flux</span>, the rate is more than three times the homogeneous rate. It was found that initial conditions have a significant impact on the initial pressure rise rate. The quasi-steady pressure rise rates are nearly independent of the initial condition after an initial transient period has passed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016EGUGA..18.3373A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016EGUGA..18.3373A"><span>Estimating sensible <span class="hlt">heat</span> <span class="hlt">flux</span> in agricultural screenhouses by the <span class="hlt">flux</span>-variance and half-order time derivative methods</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Achiman, Ori; Mekhmandarov, Yonatan; Pirkner, Moran; Tanny, Josef</p> <p>2016-04-01</p> <p>Previous studies have established that the eddy covariance (EC) technique is reliable for whole canopy <span class="hlt">flux</span> measurements in agricultural crops covered by porous screens, i.e., screenhouses. Nevertheless, the eddy covariance technique remains difficult to apply in the farm due to costs, operational complexity, and post-processing of data - thereby inviting alternative techniques to be developed. The subject of this research was estimating the sensible <span class="hlt">heat</span> <span class="hlt">flux</span> by two turbulent transport techniques, namely, <span class="hlt">Flux</span>-Variance (FV) and Half-order Time Derivative (HTD) whose instrumentation needs and operational demands are not as elaborate as the EC. The FV is based on the standard deviation of <span class="hlt">high</span> frequency temperature measurements and a similarity constant CT. The HTD method requires mean air temperature and air velocity data. Measurements were carried out in two types of screenhouses: (i) a banana plantation in a light shading (8%) screenhouse; (ii) a pepper crop in a dense insect-proof (50-mesh) screenhouse. In each screenhouse an EC system was deployed for reference and <span class="hlt">high</span> frequency air temperature measurements were conducted using miniature thermocouples installed at several levels to identify the optimal measurement height. Quality control analysis showed that turbulence development and flow stationarity conditions in the two structures were suitable for <span class="hlt">flux</span> measurements by the EC technique. Energy balance closure slopes in the two screenhouses were larger than 0.71, in agreement with results for open fields. Regressions between sensible <span class="hlt">heat</span> <span class="hlt">flux</span> measured by EC and estimated by FV resulted with CT values that were usually larger than 1, the typical value for open field. In both shading and insect-proof screenhouses the CT value generally increased with height. The optimal measurement height, defined as the height with maximum R2 of the regression between EC and FV sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span>, was just above the screen. CT value at optimal height was 2.64 and 1.52 for</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28437986','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28437986"><span>Control and design <span class="hlt">heat</span> <span class="hlt">flux</span> bending in thermal devices with transformation optics.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Guoqiang; Zhang, Haochun; Jin, Yan; Li, Sen; Li, Yao</p> <p>2017-04-17</p> <p>We propose a fundamental latent function of control <span class="hlt">heat</span> transfer and <span class="hlt">heat</span> <span class="hlt">flux</span> density vectors at random positions on thermal materials by applying transformation optics. The expressions for <span class="hlt">heat</span> <span class="hlt">flux</span> bending are obtained, and the factors influencing them are investigated in both 2D and 3D cloaking schemes. Under certain conditions, more than one degree of freedom of <span class="hlt">heat</span> <span class="hlt">flux</span> bending exists corresponding to the temperature gradients of the 3D domain. The <span class="hlt">heat</span> <span class="hlt">flux</span> path can be controlled in random space based on the geometrical azimuths, radial positions, and thermal conductivity ratios of the selected materials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2004AGUFMSM41A1109K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2004AGUFMSM41A1109K"><span>Characterizing Relativistic <span class="hlt">Electrons</span> <span class="hlt">Flux</span> Enhancement Events using sensors onboard SAMPEX and POLAR</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kanekal, S. G.; Selesnick, R. S.; Baker, D. N.; Blake, J. B.</p> <p>2004-12-01</p> <p>Relativistic <span class="hlt">electron</span> <span class="hlt">fluxes</span> in the Earth's outer Van Allen belt are <span class="hlt">highly</span> variable with <span class="hlt">flux</span> enhancements of several orders of magnitude occurring on time scales of a few days. Radiation belt <span class="hlt">electrons</span> often are energized to relativistic energies when the magnetosphere is subjected to <span class="hlt">high</span> solar wind speed and the southward turning of the interplanetary magnetic field. Characterization of <span class="hlt">electron</span> acceleration properties such as <span class="hlt">electron</span> spectra and <span class="hlt">flux</span> isotropization are important in understanding acceleration models. We use sensors onboard SAMPEX and POLAR to measure and survey systematically these properties. SAMPEX measurements cover the entire outer zone for more than a decade from mid 1992 to mid 2004 and POLAR covers the time period from mid 1996 to the present. We use the pulse height analyzed data from the PET detector onboard SAMPEX to measure <span class="hlt">electron</span> spectra. <span class="hlt">Fluxes</span> measured by the HIST detector onboard POLAR together with the PET measurements are used to characterize isotropization times. This paper presents <span class="hlt">electron</span> spectra and isotropization time scales for a few representative events. We will eventually extend these measurements and survey the entire solar cycle 23.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030063051','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030063051"><span>Momentum and <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements in the Exhaust of VASIMR using Helium Propellant</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chavers, D. Gregory; Chang-Diaz, Franklin R.; Irvine, Claude; Squire, Jared P.</p> <p>2003-01-01</p> <p>Interplanetary travel requires propulsion systems that can provide <span class="hlt">high</span> specific impulse (Isp), while also having sufficient thrust to rapidly accelerate large payloads. One such propulsion system is the Variable Specific Impulse Magneto-plasma Rocket (VASIMR), which creates, <span class="hlt">heats</span>, and ejects plasma to provide variable thrust and Isp, designed to optimally meet the mission requirements. The fraction of the total energy invested in creating the plasma, as compared to the plasma's total kinetic energy, is an important factor in determining the overall system efficiency. In VASIMR, this 'frozen flow loss' is appreciable when at <span class="hlt">high</span> thrust, but negligible at <span class="hlt">high</span> Isp. The loss applies to other electric thrusters as well. If some of this energy could be recovered through recombination processes, and reinjected as neutral kinetic energy, the efficiency of VASIMR, in its low Isp/<span class="hlt">high</span> thrust mode may be improved. An experiment is being conducted to investigate the possibility of recovering some of the energy used to create the plasma by studying the flow characteristics of the charged and neutral particles in the exhaust of the thruster. This paper will cover the measurements of momentum <span class="hlt">flux</span> and <span class="hlt">heat</span> <span class="hlt">flux</span> in the exhaust of the VASIMR test facility using helium as the propellant where the <span class="hlt">heat</span> <span class="hlt">flux</span> is comprised of both kinetic and plasma recombination energy. The <span class="hlt">flux</span> measurements also assist in diagnosing and verifying the plasma conditions in the existing experiment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018EPJWC.17405001T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018EPJWC.17405001T"><span>Multi-GEM Detectors in <span class="hlt">High</span> Particle <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Thuiner, P.; Resnati, F.; Franchino, S.; Gonzalez Diaz, D.; Hall-Wilton, R.; Müller, H.; Oliveri, E.; Pfeiffer, D.; Ropelewski, L.; Van Stenis, M.; Streli, C.; Veenhof, R.</p> <p>2018-02-01</p> <p>Gaseous <span class="hlt">Electron</span> Multipliers (GEM) are well known for stable operation at <span class="hlt">high</span> particle <span class="hlt">fluxes</span>. We present a study of the intrinsic limits of GEMdetectors when exposed to very <span class="hlt">high</span> particle <span class="hlt">fluxes</span> of the order of MHz/mm2. We give an interpretation to the variations of the effective gain, which, as a function of the particle <span class="hlt">flux</span>, first increases and then decreases. We also discuss the reduction of the ion back-flow with increasing <span class="hlt">flux</span>. We present measurements and simulations of a triple GEM detector, describing its behaviour in terms of accumulation of positive ions that results in changes of the transfer fields and the amplification fields. The behaviour is expected to be common to all multi-stage amplification devices where the efficiency of transferring the <span class="hlt">electrons</span> from one stage to the next one is not 100%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70186946','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70186946"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> from magmatic hydrothermal systems related to availability of fluid recharge</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Harvey, M. C.; Rowland, J.V.; Chiodini, G.; Rissmann, C.F.; Bloomberg, S.; Hernandez, P.A.; Mazot, A.; Viveiros, F.; Werner, Cynthia A.</p> <p>2015-01-01</p> <p>Magmatic hydrothermal systems are of increasing interest as a renewable energy source. Surface <span class="hlt">heat</span> <span class="hlt">flux</span> indicates system resource potential, and can be inferred from soil CO2 <span class="hlt">flux</span> measurements and fumarole gas chemistry. Here we compile and reanalyze results from previous CO2 <span class="hlt">flux</span> surveys worldwide to compare <span class="hlt">heat</span> <span class="hlt">flux</span> from a variety of magma-hydrothermal areas. We infer that availability of water to recharge magmatic hydrothermal systems is correlated with <span class="hlt">heat</span> <span class="hlt">flux</span>. Recharge availability is in turn governed by permeability, structure, lithology, rainfall, topography, and perhaps unsurprisingly, proximity to a large supply of water such as the ocean. The relationship between recharge and <span class="hlt">heat</span> <span class="hlt">flux</span> interpreted by this study is consistent with recent numerical modeling that relates hydrothermal system <span class="hlt">heat</span> output to rainfall catchment area. This result highlights the importance of recharge as a consideration when evaluating hydrothermal systems for electricity generation, and the utility of CO2 <span class="hlt">flux</span> as a resource evaluation tool.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009PhST..138a4059H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009PhST..138a4059H"><span>Experiences with tungsten coatings in <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> tests and under plasma load in ASDEX Upgrade</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Herrmann, A.; Greuner, H.; Fuchs, J. C.; de Marné, P.; Neu, R.; ASDEX Upgrade Team</p> <p>2009-12-01</p> <p>ASDEX Upgrade was operated with about 6400 s plasma discharge during the scientific program in 2007/2008 exploring tungsten as a first wall material in tokamaks. In the first phase, the <span class="hlt">heating</span> power was restricted to 10 MW. It was increased to 15 MW in the second phase. During this operational period, a delamination of the 200 μm W-VPS coating happened at 2 out of 128 tiles of the outer divertor and an unscheduled opening was required. In the third phase, ASDEX Upgrade was operated with partly predamaged tiles and up to 15 MW <span class="hlt">heating</span> power. The target load was actively controlled by N2-seeding. This paper presents the screening test of target tiles in the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> test facility GLADIS, experiences with operation and detected damages of the outer divertor as well as the <span class="hlt">heat</span> load to the outer divertor and the reasons for the toroidal asymmetry of the divertor load.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JAP...122j3301Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JAP...122j3301Z"><span><span class="hlt">Electron</span> kinetics in capacitively coupled plasmas modulated by <span class="hlt">electron</span> injection</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Ya; Peng, Yanli; Innocenti, Maria Elena; Jiang, Wei; Wang, Hong-yu; Lapenta, Giovanni</p> <p>2017-09-01</p> <p>The controlling effect of an <span class="hlt">electron</span> injection on the <span class="hlt">electron</span> energy distribution function (EEDF) and on the energetic <span class="hlt">electron</span> <span class="hlt">flux</span>, in a capacitive radio-frequency argon plasma, is studied using a one-dimensional particle-in-cell/Monte Carlo collisions model. The input power of the <span class="hlt">electron</span> beam is as small as several tens of Watts with laboratory achievable emission currents and energies. With the <span class="hlt">electron</span> injection, the <span class="hlt">electron</span> temperature decreases but with a significant <span class="hlt">high</span> energy tail. The <span class="hlt">electron</span> density, <span class="hlt">electron</span> temperature in the sheath, and <span class="hlt">electron</span> <span class="hlt">heating</span> rate increase with the increasing emission energy. This is attributed to the extra <span class="hlt">heating</span> of the energetic <span class="hlt">electrons</span> in the EEDF tail. The non-equilibrium EEDF is obtained for strong non-local distributions of the electric field, <span class="hlt">electron</span> <span class="hlt">heating</span> rate, excitation, and ionization rate, indicating the discharge has transited from a volume <span class="hlt">heating</span> (α-mode dominated) into a sheath <span class="hlt">heating</span> (γ-mode dominated) type. In addition, the <span class="hlt">electron</span> injection not only modifies the self-bias voltage, but also enhances the <span class="hlt">electron</span> <span class="hlt">flux</span> that can reach the electrodes. Moreover, the relative population of energetic <span class="hlt">electrons</span> significantly increases with the <span class="hlt">electron</span> injection compared to that without the <span class="hlt">electron</span> injection, relevant for modifying the gas and surface chemistry reactions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AIPC.1501..687A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AIPC.1501..687A"><span>DSMC simulation of rarefied gas flows under cooling conditions using a new iterative wall <span class="hlt">heat</span> <span class="hlt">flux</span> specifying technique</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Akhlaghi, H.; Roohi, E.; Myong, R. S.</p> <p>2012-11-01</p> <p>Micro/nano geometries with specified wall <span class="hlt">heat</span> <span class="hlt">flux</span> are widely encountered in <span class="hlt">electronic</span> cooling and micro-/nano-fluidic sensors. We introduce a new technique to impose the desired (positive/negative) wall <span class="hlt">heat</span> <span class="hlt">flux</span> boundary condition in the DSMC simulations. This technique is based on an iterative progress on the wall temperature magnitude. It is found that the proposed iterative technique has a good numerical performance and could implement both positive and negative values of wall <span class="hlt">heat</span> <span class="hlt">flux</span> rates accurately. Using present technique, rarefied gas flow through micro-/nanochannels under specified wall <span class="hlt">heat</span> <span class="hlt">flux</span> conditions is simulated and unique behaviors are observed in case of channels with cooling walls. For example, contrary to the <span class="hlt">heating</span> process, it is observed that cooling of micro/nanochannel walls would result in small variations in the density field. Upstream thermal creep effects in the cooling process decrease the velocity slip despite of the Knudsen number increase along the channel. Similarly, cooling process decreases the curvature of the pressure distribution below the linear incompressible distribution. Our results indicate that flow cooling increases the mass flow rate through the channel, and vice versa.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19850067082&hterms=Biddle&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DBiddle','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19850067082&hterms=Biddle&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DBiddle"><span>Evidence for ion <span class="hlt">heat</span> <span class="hlt">flux</span> in the light ion polar wind</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Biddle, A. P.; Moore, T. E.; Chappell, C. R.</p> <p>1985-01-01</p> <p>Cold flowing hydrogen and helium ions have been observed using the retarding ion mass spectrometer on board the Dynamics Explorer 1 spacecraft in the dayside magnetosphere at subauroral latitudes. The ions show a marked <span class="hlt">flux</span> asymmetry with respect to the relative wind direction. The observed data are fitted by a model of drifting Maxwellian distributions perturbed by a first order-Spritzer-Haerm <span class="hlt">heat</span> <span class="hlt">flux</span> distribution function. It is shown that both ion species are supersonic just equatorward of the auroral zone at L = 14, and the shape of asymmetry and direction of the asymmetry are consistent with the presence of an upward <span class="hlt">heat</span> <span class="hlt">flux</span>. At L = 6, both species evolve smoothly into warmer subsonic upward flows with downward <span class="hlt">heat</span> <span class="hlt">fluxes</span>. In the case of subsonic flows the downward <span class="hlt">heat</span> <span class="hlt">flux</span> implies a significant <span class="hlt">heat</span> source at higher altitudes. Spin curves of the spectrometer count rate versus the spin phase angle are provided.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20030061427&hterms=heat+recovery&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dheat%2Brecovery','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20030061427&hterms=heat+recovery&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dheat%2Brecovery"><span>Momentum and <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements in the Exhaust of VASIMR Using Helium Propellant</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chavers, D. Gregory</p> <p>2002-01-01</p> <p>Electromagnetic thrusters typically use electric and magnetic fields to accelerate and exhaust plasma through interactions with the charged particles in the plasma. The energy required to create the plasma, i.e. ionization energy, is potential energy between the <span class="hlt">electron</span> and ion. This potential energy is typically lost since it is not recovered as the plasma is exhausted and is known as frozen flow loss. If the frozen flow energy is a small fraction of the total plasma energy, this frozen flow loss may be negligible. However, if the frozen flow energy is a major fraction of the total plasma energy, this loss can severely reduce the energy efficiency of the thruster. Recovery and utilization of this frozen flow energy can improve the energy efficiency of a thruster during low specific impulse operating regimes when the ionization energy is a large fraction of the total plasma energy. This paper quantifies the recovery of the frozen flow energy, i.e. recombination energy, via the process of surface recombination for helium. To accomplish this task the momentum <span class="hlt">flux</span> and <span class="hlt">heat</span> <span class="hlt">flux</span> of the plasma flow were measured and compared to calculated values from electrostatic probe data. This information was used to deduce the contribution of recombination energy to the total <span class="hlt">heat</span> <span class="hlt">flux</span> on a flat plate as well as to characterize the plasma conditions. Helium propellant was investigated initially due to its <span class="hlt">high</span> ionization potential and hence available recombination energy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040086711','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040086711"><span>Thermal Conductivity of Advanced Ceramic Thermal Barrier Coatings Determined by a Steady-state Laser <span class="hlt">Heat-flux</span> Approach</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zhu, Dong-Ming; Miller, Robert A.</p> <p>2004-01-01</p> <p>The development of low conductivity and <span class="hlt">high</span> temperature capable thermal barrier coatings requires advanced testing techniques that can accurately and effectively evaluate coating thermal conductivity under future <span class="hlt">high</span>-performance and low-emission engine <span class="hlt">heat-flux</span> conditions. In this paper, a unique steady-state CO2 laser (wavelength 10.6 microns) <span class="hlt">heat-flux</span> approach is described for determining the thermal conductivity and conductivity deduced cyclic durability of ceramic thermal and environmental barrier coating systems at very <span class="hlt">high</span> temperatures (up to 1700 C) under large thermal gradients. The thermal conductivity behavior of advanced thermal and environmental barrier coatings for metallic and Si-based ceramic matrix composite (CMC) component applications has also been investigated using the laser conductivity approach. The relationships between the lattice and radiation conductivities as a function of <span class="hlt">heat</span> <span class="hlt">flux</span> and thermal gradient at <span class="hlt">high</span> temperatures have been examined for the ceramic coating systems. The steady-state laser <span class="hlt">heat-flux</span> conductivity approach has been demonstrated as a viable means for the development and life prediction of advanced thermal barrier coatings for future turbine engine applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFM.A33B0157H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFM.A33B0157H"><span>Distributed Sensible <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements for Wireless Sensor Networks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huwald, H.; Brauchli, T.; Lehning, M.; Higgins, C. W.</p> <p>2015-12-01</p> <p>The sensible <span class="hlt">heat</span> <span class="hlt">flux</span> component of the surface energy balance is typically computed using eddy covariance or two point profile measurements while alternative approaches such as the <span class="hlt">flux</span> variance method based on convective scaling has been much less explored and applied. <span class="hlt">Flux</span> variance (FV) certainly has a few limitations and constraints but may be an interesting and competitive method in low-cost and power limited wireless sensor networks (WSN) with the advantage of providing spatio-temporal sensible <span class="hlt">heat</span> <span class="hlt">flux</span> over the domain of the network. In a first step, parameters such as sampling frequency, sensor response time, and averaging interval are investigated. Then we explore the applicability and the potential of the FV method for use in WSN in a field experiment. Low-cost sensor systems are tested and compared against reference instruments (3D sonic anemometers) to evaluate the performance and limitations of the sensors as well as the method with respect to the standard calculations. Comparison experiments were carried out at several sites to gauge the <span class="hlt">flux</span> measurements over different surface types (gravel, grass, water) from the low-cost systems. This study should also serve as an example of spatially distributed sensible <span class="hlt">heat</span> <span class="hlt">flux</span> measurements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012EGUGA..1412137Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012EGUGA..1412137Z"><span>Urban <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the subsurface of Cologne, Germany</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhu, K.; Bayer, P.; Blum, P.</p> <p>2012-04-01</p> <p>Urbanization during the last hundred years has led to both environmental and thermal impacts on the subsurface. The urban <span class="hlt">heat</span> island (UHI) effect is mostly described as an atmospheric phenomenon, where the measured aboveground temperatures in cities are elevated in comparison to undisturbed rural regions. However, UHIs can be found below, as well as above ground. A large amount of anthropogenic <span class="hlt">heat</span> migrates into the urban subsurface, which also raises the ground temperature and permanently changes the thermal conditions in shallow aquifers. The main objective of our work is to study and determine the urban <span class="hlt">heat</span> <span class="hlt">fluxes</span> in Cologne, Germany, and to improve our understanding of the dynamics of subsurface energy <span class="hlt">fluxes</span> in UHIs. Ideally, our findings will contribute to strategic and more sustainable geothermal use in cities. For a quantitative analysis of the energy <span class="hlt">fluxes</span> within the subsurface and across the atmospheric boundary, two and three-dimensional coupled numerical flow and <span class="hlt">heat</span> transport models were developed. The simulation results indicate that during the past hundred years, an average vertical urban <span class="hlt">heat</span> <span class="hlt">flux</span> that ranges between 80 and 375 mW m-2 can be deduced. Thermal anomalies have migrated into the local urban aquifer system and they reach a depth of about 150 m. In this context, the influence of the regional groundwater flow on the subsurface <span class="hlt">heat</span> transport and temperature development is comprehensively discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/12836556','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/12836556"><span>[A review on research of land surface water and <span class="hlt">heat</span> <span class="hlt">fluxes</span>].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sun, Rui; Liu, Changming</p> <p>2003-03-01</p> <p>Many field experiments were done, and soil-vegetation-atmosphere transfer(SVAT) models were stablished to estimate land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>. In this paper, the processes of experimental research on land surface water and <span class="hlt">heat</span> <span class="hlt">fluxes</span> are reviewed, and three kinds of SVAT model(single layer model, two layer model and multi-layer model) are analyzed. Remote sensing data are widely used to estimate land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Based on remote sensing and energy balance equation, different models such as simplified model, single layer model, extra resistance model, crop water stress index model and two source resistance model are developed to estimate land surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> and evapotranspiration. These models are also analyzed in this paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ZaMP...69...71B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ZaMP...69...71B"><span>Systems with a constant <span class="hlt">heat</span> <span class="hlt">flux</span> with applications to radiative <span class="hlt">heat</span> transport across nanoscale gaps and layers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Budaev, Bair V.; Bogy, David B.</p> <p>2018-06-01</p> <p>We extend the statistical analysis of equilibrium systems to systems with a constant <span class="hlt">heat</span> <span class="hlt">flux</span>. This extension leads to natural generalizations of Maxwell-Boltzmann's and Planck's equilibrium energy distributions to energy distributions of systems with a net <span class="hlt">heat</span> <span class="hlt">flux</span>. This development provides a long needed foundation for addressing problems of nanoscale <span class="hlt">heat</span> transport by a systematic method based on a few fundamental principles. As an example, we consider the computation of the radiative <span class="hlt">heat</span> <span class="hlt">flux</span> between narrowly spaced half-spaces maintained at different temperatures.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhPl...23e2502Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhPl...23e2502Y"><span>The study of <span class="hlt">heat</span> <span class="hlt">flux</span> for disruption on experimental advanced superconducting tokamak</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, Zhendong; Fang, Jianan; Gong, Xianzu; Gan, Kaifu; Luo, Jiarong; Zhao, Hailin; Cui, Zhixue; Zhang, Bin; Chen, Meiwen</p> <p>2016-05-01</p> <p>Disruption of the plasma is one of the most dangerous instabilities in tokamak. During the disruption, most of the plasma thermal energy is lost, which causes damages to the plasma facing components. Infrared (IR) camera is an effective tool to detect the temperature distribution on the first wall, and the energy deposited on the first wall can be calculated from the surface temperature profile measured by the IR camera. This paper concentrates on the characteristics of <span class="hlt">heat</span> <span class="hlt">flux</span> distribution onto the first wall under different disruptions, including the minor disruption and the vertical displacement events (VDE) disruption. Several minor disruptions have been observed before the major disruption under the <span class="hlt">high</span> plasma density in experimental advanced superconducting tokamak. During the minor disruption, the <span class="hlt">heat</span> <span class="hlt">fluxes</span> are mainly deposited on the upper/lower divertors. The magnetic configuration prior to the minor disruption is a lower single null with the radial distance between the two separatrices in the outer midplane dRsep = -2 cm, while it changes to upper single null (dRsep = 1.4 cm) during the minor disruption. As for the VDE disruption, the spatial distribution of <span class="hlt">heat</span> <span class="hlt">flux</span> exhibits strong toroidal and radial nonuniformity, and the maximum <span class="hlt">heat</span> <span class="hlt">flux</span> received on the dome plate can be up to 11 MW/m2.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22597179-design-indirectly-heated-thoriated-tungsten-cathode-based-strip-electron-gun','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22597179-design-indirectly-heated-thoriated-tungsten-cathode-based-strip-electron-gun"><span>Design of indirectly <span class="hlt">heated</span> thoriated tungsten cathode based strip <span class="hlt">electron</span> gun</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Maiti, Namita; Thakur, K.B.; Patil, D.S.</p> <p></p> <p>Design of indirectly <span class="hlt">heated</span> solid cathode based <span class="hlt">electron</span> gun (200 kW, 45 kV, 270 degree bent strip type <span class="hlt">electron</span> gun) has been presented. The solid cathode is made of thoriated tungsten. The solid cathode design has been suitably done to achieve required <span class="hlt">electron</span> beam cross section. The design approach consists of simulation followed by extensive experimentation. In the design, the effort has been put to reduce the non-uniformity of the <span class="hlt">heat</span> <span class="hlt">flux</span> from the filament to the solid cathode to obtain better uniformity of temperature on the solid cathode. Trial beam experiments shows that the modified design achieves one tomore » one correspondence of the solid cathode length and the <span class="hlt">electron</span> beam length. (author)« less</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_15 --> <div id="page_16" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="301"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AGUFM.B23A0388H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AGUFM.B23A0388H"><span>Solution for Minimizing Surface <span class="hlt">Heating</span> Effect for Fast Open-Path CO2 <span class="hlt">Flux</span> Measurements in Cold Environments</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hupp, J. R.; Burba, G. G.; McDermitt, D. K.; Anderson, D. J.; Eckles, R. D.</p> <p>2010-12-01</p> <p>Open-path design of the <span class="hlt">high</span> speed gas analyzers is a well-established configuration widely used for measurements of CO2 <span class="hlt">fluxes</span> and concentrations. This configuration has advantages and deficiencies. Advantages include excellent frequency response, long-term stability, low sensitivity to window contamination, low-power pump-free operation, and infrequent calibration requirements. Deficiencies include susceptibility to precipitation and icing, and a potential need for instrument surface <span class="hlt">heating</span> correction in extremely cold environments. In spite of the deficiencies, open-path measurements often provide data coverage that would not have been possible using traditional closed-path approach. Data loss from precipitation and icing may not always be prevented for the open-path instruments, while <span class="hlt">heating</span> effect does not pose a problem for CO2 <span class="hlt">flux</span> in warm environments. Even in cold environments, the impact of <span class="hlt">heating</span> on CO2 <span class="hlt">flux</span> is much smaller than other well-known effects, such as Webb-Pearman-Leuning terms, or frequency response corrections for closed-path analyzers. Nonetheless, instrument surface <span class="hlt">heating</span> effect in cold environments could be addressed scientifically, via developing the theoretical corrections, and instrumentally, via measuring fast integrated air temperature in the optical path, or via enclosing the open-path instrument into a low-power short-intake design. Here we provide an alternative way to minimize or eliminate open-path <span class="hlt">heating</span> effect, achieved by minimizing or eliminating the temperature gradient between the instrument surface and ambient air. Open-path low temperature controlled design is discussed in comparison with two other approaches (e.g., traditional open-path design and closed-path design) in terms of their field performance for Eddy Covariance <span class="hlt">flux</span> measurements in the cold. This study presents field data from a new open-path CO2/H2O gas analyzer, LI-7500A, based on the LI-7500 model modified to produce substantially less <span class="hlt">heat</span> during</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/6048380-atmospheric-electron-flux-airplane-altitude','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/6048380-atmospheric-electron-flux-airplane-altitude"><span>Atmospheric <span class="hlt">electron</span> <span class="hlt">flux</span> at airplane altitude</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Enomoto, R.; Chiba, J.; Ogawa, K.</p> <p>1991-12-01</p> <p>We have developed a new detector to systematically measure the cosmic-ray <span class="hlt">electron</span> <span class="hlt">flux</span> at airplane altitudes. We loaded a lead-glass-based <span class="hlt">electron</span> telescope onto a commercial cargo airplane. The first experiment was carried out using the air route between Narita (Japan) and Sydney (Australia); during this flight we measured the <span class="hlt">electron</span> <span class="hlt">flux</span> at various altitudes and latitudes. The thresholds of the <span class="hlt">electron</span> energies were 1, 2, and 4 GeV. The results agree with a simple estimation using one-dimensional shower theory. A comparison with a Monte Carlo calculation was made.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhFl...28i2102V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhFl...28i2102V"><span>Expanding Taylor bubble under constant <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Voirand, Antoine; Benselama, Adel M.; Ayel, Vincent; Bertin, Yves</p> <p>2016-09-01</p> <p>Modelization of non-isothermal bubbles expanding in a capillary, as a contribution to the understanding of the physical phenomena taking place in Pulsating <span class="hlt">Heat</span> Pipes (PHPs), is the scope of this paper. The liquid film problem is simplified and solved, while the thermal problem takes into account a constant <span class="hlt">heat</span> <span class="hlt">flux</span> density applied at the capillary tube wall, exchanging with the liquid film surrounding the bubble and also with the capillary tube outside medium. The liquid slug dynamics is solved using the Lucas-Washburn equation. Mass and energy balance on the vapor phase allow governing equations of bubble expansion to be written. The liquid and vapor phases are coupled only through the saturation temperature associated with the vapor pressure, assumed to be uniform throughout the bubble. Results show an over-<span class="hlt">heating</span> of the vapor phase, although the particular thermal boundary condition used here always ensures an evaporative mass <span class="hlt">flux</span> at the liquid-vapor interface. Global <span class="hlt">heat</span> exchange is also investigated, showing a strong decreasing of the PHP performance to convey <span class="hlt">heat</span> by phase change means for large meniscus velocities.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSH41C..02G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSH41C..02G"><span>Chromospheric <span class="hlt">Heating</span> Driven by Cancellations of Internetwork Magnetic <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gosic, M.; de la Cruz Rodriguez, J.; De Pontieu, B.; Bellot Rubio, L.; Esteban Pozuelo, S.; Ortiz-Carbonell, A. N.</p> <p>2017-12-01</p> <p>The <span class="hlt">heating</span> of the solar chromosphere remains to be one of the most important questions in solar physics. It is believed that this phenomenon may significantly be supported by small-scale internetwork (IN) magnetic fields. Indeed, cancellations of IN magnetic <span class="hlt">flux</span> can generate transient brightenings in the chromosphere and transition region. These bright structures might be the signature of energy release and plasma <span class="hlt">heating</span>, probably driven by magnetic reconnection of IN field lines. Using <span class="hlt">high</span> resolution, multiwavelength, coordinated observations recorded with the Interface Region Imaging Spectrograph (IRIS) and the Swedish 1-m Solar Telescope (SST), we analyzed cancellations of IN <span class="hlt">flux</span> and their impact on the energetics and dynamics of the quiet Sun atmosphere. From their temporal and spatial evolution, we determine that these events can <span class="hlt">heat</span> locally the upper atmospheric layers. However, employing multi-line inversions of the Mg II h & k lines, we show that cancellations, although occurring ubiquitously over IN regions, are not capable of sustaining the total radiative losses of the quiet Sun chromosphere.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960023961','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960023961"><span>An Investigation of the Compatibility of Radiation and Convection <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Liebert, Curt H.</p> <p>1996-01-01</p> <p>A method for determining time-resolved absorbed surface <span class="hlt">heat</span> <span class="hlt">flux</span> and surface temperature in radiation and convection environments is described. The method is useful for verification of aerodynamic, <span class="hlt">heat</span> transfer and durability models. A practical <span class="hlt">heat</span> <span class="hlt">flux</span> gage fabrication procedure and a simple one-dimensional inverse <span class="hlt">heat</span> conduction model and calculation procedure are incorporated in this method. The model provides an estimate of the temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> gradient in the direction of <span class="hlt">heat</span> transfer through the gage. This paper discusses several successful time-resolved tests of this method in hostile convective <span class="hlt">heating</span> and cooling environments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1267036-temperature-measurements-during-high-flux-ion-beam-irradiations','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1267036-temperature-measurements-during-high-flux-ion-beam-irradiations"><span>Temperature measurements during <span class="hlt">high</span> <span class="hlt">flux</span> ion beam irradiations</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Crespillo, Miguel L.; Graham, Joseph T.; Zhang, Yanwen; ...</p> <p>2016-02-16</p> <p>A systematic study of the ion beam <span class="hlt">heating</span> effect was performed in a temperature range of –170 to 900 °C using a 10 MeV Au 3+ ion beam and a Yttria stabilized Zirconia (YSZ) sample at a <span class="hlt">flux</span> of 5.5 × 10 12 cm –2 s –1. Different geometric configurations of beam, sample, thermocouple positioning, and sample holder were compared to understand the <span class="hlt">heat</span>/charge transport mechanisms responsible for the observed temperature increase. The beam <span class="hlt">heating</span> exhibited a strong dependence on the background (initial) sample temperature with the largest temperature increases occurring at cryogenic temperatures and decreasing with increasing temperature. Comparisonmore » with numerical calculations suggests that the observed <span class="hlt">heating</span> effect is, in reality, a predominantly <span class="hlt">electronic</span> effect and the true temperature rise is small. Furthermore, a simple model was developed to explain this <span class="hlt">electronic</span> effect in terms of an electrostatic potential that forms during ion irradiation. Such an artificial beam <span class="hlt">heating</span> effect is potentially problematic in thermostated ion irradiation and ion beamanalysis apparatus, as the operation of temperature feedback systems can be significantly distorted by this effect.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1373693-gyrokinetic-projection-divertor-heat-flux-width-from-present-tokamaks-iter','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1373693-gyrokinetic-projection-divertor-heat-flux-width-from-present-tokamaks-iter"><span>Gyrokinetic projection of the divertor <span class="hlt">heat-flux</span> width from present tokamaks to ITER</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Chang, Choong Seock; Ku, Seung -Hoe; Loarte, Alberto; ...</p> <p>2017-07-11</p> <p>Here, the XGC1 edge gyrokinetic code is used to study the width of the <span class="hlt">heat-flux</span> to divertor plates in attached plasma condition. The <span class="hlt">flux</span>-driven simulation is performed until an approximate power balance is achieved between the <span class="hlt">heat-flux</span> across the steep pedestal pressure gradient and the <span class="hlt">heat-flux</span> on the divertor plates.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EGUGA..17.1791W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EGUGA..17.1791W"><span>Modelling storm development and the impact when introducing waves, sea spray and <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wu, Lichuan; Rutgersson, Anna; Sahlée, Erik</p> <p>2015-04-01</p> <p>In <span class="hlt">high</span> wind speed conditions, sea spray generated due to intensity breaking waves have big influence on the wind stress and <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Measurements show that drag coefficient will decrease in <span class="hlt">high</span> wind speed. Sea spray generation function (SSGF), an important term of wind stress parameterization in <span class="hlt">high</span> wind speed, usually treated as a function of wind speed/friction velocity. In this study, we introduce a wave state depended SSGG and wave age depended Charnock number into a <span class="hlt">high</span> wind speed wind stress parameterization (Kudryavtsev et al., 2011; 2012). The proposed wind stress parameterization and sea spray <span class="hlt">heat</span> <span class="hlt">fluxes</span> parameterization from Andreas et al., (2014) were applied to an atmosphere-wave coupled model to test on four storm cases. Compared with measurements from the FINO1 platform in the North Sea, the new wind stress parameterization can reduce the forecast errors of wind in <span class="hlt">high</span> wind speed range, but not in low wind speed. Only sea spray impacted on wind stress, it will intensify the storms (minimum sea level pressure and maximum wind speed) and lower the air temperature (increase the errors). Only the sea spray impacted on the <span class="hlt">heat</span> <span class="hlt">fluxes</span>, it can improve the model performance on storm tracks and the air temperature, but not change much in the storm intensity. If both of sea spray impacted on the wind stress and <span class="hlt">heat</span> <span class="hlt">fluxes</span> are taken into account, it has the best performance in all the experiment for minimum sea level pressure and maximum wind speed and air temperature. Andreas, E. L., Mahrt, L., and Vickers, D. (2014). An improved bulk air-sea surface <span class="hlt">flux</span> algorithm, including spray-mediated transfer. Quarterly Journal of the Royal Meteorological Society. Kudryavtsev, V. and Makin, V. (2011). Impact of ocean spray on the dynamics of the marine atmospheric boundary layer. Boundary-layer meteorology, 140(3):383-410. Kudryavtsev, V., Makin, V., and S, Z. (2012). On the sea-surface drag and <span class="hlt">heat</span>/mass transfer at strong winds. Technical report, Royal</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22599975-effect-quantum-correction-nonlinear-thermal-wave-electrons-driven-laser-heating','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22599975-effect-quantum-correction-nonlinear-thermal-wave-electrons-driven-laser-heating"><span>Effect of quantum correction on nonlinear thermal wave of <span class="hlt">electrons</span> driven by laser <span class="hlt">heating</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Nafari, F.; Ghoranneviss, M., E-mail: ghoranneviss@gmail.com</p> <p>2016-08-15</p> <p>In thermal interaction of laser pulse with a deuterium-tritium (DT) plane, the thermal waves of <span class="hlt">electrons</span> are generated instantly. Since the thermal conductivity of <span class="hlt">electron</span> is a nonlinear function of temperature, a nonlinear <span class="hlt">heat</span> conduction equation is used to investigate the propagation of waves in solid DT. This paper presents a self-similar analytic solution for the nonlinear <span class="hlt">heat</span> conduction equation in a planar geometry. The thickness of the target material is finite in numerical computation, and it is assumed that the laser energy is deposited at a finite initial thickness at the initial time which results in a finite temperaturemore » for <span class="hlt">electrons</span> at initial time. Since the required temperature range for solid DT ignition is higher than the critical temperature which equals 35.9 eV, the effects of quantum correction in thermal conductivity should be considered. This letter investigates the effects of quantum correction on characteristic features of nonlinear thermal wave, including temperature, penetration depth, velocity, <span class="hlt">heat</span> <span class="hlt">flux</span>, and <span class="hlt">heating</span> and cooling domains. Although this effect increases <span class="hlt">electron</span> temperature and thermal <span class="hlt">flux</span>, penetration depth and propagation velocity are smaller. This effect is also applied to re-evaluate the side-on laser ignition of uncompressed DT.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PlST...17..792C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PlST...17..792C"><span>Numerical Study of <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Performances of Flat-Tile Divertor Mock-ups with Hypervapotron Cooling Concept</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Lei; Liu, Xiang; Lian, Youyun; Cai, Laizhong</p> <p>2015-09-01</p> <p>The hypervapotron (HV), as an enhanced <span class="hlt">heat</span> transfer technique, will be used for ITER divertor components in the dome region as well as the enhanced <span class="hlt">heat</span> <span class="hlt">flux</span> first wall panels. W-Cu brazing technology has been developed at SWIP (Southwestern Institute of Physics), and one W/CuCrZr/316LN component of 450 mm×52 mm×166 mm with HV cooling channels will be fabricated for <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> (HHF) tests. Before that a relevant analysis was carried out to optimize the structure of divertor component elements. ANSYS-CFX was used in CFD analysis and ABAQUS was adopted for thermal-mechanical calculations. Commercial code FE-SAFE was adopted to compute the fatigue life of the component. The tile size, thickness of tungsten tiles and the slit width among tungsten tiles were optimized and its HHF performances under International Thermonuclear Experimental Reactor (ITER) loading conditions were simulated. One brand new tokamak HL-2M with advanced divertor configuration is under construction in SWIP, where ITER-like flat-tile divertor components are adopted. This optimized design is expected to supply valuable data for HL-2M tokamak. supported by the National Magnetic Confinement Fusion Science Program of China (Nos. 2011GB110001 and 2011GB110004)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21096099','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21096099"><span>Theoretical simulation of the dual-<span class="hlt">heat-flux</span> method in deep body temperature measurements.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Huang, Ming; Chen, Wenxi</p> <p>2010-01-01</p> <p>Deep body temperature reveals individual physiological states, and is important in patient monitoring and chronobiological studies. An innovative dual-<span class="hlt">heat-flux</span> method has been shown experimentally to be competitive with the conventional zero-<span class="hlt">heat</span>-flow method in its performance, in terms of measurement accuracy and step response to changes in the deep temperature. We have utilized a finite element method to model and simulate the dynamic process of a dual-<span class="hlt">heat-flux</span> probe in deep body temperature measurements to validate the fundamental principles of the dual-<span class="hlt">heat-flux</span> method theoretically, and to acquire a detailed quantitative description of the thermal profile of the dual-<span class="hlt">heat-flux</span> probe. The simulation results show that the estimated deep body temperature is influenced by the ambient temperature (linearly, at a maximum rate of 0.03 °C/°C) and the blood perfusion rate. The corresponding depth of the estimated temperature in the skin and subcutaneous tissue layer is consistent when using the dual-<span class="hlt">heat-flux</span> probe. Insights in improving the performance of the dual-<span class="hlt">heat-flux</span> method were discussed for further studies of dual-<span class="hlt">heat-flux</span> probes, taking into account structural and geometric considerations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000056863','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000056863"><span>Critical <span class="hlt">Heat</span> <span class="hlt">Flux</span> in Pool Boiling on Metal-Graphite Composite Surfaces</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zhang, Nengli; Yang, Wen-Jei; Chao, David F.; Chao, David F. (Technical Monitor)</p> <p>2000-01-01</p> <p>A study is conducted on <span class="hlt">high</span> <span class="hlt">heat-flux</span> pool boiling of pentane on micro-configured composite surfaces. The boiling surfaces are copper-graphite (Cu-Gr) and aluminum-graphite (Al-Gr) composites with a fiber volume concentration of 50%. The micro-graphite fibers embedded in the matrix contribute to a substantial enhancement in boiling <span class="hlt">heat</span>-transfer performance. Correlation equations are obtained for both the isolated and coalesced bubble regimes, utilizing a mathematical model based on a metal-graphite, two-tier configuration with the aid of experimental data. A new model to predict the critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) on the composites is proposed to explain the fundamental aspects of the boiling phenomena. Three different factors affecting the CHF are considered in the model. Two of them are expected to become the main agents driving vapor volume detachment under microgravity conditions, using the metal-graphite composite surfaces as the <span class="hlt">heating</span> surface and using liquids with an unusual Marangoni effect as the working fluid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMSM41B2433G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMSM41B2433G"><span><span class="hlt">Electron</span> Injections: A Study of <span class="hlt">Electron</span> Acceleration by Multiple Dipolarizing <span class="hlt">Flux</span> Bundles Using an Analytical Model</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gabrielse, C.; Angelopoulos, V.; Artemyev, A.; Runov, A.; Harris, C.</p> <p>2016-12-01</p> <p>We study energetic <span class="hlt">electron</span> injections using an analytical model that self-consistently describes electric and magnetic field perturbations of transient, localized dipolarizing <span class="hlt">flux</span> bundles (DFBs). Previous studies using THEMIS, Van Allen Probes, and the Magnetospheric Multiscale Mission have shown that injections can occur on short (minutes) or long (10s of minutes) timescales. These studies suggest that the short timescale injections correspond to a single DFB, whereas long timescale injections are likely caused by an aggregate of multiple DFBs, each incrementally <span class="hlt">heating</span> the particle population. We therefore model the effects of multiple DFBs on the <span class="hlt">electron</span> population using multi-spacecraft observations of the fields and particle <span class="hlt">fluxes</span> to constrain the model parameters. The analytical model is the first of its kind to model multiple dipolarization fronts in order to better understand the transport and acceleration process throughout the plasma sheet. It can reproduce most injection signatures at multiple locations simultaneously, reaffirming earlier findings that multiple earthward-traveling DFBs can both transport and accelerate <span class="hlt">electrons</span> to suprathermal energies, and can thus be considered the injections' primary driver.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA486411','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA486411"><span>Two-Phase Flow in <span class="hlt">High-Heat-Flux</span> Micro-Channel <span class="hlt">Heat</span> Sink for Refrigeration Cooling Applications. Part 2: Low Temperature Hybrid Micro-Channel/Micro-Jet Impingement Cooling</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2008-09-01</p> <p>TWO-PHASE FLOW IN <span class="hlt">HIGH-HEAT-FLUX</span> MICRO-CHANNEL <span class="hlt">HEAT</span> SINK FOR REFRIGERATION COOLING APPLICATIONS (Contract No. N00014-05-1-0408) by Issam Mudawar ...Refrigeration Cooling Applications 5b. GRANT NUMBER N00014-04-1-0408 5c. PROGRAM ELEMENT NUMBER NA 6. AUTHOR(S) 5d. PROJECT NUMBER Mudawar , Issam NA...ABSTRACT OF Mudawar , Issam PAGES U U U UU 465 19b. TELEPHONE NUMBER (Include area code) 765-494-5705 Standard Form 298 (Rev. 8/98) Prescribed by ANSI Std</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhyB..503...64M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhyB..503...64M"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> measurements of Tb3M series (M=Co, Rh and Ru): Specific <span class="hlt">heat</span> and magnetocaloric properties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Monteiro, J. C. B.; Lombardi, G. A.; dos Reis, R. D.; Freitas, H. E.; Cardoso, L. P.; Mansanares, A. M.; Gandra, F. G.</p> <p>2016-12-01</p> <p>We report on the magnetic properties and magnetocaloric effect (MCE) for the Tb3M series, with M=Co, Rh and Ru, obtained using a <span class="hlt">heat</span> <span class="hlt">flux</span> technique. The specific <span class="hlt">heat</span> of Tb3Co and Tb3Rh are very similar, with a first order type transition occurring around 6 K below the magnetic ordering temperature without any corresponding feature on the magnetization. The slightly enhanced <span class="hlt">electronic</span> specific <span class="hlt">heat</span>, the Debye temperature around 150 K and the presence of the magnetic specific <span class="hlt">heat</span> well above the ordering temperature are also characteristic of many other compounds of the R3M family (R=Rare Earth). The specific <span class="hlt">heat</span> for Tb3Ru, however, presents two peaks at 37 K and 74 K. The magnetization shows that below the first peak the system presents an antiferromagnetic behavior and is paramagnetic above 74 K. We obtained a magnetocaloric effect for M=Co and Rh, -∆S=12 J/kg K, but for Tb3Ru it is less than 3 J/kg K (μ0∆H=5 T). We believe that the experimental results show that the MCE is directly related with the process of hybridization of the (R)5d-(M)d <span class="hlt">electrons</span> that occurs in the R3M materials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/23962','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/23962"><span>A modified force-restore approach to modeling snow-surface <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Charles H. Luce; David G. Tarboton</p> <p>2001-01-01</p> <p>Accurate modeling of the energy balance of a snowpack requires good estimates of the snow surface temperature. The snow surface temperature allows a balance between atmospheric <span class="hlt">heat</span> <span class="hlt">fluxes</span> and the conductive <span class="hlt">flux</span> into the snowpack. While the dependency of atmospheric <span class="hlt">fluxes</span> on surface temperature is reasonably well understood and parameterized, conduction of <span class="hlt">heat</span> from...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980206267','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980206267"><span>Experimental Performance of a Micromachined <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stefanescu, S.; DeAnna, R. G.; Mehregany, M.</p> <p>1998-01-01</p> <p>Steady-state and frequency response calibration of a microfabricated <span class="hlt">heat-flux</span> sensor have been completed. This sensor is batch fabricated using standard, micromachining techniques, allowing both miniaturization and the ability to create arrays of sensors and their corresponding interconnects. Both <span class="hlt">high</span>-frequency and spatial response is desired, so the sensors are both thin and of small cross-sectional area. Thin-film, temperature-sensitive resistors are used as the active gauge elements. Two sensor configurations are investigated: (1) a Wheatstone-bridge using four resistors; and (2) a simple, two-resistor design. In each design, one resistor (or pair) is covered by a thin layer (5000 A) thermal barrier; the other resistor (or pair) is covered by a thick (5 microns) thermal barrier. The active area of a single resistor is 360 microns by 360 microns; the total gauge area is 1.5 mm square. The resistors are made of 2000 A-thick metal; and the entire gauge is fabricated on a 25 microns-thick flexible, polyimide substrate. <span class="hlt">Heat</span> <span class="hlt">flux</span> through the surface changes the temperature of the resistors and produces a corresponding change in resistance. Sensors were calibrated using two radiation <span class="hlt">heat</span> sources: (1) a furnace for steady-state, and (2) a light and chopper for frequency response.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2002mwoc.conf...39M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2002mwoc.conf...39M"><span>Contagious Coronal <span class="hlt">Heating</span> from Recurring Emergence of Magnetic <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Moore, R. L.; Falconer, D. A.; Sterling, A. C.</p> <p>2002-01-01</p> <p>For each of six old bipolar active regions, we present and interpret Yohkoh/SXT and SOHO/MDI observations of the development, over several days, of enhanced coronal <span class="hlt">heating</span> in and around the old bipole in response to new magnetic <span class="hlt">flux</span> emergence within the old bipole. The observations show: 1. In each active region, new <span class="hlt">flux</span> emerges in the equatorward side of the old bipole, around a lone remaining leading sunspot and/or on the equatorward end of the neutral line of the old bipole. 2. The emerging field is marked by intense internal coronal <span class="hlt">heating</span>, and enhanced coronal <span class="hlt">heating</span> occurs in extended loops stemming from the emergence site. 3. In five of the six cases, a "rooster tail" of coronal loops in the poleward extent of the old bipole also brightens in response to the <span class="hlt">flux</span> emergence. 4. There are episodes of enhanced coronal <span class="hlt">heating</span> in surrounding magnetic fields that are contiguous with the old bipole but are not directly connected to the emerging field. From these observations, we suggest that the accommodation of localized newly emerged <span class="hlt">flux</span> within an old active region entails far reaching adjustments in the 3D magnetic field throughout the active region and in surrounding fields in which the active region is embedded, and that these adjustments produce the extensive enhanced coronal <span class="hlt">heating</span>. We Also Note That The Reason For The recurrence of <span class="hlt">flux</span> emergence in old active regions may be that active-region <span class="hlt">flux</span> tends to emerge in giant-cell convection downflows. If so, the poleward "rooster tail" is a coronal flag of a long-lasting downflow in the convection zone. This work was funded by NASA's Office of Space Science through the Solar Physics Supporting Research and Technology Program and the Sun-Earth Connection Guest Investigator Program.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20020022350&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DMagnetic%2BFlux','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20020022350&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DMagnetic%2BFlux"><span>Contagious Coronal <span class="hlt">Heating</span> from Recurring Emergence of Magnetic <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moore, Ronald L.; Falconer, David; Sterling, Alphonse; Whitaker, Ann F. (Technical Monitor)</p> <p>2001-01-01</p> <p>For each of six old bipolar active regions, we present and interpret Yohkoh/SXT and SOHO/MDI observations of the development, over several days, of enhanced coronal <span class="hlt">heating</span> in and around the old bipole in response to new magnetic <span class="hlt">flux</span> emerge= within the old bipole. The observations show: 1. In each active region, new <span class="hlt">flux</span> emerges in the equatorward side of the old bipole, around a lone remaining leading sunspot and/or on the equatorward end of the neutral line of the old bipole. 2. The emerging field is marked by intense internal coronal <span class="hlt">heating</span>, and enhanced coronal <span class="hlt">heating</span> occurs in extended loops stemming from the emergence site. 3. In five of the six cases, a "rooster tail" of coronal loops in the poleward extent of the old bipole also brightens in response to the <span class="hlt">flux</span> emergence. 4. There are episodes of enhanced coronal <span class="hlt">heating</span> in surrounding magnetic fields that are contiguous with the old bipole but are not directly connected to the emerging field. From these observations, we suggest that the accommodation of localized newly emerged <span class="hlt">flux</span> within an old active region entails far reaching adjustments in the 3D magnetic field throughout the active region and in surrounding fields in which the active region is embedded, and that these adjustments produce the extensive enhanced coronal <span class="hlt">heating</span>. We also note that the reason for the recurrence of <span class="hlt">flux</span> emergence in old active regions may be that active region <span class="hlt">flux</span> tends to emerge in giant-cell convection downflows. If so, the poleward "rooster tail" is a coronal flag of a long-lasting downflow in the convection zone. This work was funded by NASA's Office of Space Science through the Solar Physics Supporting Research and Technology Program and the Sun-Earth Connection Guest Investigator Program.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016cosp...41E1885T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016cosp...41E1885T"><span>Ion and <span class="hlt">Electron</span> <span class="hlt">Heating</span> Characteristics of Magnetic Re- Connection in Mast Tokamak Merging Experiment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tanabe, Hiroshi; Inomoto, Michiaki; Ono, Yasushi; Yamada, Takuma; Imazawa, Ryota; Cheng, Chio-Zong</p> <p>2016-07-01</p> <p>We present results of recent studies of <span class="hlt">high</span> power <span class="hlt">heating</span> of magnetic reconnection, the fundamental process of several astrophysical events such as solar flare, in the Mega Amp Spherical Tokamak (MAST) - the world largest merging experiment. In addition to the previously reported significant reconnection <span class="hlt">heating</span> up to ˜1keV [1], detailed local profiles of <span class="hlt">electron</span> and ion temperature have been measured using a ultra-fine 300 channel Ruby- and a 130 channel YAG-Thomson scattering and a new 32 channel ion Doppler tomography diagnostics [2]. 2D profile measurement of <span class="hlt">electron</span> temperature revealed <span class="hlt">highly</span> localized <span class="hlt">heating</span> structure at the X point with the characteristic scale length of 0.02-0.05m<c/ω_{pi}, while the ion temperature increases in the downstream region of outflow jet with the width of c/ω_{pi}˜0.1m [3]. For the push merging experiment under <span class="hlt">high</span> guide field condition (B_t>0.3T), a thick layer of closed <span class="hlt">flux</span> surface surrounding the current sheet sustains the temperature profile for longer time than the <span class="hlt">electron</span> and ion energy relaxation time ˜4-10ms, finally forming triple peak structures of ion and <span class="hlt">electron</span> temperatures at the X point and in the downstream. While the peak <span class="hlt">electron</span> temperature at the X point increases with toroidal field, the bulk <span class="hlt">electron</span> temperature and the ion temperature in the downstream are unaffected. [1] Y. Ono et.al., Plasma Phys. Control. Fusion 54, 124039 (2012) [2] H. Tanabe et. al., Nucl. Fusion 53, 093027 (2013). [3] H. Tanabe et.al., Phys. Rev. Lett. 115, 215004 (2015)</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_16 --> <div id="page_17" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="321"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSA43B2648L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSA43B2648L"><span>Ionospheric <span class="hlt">electron</span> <span class="hlt">heating</span> associated with pulsating auroras: joint optical and PFISR observations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liang, J.; Donovan, E.; Spanswick, E.; Reimer, A.; Hampton, D. L.; Varney, R. H.</p> <p>2017-12-01</p> <p>In a recent survey based upon Swarm satellite data, Liang et al. [2017] repeatedly identified a strong <span class="hlt">electron</span> temperature (Te) enhancement associated with the pulsating aurora at Swarm altitudes ( 460 km). The observation of Te enhancement is not contingent upon whether the pulsating patch is "on" or "off" at the satellite traversal epoch. In this study, we use joint optical and Poker Flat Incoherent Scatter Radar (PFISR) observations to further investigate the 4D (space-time) variations of the Te enhancement in association with the pulsating aurora. In a long-lasting pulsating auroral event on 19 March 2015, we identify strong Te enhancements ( 600-1200 K) in the upper F-region ionosphere ( 300-600 km altitude) in conjunction to the passage of pulsating auroras over PFISR beams. The spatial-temporal variations of PFISR Te enhancement are found to generally conform to the variations of pulsating auroras. However, collocated meridian spectrograph observations suggest that the pulsating auroras of interest are composed of energetic <span class="hlt">electron</span> precipitation with characteristic energy ≥10 keV, which is not supposed to be efficient in <span class="hlt">heating</span> <span class="hlt">electrons</span> in the upper F-region. On the other hand, only moderate (<27%) Ne enhancements are found in the upper F-region during the pulsating aurora and Te enhancement interval. There are also moderate Te enhancements ( 100 K) in the E-region accompanying the pulsating auroras, but no clue of Te enhancement is found in the lower F-region. Based upon the above observations and simulations using the model developed in Liang et al. [2017], we propose that thermal conduction from the topside ionosphere, led by magnetospheric <span class="hlt">heat</span> <span class="hlt">fluxes</span>, constitutes the most likely underlying mechanism for the upper F-region <span class="hlt">electron</span> <span class="hlt">heating</span> associated with pulsating auroras. Such magnetospheric <span class="hlt">heat</span> <span class="hlt">fluxes</span> may be pertinent to one long-hypothesized feature of pulsating auroras, namely the existence of an enhanced low-energy plasma population in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19780002468','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19780002468"><span>Study of a <span class="hlt">high</span> performance evaporative <span class="hlt">heat</span> transfer surface</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Saaski, E. W.; Hamasaki, R. H.</p> <p>1977-01-01</p> <p>An evaporative surface is described for <span class="hlt">heat</span> pipes and other two-phase <span class="hlt">heat</span> transfer applications that consists of a hybrid composition of V-grooves and capillary wicking. Characteristics of the surface include both a <span class="hlt">high</span> <span class="hlt">heat</span> transfer coefficient and <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> capability relative to conventional open-faced screw thread surfaces. With a groove density of 12.6 cm/1 and ammonia working fluid, <span class="hlt">heat</span> transfer coefficients in the range of 1 to 2 W/sq cm have been measured along with maximum <span class="hlt">heat</span> <span class="hlt">flux</span> densities in excess of 20 W/sq cm. A peak <span class="hlt">heat</span> transfer coefficient in excess of 2.3 W/sq cm was measured with a 37.8 cm/1 hybrid surface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24360191','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24360191"><span>Assessment of land surface temperature and <span class="hlt">heat</span> <span class="hlt">fluxes</span> over Delhi using remote sensing data.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chakraborty, Surya Deb; Kant, Yogesh; Mitra, Debashis</p> <p>2015-01-15</p> <p>Surface energy processes has an essential role in urban weather, climate and hydrosphere cycles, as well in urban <span class="hlt">heat</span> redistribution. The research was undertaken to analyze the potential of Landsat and MODIS data in retrieving biophysical parameters in estimating land surface temperature & <span class="hlt">heat</span> <span class="hlt">fluxes</span> diurnally in summer and winter seasons of years 2000 and 2010 and understanding its effect on anthropogenic <span class="hlt">heat</span> disturbance over Delhi and surrounding region. Results show that during years 2000-2010, settlement and industrial area increased from 5.66 to 11.74% and 4.92 to 11.87% respectively which in turn has direct effect on land surface temperature (LST) and <span class="hlt">heat</span> <span class="hlt">fluxes</span> including anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span>. Based on the energy balance model for land surface, a method to estimate the increase in anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> (Has) has been proposed. The settlement and industrial areas has higher amounts of energy consumed and has <span class="hlt">high</span> values of Has in all seasons. The comparison of satellite derived LST with that of field measured values show that Landsat estimated values are in close agreement within error of ±2 °C than MODIS with an error of ±3 °C. It was observed that, during 2000 and 2010, the average change in surface temperature using Landsat over settlement & industrial areas of both seasons is 1.4 °C & for MODIS data is 3.7 °C. The seasonal average change in anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> (Has) estimated using Landsat & MODIS is up by around 38 W/m(2) and 62 W/m(2) respectively while higher change is observed over settlement and concrete structures. The study reveals that the dynamic range of Has values has increased in the 10 year period due to the strong anthropogenic influence over the area. The study showed that anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> is an indicator of the strength of urban <span class="hlt">heat</span> island effect, and can be used to quantify the magnitude of the urban <span class="hlt">heat</span> island effect. Copyright © 2013 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NucFu..57i2007L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NucFu..57i2007L"><span>Development of advanced <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> and plasma-facing materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Linsmeier, Ch.; Rieth, M.; Aktaa, J.; Chikada, T.; Hoffmann, A.; Hoffmann, J.; Houben, A.; Kurishita, H.; Jin, X.; Li, M.; Litnovsky, A.; Matsuo, S.; von Müller, A.; Nikolic, V.; Palacios, T.; Pippan, R.; Qu, D.; Reiser, J.; Riesch, J.; Shikama, T.; Stieglitz, R.; Weber, T.; Wurster, S.; You, J.-H.; Zhou, Z.</p> <p>2017-09-01</p> <p>Plasma-facing materials and components in a fusion reactor are the interface between the plasma and the material part. The operational conditions in this environment are probably the most challenging parameters for any material: <span class="hlt">high</span> power loads and large particle and neutron <span class="hlt">fluxes</span> are simultaneously impinging at their surfaces. To realize fusion in a tokamak or stellarator reactor, given the proven geometries and technological solutions, requires an improvement of the thermo-mechanical capabilities of currently available materials. In its first part this article describes the requirements and needs for new, advanced materials for the plasma-facing components. Starting points are capabilities and limitations of tungsten-based alloys and structurally stabilized materials. Furthermore, material requirements from the fusion-specific loading scenarios of a divertor in a water-cooled configuration are described, defining directions for the material development. Finally, safety requirements for a fusion reactor with its specific accident scenarios and their potential environmental impact lead to the definition of inherently passive materials, avoiding release of radioactive material through intrinsic material properties. The second part of this article demonstrates current material development lines answering the fusion-specific requirements for <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> materials. New composite materials, in particular fiber-reinforced and laminated structures, as well as mechanically alloyed tungsten materials, allow the extension of the thermo-mechanical operation space towards regions of extreme steady-state and transient loads. Self-passivating tungsten alloys, demonstrating favorable tungsten-like plasma-wall interaction behavior under normal operation conditions, are an intrinsic solution to otherwise catastrophic consequences of loss-of-coolant and air ingress events in a fusion reactor. Permeation barrier layers avoid the escape of tritium into structural and cooling</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..GECSF1002S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..GECSF1002S"><span><span class="hlt">Electron</span> <span class="hlt">heating</span> and the Electrical Asymmetry Effect in capacitively coupled RF discharges</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schulze, Julian</p> <p>2011-10-01</p> <p>For applications of capacitive radio frequency discharges, the control of particle distribution functions at the substrate surface is essential. Their spatio-temporal shape is the result of complex <span class="hlt">heating</span> mechanisms of the respective species. Enhanced process control, therefore, requires a detailed understanding of the <span class="hlt">heating</span> dynamics. There are two known modes of discharge operation: α- and γ-mode. In α-mode, most ionization is caused by <span class="hlt">electron</span> beams generated by the expanding sheaths and field reversals during sheath collapse, while in γ-mode secondary <span class="hlt">electrons</span> dominate the ionisation. In strongly electronegative discharges, a third <span class="hlt">heating</span> mode is observed. Due to the low <span class="hlt">electron</span> density in the discharge center the bulk conductivity is reduced and a <span class="hlt">high</span> electric field is generated to drive the RF current through the discharge center. In this field, <span class="hlt">electrons</span> are accelerated and cause significant ionisation in the bulk. This bulk <span class="hlt">heating</span> mode is observed experimentally and by PIC simulations in CF4 discharges. The <span class="hlt">electron</span> dynamics and mode transitions as a function of driving voltage and pressure are discussed. Based on a detailed understanding of the <span class="hlt">heating</span> dynamics, the concept of separate control of the ion mean energy and <span class="hlt">flux</span> in classical dual-frequency discharges is demonstrated to fail under process relevant conditions. To overcome these limitations of process control, the Electrical Asymmetry Effect (EAE) is proposed in discharges driven at multiple consecutive harmonics with adjustable phase shifts between the driving frequencies. Its concept and a recipe to optimize the driving voltage waveform are introduced. The functionality of the EAE in different gases and first applications to large area solar cell manufacturing are discussed. Finally, limitations caused by the bulk <span class="hlt">heating</span> in strongly electronegative discharges are outlined.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22600185-study-heat-flux-disruption-experimental-advanced-superconducting-tokamak','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22600185-study-heat-flux-disruption-experimental-advanced-superconducting-tokamak"><span>The study of <span class="hlt">heat</span> <span class="hlt">flux</span> for disruption on experimental advanced superconducting tokamak</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Yang, Zhendong, E-mail: dongyz@ipp.ac.cn, E-mail: jafang@dhu.edu.cn; Institute of Plasma Physics, Chinese Academy of Sciences, Hefei 230031; Fang, Jianan, E-mail: dongyz@ipp.ac.cn, E-mail: jafang@dhu.edu.cn</p> <p></p> <p>Disruption of the plasma is one of the most dangerous instabilities in tokamak. During the disruption, most of the plasma thermal energy is lost, which causes damages to the plasma facing components. Infrared (IR) camera is an effective tool to detect the temperature distribution on the first wall, and the energy deposited on the first wall can be calculated from the surface temperature profile measured by the IR camera. This paper concentrates on the characteristics of <span class="hlt">heat</span> <span class="hlt">flux</span> distribution onto the first wall under different disruptions, including the minor disruption and the vertical displacement events (VDE) disruption. Several minor disruptionsmore » have been observed before the major disruption under the <span class="hlt">high</span> plasma density in experimental advanced superconducting tokamak. During the minor disruption, the <span class="hlt">heat</span> <span class="hlt">fluxes</span> are mainly deposited on the upper/lower divertors. The magnetic configuration prior to the minor disruption is a lower single null with the radial distance between the two separatrices in the outer midplane dR{sub sep} = −2 cm, while it changes to upper single null (dR{sub sep} = 1.4 cm) during the minor disruption. As for the VDE disruption, the spatial distribution of <span class="hlt">heat</span> <span class="hlt">flux</span> exhibits strong toroidal and radial nonuniformity, and the maximum <span class="hlt">heat</span> <span class="hlt">flux</span> received on the dome plate can be up to 11 MW/m{sup 2}.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/863787','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/863787"><span>Device and method for relativistic <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span>-density plasma to drive fast liners</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Thode, Lester E.</p> <p>1981-01-01</p> <p>A device and method for relativistic <span class="hlt">electron</span> beam <span class="hlt">heating</span> of a <span class="hlt">high</span>-density plasma in a small localized region. A relativistic <span class="hlt">electron</span> beam generator or accelerator produces a <span class="hlt">high</span>-voltage <span class="hlt">electron</span> beam which propagates along a vacuum drift tube and is modulated to initiate <span class="hlt">electron</span> bunching within the beam. The beam is then directed through a low-density gas chamber which provides isolation between the vacuum modulator and the relativistic <span class="hlt">electron</span> beam target. The relativistic beam is then applied to a <span class="hlt">high</span>-density target plasma which typically comprises DT, DD, hydrogen boron or similar thermonuclear gas at a density of 10.sup.17 to 10.sup.20 <span class="hlt">electrons</span> per cubic centimeter. The target gas is ionized prior to application of the <span class="hlt">electron</span> beam by means of a laser or other preionization source to form a plasma. Utilizing a relativistic <span class="hlt">electron</span> beam with an individual particle energy exceeding 3 MeV, classical scattering by relativistic <span class="hlt">electrons</span> passing through isolation foils is negligible. As a result, relativistic streaming instabilities are initiated within the <span class="hlt">high</span>-density target plasma causing the relativistic <span class="hlt">electron</span> beam to efficiently deposit its energy and momentum into a small localized region of the <span class="hlt">high</span>-density plasma target. Fast liners disposed in the <span class="hlt">high</span>-density target plasma are explosively or ablatively driven to implosion by a <span class="hlt">heated</span> annular plasma surrounding the fast liner which is generated by an annular relativistic <span class="hlt">electron</span> beam. An azimuthal magnetic field produced by axial current flow in the annular plasma, causes the energy in the <span class="hlt">heated</span> annular plasma to converge on the fast liner.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860002759','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860002759"><span>Turbine blade and vane <span class="hlt">heat</span> <span class="hlt">flux</span> sensor development, phase 2</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Atkinson, W. H.; Cyr, M. A.; Strange, R. R.</p> <p>1985-01-01</p> <p>The development of <span class="hlt">heat</span> <span class="hlt">flux</span> sensors for gas turbine blades and vanes and the demonstration of <span class="hlt">heat</span> transfer measurement methods are reported. The performance of the <span class="hlt">heat</span> <span class="hlt">flux</span> sensors was evaluated in a cylinder in cross flow experiment and compared with two other <span class="hlt">heat</span> <span class="hlt">flux</span> measurement methods, the slug calorimeter and a dynamic method based on fluctuating gas and surface temperature. Two cylinders, each instrumented with an embedded thermocouple sensor, a Gardon gauge, and a slug calorimeter, were fabricated. Each sensor type was calibrated using a quartz lamp bank facility. The instrumented cylinders were then tested in an atmospheric pressure combustor rig at conditions up to gas stream temperatures of 1700K and velocities to Mach 0.74. The test data are compared to other measurements and analytical prediction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC21D0970Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC21D0970Z"><span>Two-wavelength Method Estimates <span class="hlt">Heat</span> <span class="hlt">fluxes</span> over Heterogeneous Surface in North-China</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, G.; Zheng, N.; Zhang, J.</p> <p>2017-12-01</p> <p><span class="hlt">Heat</span> <span class="hlt">fluxes</span> is a key process of hydrological and <span class="hlt">heat</span> transfer of soil-plant-atmosphere continuum (SPAC), and now it is becoming an important topic in meteorology, hydrology, ecology and other related research areas. Because the temporal and spatial variation of <span class="hlt">fluxes</span> at regional scale is very complicated, it is still difficult to measure <span class="hlt">fluxes</span> at the kilometer scale over a heterogeneous surface. A technique called "two-wavelength method" which combines optical scintillometer with microwave scintillometer is able to measure both sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> over large spatial scales at the same time. The main purpose of this study is to investigate the <span class="hlt">fluxes</span> over non-uniform terrain in North-China. Estimation of <span class="hlt">heat</span> <span class="hlt">fluxes</span> was carried out with the optical-microwave scintillometer and an eddy covariance (EC) system over heterogeneous surface in Tai Hang Mountains, China. EC method was set as a benchmark in the study. Structure parameters obtained from scintillometer showed that the typical measurement values of Cn2 are around 10-13 m-2/3 for microwave scintillometer, and values of Cn2 were around 10-15 m-2/3 for optical scintillometer. The correlation of <span class="hlt">heat</span> <span class="hlt">fluxes</span> (H) derived from scintillometer and EC system showed as a ratio of 1.05,and with R2=0.75, while the correlation of latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> (LE) showed as 1.29 with R2=0.67. It was also found that <span class="hlt">heat</span> <span class="hlt">fluxes</span> derived from the two system showed good agreement (R2=0.9 for LE, R2=0.97 for H) when the Bowen ratio (β) was 1.03, while discrepancies showed significantly when β=0.75, and RMSD in H was 139.22 W/m2, 230.85 W/m2 in LE respectively.Experiment results in our research shows that, the two-wavelength method gives a larger <span class="hlt">heat</span> <span class="hlt">fluxes</span> over the study area, and a deeper study should be conduct. We expect that our investigate and analysis can be promoted the application of scintillometry method in regional evapotranspiration measurements and relevant disciplines.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930036590&hterms=carbon+footprint&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcarbon%2Bfootprint','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930036590&hterms=carbon+footprint&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcarbon%2Bfootprint"><span>Aircraft- and tower-based <span class="hlt">fluxes</span> of carbon dioxide, latent, and sensible <span class="hlt">heat</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Desjardins, R. L.; Hart, R. L.; Macpherson, J. I.; Schuepp, P. H.; Verma, S. B.</p> <p>1992-01-01</p> <p><span class="hlt">Fluxes</span> of carbon dioxide, water vapor, and sensible <span class="hlt">heat</span> obtained over a grassland ecosystem, during the First International Satellite Land Surface Climatology Project (ISLSCP) Field Experiment (FIFE), using an aircraft- and two tower-based systems are compared for several days in 1987 and in 1989. The tower-based cospectral estimates of CO2, sensible <span class="hlt">heat</span>, water vapor, and momentum, expressed as a function of wavenumber K times sampling height z, are relatively similar to the aircraft-based estimates for K x z greater than 0.1. A measurable contribution to the <span class="hlt">fluxes</span> is observed by tower-based systems at K x z less than 0.01 but not by the aircraft-based system operating at an altitude of approximately 100 m over a 15 x 15 km area. Using all available simultaneous aircraft and tower data, <span class="hlt">flux</span> estimates by both systems were shown to be <span class="hlt">highly</span> correlated. As expected from the spatial variations of the greenness index, surface extrapolation of airborne <span class="hlt">flux</span> estimates tended to lie between those of the two tower sites. The average <span class="hlt">fluxes</span> obtained, on July 11, 1987, and August 4, 1989, by flying a grid pattern over the FIFE site agreed with the two tower data sets for CO2, but sensible and latent <span class="hlt">heat</span> were smaller than those obtained by the tower-based systems. However, in general, except for a small underestimation due to the long wavelength contributions and due to <span class="hlt">flux</span> divergence with height, the differences between the aircraft- and tower-based surface estimates of <span class="hlt">fluxes</span> appear to be mainly attributable to differences in footprint, that is, differences in the area contributing to the surface <span class="hlt">flux</span> estimates.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1374055-effect-electron-cyclotron-heating-density-fluctuations-ion-electron-scales-iter-baseline-scenario-discharges-diii-tokamak','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1374055-effect-electron-cyclotron-heating-density-fluctuations-ion-electron-scales-iter-baseline-scenario-discharges-diii-tokamak"><span>The effect of <span class="hlt">Electron</span> Cyclotron <span class="hlt">Heating</span> on density fluctuations at ion and <span class="hlt">electron</span> scales in ITER Baseline Scenario discharges on the DIII-D tokamak</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Marinoni, Alessandro; Pinsker, Robert I.; Porkolab, Miklos; ...</p> <p>2017-08-01</p> <p>Experiments simulating the ITER Baseline Scenario on the DIII-D tokamak show that torque-free pure <span class="hlt">electron</span> <span class="hlt">heating</span>, when coupled to plasmas subject to a net co-current beam torque, affects density fluctuations at <span class="hlt">electron</span> scales on a sub-confinement time scale, whereas fluctuations at ion scales change only after profiles have evolved to a new stationary state. Modifications to the density fluctuations measured by the Phase Contrast Imaging diagnostic (PCI) are assessed by analyzing the time evolution following the switch-off of <span class="hlt">Electron</span> Cyclotron <span class="hlt">Heating</span> (ECH), thus going from mixed beam/ECH to pure neutral beam <span class="hlt">heating</span> at fixed β N . Within 20 msmore » after turning off ECH, the intensity of fluctuations is observed to increase at frequencies higher than 200 kHz; in contrast, fluctuations at lower frequency are seen to decrease in intensity on a longer time scale, after other equilibrium quantities have evolved. Non-linear gyro-kinetic modeling at ion and <span class="hlt">electron</span> scales scales suggest that, while the low frequency response of the diagnostic is consistent with the dominant ITG modes being weakened by the slow-time increase in flow shear, the <span class="hlt">high</span> frequency response is due to prompt changes to the <span class="hlt">electron</span> temperature profile that enhance <span class="hlt">electron</span> modes and generate a larger <span class="hlt">heat</span> <span class="hlt">flux</span> and an inward particle pinch. Furthermore, these results suggest that <span class="hlt">electron</span> <span class="hlt">heated</span> regimes in ITER will feature multi-scale fluctuations that might affect fusion performance via modifications to profiles.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NucFu..57l6014M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NucFu..57l6014M"><span>The effect of <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> on density fluctuations at ion and <span class="hlt">electron</span> scales in ITER baseline scenario discharges on the DIII-D tokamak</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Marinoni, A.; Pinsker, R. I.; Porkolab, M.; Rost, J. C.; Davis, E. M.; Burrell, K. H.; Candy, J.; Staebler, G. M.; Grierson, B. A.; McKee, G. R.; Rhodes, T. L.; The DIII-D Team</p> <p>2017-12-01</p> <p>Experiments simulating the ITER baseline scenario on the DIII-D tokamak show that torque-free pure <span class="hlt">electron</span> <span class="hlt">heating</span>, when coupled to plasmas subject to a net co-current beam torque, affects density fluctuations at <span class="hlt">electron</span> scales on a sub-confinement time scale, whereas fluctuations at ion scales change only after profiles have evolved to a new stationary state. Modifications to the density fluctuations measured by the phase contrast imaging diagnostic (PCI) are assessed by analyzing the time evolution following the switch-off of <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> (ECH), thus going from mixed beam/ECH to pure neutral beam <span class="hlt">heating</span> at fixed βN . Within 20 ms after turning off ECH, the intensity of fluctuations is observed to increase at frequencies higher than 200 kHz in contrast, fluctuations at lower frequency are seen to decrease in intensity on a longer time scale, after other equilibrium quantities have evolved. Non-linear gyro-kinetic modeling at ion and <span class="hlt">electron</span> scales scales suggest that, while the low frequency response of the diagnostic is consistent with the dominant ITG modes being weakened by the slow-time increase in flow shear, the <span class="hlt">high</span> frequency response is due to prompt changes to the <span class="hlt">electron</span> temperature profile that enhance <span class="hlt">electron</span> modes and generate a larger <span class="hlt">heat</span> <span class="hlt">flux</span> and an inward particle pinch. These results suggest that <span class="hlt">electron</span> <span class="hlt">heated</span> regimes in ITER will feature multi-scale fluctuations that might affect fusion performance via modifications to profiles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EPJWC.15703047S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EPJWC.15703047S"><span>Extension of <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> at ASDEX Upgrade with respect to <span class="hlt">high</span> density operation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schubert, Martin; Stober, Jörg; Herrmann, Albrecht; Kasparek, Walter; Leuterer, Fritz; Monaco, Francesco; Petzold, Bernhard; Plaum, Burkhard; Vorbrugg, Stefan; Wagner, Dietmar; Zohm, Hartmut</p> <p>2017-10-01</p> <p>The ASDEX Upgrade <span class="hlt">electron</span> cyclotron resonance <span class="hlt">heating</span> operates at 105 GHz and 140 GHz with flexible launching geometry and polarization. In 2016 four Gyrotrons with 10 sec pulse length and output power close to 1 MW per unit were available. The system is presently being extended to eight similar units in total. <span class="hlt">High</span> <span class="hlt">heating</span> power and <span class="hlt">high</span> plasma density operation will be a part of the future ASDEX Upgrade experiment program. For the <span class="hlt">electron</span> cyclotron resonance <span class="hlt">heating</span>, an O-2 mode scheme is proposed, which is compatible with the expected <span class="hlt">high</span> plasma densities. It may, however, suffer from incomplete single-pass absorption. The situation can be improved significantly by installing holographic mirrors on the inner column, which allow for a second pass of the unabsorbed fraction of the millimetre wave beam. Since the beam path in the plasma is subject to refraction, the beam position on the holographic mirror has to be controlled. Thermocouples built into the mirror surface are used for this purpose. As a protective measure, the tiles of the <span class="hlt">heat</span> shield on the inner column were modified in order to increase the shielding against unabsorbed millimetre wave power.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19840052365&hterms=coke&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dcoke','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19840052365&hterms=coke&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dcoke"><span>Supercritical convection, critical <span class="hlt">heat</span> <span class="hlt">flux</span>, and coking characteristics of propane</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rousar, D. C.; Gross, R. S.; Boyd, W. C.</p> <p>1984-01-01</p> <p>The <span class="hlt">heat</span> transfer characteristics of propane at subcritical and supercritical pressure were experimentally evaluated using electrically <span class="hlt">heated</span> Monel K-500 tubes. A design correlation for supercritical <span class="hlt">heat</span> transfer coefficient was established using the approach previously applied to supercritical oxygen. Flow oscillations were observed and the onset of these oscillations at supercritical pressures was correlated with wall-to-bulk temperature ratio and velocity. The critical <span class="hlt">heat</span> <span class="hlt">flux</span> measured at subcritical pressure was correlated with the product of velocity and subcooling. Long duration tests at fixed <span class="hlt">heat</span> <span class="hlt">flux</span> conditions were conducted to evaluate coking on the coolant side tube wall and coking rates comparable to RP-1 were observed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010EGUGA..12.7262B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010EGUGA..12.7262B"><span>Anthropogenic <span class="hlt">heat</span> <span class="hlt">fluxes</span> over Moscow agglomeration and other Russian and world cities</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Belova, Iya; Ginzburg, Alexander</p> <p>2010-05-01</p> <p>Urbanization, particularly with respect to its sustainability, remains to be a great challenge in all regions of the world. Urbanization has an influence on soils, hydrology, and climate, these changes have effect on global climate, pollution, increase of anthropogenic greenhouse gases in the earth's atmosphere and human health. Thus anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> is an important factor for estimation of development of global climate. The simple formula for anthropogenic <span class="hlt">heat</span> <span class="hlt">fluxes</span> (AHF) was proposed in the EGU General Assembly 2008 presentation [1] AHF = k × PD × EC, were PD is urban population density and EC is total energy consumption per capita. It was estimated that two of the world megacities - Seoul and Moscow - have the highest AHF values - 83 and 56 W/m2 correspondently. In presented paper it was studied the reasons of such <span class="hlt">high</span> anthropogenic <span class="hlt">heat</span> <span class="hlt">fluxes</span> within Moscow region as well as AHF over the major Russian cities. It was shown that main reason of this circumstance is the administrative divisions in Moscow region. Moscow is ringed by Moscow circle motor road. Accordingly the city has sharply defined boundaries and densely populated residential suburbs are cut off and don't included in Moscow city administrative area. It was constructed the special graph to illuminate why Moscow city has such a <span class="hlt">high</span> anthropogenic <span class="hlt">heat</span> factor and how much Moscow agglomeration AHF could be if consider not only Moscow city itself but also the nearest suburb towns. Using the data from World Bank [2] and Russian governmental statistic agency [3] anthropogenic <span class="hlt">heat</span> <span class="hlt">fluxes</span> for Russian cities with population more than 500 000 were estimated. Energy consumption data for different Russian regions were calculated by special routine using in the Web-atlas [4]. This research is supported by RAS Fundamental Research Project 'Influence of anthropogenic <span class="hlt">heat</span> <span class="hlt">fluxes</span> and aerosol pollution on <span class="hlt">heat</span> balance and climate of urbanized areas'. Other results of this project is presented in paper [5</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19800057302&hterms=Hartl&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DHartl','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19800057302&hterms=Hartl&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DHartl"><span>A <span class="hlt">high</span> performance cocurrent-flow <span class="hlt">heat</span> pipe for <span class="hlt">heat</span> recovery applications</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Saaski, E. W.; Hartl, J. C.</p> <p>1980-01-01</p> <p>By the introduction of a plate-and-tube separator assembly into a <span class="hlt">heat</span> pipe vapor core, it has been demonstrated that axial transport capacity in reflux mode can be improved by up to a factor of 10. This improvement is largely the result of eliminating the countercurrent shear that commonly limits reflux <span class="hlt">heat</span> pipe axial capacity. With benzene, axial <span class="hlt">heat</span> <span class="hlt">fluxes</span> up to 1800 W/sq cm were obtained in the temperature range 40 to 80 C, while <span class="hlt">heat</span> <span class="hlt">flux</span> densities up to 3000 W/sq cm were obtained with R-11 over the temperature range 40 to 80 C. These very <span class="hlt">high</span> axial capacities compare favorably with liquid metal limits; the sonic limit for liquid sodium, for example, is 3000 W/sq cm at 657 C. Computational models developed for these cocurrent flow <span class="hlt">heat</span> pipes agreed with experimental data within + or - 25%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15644358','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15644358"><span>Development of a <span class="hlt">high</span>-performance boiling <span class="hlt">heat</span> exchanger by improved liquid supply to narrow channels.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ohta, Haruhiko; Ohno, Toshiyuki; Hioki, Fumiaki; Shinmoto, Yasuhisa</p> <p>2004-11-01</p> <p>A two-phase flow loop is a promising method for application to thermal management systems for large-scale space platforms handling large amounts of energy. Boiling <span class="hlt">heat</span> transfer reduces the size and weight of cold plates. The transportation of latent <span class="hlt">heat</span> reduces the mass flow rate of working fluid and pump power. To develop compact <span class="hlt">heat</span> exchangers for the removal of waste <span class="hlt">heat</span> from <span class="hlt">electronic</span> devices with <span class="hlt">high</span> <span class="hlt">heat</span> generation density, experiments on a method to increase the critical <span class="hlt">heat</span> <span class="hlt">flux</span> for a narrow <span class="hlt">heated</span> channel between parallel <span class="hlt">heated</span> and unheated plates were conducted. Fine grooves are machined on the <span class="hlt">heating</span> surface in a transverse direction to the flow and liquid is supplied underneath flattened bubbles by the capillary pressure difference from auxiliary liquid channels separated by porous metal plates from the main <span class="hlt">heated</span> channel. The critical <span class="hlt">heat</span> <span class="hlt">flux</span> values for the present <span class="hlt">heated</span> channel structure are more than twice those for a flat surface at gap sizes 2 mm and 0.7 mm. The validity of the present structure with auxiliary liquid channels is confirmed by experiments in which the liquid supply to the grooves is interrupted. The increment in the critical <span class="hlt">heat</span> <span class="hlt">flux</span> compared to those for a flat surface takes a maximum value at a certain flow rate of liquid supply to the <span class="hlt">heated</span> channel. The increment is expected to become larger when the length of the <span class="hlt">heated</span> channel is increased and/or the gravity level is reduced.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMSH11B2227Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMSH11B2227Y"><span>The association of spacecraft anomalies with <span class="hlt">electron</span>/proton particle <span class="hlt">fluxes</span> at different orbits</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yi, K.; Moon, Y. J.</p> <p>2016-12-01</p> <p>In this study, we investigate 195 satellite anomaly data from 1998 to 2010 from Satellite News Digest (SND) to understand the association between spacecraft anomaly and space weather condition. The spacecraft anomalies are classified into Attitude & Propulsion, Power, Control, Telemetry, Instrument and unknown. For the investigation we divide these data according to the spacecraft orbit and launched year. Spacecraft's orbits are classified into the following two groups : (1) <span class="hlt">high</span> altitude and low inclination, and (2) low altitude and <span class="hlt">high</span> inclination. Launched year of spacecraft are divided into two groups: 1991 1998 and 1999 2007. We examine the association between these anomaly data and daily peak particle (<span class="hlt">electron</span> and proton) <span class="hlt">flux</span> data from GOES as well as their occurrence rates. To determine the association, we use two criteria that <span class="hlt">electron</span> criterion is >10,000 pfu and proton criterion is >100 pfu. Main results from this study are as follows. First, the number of days satisfying the criteria for <span class="hlt">electron</span> <span class="hlt">flux</span> has a peak near a week before the anomaly day and decreases from the peak day to the anomaly day, while that for proton <span class="hlt">flux</span> has a peak near the anomaly day. Second, we found a similar pattern for the mean daily peak particle (<span class="hlt">electron</span> and proton) <span class="hlt">flux</span> as a function of day before the anomaly day. Third, an examination of multiple spacecraft anomaly events, which are likely to occur by severe space weather effects, shows that anomalies mostly occur either when <span class="hlt">electron</span> <span class="hlt">fluxes</span> are in the declining stage, or when daily proton peak <span class="hlt">fluxes</span> are strongly enhanced. Fourth, the time delay between the anomaly day and the day having the highest daily peak <span class="hlt">electron</span> <span class="hlt">flux</span> for the recent launching period (1999-2007) is noticeably larger than those for the older periods, implying that the anomaly characteristics associated with <span class="hlt">electron</span> <span class="hlt">flux</span> change with time.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSM21A2575O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSM21A2575O"><span>Temporal Characteristics of <span class="hlt">Electron</span> <span class="hlt">Flux</span> Events at Geosynchronous Orbit</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Olson, D. K.; Larsen, B.; Henderson, M. G.</p> <p>2017-12-01</p> <p>Geosynchronous satellites such as the LANL-GEO fleet are exposed to hazardous conditions when they encounter regions of hot, intense plasma such as that from the plasma sheet. These conditions can lead to the build-up of charge on the surface of a spacecraft, with undesired, and often dangerous, side effects. Observation of <span class="hlt">electron</span> <span class="hlt">flux</span> levels at geosynchronous orbit (GEO) with multiple satellites provides a unique view of plasma sheet access to that region. <span class="hlt">Flux</span> "events", or periods when <span class="hlt">fluxes</span> are elevated continuously above the LANL-GEO spacecraft charging threshold, can be characterized by duration in two dimensions: a spatial dimension of local time, describing the duration of an event from the perspective of a single spacecraft, and a temporal dimension describing the duration in time in which <span class="hlt">high</span> energy plasma sheet particles have access to geosynchronous orbit. We examine the statistical properties of the temporal duration of 8 keV <span class="hlt">electron</span> <span class="hlt">flux</span> events at geosynchronous orbit over a twelve-year period. These results, coupled with the spatial duration characteristics, provide the key information needed to formulate a statistical model for forecasting the <span class="hlt">electron</span> <span class="hlt">flux</span> conditions at GEO that are correlated with LANL-GEO surface charging. Forecasting models are an essential component to understanding space weather and mitigating the dangers of surface charging on our satellites. We also examine the correlation of <span class="hlt">flux</span> event durations with solar wind parameters and geomagnetic indices, identifying the data needed to improve upon a statistical forecasting model</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AGUFM.C43A0587P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AGUFM.C43A0587P"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> variations over sea-ice observed at the coastal area of the Sejong Station, Antarctica</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Park, S.; Choi, T.; Kim, S.</p> <p>2012-12-01</p> <p>This study presents variations of sensible <span class="hlt">heat</span> <span class="hlt">flux</span> and latent <span class="hlt">heat</span> <span class="hlt">flux</span> over sea-ice observed in 2011 from the 10-m <span class="hlt">flux</span> tower located at the coast of the Sejong Station on King George Island, Antarctica. A period from June to November was divided into three parts: "Freezing", "Frozen", and "Melting" periods based on daily monitoring of sea state and hourly photos looking at the Marian Cove in front of the Sejong Station. The division of periods enabled us to look into the <span class="hlt">heat</span> <span class="hlt">flux</span> variations depending on the sea-ice conditions. Over freezing sea surface during the freezing period of late June, daily mean sensible <span class="hlt">heat</span> <span class="hlt">flux</span> was -11.9 Wm-2 and daily mean latent <span class="hlt">heat</span> <span class="hlt">flux</span> was +16.3 Wm-2. Over the frozen sea-ice, daily mean sensible <span class="hlt">heat</span> <span class="hlt">flux</span> was -10.4 Wm-2 while daily mean latent <span class="hlt">heat</span> <span class="hlt">flux</span> was +2.4 Wm-2. During the melting period of mid-October to early November, magnitudes of sensible <span class="hlt">heat</span> <span class="hlt">flux</span> increased to -14.2 Wm-2 and latent <span class="hlt">heat</span> <span class="hlt">flux</span> also increased to +13.5 Wm-2. In short, latent <span class="hlt">heat</span> <span class="hlt">flux</span> was usually upward over sea-ice most of the time while sensible <span class="hlt">heat</span> <span class="hlt">flux</span> was downward from atmosphere to sea-ice. Magnitudes of the <span class="hlt">fluxes</span> were small but increased when freezing or melting of sea-ice was occurring. Especially, latent <span class="hlt">heat</span> <span class="hlt">flux</span> increased five to six times compared to that of "frozen" period implying that early melting of sea-ice may cause five to six times larger supply of moisture to the atmosphere.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_17 --> <div id="page_18" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="341"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1130204-interaction-between-marine-boundary-layer-cellular-cloudiness-surface-heat-fluxes','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1130204-interaction-between-marine-boundary-layer-cellular-cloudiness-surface-heat-fluxes"><span>On the Interaction between Marine Boundary Layer Cellular Cloudiness and Surface <span class="hlt">Heat</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kazil, J.; Feingold, G.; Wang, Hailong</p> <p>2014-01-02</p> <p>The interaction between marine boundary layer cellular cloudiness and surface uxes of sensible and latent <span class="hlt">heat</span> is investigated. The investigation focuses on the non-precipitating closed-cell state and the precipitating open-cell state at low geostrophic wind speed. The Advanced Research WRF model is used to conduct cloud-system-resolving simulations with interactive surface <span class="hlt">fluxes</span> of sensible <span class="hlt">heat</span>, latent <span class="hlt">heat</span>, and of sea salt aerosol, and with a detailed representation of the interaction between aerosol particles and clouds. The mechanisms responsible for the temporal evolution and spatial distribution of the surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the closed- and open-cell state are investigated and explained. Itmore » is found that the horizontal spatial structure of the closed-cell state determines, by entrainment of dry free tropospheric air, the spatial distribution of surface air temperature and water vapor, and, to a lesser degree, of the surface sensible and latent <span class="hlt">heat</span> <span class="hlt">flux</span>. The synchronized dynamics of the the open-cell state drives oscillations in surface air temperature, water vapor, and in the surface <span class="hlt">fluxes</span> of sensible and latent <span class="hlt">heat</span>, and of sea salt aerosol. Open-cell cloud formation, cloud optical depth and liquid water path, and cloud and rain water path are identified as good predictors of the spatial distribution of surface air temperature and sensible <span class="hlt">heat</span> <span class="hlt">flux</span>, but not of surface water vapor and latent <span class="hlt">heat</span> <span class="hlt">flux</span>. It is shown that by enhancing the surface sensible <span class="hlt">heat</span> <span class="hlt">flux</span>, the open-cell state creates conditions by which it is maintained. While the open-cell state under consideration is not depleted in aerosol, and is insensitive to variations in sea-salt <span class="hlt">fluxes</span>, it also enhances the sea-salt <span class="hlt">flux</span> relative to the closed-cell state. In aerosol-depleted conditions, this enhancement may replenish the aerosol needed for cloud formation, and hence contribute to the perpetuation of the open-cell state as well. Spatial homogenization of the surface <span class="hlt">fluxes</span> is found</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007AGUSMSM53A..03K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007AGUSMSM53A..03K"><span>Observational constraints on relativistic <span class="hlt">electron</span> dynamics: temporal evolution of <span class="hlt">electron</span> spectra and <span class="hlt">flux</span> isotropization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kanekal, S. G.; Selesnick, R. S.; Baker, D. N.; Blake, J. B.</p> <p>2007-05-01</p> <p>Models of energization of <span class="hlt">electrons</span> in the Earth's outer radiation belts invoke two classes of processes, radial transport and in-situ wave-particle interactions. Temporal evolution of <span class="hlt">electron</span> spectra and <span class="hlt">flux</span> isotropization during energization events provide useful observational constraints on models of <span class="hlt">electron</span> energization. Events dominated by radial diffusion result in pancake type pitch angle distributions whereas some in-situ wave-particle energization mechanisms include pitch angle scattering leading to rapid <span class="hlt">flux</span> isotropization. We present a survey of <span class="hlt">flux</span> isotrpization time scales and <span class="hlt">electron</span> spectra during relativstic <span class="hlt">electron</span> enhancement events. We will use data collected by detectors onboard SAMPEX in low earth orbit and Polar which measures <span class="hlt">electron</span> <span class="hlt">fluxes</span> at higher altitude to measure <span class="hlt">flux</span> isotropization. <span class="hlt">Electron</span> spectra are obtained by pulse height analyzed data from the PET detector onboard SAMPEX.SAMPEX measurements cover the entire outer zone for more than a decade from mid 1992 to mid 2004 and Polar covers the time period from mid 1996 to the present.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120002868','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120002868"><span>Characterization of Turbulent Latent and Sensible <span class="hlt">Heat</span> <span class="hlt">Flux</span> Exchange Between the Atmosphere and Ocean in MERRA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Robert, J. Brent; Robertson, Franklin R.; Clayson, Carol Anne; Bosilovich, Michael G.</p> <p>2012-01-01</p> <p>Turbulent <span class="hlt">fluxes</span> of <span class="hlt">heat</span> and moisture across the atmosphere-ocean interface are fundamental components of the Earth's energy and water balance. Characterizing both the spatiotemporal variability and the fidelity of these exchanges of <span class="hlt">heat</span> and moisture is critical to understanding the global water and energy cycle variations, quantifying atmosphere-ocean feedbacks, and improving model predictability. This study examines the veracity of the recently completed NASA Modern-Era Retrospective analysis for Research and Applications (MERRA) product with respect to its representation of the surface turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. A validation of MERRA turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> and near-surface bulk variables at local, <span class="hlt">high</span>-resolution space and time scales is achieved by making comparisons to a large suite of direct observations. Both in situ and satellite-observed gridded surface <span class="hlt">heat</span> <span class="hlt">flux</span> estimates are employed to investigate the spatial and temporal variability of the surface <span class="hlt">fluxes</span> with respect to their annual mean climatologies, their seasonal covariability of near-surface bulk parameters, and their representation of extremes. The impact of data assimilation on the near-surface parameters is assessed through evaluation of incremental analysis update tendencies produced by the assimilation procedure. It is found that MERRA turbulent surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> are relatively accurate for typical conditions but have systematically weak vertical gradients in moisture and temperature and have a weaker covariability between the near-surface gradients and wind speed than found in observations. This results in an underestimate of the surface latent and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> over the western boundary current and storm track regions. The assimilation of observations mostly acts to bring MERRA closer to observational products by increasing moisture and temperature near the surface and decreasing the near-surface wind speeds. The major patterns of spatial and temporal variability of the turbulent <span class="hlt">heat</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120007430','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120007430"><span>Characterization of Turbulent Latent and Sensible <span class="hlt">Heat</span> <span class="hlt">Flux</span> Exchange Between the Atmosphere and Ocean in MERRA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Roberts, J. Brent; Robertson, Franklin R.; Clayson, Carol Anne; Bosilovich, Michael G.</p> <p>2012-01-01</p> <p>Turbulent <span class="hlt">fluxes</span> of <span class="hlt">heat</span> and moisture across the atmosphere-ocean interface are fundamental components of the Earth s energy and water balance. Characterizing both the spatiotemporal variability and the fidelity of these exchanges of <span class="hlt">heat</span> and moisture is critical to understanding the global water and energy cycle variations, quantifying atmosphere-ocean feedbacks, and improving model predictability. This study examines the veracity of the recently completed NASA Modern-Era Retrospective analysis for Research and Applications (MERRA) product with respect to its representation of the surface turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. A validation of MERRA turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> and near-surface bulk variables at local, <span class="hlt">high</span>-resolution space and time scales is achieved by making comparisons to a large suite of direct observations. Both in situ and satellite-observed gridded surface <span class="hlt">heat</span> <span class="hlt">flux</span> estimates are employed to investigate the spatial and temporal variability of the surface <span class="hlt">fluxes</span> with respect to their annual mean climatologies, their seasonal covariability of near-surface bulk parameters, and their representation of extremes. The impact of data assimilation on the near-surface parameters is assessed through evaluation of incremental analysis update tendencies produced by the assimilation procedure. It is found that MERRA turbulent surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> are relatively accurate for typical conditions but have systematically weak vertical gradients in moisture and temperature and have a weaker covariability between the near-surface gradients and wind speed than found in observations. This results in an underestimate of the surface latent and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> over the western boundary current and storm track regions. The assimilation of observations mostly acts to bring MERRA closer to observational products by increasing moisture and temperature near the surface and decreasing the near-surface wind speeds. The major patterns of spatial and temporal variability of the turbulent <span class="hlt">heat</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1995SPIE.2586..241X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1995SPIE.2586..241X"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> exchange estimation by using ATSR SST data in TOGA area</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xue, Yong; Lawrence, Sean P.; Llewellyn-Jones, David T.</p> <p>1995-12-01</p> <p>The study of phenomena such as ENSO requires consideration of the dynamics and thermodynamics of the coupled ocean-atmosphere system. The dynamic and thermal properties of the atmosphere and ocean are directly affected by air-sea transfers of <span class="hlt">fluxes</span> of momentum, <span class="hlt">heat</span> and moisture. In this paper, we present results of turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> calculated by using two years (1992 and 1993) monthly average TOGA data and ATSR SST data in TOGA area. A comparison with published results indicates good qualitative agreement. Also, we compared the results of <span class="hlt">heat</span> <span class="hlt">flux</span> exchange by using ATSR SST data and by using the TOGA bucket SST data. The ATSR SST data set has been shown to be useful in helping to estimate the large space scale <span class="hlt">heat</span> <span class="hlt">flux</span> exchange.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1997PhDT.......186G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1997PhDT.......186G"><span>Closed-form solution of temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> in embedded cooling channels</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Griggs, Steven Craig</p> <p>1997-11-01</p> <p>An analytical method is discussed for predicting temperature in a layered composite material with embedded cooling channels. The cooling channels are embedded in the material to maintain its temperature at acceptable levels. Problems of this type are encountered in the aerospace industry and include <span class="hlt">high</span>-temperature or <span class="hlt">high-heat-flux</span> protection for advanced composite-material skins of <span class="hlt">high</span>-speed air vehicles; thermal boundary-layer flow control on supersonic transports; or infrared signature suppression on military vehicles. A Green's function solution of the diffusion equation is used to simultaneously predict the global and localized effects of temperature in the material and in the embedded cooling channels. The integral method is used to solve the energy equation with fluid flow to find the solution of temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> in the cooling fluid and material simultaneously. This method of calculation preserves the three-dimensional nature of this problem.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011WRR....47.5545M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011WRR....47.5545M"><span>Estimation of evaporation and sensible <span class="hlt">heat</span> <span class="hlt">flux</span> from open water using a large-aperture scintillometer</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>McJannet, D. L.; Cook, F. J.; McGloin, R. P.; McGowan, H. A.; Burn, S.</p> <p>2011-05-01</p> <p>The use of scintillometers to determine sensible and latent <span class="hlt">heat</span> <span class="hlt">flux</span> is becoming increasingly common because of their ability to quantify convective <span class="hlt">fluxes</span> over distances of hundreds of meters to several kilometers. The majority of investigations using scintillometry have focused on processes above land surfaces, but here we propose a new methodology for obtaining sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> from a scintillometer deployed over open water. This methodology has been tested by comparison with eddy covariance measurements and through comparison with alternative scintillometer calculation approaches that are commonly used in the literature. The methodology is based on linearization of the Bowen ratio, which is a common assumption in models such as Penman's model and its derivatives. Comparison of latent <span class="hlt">heat</span> <span class="hlt">flux</span> estimates from the eddy covariance system and the scintillometer showed excellent agreement across a range of weather conditions and <span class="hlt">flux</span> rates, giving a <span class="hlt">high</span> level of confidence in scintillometry-derived latent <span class="hlt">heat</span> <span class="hlt">fluxes</span>. The proposed approach produced better estimates than other scintillometry calculation methods because of the reliance of alternative methods on measurements of water temperature or water body <span class="hlt">heat</span> storage, which are both notoriously hard to quantify. The proposed methodology requires less instrumentation than alternative scintillometer calculation approaches, and the spatial scales of required measurements are arguably more compatible. In addition to scintillometer measurements of the structure parameter of the refractive index of air, the only measurements required are atmospheric pressure, air temperature, humidity, and wind speed at one height over the water body.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013JNuM..438S.229Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013JNuM..438S.229Y"><span>Melt layer erosion of pure and lanthanum doped tungsten under VDE-like <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> loads</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yuan, Y.; Greuner, H.; Böswirth, B.; Luo, G.-N.; Fu, B. Q.; Xu, H. Y.; Liu, W.</p> <p>2013-07-01</p> <p><span class="hlt">Heat</span> loads expected for VDEs in ITER were applied in the neutral beam facility GLADIS at IPP Garching. Several ˜3 mm thick rolled pure W and W-1 wt% La2O3 plates were exposed to pulsed hydrogen beams with a central <span class="hlt">heat</span> <span class="hlt">flux</span> of 23 MW/m2 for 1.5-1.8 s. The melting thresholds are determined, and melt layer motion as well as material structure evolutions are shown. The melting thresholds of the two W grades are very close in this experimental setup. Lots of big bubbles with diameters from several μm to several 10 μm in the re-solidified layer of W were observed and they spread deeper with increasing <span class="hlt">heat</span> <span class="hlt">flux</span>. However, for W-1 wt% La2O3, no big bubbles were found in the corrugated melt layer. The underlying mechanisms referred to the melt layer motion and bubble issues are tentatively discussed based on comparison of the erosion characteristics between the two W grades.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSM21A2567T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSM21A2567T"><span>Quasiperiodic modulations of energetic <span class="hlt">electron</span> <span class="hlt">fluxes</span> in the ULF range observed by the ERG satellite</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Teramoto, M.; Hori, T.; Kurita, S.; Yoshizumi, M.; Saito, S.; Higashio, N.; Mitani, T.; Matsuoka, A.; Park, I.; Takashima, T.; Nomura, R.; Nose, M.; Fujimoto, A.; Tanaka, Y.; Shinohara, M.; Shinohara, I.</p> <p>2017-12-01</p> <p>Exploration of energization and Radiation in Geospace (ERG) satellite was successfully launched on December 20, 2016. The Extremely <span class="hlt">High</span>-Energy <span class="hlt">Electron</span> Experiment (XEP) and <span class="hlt">High</span>-Energy <span class="hlt">Electron</span> Experiments (HEP-L and HEP-H) are carried by the ERG satellite to observe energetic <span class="hlt">electrons</span>. These instruments frequently observed quasiperiodic modulations of energetic <span class="hlt">electron</span> <span class="hlt">fluxes</span> with period of 100-600 sec. Continuous <span class="hlt">flux</span> modulations with the period of 600 s appeared in the 700keV-3.6MeV energy range during the period 0920UT-1120UT on March 31, 2017 when the ERG satellite was located at L 5.5-6.1 and MLT 3-4 h. We compare these <span class="hlt">flux</span> modulations with the magnetic field observed by the Magnetic Field Experiment (MGF) on the ERG satellite. It is found that these <span class="hlt">flux</span> modulations are not accompanied by corresponding magnetic signatures. It indicates that these quasiperiodic <span class="hlt">flux</span> modulations are not caused by drift-resonant interactions between ULF waves and energetic <span class="hlt">electrons</span>, at least locally. In this study, we will show several events and discuss possible mechanism for quasiperiodic <span class="hlt">flux</span> modulations of energetic <span class="hlt">electrons</span> on XEP and HEP.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050201899','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050201899"><span>Thermal Cyclic Behavior of Thermal and Environmental Barrier Coatings Investigated Under <span class="hlt">High-Heat-Flux</span> Conditions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zhu, Dongming; Lee, Kang N.; Miller, Robert A.</p> <p>2002-01-01</p> <p>Environmental barrier coatings (EBC's) have been developed to protect silicon-carbide- (SiC) based ceramic components in gas turbine engines from <span class="hlt">high</span>-temperature environmental attack. With continuously increasing demands for significantly higher engine operating temperature, future EBC systems must be designed for both thermal and environmental protection of the engine components in combustion gases. In particular, the thermal barrier functions of EBC's become a necessity for reducing the engine-component thermal loads and chemical reaction rates, thus maintaining the required mechanical properties and durability of these components. Advances in the development of thermal and environmental barrier coatings (TBC's and EBC's, respectively) will directly impact the successful use of ceramic components in advanced engines. To develop <span class="hlt">high</span>-performance coating systems, researchers must establish advanced test approaches. In this study, a laser <span class="hlt">high-heat-flux</span> technique was employed to investigate the thermal cyclic behavior of TBC's and EBC's on SiC-reinforced SiC ceramic matrix composite substrates (SiC/SiC) under <span class="hlt">high</span> thermal gradient and thermal cycling conditions. Because the laser <span class="hlt">heat</span> <span class="hlt">flux</span> test approach can monitor the coating's real-time thermal conductivity variations at <span class="hlt">high</span> temperature, the coating thermal insulation performance, sintering, and delamination can all be obtained during thermal cycling tests. Plasma-sprayed yttria-stabilized zirconia (ZrO2-8 wt% Y2O3) thermal barrier and barium strontium aluminosilicate-based environmental barrier coatings (BSAS/BSAS+mullite/Si) on SiC/SiC ceramic matrix composites were investigated in this study. These coatings were laser tested in air under thermal gradients (the surface and interface temperatures were approximately 1482 and 1300 C, respectively). Some coating specimens were also subject to alternating furnace cycling (in a 90-percent water vapor environment at 1300 C) and laser thermal gradient cycling tests</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PPCF...60e5007W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PPCF...60e5007W"><span>Simulations of particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> in an ELMy H-mode discharge on EAST using BOUT++ code</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wu, Y. B.; Xia, T. Y.; Zhong, F. C.; Zheng, Z.; Liu, J. B.; team3, EAST</p> <p>2018-05-01</p> <p>In order to study the distribution and evolution of the transient particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> during edge-localized mode (ELM) bursts on the Experimental Advanced Superconducting Tokamak (EAST), the BOUT++ six-field two-fluid model is used to simulate the pedestal collapse. The profiles from the EAST H-mode discharge #56129 are used as the initial conditions. Linear analysis shows that the resistive ballooning mode and drift-Alfven wave are two dominant instabilities for the equilibrium, and play important roles in driving ELMs. The evolution of the density profile and the growing process of the <span class="hlt">heat</span> <span class="hlt">flux</span> at divertor targets during the burst of ELMs are reproduced. The time evolution of the poloidal structures of T e is well simulated, and the dominant mode in each stage of the ELM crash process is found. The studies show that during the nonlinear phase, the dominant mode is 5, and it changes to 0 when the nonlinear phase goes to saturation after the ELM crash. The time evolution of the radial <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">flux</span>, ion <span class="hlt">heat</span> <span class="hlt">flux</span>, and particle density <span class="hlt">flux</span> at the outer midplane (OMP) are obtained, and the corresponding transport coefficients D r, χ ir, and χ er reach maximum around 0.3 ∼ 0.5 m2 s‑1 at ΨN = 0.9. The <span class="hlt">heat</span> <span class="hlt">fluxes</span> at outer target plates are several times larger than that at inner target plates, which is consistent with the experimental observations. The simulated profiles of ion saturation current density (j s) at the lower outboard (LO) divertor target are compared to those of experiments by Langmuir probes. The profiles near the strike point are similar, and the peak values of j s from simulation are very close to the measurements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22390552-effect-electronic-excitation-high-temperature-flows-behind-strong-shock-waves','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22390552-effect-electronic-excitation-high-temperature-flows-behind-strong-shock-waves"><span>Effect of <span class="hlt">electronic</span> excitation on <span class="hlt">high</span>-temperature flows behind strong shock waves</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Istomin, V. A.; Kustova, E. V.</p> <p>2014-12-09</p> <p>In the present paper, a strongly non-equilibrium one-dimensional steady-state flow behind the plane shock wave is studied. We consider a <span class="hlt">high</span>-temperature chemically reacting five-component ionized mixture of nitrogen species (N{sub 2}/N{sub 2}{sup 2}/N/N{sup +}/e{sup −}) taking into account <span class="hlt">electronic</span> degrees of freedom in N and N{sup +} (170 and 625 <span class="hlt">electronic</span> energy levels respectively), and <span class="hlt">electronic</span>-rotational-vibrational modes in N{sub 2} and N{sub 2}{sup +} (5 and 7 <span class="hlt">electronic</span> terms). Non-equilibrium reactions of ionization, dissociation, recombination and charge-transfer are included to the kinetic scheme. The system of governing equations is written under the assumption that translation and internal energy relaxation ismore » fast whereas chemical reactions and ionization proceed on the macroscopic gas-dynamics time-scale. The developed model is applied to simulate the flow behind a plane shock wave under initial conditions characteristic for the spacecraft re-entry from an interplanetary flight (Hermes and Fire II experiments). Fluid-dynamic parameters behind the shock wave as well as transport coefficients and the <span class="hlt">heat</span> <span class="hlt">flux</span> are calculated for the (N{sub 2}/N{sub 2}{sup +}/N/N{sup +}/e{sup −}) mixture. The effect of <span class="hlt">electronic</span> excitation on kinetics, dynamics and <span class="hlt">heat</span> transfer is analyzed. Whereas the contribution of <span class="hlt">electronic</span> degrees of freedom to the flow macroparameters is negligible, their influence on the <span class="hlt">heat</span> <span class="hlt">flux</span> is found to be important under conditions of Hermes re-entry.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1394229-thermal-hydraulics-modeling-prototype-testing-w7-high-heat-flux-scraper-element','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1394229-thermal-hydraulics-modeling-prototype-testing-w7-high-heat-flux-scraper-element"><span>Thermal-hydraulics modeling for prototype testing of the W7-X <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> scraper element</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Clark, Emily; Lumsdaine, Arnold; Boscary, Jean; ...</p> <p>2017-07-28</p> <p>The long-pulse operation of the Wendelstein 7-X (W7-X) stellarator experiment is scheduled to begin in 2020. This operational phase will be equipped with water-cooled plasma facing components to allow for longer pulse durations. Certain simulated plasma scenarios have been shown to produce <span class="hlt">heat</span> <span class="hlt">fluxes</span> that surpass the technological limits on the edges of the divertor target elements during steady-state operation. In order to reduce the <span class="hlt">heat</span> load on the target elements, the addition of a “scraper element” (SE) is under investigation. The SE is composed of 24 water-cooled carbon fiber reinforced carbon composite monoblock units. Multiple full-scale prototypes have beenmore » tested in the GLADIS <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> test facility. Previous computational studies revealed discrepancies between the simulations and experimental measurements. In this work, single-phase thermal-hydraulics modeling was performed in ANSYS CFX to identify potential causes for such discrepancies. Possible explanations investigated were the effects of a non-uniform thermal contact resistance and a potential misalignment of the monoblock fibers. And while the difference between the experimental and computational results was not resolved by a non-uniform thermal contact resistance, the computational results provided insight into the potential performance of a W7-X monoblock unit. Circumferential temperature distributions highlighted the expected boiling regions of such a unit. Finally, simulations revealed that modest angles of fiber misalignment in the monoblocks result in asymmetries at the unit edges and provide temperature differences similar to the experimental results.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1394229-thermal-hydraulics-modeling-prototype-testing-w7-high-heat-flux-scraper-element','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1394229-thermal-hydraulics-modeling-prototype-testing-w7-high-heat-flux-scraper-element"><span>Thermal-hydraulics modeling for prototype testing of the W7-X <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> scraper element</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Clark, Emily; Lumsdaine, Arnold; Boscary, Jean</p> <p></p> <p>The long-pulse operation of the Wendelstein 7-X (W7-X) stellarator experiment is scheduled to begin in 2020. This operational phase will be equipped with water-cooled plasma facing components to allow for longer pulse durations. Certain simulated plasma scenarios have been shown to produce <span class="hlt">heat</span> <span class="hlt">fluxes</span> that surpass the technological limits on the edges of the divertor target elements during steady-state operation. In order to reduce the <span class="hlt">heat</span> load on the target elements, the addition of a “scraper element” (SE) is under investigation. The SE is composed of 24 water-cooled carbon fiber reinforced carbon composite monoblock units. Multiple full-scale prototypes have beenmore » tested in the GLADIS <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> test facility. Previous computational studies revealed discrepancies between the simulations and experimental measurements. In this work, single-phase thermal-hydraulics modeling was performed in ANSYS CFX to identify potential causes for such discrepancies. Possible explanations investigated were the effects of a non-uniform thermal contact resistance and a potential misalignment of the monoblock fibers. And while the difference between the experimental and computational results was not resolved by a non-uniform thermal contact resistance, the computational results provided insight into the potential performance of a W7-X monoblock unit. Circumferential temperature distributions highlighted the expected boiling regions of such a unit. Finally, simulations revealed that modest angles of fiber misalignment in the monoblocks result in asymmetries at the unit edges and provide temperature differences similar to the experimental results.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AGUFMSA41A4056H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AGUFMSA41A4056H"><span>Direct measurements of vertical <span class="hlt">heat</span> <span class="hlt">flux</span> and Na <span class="hlt">flux</span> in the mesosphere and lower thermosphere by lidar at Boulder (40°N, 105°W), Colorado</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huang, W.; Chu, X.; Gardner, C. S.; Barry, I. F.; Smith, J. A.; Fong, W.; Yu, Z.; Chen, C.</p> <p>2014-12-01</p> <p>The vertical transport of <span class="hlt">heat</span> and constituent by gravity waves and tides plays a fundamental role in establishing the thermal and constituent structures of the mesosphere and lower thermosphere (MLT), but has not been thoroughly investigated by observations. In particular, direct measurements of vertical <span class="hlt">heat</span> <span class="hlt">flux</span> and metal constituent <span class="hlt">flux</span> caused by dissipating waves are extremely rare, which demand precise measurements with <span class="hlt">high</span> spatial and temporal resolutions over a long period. Such requirements are necessary to overcome various uncertainties to reveal the small quantities of the <span class="hlt">heat</span> and constituent <span class="hlt">fluxes</span> induced by dissipating waves. So far such direct observations have only been reported for vertical <span class="hlt">heat</span> and Na <span class="hlt">fluxes</span> using a Na Doppler lidar at Starfire Optical Range (SOR) in Albuquerque, New Mexico. Furthermore, estimate of eddy <span class="hlt">heat</span> and constituent <span class="hlt">fluxes</span> from the turbulent mixing generated by breaking waves is even more challenging due to the even smaller temporal and spatial scales of the eddy. Consequently, the associated coefficients of thermal (kH) and constituent (kzz) diffusion have not been well characterized and remain as large uncertainties in models. We attempt to address these issues with direct measurements by a Na Doppler lidar with exceptional <span class="hlt">high</span>-resolution measurement capabilities. Since summer 2010, we have been operating a Na Doppler lidar at Boulder, Colorado. The efficiency of the lidar has been greatly improved in summer of 2011 and achieved generally over 1000 counts of Na signal per lidar pulse in winter. In 2013, we made extensive Na lidar observations in 98 nights. These data covering each month of a full year will be used to characterize the seasonal variations of <span class="hlt">heat</span> and Na <span class="hlt">fluxes</span> and to be compared with the pioneering observations at SOR. In November 2013, we further upgraded the lidar with two new frequency shifters and a new data acquisition scheme, which are optimized for estimating eddy <span class="hlt">fluxes</span> and reducing the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009HMT....45..967S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009HMT....45..967S"><span>Flow boiling <span class="hlt">heat</span> transfer of R134a and R404A in a microfin tube at low mass <span class="hlt">fluxes</span> and low <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Spindler, Klaus; Müller-Steinhagen, Hans</p> <p>2009-05-01</p> <p>An experimental investigation of flow boiling <span class="hlt">heat</span> transfer in a commercially available microfin tube with 9.52 mm outer diameter has been carried out. The microfin tube is made of copper with a total fin number of 55 and a helix angle of 15°. The fin height is 0.24 mm and the inner tube diameter at fin root is 8.95 mm. The test tube is 1 m long and is electrically <span class="hlt">heated</span>. The experiments have been performed at saturation temperatures between 0 and -20°C. The mass <span class="hlt">flux</span> was varied between 25 and 150 kg/m2s, the <span class="hlt">heat</span> <span class="hlt">flux</span> from 15,000 W/m2 down to 1,000 W/m2. All measurements have been performed at constant inlet vapour quality ranging from 0.1 to 0.7. The measured <span class="hlt">heat</span> transfer coefficients range from 1,300 to 15,700 W/m2K for R134a and from 912 to 11,451 W/m2K for R404A. The mean <span class="hlt">heat</span> transfer coefficient of R134a is in average 1.5 times higher than for R404A. The mean <span class="hlt">heat</span> transfer coefficient has been compared with the correlations by Koyama et al. and by Kandlikar. The deviations are within ±30% and ±15%, respectively. The influence of the mass <span class="hlt">flux</span> on the <span class="hlt">heat</span> transfer is most significant between 25 and 62.5 kg/m2s, where the flow pattern changes from stratified wavy flow to almost annular flow. This flow pattern transition is shifted to lower mass <span class="hlt">fluxes</span> for the microfin tube compared to the smooth tube.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvA..97b3414W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvA..97b3414W"><span>Tracking the ultrafast XUV optical properties of x-ray free-<span class="hlt">electron</span>-laser <span class="hlt">heated</span> matter with <span class="hlt">high</span>-order harmonics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Williams, Gareth O.; Künzel, S.; Daboussi, S.; Iwan, B.; Gonzalez, A. I.; Boutu, W.; Hilbert, V.; Zastrau, U.; Lee, H. J.; Nagler, B.; Granados, E.; Galtier, E.; Heimann, P.; Barbrel, B.; Dovillaire, G.; Lee, R. W.; Dunn, J.; Recoules, V.; Blancard, C.; Renaudin, P.; de la Varga, A. G.; Velarde, P.; Audebert, P.; Merdji, H.; Zeitoun, Ph.; Fajardo, M.</p> <p>2018-02-01</p> <p>We present measurements of photon absorption by free <span class="hlt">electrons</span> as a solid is transformed to plasma. A femtosecond x-ray free-<span class="hlt">electron</span> laser is used to <span class="hlt">heat</span> a solid, which separates the <span class="hlt">electron</span> and ion <span class="hlt">heating</span> time scales. The changes in absorption are measured with an independent probe pulse created through <span class="hlt">high</span>-order-harmonic generation. We find an increase in <span class="hlt">electron</span> temperature to have a relatively small impact on absorption, contrary to several predictions, whereas ion <span class="hlt">heating</span> increases absorption. We compare the data to current theoretical and numerical approaches and find that a smoother <span class="hlt">electronic</span> structure yields a better fit to the data, suggestive of a temperature-dependent <span class="hlt">electronic</span> structure in warm dense matter.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/128767-two-dimensional-stefan-problem-slightly-varying-heat-flux','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/128767-two-dimensional-stefan-problem-slightly-varying-heat-flux"><span>The two-dimensional Stefan problem with slightly varying <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Gammon, J.; Howarth, J.A.</p> <p>1995-09-01</p> <p>The authors solve the two-dimensional stefan problem of solidification in a half-space, where the <span class="hlt">heat</span> <span class="hlt">flux</span> at the wall is a slightly varying function of positioning along the wall, by means of a large Stefan number approximation (which turns out to be equivalent to a small time solution), and then by means of the <span class="hlt">Heat</span> Balance Integral Method, which is valid for all time, and which agrees with the large Stefan number solution for small times. A representative solution is given for a particular form of the <span class="hlt">heat</span> <span class="hlt">flux</span> perturbation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840024719','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840024719"><span>Turbine blade and vane <span class="hlt">heat</span> <span class="hlt">flux</span> sensor development, phase 1</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Atkinson, W. H.; Cyr, M. A.; Strange, R. R.</p> <p>1984-01-01</p> <p><span class="hlt">Heat</span> <span class="hlt">flux</span> sensors available for installation in the hot section airfoils of advanced aircraft gas turbine engines were developed. Two <span class="hlt">heat</span> <span class="hlt">flux</span> sensors were designed, fabricated, calibrated, and tested. Measurement techniques are compared in an atmospheric pressure combustor rig test. Sensors, embedded thermocouple and the Gordon gauge, were fabricated that met the geometric and fabricability requirements and could withstand the hot section environmental conditions. Calibration data indicate that these sensors yielded repeatable results and have the potential to meet the accuracy goal of measuring local <span class="hlt">heat</span> <span class="hlt">flux</span> to within 5%. Thermal cycle tests and thermal soak tests indicated that the sensors are capable of surviving extended periods of exposure to the environment conditions in the turbine. Problems in calibration of the sensors caused by severe non-one dimensional <span class="hlt">heat</span> flow were encountered. Modifications to the calibration techniques are needed to minimize this problem and proof testing of the sensors in an engine is needed to verify the designs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1984pwa..rept.....A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1984pwa..rept.....A"><span>Turbine blade and vane <span class="hlt">heat</span> <span class="hlt">flux</span> sensor development, phase 1</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Atkinson, W. H.; Cyr, M. A.; Strange, R. R.</p> <p>1984-08-01</p> <p><span class="hlt">Heat</span> <span class="hlt">flux</span> sensors available for installation in the hot section airfoils of advanced aircraft gas turbine engines were developed. Two <span class="hlt">heat</span> <span class="hlt">flux</span> sensors were designed, fabricated, calibrated, and tested. Measurement techniques are compared in an atmospheric pressure combustor rig test. Sensors, embedded thermocouple and the Gordon gauge, were fabricated that met the geometric and fabricability requirements and could withstand the hot section environmental conditions. Calibration data indicate that these sensors yielded repeatable results and have the potential to meet the accuracy goal of measuring local <span class="hlt">heat</span> <span class="hlt">flux</span> to within 5%. Thermal cycle tests and thermal soak tests indicated that the sensors are capable of surviving extended periods of exposure to the environment conditions in the turbine. Problems in calibration of the sensors caused by severe non-one dimensional <span class="hlt">heat</span> flow were encountered. Modifications to the calibration techniques are needed to minimize this problem and proof testing of the sensors in an engine is needed to verify the designs.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_18 --> <div id="page_19" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="361"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT....54..385S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT....54..385S"><span>Estimation of transient <span class="hlt">heat</span> <span class="hlt">flux</span> density during the <span class="hlt">heat</span> supply of a catalytic wall steam methane reformer</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Settar, Abdelhakim; Abboudi, Saïd; Madani, Brahim; Nebbali, Rachid</p> <p>2018-02-01</p> <p>Due to the endothermic nature of the steam methane reforming reaction, the process is often limited by the <span class="hlt">heat</span> transfer behavior in the reactors. Poor thermal behavior sometimes leads to slow reaction kinetics, which is characterized by the presence of cold spots in the catalytic zones. Within this framework, the present work consists on a numerical investigation, in conjunction with an experimental one, on the one-dimensional <span class="hlt">heat</span> transfer phenomenon during the <span class="hlt">heat</span> supply of a catalytic-wall reactor, which is designed for hydrogen production. The studied reactor is inserted in an electric furnace where the <span class="hlt">heat</span> requirement of the endothermic reaction is supplied by electric <span class="hlt">heating</span> system. During the <span class="hlt">heat</span> supply, an unknown <span class="hlt">heat</span> <span class="hlt">flux</span> density, received by the reactive flow, is estimated using inverse methods. In the basis of the catalytic-wall reactor model, an experimental setup is engineered in situ to measure the temperature distribution. Then after, the measurements are injected in the numerical <span class="hlt">heat</span> <span class="hlt">flux</span> estimation procedure, which is based on the Function Specification Method (FSM). The measured and estimated temperatures are confronted and the <span class="hlt">heat</span> <span class="hlt">flux</span> density which crosses the reactor wall is determined.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPB11080B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPB11080B"><span>Observations of temperature rise during <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> application in Proto-MPEX</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Biewer, T. M.; Bigelow, T.; Caneses, J. F.; Diem, S. J.; Rapp, J.; Reinke, M.; Kafle, N.; Ray, H. B.; Showers, M.</p> <p>2017-10-01</p> <p>The Prototype Material Plasma Exposure eXperiment (Proto-MPEX) at ORNL utilizes a variety of power systems to generate and deliver a <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> plasma (1 MW/m2 for these discharges) onto the surface of material targets. In the experiments described here, up to 120 kW of 13.56 MHz ``helicon'' waves are combined with 20 kW of 28 GHz microwaves to produce Deuterium plasma discharges. The 28 GHz waves are launched in a region of the device where the magnetic field is axially varying near 0.8 T, resulting in the presence of a 2nd harmonic <span class="hlt">electron</span> cyclotron <span class="hlt">heating</span> (ECH) resonance layer that transects the plasma column. The <span class="hlt">electron</span> density and temperature profiles are measured using a Thomson scattering (TS) diagnostic, and indicate that the <span class="hlt">electron</span> density is radially peaked. In the core of the plasma column the <span class="hlt">electron</span> density is higher than the cut-off density (0.9x1019 m-3) for ECH waves to propagate and O-X-B mode conversion into <span class="hlt">electron</span> Bernstien waves (EBW) is expected. TS measurements indicate <span class="hlt">electron</span> temperature increases during 28 GHz wave application, rising (from 5 eV to 20 eV) as the neutral Deuterium pressure is reduced below 1 mTorr. This work was supported by the US. D.O.E. contract DE-AC05-00OR22725.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JGRD..121.7853K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JGRD..121.7853K"><span>Re-examining the roles of surface <span class="hlt">heat</span> <span class="hlt">flux</span> and latent <span class="hlt">heat</span> release in a "hurricane-like" polar low over the Barents Sea</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kolstad, Erik W.; Bracegirdle, Thomas J.; Zahn, Matthias</p> <p>2016-07-01</p> <p>Polar lows are intense mesoscale cyclones that occur at <span class="hlt">high</span> latitudes in both hemispheres during winter. Their sometimes evidently convective nature, fueled by strong surface <span class="hlt">fluxes</span> and with cloud-free centers, have led to some polar lows being referred to as "arctic hurricanes." Idealized studies have shown that intensification by hurricane development mechanisms is theoretically possible in polar winter atmospheres, but the lack of observations and realistic simulations of actual polar lows have made it difficult to ascertain if this occurs in reality. Here the roles of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> and latent <span class="hlt">heat</span> release in the development of a Barents Sea polar low, which in its cloud structures showed some similarities to hurricanes, are studied with an ensemble of sensitivity experiments, where latent <span class="hlt">heating</span> and/or surface <span class="hlt">fluxes</span> of sensible and latent <span class="hlt">heat</span> were switched off before the polar low peaked in intensity. To ensure that the polar lows in the sensitivity runs did not track too far away from the actual environmental conditions, a technique known as spectral nudging was applied. This was shown to be crucial for enabling comparisons between the different model runs. The results presented here show that (1) no intensification occurred during the mature, postbaroclinic stage of the simulated polar low; (2) surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>, i.e., air-sea interaction, were crucial processes both in order to attain the polar low's peak intensity during the baroclinic stage and to maintain its strength in the mature stage; and (3) latent <span class="hlt">heat</span> release played a less important role than surface <span class="hlt">fluxes</span> in both stages.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PhRvA..91b2121L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PhRvA..91b2121L"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> and quantum correlations in dissipative cascaded systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lorenzo, Salvatore; Farace, Alessandro; Ciccarello, Francesco; Palma, G. Massimo; Giovannetti, Vittorio</p> <p>2015-02-01</p> <p>We study the dynamics of <span class="hlt">heat</span> <span class="hlt">flux</span> in the thermalization process of a pair of identical quantum systems that interact dissipatively with a reservoir in a cascaded fashion. Despite that the open dynamics of the bipartite system S is globally Lindbladian, one of the subsystems "sees" the reservoir in a state modified by the interaction with the other subsystem and hence it undergoes a non-Markovian dynamics. As a consequence, the <span class="hlt">heat</span> flow exhibits a nonexponential time behavior which can greatly deviate from the case where each party is independently coupled to the reservoir. We investigate both thermal and correlated initial states of S and show that the presence of correlations at the beginning can considerably affect the <span class="hlt">heat-flux</span> rate. We carry out our study in two paradigmatic cases—a pair of harmonic oscillators with a reservoir of bosonic modes and two qubits with a reservoir of fermionic modes—and compare the corresponding behaviors. In the case of qubits and for initial thermal states, we find that the trace distance discord is at any time interpretable as the correlated contribution to the total <span class="hlt">heat</span> <span class="hlt">flux</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014APS..DPPTP8051M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014APS..DPPTP8051M"><span>Turbulent transport regimes and the SOL <span class="hlt">heat</span> <span class="hlt">flux</span> width</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Myra, J. R.; D'Ippolito, D. A.; Russell, D. A.</p> <p>2014-10-01</p> <p>Understanding the responsible mechanisms and resulting scaling of the scrape-off layer (SOL) <span class="hlt">heat</span> <span class="hlt">flux</span> width is important for predicting viable operating regimes in future tokamaks, and for seeking possible mitigation schemes. Simulation and theory results using reduced edge/SOL turbulence models have produced SOL widths and scalings in reasonable accord with experiments in many cases. In this work, we attempt to qualitatively and conceptually understand various regimes of edge/SOL turbulence and the role of turbulent transport in establishing the SOL <span class="hlt">heat</span> <span class="hlt">flux</span> width. Relevant considerations include the type and spectral characteristics of underlying instabilities, the location of the gradient drive relative to the SOL, the nonlinear saturation mechanism, and the parallel <span class="hlt">heat</span> transport regime. Recent SOLT turbulence code results are employed to understand the roles of these considerations and to develop analytical scalings. We find a <span class="hlt">heat</span> <span class="hlt">flux</span> width scaling with major radius R that is generally positive, consistent with older results reviewed in. The possible relationship of turbulence mechanisms to the heuristic drift mechanism is considered, together with implications for future experiments. Work supported by US DOE grant DE-FG02-97ER54392.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1126550','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1126550"><span>Impact of the <span class="hlt">High</span> <span class="hlt">Flux</span> Isotope Reactor HEU to LEU Fuel Conversion on Cold Source Nuclear <span class="hlt">Heat</span> Generation Rates</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Chandler, David</p> <p>2014-03-01</p> <p>Under the sponsorship of the US Department of Energy National Nuclear Security Administration, staff members at the Oak Ridge National Laboratory have been conducting studies to determine whether the <span class="hlt">High</span> <span class="hlt">Flux</span> Isotope Reactor (HFIR) can be converted from <span class="hlt">high</span> enriched uranium (HEU) fuel to low enriched uranium (LEU) fuel. As part of these ongoing studies, an assessment of the impact that the HEU to LEU fuel conversion has on the nuclear <span class="hlt">heat</span> generation rates in regions of the HFIR cold source system and its moderator vessel was performed and is documented in this report. Silicon production rates in the coldmore » source aluminum regions and few-group neutron <span class="hlt">fluxes</span> in the cold source moderator were also estimated. Neutronics calculations were performed with the Monte Carlo N-Particle code to determine the nuclear <span class="hlt">heat</span> generation rates in regions of the HFIR cold source and its vessel for the HEU core operating at a full reactor power (FP) of 85 MW(t) and the reference LEU core operating at an FP of 100 MW(t). Calculations were performed with beginning-of-cycle (BOC) and end-of-cycle (EOC) conditions to bound typical irradiation conditions. Average specific BOC <span class="hlt">heat</span> generation rates of 12.76 and 12.92 W/g, respectively, were calculated for the hemispherical region of the cold source liquid hydrogen (LH2) for the HEU and LEU cores, and EOC <span class="hlt">heat</span> generation rates of 13.25 and 12.86 W/g, respectively, were calculated for the HEU and LEU cores. Thus, the greatest <span class="hlt">heat</span> generation rates were calculated for the EOC HEU core, and it is concluded that the conversion from HEU to LEU fuel and the resulting increase of FP from 85 MW to 100 MW will not impact the ability of the <span class="hlt">heat</span> removal equipment to remove the <span class="hlt">heat</span> deposited in the cold source system. Silicon production rates in the cold source aluminum regions are estimated to be about 12.0% greater at BOC and 2.7% greater at EOC for the LEU core in comparison to the HEU core. Silicon is aluminum s major transmutation</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007APS..MAR.K1066B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007APS..MAR.K1066B"><span>Large cooling differentials and <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> capability with p-type Bi2Te3/Sb2Te3 and n-type Bi2Te3/Bi2SexTe3-x Superlattice Thermoelectric Devices</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bulman, Gary; Siivola, Ed; Wiitala, Ryan; Grant, Brian; Pierce, Jonathan; Venkatasubramanian, Rama</p> <p>2007-03-01</p> <p>Thin film superlattice (SL) based thermoelectric (TE) devices offer the potential for improved efficiency and <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> cooling over conventional bulk materials. Recently, we have demonstrated external cooling of 55K and <span class="hlt">heat</span> pumping capacity of 128 W/cm^2. These <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> in thin film devices, while attractive for cooling hot-spots in <span class="hlt">electronics</span>, also make the device performance sensitive to various thermal resistances in the device structure. We will discuss advances in the cooling performance of Bi2Te3-based SL TE devices and describe a method to extract device material parameters, including thermal resistance, from measurements of their δT-I-V characteristics. These parameters will be compared to values obtained through Hall and Seebeck coefficient measurement on epitaxial materials. Results will be presented for both single couple and multi-couple modules, as well as multi-stage cascaded devices made with these materials. Single stage cooling couples with δTmax of 57.8K (Tc˜242K) and multi-stage modules with δTmax˜92.2K (Tc˜209K) have been measured. G.E. Bulman, E. Siivola, B. Shen and R. Venkatasubramanian, Appl. Phys. Lett. 89, 122117 (2006).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840007873','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840007873"><span>Thermal <span class="hlt">electron</span> <span class="hlt">heating</span> rate: A derivation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hoegy, W. R.</p> <p>1983-01-01</p> <p>The thermal <span class="hlt">electron</span> <span class="hlt">heating</span> rate is an important <span class="hlt">heat</span> source term in the ionospheric <span class="hlt">electron</span> energy balance equation, representing <span class="hlt">heating</span> by photoelectrons or by precipitating higher energy <span class="hlt">electrons</span>. A formula for the thermal <span class="hlt">electron</span> <span class="hlt">heating</span> rate is derived from the kinetic equation using the <span class="hlt">electron-electron</span> collision operator as given by the unified theory of Kihara and Aono. This collision operator includes collective interactions to produce a finite collision operator with an exact Coulomb logarithm term. The derived <span class="hlt">heating</span> rate O(e) is the sum of three terms, O(e) = O(p) + S + O(int), which are respectively: (1) primary <span class="hlt">electron</span> production term giving the <span class="hlt">heating</span> from newly created <span class="hlt">electrons</span> that have not yet suffered collisions with the ambient <span class="hlt">electrons</span>; (2) a <span class="hlt">heating</span> term evaluated on the energy surface m(e)/2 = E(T) at the transition between Maxwellian and tail <span class="hlt">electrons</span> at E(T); and (3) the integral term representing <span class="hlt">heating</span> of Maxwellian <span class="hlt">electrons</span> by energetic tail <span class="hlt">electrons</span> at energies ET. Published ionospheric <span class="hlt">electron</span> temperature studies used only the integral term O(int) with differing lower integration limits. Use of the incomplete <span class="hlt">heating</span> rate could lead to erroneous conclusions regarding <span class="hlt">electron</span> <span class="hlt">heat</span> balance, since O(e) is greater than O(int) by as much as a factor of two.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21033889','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21033889"><span>Collective Thomson scattering of a <span class="hlt">high</span> power <span class="hlt">electron</span> cyclotron resonance <span class="hlt">heating</span> beam in LHD (invited).</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kubo, S; Nishiura, M; Tanaka, K; Shimozuma, T; Yoshimura, Y; Igami, H; Takahash, H; Mutoh, T; Tamura, N; Tatematsu, Y; Saito, T; Notake, T; Korsholm, S B; Meo, F; Nielsen, S K; Salewski, M; Stejner, M</p> <p>2010-10-01</p> <p>Collective Thomson scattering (CTS) system has been constructed at LHD making use of the <span class="hlt">high</span> power <span class="hlt">electron</span> cyclotron resonance <span class="hlt">heating</span> (ECRH) system in Large Helical Device (LHD). The necessary features for CTS, <span class="hlt">high</span> power probing beams and receiving beams, both with well defined Gaussian profile and with the fine controllability, are endowed in the ECRH system. The 32 channel radiometer with sharp notch filter at the front end is attached to the ECRH system transmission line as a CTS receiver. The validation of the CTS signal is performed by scanning the scattering volume. A new method to separate the CTS signal from background <span class="hlt">electron</span> cyclotron emission is developed and applied to derive the bulk and <span class="hlt">high</span> energy ion components for several combinations of neutral beam <span class="hlt">heated</span> plasmas.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EGUGA..17.6733B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EGUGA..17.6733B"><span>Ground <span class="hlt">heat</span> <span class="hlt">flux</span> and power sources of low-enthalpy geothermal systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bayer, Peter; Blum, Philipp; Rivera, Jaime A.</p> <p>2015-04-01</p> <p>Geothermal <span class="hlt">heat</span> pumps commonly extract energy from the shallow ground at depths as low as approximately 400 m. Vertical borehole <span class="hlt">heat</span> exchangers are often applied, which are seasonally operated for decades. During this lifetime, thermal anomalies are induced in the ground and surface-near aquifers, which often grow over the years and which alleviate the overall performance of the geothermal system. As basis for prediction and control of the evolving energy imbalance in the ground, focus is typically set on the ground temperatures. This is reflected in regulative temperature thresholds, and in temperature trends, which serve as indicators for renewability and sustainability. In our work, we examine the fundamental <span class="hlt">heat</span> <span class="hlt">flux</span> and power sources, as well as their temporal and spatial variability during geothermal <span class="hlt">heat</span> pump operation. The underlying rationale is that for control of ground temperature evolution, knowledge of the primary <span class="hlt">heat</span> sources is fundamental. This insight is also important to judge the validity of simplified modelling frameworks. For instance, we reveal that vertical <span class="hlt">heat</span> <span class="hlt">flux</span> from the surface dominates the basal <span class="hlt">heat</span> <span class="hlt">flux</span> towards a borehole. Both <span class="hlt">fluxes</span> need to be accounted for as proper vertical boundary conditions in the model. Additionally, the role of horizontal groundwater advection is inspected. Moreover, by adopting the ground energy deficit and long-term replenishment as criteria for system sustainability, an uncommon perspective is adopted that is based on the primary parameter rather than induced local temperatures. In our synthetic study and dimensionless analysis, we demonstrate that time of ground energy recovery after system shutdown may be longer than what is expected from local temperature trends. In contrast, unrealistically long recovery periods and extreme thermal anomalies are predicted without account for vertical ground <span class="hlt">heat</span> <span class="hlt">fluxes</span> and only when the energy content of the geothermal reservoir is considered.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhST..170a4071S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhST..170a4071S"><span>Progress in extrapolating divertor <span class="hlt">heat</span> <span class="hlt">fluxes</span> towards large fusion devices</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sieglin, B.; Faitsch, M.; Eich, T.; Herrmann, A.; Suttrop, W.; Collaborators, JET; the MST1 Team; the ASDEX Upgrade Team</p> <p>2017-12-01</p> <p><span class="hlt">Heat</span> load to the plasma facing components is one of the major challenges for the development and design of large fusion devices such as ITER. Nowadays fusion experiments can operate with <span class="hlt">heat</span> load mitigation techniques, e.g. sweeping, impurity seeding, but do not generally require it. For large fusion devices however, <span class="hlt">heat</span> load mitigation will be essential. This paper presents the current progress of the extrapolation of steady state and transient <span class="hlt">heat</span> loads towards large fusion devices. For transient <span class="hlt">heat</span> loads, so-called edge localized modes are considered a serious issue for the lifetime of divertor components. In this paper, the ITER operation at half field (2.65 T) and half current (7.5 MA) will be discussed considering the current material limit for the divertor peak energy fluence of 0.5 {MJ}/{{{m}}}2. Recent studies were successful in describing the observed energy fluence in the JET, MAST and ASDEX Upgrade using the pedestal pressure prior to the ELM crash. Extrapolating this towards ITER results in a more benign <span class="hlt">heat</span> load compared to previous scalings. In the presence of magnetic perturbation, the axisymmetry is broken and a 2D <span class="hlt">heat</span> <span class="hlt">flux</span> pattern is induced on the divertor target, leading to local increase of the <span class="hlt">heat</span> <span class="hlt">flux</span> which is a concern for ITER. It is shown that for a moderate divertor broadening S/{λ }{{q}}> 0.5 the toroidal peaking of the <span class="hlt">heat</span> <span class="hlt">flux</span> disappears.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PEPI..250...35S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PEPI..250...35S"><span>Dynamos driven by weak thermal convection and heterogeneous outer boundary <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sahoo, Swarandeep; Sreenivasan, Binod; Amit, Hagay</p> <p>2016-01-01</p> <p>We use numerical dynamo models with heterogeneous core-mantle boundary (CMB) <span class="hlt">heat</span> <span class="hlt">flux</span> to show that lower mantle lateral thermal variability may help support a dynamo under weak thermal convection. In our reference models with homogeneous CMB <span class="hlt">heat</span> <span class="hlt">flux</span>, convection is either marginally supercritical or absent, always below the threshold for dynamo onset. We find that lateral CMB <span class="hlt">heat</span> <span class="hlt">flux</span> variations organize the flow in the core into patterns that favour the growth of an early magnetic field. <span class="hlt">Heat</span> <span class="hlt">flux</span> patterns symmetric about the equator produce non-reversing magnetic fields, whereas anti-symmetric patterns produce polarity reversals. Our results may explain the existence of the geodynamo prior to inner core nucleation under a tight energy budget. Furthermore, in order to sustain a strong geomagnetic field, the lower mantle thermal distribution was likely dominantly symmetric about the equator.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhPl...25d2305H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhPl...25d2305H"><span><span class="hlt">Electron</span> critical gradient scale length measurements of ICRF <span class="hlt">heated</span> L-mode plasmas at Alcator C-Mod tokamak</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Houshmandyar, S.; Hatch, D. R.; Horton, C. W.; Liao, K. T.; Phillips, P. E.; Rowan, W. L.; Zhao, B.; Cao, N. M.; Ernst, D. R.; Greenwald, M.; Howard, N. T.; Hubbard, A. E.; Hughes, J. W.; Rice, J. E.</p> <p>2018-04-01</p> <p>A profile for the critical gradient scale length (Lc) has been measured in L-mode discharges at the Alcator C-Mod tokamak, where <span class="hlt">electrons</span> were <span class="hlt">heated</span> by an ion cyclotron range of frequency through minority <span class="hlt">heating</span> with the intention of simultaneously varying the <span class="hlt">heat</span> <span class="hlt">flux</span> and changing the local gradient. The <span class="hlt">electron</span> temperature gradient scale length (LTe-1 = |∇Te|/Te) profile was measured via the BT-jog technique [Houshmandyar et al., Rev. Sci. Instrum. 87, 11E101 (2016)] and it was compared with <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">flux</span> from power balance (TRANSP) analysis. The Te profiles were found to be very stiff and already above the critical values, however, the stiffness was found to be reduced near the q = 3/2 surface. The measured Lc profile is in agreement with <span class="hlt">electron</span> temperature gradient (ETG) models which predict the dependence of Lc-1 on local Zeff, Te/Ti, and the ratio of the magnetic shear to the safety factor. The results from linear Gene gyrokinetic simulations suggest ETG to be the dominant mode of turbulence in the <span class="hlt">electron</span> scale (k⊥ρs > 1), and ion temperature gradient/trapped <span class="hlt">electron</span> mode modes in the ion scale (k⊥ρs < 1). The measured Lc profile is in agreement with the profile of ETG critical gradients deduced from Gene simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPJ11027G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPJ11027G"><span>Study of <span class="hlt">high</span> field side/low field side asymmetry in the <span class="hlt">electron</span> temperature profile with <span class="hlt">electron</span> cyclotron emission</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gugliada, V. R.; Austin, M. E.; Brookman, M. W.</p> <p>2017-10-01</p> <p><span class="hlt">Electron</span> cyclotron emission (ECE) provides <span class="hlt">high</span> resolution measurements of <span class="hlt">electron</span> temperature profiles (Te(R , t)) in tokamaks. Calibration accuracy of this data can be improved using a sawtooth averaging technique. This improved calibration will then be utilized to determine the symmetry of Te profiles by comparing low field side (LFS) and <span class="hlt">high</span> field side (HFS) measurements. Although Te is considered constant on <span class="hlt">flux</span> surfaces, cases have been observed in which there are pronounced asymmetries about the magnetic axis, particularly with increased pressure. Trends in LFS/HFS overlap are examined as functions of plasma pressure, MHD mode presence, <span class="hlt">heating</span> techniques, and other discharge conditions. This research will provide information on the accuracy of the current two-dimensional mapping of <span class="hlt">flux</span> surfaces in the tokamak. Findings can be used to generate higher quality EFITs and inform ECE calibration. Work supported in part by US DoE under the Science Undergraduate Laboratory Internship (SULI) program and under DE-FC02-04ER549698.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1423540-tracking-ultrafast-xuv-optical-properties-ray-free-electron-laser-heated-matter-high-order-harmonics','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1423540-tracking-ultrafast-xuv-optical-properties-ray-free-electron-laser-heated-matter-high-order-harmonics"><span>Tracking the ultrafast XUV optical properties of x-ray free-<span class="hlt">electron</span>-laser <span class="hlt">heated</span> matter with <span class="hlt">high</span>-order harmonics</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Williams, Gareth O.; Künzel, S.; Daboussi, S.</p> <p></p> <p>We present measurements of photon absorption by free <span class="hlt">electrons</span> as a solid is transformed to plasma. A femtosecond x-ray free-<span class="hlt">electron</span> laser is used to <span class="hlt">heat</span> a solid, which separates the <span class="hlt">electron</span> and ion <span class="hlt">heating</span> time scales. The changes in absorption are measured with an independent probe pulse created through <span class="hlt">high</span>-order-harmonic generation. We find an increase in <span class="hlt">electron</span> temperature to have a relatively small impact on absorption, contrary to several predictions, whereas ion <span class="hlt">heating</span> increases absorption. Here, we compare the data to current theoretical and numerical approaches and find that a smoother <span class="hlt">electronic</span> structure yields a better fit to the data,more » suggestive of a temperature-dependent <span class="hlt">electronic</span> structure in warm dense matter.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1423540-tracking-ultrafast-xuv-optical-properties-ray-free-electron-laser-heated-matter-high-order-harmonics','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1423540-tracking-ultrafast-xuv-optical-properties-ray-free-electron-laser-heated-matter-high-order-harmonics"><span>Tracking the ultrafast XUV optical properties of x-ray free-<span class="hlt">electron</span>-laser <span class="hlt">heated</span> matter with <span class="hlt">high</span>-order harmonics</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Williams, Gareth O.; Künzel, S.; Daboussi, S.; ...</p> <p>2018-02-14</p> <p>We present measurements of photon absorption by free <span class="hlt">electrons</span> as a solid is transformed to plasma. A femtosecond x-ray free-<span class="hlt">electron</span> laser is used to <span class="hlt">heat</span> a solid, which separates the <span class="hlt">electron</span> and ion <span class="hlt">heating</span> time scales. The changes in absorption are measured with an independent probe pulse created through <span class="hlt">high</span>-order-harmonic generation. We find an increase in <span class="hlt">electron</span> temperature to have a relatively small impact on absorption, contrary to several predictions, whereas ion <span class="hlt">heating</span> increases absorption. Here, we compare the data to current theoretical and numerical approaches and find that a smoother <span class="hlt">electronic</span> structure yields a better fit to the data,more » suggestive of a temperature-dependent <span class="hlt">electronic</span> structure in warm dense matter.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhD...51z4001B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhD...51z4001B"><span>MHD <span class="hlt">heat</span> <span class="hlt">flux</span> mitigation in hypersonic flow around a blunt body with ablating surface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bityurin, V. A.; Bocharov, A. N.</p> <p>2018-07-01</p> <p>One of the possible applications of magnetohydrodynamic flow control is considered. Namely, the surface <span class="hlt">heat</span> <span class="hlt">flux</span> mitigation by means of magnetohydrodynamic (MHD) interaction in hypersonic flow around a blunt body. The 2D computational model realizes a coupled solution of chemically non-equilibrium ionized airflow in magnetic field. <span class="hlt">Heat</span>- and mass-transfer due to the ablation of materials from the body surface is taken into account. Two cases of free-stream flow conditions are considered: moderate free-stream velocity (7500 m s‑1) case and <span class="hlt">high</span> free-stream velocity (11 000 m s‑1) case. It is shown that the first flow case results in moderate ionization in the shock layer, while the second flow case results in <span class="hlt">high</span> ionization. In the first case, the Hall effect is significant, and effective electrical conductivity in the shock layer is rather low. In the second case, the Hall effect reduces, and effective conductivity is <span class="hlt">high</span>. Even if the Hall effect is strong, as in the first case, intensive MHD deceleration of the flow behind the shock is provided due to the presence of insulating boundaries, the bow shock front and non-conductive wall of the blunt body. In the second case, <span class="hlt">high</span> effective conductivity provides a <span class="hlt">high</span> intensity of MHD flow deceleration. In both cases, a strong effect of MHD interaction on the flow structure is observed. As a consequence, a noticeable reduction of the surface <span class="hlt">heat</span> <span class="hlt">flux</span> is revealed for reasonable values of magnetic induction. The new treatment of mechanism for the surface <span class="hlt">heat</span> <span class="hlt">flux</span> reduction is proposed, which is different from commonly used one assuming that MHD interaction increases the bow shock stand-off distance, and, consequently results in a decrease of the mean temperature drop across the shock layer. The new effect of ‘saturation of <span class="hlt">heat</span> flux’ is discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PEPI..277...10L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PEPI..277...10L"><span>Linking lowermost mantle structure, core-mantle boundary <span class="hlt">heat</span> <span class="hlt">flux</span> and mantle plume formation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Mingming; Zhong, Shijie; Olson, Peter</p> <p>2018-04-01</p> <p>The dynamics of Earth's lowermost mantle exert significant control on the formation of mantle plumes and the core-mantle boundary (CMB) <span class="hlt">heat</span> <span class="hlt">flux</span>. However, it is not clear if and how the variation of CMB <span class="hlt">heat</span> <span class="hlt">flux</span> and mantle plume activity are related. Here, we perform geodynamic model experiments that show how temporal variations in CMB <span class="hlt">heat</span> <span class="hlt">flux</span> and pulses of mantle plumes are related to morphologic changes of the thermochemical piles of large-scale compositional heterogeneities in Earth's lowermost mantle, represented by the large low shear velocity provinces (LLSVPs). We find good correlation between the morphologic changes of the thermochemical piles and the time variation of CMB <span class="hlt">heat</span> <span class="hlt">flux</span>. The morphology of the thermochemical piles is significantly altered during the initiation and ascent of strong mantle plumes, and the changes in pile morphology cause variations in the local and the total CMB <span class="hlt">heat</span> <span class="hlt">flux</span>. Our modeling results indicate that plume-induced episodic variations of CMB <span class="hlt">heat</span> <span class="hlt">flux</span> link geomagnetic superchrons to pulses of surface volcanism, although the relative timing of these two phenomena remains problematic. We also find that the density distribution in thermochemical piles is heterogeneous, and that the piles are denser on average than the surrounding mantle when both thermal and chemical effects are included.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009APS..DPPPP8020L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009APS..DPPPP8020L"><span>Initial results from divertor <span class="hlt">heat-flux</span> instrumentation on Alcator C-Mod</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Labombard, B.; Brunner, D.; Payne, J.; Reinke, M.; Terry, J. L.; Hughes, J. W.; Lipschultz, B.; Whyte, D.</p> <p>2009-11-01</p> <p>Physics-based plasma transport models that can accurately simulate the <span class="hlt">heat-flux</span> power widths observed in the tokamak boundary are lacking at the present time. Yet this quantity is of fundamental importance for ITER and most critically important for DEMO, a reactor similar to ITER but with ˜4 times the power exhaust. In order to improve our understanding, C-Mod, DIII-D and NSTX will aim experiments in FY10 towards characterizing the divertor ``footprint'' and its connection to conditions ``upstream'' in the boundary and core plasmas [2]. Standard IR-based <span class="hlt">heat-flux</span> measurements are particularly difficult in C-Mod, due to its vertical-oriented divertor targets. To overcome this, a suite of embedded <span class="hlt">heat-flux</span> sensor probes (tile thermocouples, calorimeters, surface thermocouples) combined with IR thermography was installed during the FY09 opening, along with a new divertor bolometer system. This paper will report on initial experiments aimed at unfolding the <span class="hlt">heat-flux</span> dependencies on plasma operating conditions. [2] a proposed US DoE Joint Facilities Milestone.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EM%26P..116....1C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EM%26P..116....1C"><span>HF Accelerated <span class="hlt">Electron</span> <span class="hlt">Fluxes</span>, Spectra, and Ionization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Carlson, Herbert C.; Jensen, Joseph B.</p> <p>2015-10-01</p> <p>Wave particle interactions, an essential aspect of laboratory, terrestrial, and astrophysical plasmas, have been studied for decades by transmitting <span class="hlt">high</span> power HF radio waves into Earth's weakly ionized space plasma, to use it as a laboratory without walls. Application to HF <span class="hlt">electron</span> acceleration remains an active area of research (Gurevich in Usp Fizicheskikh Nauk 177(11):1145-1177, 2007) today. HF <span class="hlt">electron</span> acceleration studies began when plasma line observations proved (Carlson et al. in J Atmos Terr Phys 44:1089-1100, 1982) that <span class="hlt">high</span> power HF radio wave-excited processes accelerated <span class="hlt">electrons</span> not to ~eV, but instead to -100 times thermal energy (10 s of eV), as a consequence of inelastic collision effects on <span class="hlt">electron</span> transport. Gurevich et al (J Atmos Terr Phys 47:1057-1070, 1985) quantified the theory of this transport effect. Merging experiment with theory in plasma physics and aeronomy, enabled prediction (Carlson in Adv Space Res 13:1015-1024, 1993) of creating artificial ionospheres once ~GW HF effective radiated power could be achieved. Eventual confirmation of this prediction (Pedersen et al. in Geophys Res Lett 36:L18107, 2009; Pedersen et al. in Geophys Res Lett 37:L02106, 2010; Blagoveshchenskaya et al. in Ann Geophys 27:131-145, 2009) sparked renewed interest in optical inversion to estimate <span class="hlt">electron</span> spectra in terrestrial (Hysell et al. in J Geophys Res Space Phys 119:2038-2045, 2014) and planetary (Simon et al. in Ann Geophys 29:187-195, 2011) atmospheres. Here we present our unpublished optical data, which combined with our modeling, lead to conclusions that should meaningfully improve future estimates of the spectrum of HF accelerated <span class="hlt">electron</span> <span class="hlt">fluxes</span>. Photometric imaging data can significantly improve detection of emissions near ionization threshold, and confirm depth of penetration of accelerated <span class="hlt">electrons</span> many km below the excitation altitude. Comparing observed to modeled emission altitude shows future experiments need <span class="hlt">electron</span> density profiles</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_19 --> <div id="page_20" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="381"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMGC34B..06G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMGC34B..06G"><span>Capabilities of VOS-based <span class="hlt">fluxes</span> for estimating ocean <span class="hlt">heat</span> budget and its variability</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gulev, S.; Belyaev, K.</p> <p>2016-12-01</p> <p>We consider here the perspective of using VOS observations by merchant ships available form the ICOADS data for estimating ocean surface <span class="hlt">heat</span> budget at different time scale. To this purpose we compute surface turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> as well as short- and long-wave radiative <span class="hlt">fluxes</span> from the ICOADS reports for the last several decades in the North Atlantic mid latitudes. Turbulent <span class="hlt">fluxes</span> were derived using COARE-3 algorithm and for computation of radiative <span class="hlt">fluxes</span> new algorithms accounting for cloud types were used. Sampling uncertainties in the VOS-based <span class="hlt">fluxes</span> were estimated by sub-sampling of the recomputed reanalysis (ERA-Interim) <span class="hlt">fluxes</span> according to the VOS sampling scheme. For the turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> we suggest an approach to minimize sampling uncertainties. The approach is based on the integration of the turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the coordinates of steering parameters (vertical surface temperature and humidity gradients on one hand and wind speed on the other) for which theoretical probability distributions are known. For short-wave radiative <span class="hlt">fluxes</span> sampling uncertainties were minimized by "rotating local observation time around the clock" and using probability density functions for the cloud cover occurrence distributions. Analysis was performed for the North Atlantic latitudinal band from 25 N to 60 N, for which also estimates of the meridional <span class="hlt">heat</span> transport are available from the ocean cross-sections. Over the last 35 years turbulent <span class="hlt">fluxes</span> within the region analysed increase by about 6 W/m2 with the major growth during the 1990s and early 2000s. Decreasing incoming short wave radiation during the same time (about 1 W/m2) implies upward change of the ocean surface <span class="hlt">heat</span> loss by about 7-8 W/m2. We discuss different sources of uncertainties of computations as well as potential of the application of the analysis concept to longer time series going back to 1920s.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22408328-magnetic-flux-heat-losses-diffusive-advective-nernst-effects-magnetized-liner-inertial-fusion-like-plasma','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22408328-magnetic-flux-heat-losses-diffusive-advective-nernst-effects-magnetized-liner-inertial-fusion-like-plasma"><span>Magnetic <span class="hlt">flux</span> and <span class="hlt">heat</span> losses by diffusive, advective, and Nernst effects in magnetized liner inertial fusion-like plasma</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Velikovich, A. L.; Giuliani, J. L.; Zalesak, S. T.</p> <p></p> <p>The magnetized liner inertial fusion (MagLIF) approach to inertial confinement fusion [Slutz et al., Phys. Plasmas 17, 056303 (2010); Cuneo et al., IEEE Trans. Plasma Sci. 40, 3222 (2012)] involves subsonic/isobaric compression and <span class="hlt">heating</span> of a deuterium-tritium plasma with frozen-in magnetic <span class="hlt">flux</span> by a heavy cylindrical liner. The losses of <span class="hlt">heat</span> and magnetic <span class="hlt">flux</span> from the plasma to the liner are thereby determined by plasma advection and gradient-driven transport processes, such as thermal conductivity, magnetic field diffusion, and thermomagnetic effects. Theoretical analysis based on obtaining exact self-similar solutions of the classical collisional Braginskii's plasma transport equations in one dimension demonstratesmore » that the <span class="hlt">heat</span> loss from the hot compressed magnetized plasma to the cold liner is dominated by transverse <span class="hlt">heat</span> conduction and advection, and the corresponding loss of magnetic <span class="hlt">flux</span> is dominated by advection and the Nernst effect. For a large <span class="hlt">electron</span> Hall parameter (ω{sub e}τ{sub e}≫1), the effective diffusion coefficients determining the losses of <span class="hlt">heat</span> and magnetic <span class="hlt">flux</span> to the liner wall are both shown to decrease with ω{sub e}τ{sub e} as does the Bohm diffusion coefficient cT/(16eB), which is commonly associated with low collisionality and two-dimensional transport. We demonstrate how this family of exact solutions can be used for verification of codes that model the MagLIF plasma dynamics.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22251848-abnormal-electron-heating-mode-formation-secondary-energetic-electrons-pulsed-microwave-frequency-atmospheric-microplasmas','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22251848-abnormal-electron-heating-mode-formation-secondary-energetic-electrons-pulsed-microwave-frequency-atmospheric-microplasmas"><span>Abnormal <span class="hlt">electron-heating</span> mode and formation of secondary-energetic <span class="hlt">electrons</span> in pulsed microwave-frequency atmospheric microplasmas</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kwon, H. C.; Research and Development Division, SK Hynix Semiconductor Inc., Icheon 467-701; Jung, S. Y.</p> <p>2014-03-15</p> <p>The formation of secondary energetic <span class="hlt">electrons</span> induced by an abnormal <span class="hlt">electron-heating</span> mode in pulsed microwave-frequency atmospheric microplasmas was investigated using particle-in-cell simulation. We found that additional <span class="hlt">high</span> <span class="hlt">electron</span> <span class="hlt">heating</span> only occurs during the first period of the ignition phase after the start of a second pulse at sub-millimeter dimensions. During this period, the <span class="hlt">electrons</span> are unable to follow the abruptly retreating sheath through diffusion alone. Thus, a self-consistent electric field is induced to drive the <span class="hlt">electrons</span> toward the electrode. These behaviors result in an abnormal <span class="hlt">electron-heating</span> mode that produces <span class="hlt">high</span>-energy <span class="hlt">electrons</span> at the electrode with energies greater than 50 eV.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19840050813&hterms=high+current+electron+beam&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dhigh%2Bcurrent%2Belectron%2Bbeam','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19840050813&hterms=high+current+electron+beam&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dhigh%2Bcurrent%2Belectron%2Bbeam"><span>Gas dynamics in the impulsive phase of solar flares. I Thick-target <span class="hlt">heating</span> by nonthermal <span class="hlt">electrons</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Nagai, F.; Emslie, A. G.</p> <p>1984-01-01</p> <p>A numerical investigation is carried out of the gas dynamical response of the solar atmosphere to a flare energy input in the form of precipitating nonthermal <span class="hlt">electrons</span>. Rather than discussing the origin of these <span class="hlt">electrons</span>, the spectral and temporal characteristics of the injected <span class="hlt">flux</span> are inferred through a thick-target model of hard X-ray bremsstrahlung production. It is assumed that the <span class="hlt">electrons</span> spiral about preexisting magnetic field lines, making it possible for a one-dimensional spatial treatment to be performed. It is also assumed that all <span class="hlt">electron</span> energy losses are due to Coulomb collisions with ambient particles; that is, return-current ohmic effects and collective plasma processes are neglected. The results are contrasted with earlier work on conductive <span class="hlt">heating</span> of the flare atmosphere. A local temperature peak is seen at a height of approximately 1500 km above the photosphere. This derives from a spatial maximum in the energy deposition rate from an <span class="hlt">electron</span> beam. It is noted that such a feature is not present in conductively <span class="hlt">heated</span> models. The associated localized region of <span class="hlt">high</span> pressure drives material both upward and downward.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT...tmp..114M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT...tmp..114M"><span>A combined ANN-GA and experimental based technique for the estimation of the unknown <span class="hlt">heat</span> <span class="hlt">flux</span> for a conjugate <span class="hlt">heat</span> transfer problem</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>M K, Harsha Kumar; P S, Vishweshwara; N, Gnanasekaran; C, Balaji</p> <p>2018-05-01</p> <p>The major objectives in the design of thermal systems are obtaining the information about thermophysical, transport and boundary properties. The main purpose of this paper is to estimate the unknown <span class="hlt">heat</span> <span class="hlt">flux</span> at the surface of a solid body. A constant area mild steel fin is considered and the base is subjected to constant <span class="hlt">heat</span> <span class="hlt">flux</span>. During <span class="hlt">heating</span>, natural convection <span class="hlt">heat</span> transfer occurs from the fin to ambient. The direct solution, which is the forward problem, is developed as a conjugate <span class="hlt">heat</span> transfer problem from the fin and the steady state temperature distribution is recorded for any assumed <span class="hlt">heat</span> <span class="hlt">flux</span>. In order to model the natural convection <span class="hlt">heat</span> transfer from the fin, an extended domain is created near the fin geometry and air is specified as a fluid medium and Navier Stokes equation is solved by incorporating the Boussinesq approximation. The computational time involved in executing the forward model is then reduced by developing a neural network (NN) between <span class="hlt">heat</span> <span class="hlt">flux</span> values and temperatures based on back propagation algorithm. The conjugate <span class="hlt">heat</span> transfer NN model is now coupled with Genetic algorithm (GA) for the solution of the inverse problem. Initially, GA is applied to the pure surrogate data, the results are then used as input to the Levenberg- Marquardt method and such hybridization is proven to result in accurate estimation of the unknown <span class="hlt">heat</span> <span class="hlt">flux</span>. The hybrid method is then applied for the experimental temperature to estimate the unknown <span class="hlt">heat</span> <span class="hlt">flux</span>. A satisfactory agreement between the estimated and actual <span class="hlt">heat</span> <span class="hlt">flux</span> is achieved by incorporating the hybrid method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990047263','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990047263"><span>Thermal Conductivity and Elastic Modulus Evolution of Thermal Barrier Coatings under <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Conditions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zhu, Dongming; Miller, Robert A.</p> <p>1999-01-01</p> <p>Laser <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> test approaches have been established to obtain critical properties of ceramic thermal barrier coatings (TBCs) under near-realistic temperature and thermal gradients that may he encountered in advanced engine systems. Thermal conductivity change kinetics of a thin ceramic coating were continuously monitored in real time at various test temperatures. A significant thermal conductivity increase was observed during the laser simulated engine <span class="hlt">heat</span> <span class="hlt">flux</span> tests. For a 0.25 mm thick ZrO2-8%Y2O3 coating system, the overall thermal conductivity increased from the initial value of 1.0 W/m-K to 1. 15 W/m-K, 1. 19 W/m-K and 1.5 W/m-K after 30 hour testing at surface temperatures of 990C, 1100C, and 1320C. respectively. Hardness and modulus gradients across a 1.5 mm thick TBC system were also determined as a function of laser testing time using the laser sintering/creep and micro-indentation techniques. The coating Knoop hardness values increased from the initial hardness value of 4 GPa to 5 GPa near the ceramic/bond coat interface, and to 7.5 GPa at the ceramic coating surface after 120 hour testing. The ceramic surface modulus increased from an initial value of about 70 GPa to a final value of 125 GPa. The increase in thermal conductivity and the evolution of significant hardness and modulus gradients in the TBC systems are attributed to sintering-induced micro-porosity gradients under the laser-imposed <span class="hlt">high</span> thermal gradient conditions. The test techniques provide a viable means for obtaining coating data for use in design, development, stress modeling, and life prediction for various thermal barrier coating applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ClDy...49..391C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ClDy...49..391C"><span>ENSO related SST anomalies and relation with surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> over south Pacific and Atlantic</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chatterjee, S.; Nuncio, M.; Satheesan, K.</p> <p>2017-07-01</p> <p>The role of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> in Southern Pacific and Atlantic Ocean SST anomalies associated with El Nino Southern Oscillation (ENSO) is studied using observation and ocean reanalysis products. A prominent dipole structure in SST anomaly is found with a positive (negative) anomaly center over south Pacific (65S-45S, 120W-70W) and negative (positive) one over south Atlantic (50S-30S, 30W-0E) during austral summer (DJF) of El Nino (LaNina). During late austral spring-early summer (OND) of El Nino (LaNina), anomalous northerly (southerly) meridional moisture transport and a positive (negative) sea level pressure anomaly induces a suppressed (enhanced) latent <span class="hlt">heat</span> <span class="hlt">flux</span> from the ocean surface over south Pacific. This in turn results in a shallower than normal mixed layer depth which further helps in development of the SST anomaly. Mixed layer thins further due to anomalous shortwave radiation during summer and a well developed SST anomaly evolves. The south Atlantic pole exhibits exactly opposite characteristics at the same time. The contribution from the surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> to mixed layer temperature change is found to be dominant over the advective processes over both the basins. Net surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> anomaly is also found to be maximum during late austral spring-early summer period, with latent <span class="hlt">heat</span> <span class="hlt">flux</span> having a major contribution to it. The anomalous latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> between atmosphere and ocean surface play important role in the growth of observed summertime SST anomaly. Sea-surface height also shows similar out-of-phase signatures over the two basins and are well correlated with the ENSO related SST anomalies. It is also observed that the magnitude of ENSO related anomalies over the southern ocean are weaker in LaNina years than in El Nino years, suggesting an intensified tropics-<span class="hlt">high</span> latitude tele-connection during warm phases of ENSO.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/21192402-electron-impact-emission-spectroscopy-flux-sensor-monitoring-deposition-rate-high-background-gas-pressure-improved-accuracy','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/21192402-electron-impact-emission-spectroscopy-flux-sensor-monitoring-deposition-rate-high-background-gas-pressure-improved-accuracy"><span>An <span class="hlt">electron</span> impact emission spectroscopy <span class="hlt">flux</span> sensor for monitoring deposition rate at <span class="hlt">high</span> background gas pressure with improved accuracy</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Lu, C.; Blissett, C. D.; Diehl, G.</p> <p>2008-07-15</p> <p><span class="hlt">Electron</span> impact emission spectroscopy (EIES) has been proven to be a critical tool for film composition control during codeposition processes for the fabrication of multicomponent thin film materials including the <span class="hlt">high</span>-efficiency copper-indium-gallium-diselenide photovoltaic cells. This technique is <span class="hlt">highly</span> specific to atomic species because the emission spectrum of each element is unique, and the typical width of atomic emission lines is very narrow. Noninterfering emission lines can generally be allocated to different atomic species. However, the <span class="hlt">electron</span> impact emission spectra of many molecular species are often broadband in nature. When the optical emission from an EIES sensor is measured by usingmore » a wavelength selection device with a modest resolution, such as an optical filter or monochromator, the emissions from common residual gases may interfere with that from the vapor <span class="hlt">flux</span> and cause erroneous <span class="hlt">flux</span> measurement. The interference is most pronounced when measuring low <span class="hlt">flux</span> density with the presence of gases such as in reactive deposition processes. This problem is solved by using a novel EIES sensor that has two <span class="hlt">electron</span> impact excitation sources in separate compartments but with one common port for optical output. The vapor <span class="hlt">flux</span> is allowed to pass through one compartment only. Using a tristate excitation scheme and appropriate signal processing technique, the interfering signals from residual gases can be completely eliminated from the output signal of the EIES monitor for process control. Data obtained from Cu and Ga evaporations with the presence of common residual gases such as CO{sub 2} and H{sub 2}O are shown to demonstrate the improvement in sensor performance. The new EIES sensor is capable of eliminating the effect of interfering residual gases with pressure as <span class="hlt">high</span> as in the upper 10{sup -5} Torr range.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880009508','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880009508"><span>Prototype thin-film thermocouple/<span class="hlt">heat-flux</span> sensor for a ceramic-insulated diesel engine</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kim, Walter S.; Barrows, Richard F.</p> <p>1988-01-01</p> <p>A platinum versus platinum-13 percent rhodium thin-film thermocouple/<span class="hlt">heat-flux</span> sensor was devised and tested in the harsh, <span class="hlt">high</span>-temperature environment of a ceramic-insulated, low-<span class="hlt">heat</span>-rejection diesel engine. The sensor probe assembly was developed to provide experimental validation of <span class="hlt">heat</span> transfer and thermal analysis methodologies applicable to the insulated diesel engine concept. The thin-film thermocouple configuration was chosen to approximate an uninterrupted chamber surface and provide a 1-D <span class="hlt">heat-flux</span> path through the probe body. The engine test was conducted by Purdue University for Integral Technologies, Inc., under a DOE-funded contract managed by NASA Lewis Research Center. The thin-film sensor performed reliably during 6 to 10 hr of repeated engine runs at indicated mean surface temperatures up to 950 K. However, the sensor suffered partial loss of adhesion in the thin-film thermocouple junction area following maximum cyclic temperature excursions to greater than 1150 K.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950053067&hterms=TIDE+POOLS&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DTIDE%2BPOOLS','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950053067&hterms=TIDE+POOLS&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DTIDE%2BPOOLS"><span>Tidal and atmospheric forcing of the upper ocean in the Gulf of California. 2: Surface <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Paden, Cynthia A.; Winant, Clinton D.; Abbott, Mark R.</p> <p>1993-01-01</p> <p>Satellite infrared imagery and coastal meteorological data for March 1984 through February 1985 are used to estimate the net annual surface <span class="hlt">heat</span> <span class="hlt">flux</span> for the northern Gulf of California. The average annual surface <span class="hlt">heat</span> <span class="hlt">flux</span> for the area north of Guaymas and Santa Rosalia is estimated to be +74 W/sq m for the 1984-1985 time period. This is comparable to the +20-50 W/sq m previously obtained from <span class="hlt">heat</span> and freshwater transport estimates made with hydrographic surveys from different years and months. The spatial distribution of the net surface <span class="hlt">heat</span> <span class="hlt">flux</span> shows a net gain of <span class="hlt">heat</span> over the whole northern gulf. Except for a local maximum near San Esteban Island, the largest <span class="hlt">heat</span> gain (+110-120 W/sq m) occurs in the Ballenas and Salsipuedes channels, where strong tidal mixing produces anomalously cold sea surface temperatures (SSTs) over much of the year. The lowest <span class="hlt">heat</span> gain occurs in the Guayamas Basin (+40-50 W/sq m), where SSTs are consistently warmer. In the relatively shallow northern basin the net surface <span class="hlt">heat</span> <span class="hlt">flux</span> is farily uniform, with a net annual gain of approxmately +70 W/sq m. A local minimum in <span class="hlt">heat</span> gain (approximately +60 W/sq m) is observed over the shelf in the northwest, where spring and summer surface temperatures are particularly <span class="hlt">high</span>. A similar minimum in <span class="hlt">heat</span> gain over the shelf was observed in a separate study in which historical SSTs and 7 years (1979-1986) of meteorological data from Puerto Penasco were used to estimate the net surface <span class="hlt">heat</span> <span class="hlt">flux</span> for the northern basin. In that study, however, the <span class="hlt">heat</span> <span class="hlt">fluxes</span> were higher, with a gain of +100 W/sq m over the shelf and +114 W/sq m in the northern basin. These larger values are directly attributable to the higher humidities in the 1979-1986 study compared to the 1984-1985 satellite study. <span class="hlt">High</span> humidities reduce evaporation and the associated latent <span class="hlt">heat</span> loss, promoting a net annual <span class="hlt">heat</span> gain. In the norther Gulf of California, however, tidal mixing appears to play a key role in the observed gain of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DPPJP2043P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DPPJP2043P"><span>Scaling Relationships for ELM Diverter <span class="hlt">Heat</span> <span class="hlt">Flux</span> on DIII D</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Peters, E. A.; Makowski, M. A.; Leonard, A. W.</p> <p>2015-11-01</p> <p>Edge Localized Modes (ELMs) are periodic plasma instabilities that occur during H-mode operation in tokamaks. Left unmitigated, these instabilities result in concentrated particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> at the divertor and stand to cause serious damage to the plasma facing components of tokamaks. The purpose of this research is to find scaling relationships that predict divertor <span class="hlt">heat</span> <span class="hlt">flux</span> due to ELMs based on plasma parameters at the time of instability. This will be accomplished by correlating characteristic ELM parameters with corresponding plasma measurements and analyzing the data for trends. One early assessment is the effect of the <span class="hlt">heat</span> transmission coefficient ? on the in/out asymmetry of the calculated ELM <span class="hlt">heat</span> <span class="hlt">fluxes</span>. Using IR camera data, further assessments in this study will continue to emphasize in/out asymmetry in ELMs, as this has important implications for ITER operation. Work supported in part by the US DOE, DE-AC52-07NA27344, DE-FC02-04ER54698, Office of Workforce Development for Teachers and Scientists (WDTS) under the Science Undergraduate Laboratory Internships Program (SULI).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMNG21A0138D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMNG21A0138D"><span>The Influence of <span class="hlt">Heat</span> <span class="hlt">Flux</span> Boundary Heterogeneity on <span class="hlt">Heat</span> Transport in Earth's Core</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Davies, C. J.; Mound, J. E.</p> <p>2017-12-01</p> <p>Rotating convection in planetary systems can be subjected to large lateral variations in <span class="hlt">heat</span> <span class="hlt">flux</span> from above; for example, due to the interaction between the metallic cores of terrestrial planets and their overlying silicate mantles. The boundary anomalies can significantly reorganise the pattern of convection and influence global diagnostics such as the Nusselt number. We have conducted a suite of numerical simulations of rotating convection in a spherical shell geometry comparing convection with homogeneous boundary conditions to that with two patterns of <span class="hlt">heat</span> <span class="hlt">flux</span> variation at the outer boundary: one hemispheric pattern, and one derived from seismic tomographic imaging of Earth's lower mantle. We consider Ekman numbers down to 10-6 and <span class="hlt">flux</span>-based Rayleigh numbers up to 800 times critical. The heterogeneous boundary conditions tend to increase the Nusselt number relative to the equivalent homogeneous case by altering both the flow and temperature fields, particularly near the top of the convecting region. The enhancement in Nusselt number tends to increase as the amplitude and wavelength of the boundary heterogeneity is increased and as the system becomes more supercritical. In our suite of models, the increase in Nusselt number can be as large as 25%. The slope of the Nusselt-Rayleigh scaling also changes when boundary heterogeneity is included, which has implications when extrapolating to planetary conditions. Additionally, regions of effective thermal stratification can develop when strongly heterogeneous <span class="hlt">heat</span> <span class="hlt">flux</span> conditions are applied at the outer boundary.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/19747','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/19747"><span>An inverse method to estimate stem surface <span class="hlt">heat</span> <span class="hlt">flux</span> in wildland fires</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Anthony S. Bova; Matthew B. Dickinson</p> <p>2009-01-01</p> <p>Models of wildland fire-induced stem <span class="hlt">heating</span> and tissue necrosis require accurate estimates of inward <span class="hlt">heat</span> <span class="hlt">flux</span> at the bark surface. Thermocouple probes or <span class="hlt">heat</span> <span class="hlt">flux</span> sensors placed at a stem surface do not mimic the thermal response of tree bark to flames.We show that data from thin thermocouple probes inserted just below the bark can be used, by means of a one-...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70033363','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70033363"><span>Modern perspectives on measuring and interpreting seafloor <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Harris, Reid N.; Fisher, A.; Ruppel, C.; Martinez, F.</p> <p>2008-01-01</p> <p>There has been a resurgence of interest in marine <span class="hlt">heat</span> flow in the past 10–15 years, coinciding with fundamental achievements in understanding the Earth's thermal state and quantifying the dynamics and impacts of material and energy <span class="hlt">fluxes</span> within and between the lithosphere and hydrosphere. At the same time, technical capabilities have dwindled to the point that no U.S. academic institution currently operates a seagoing <span class="hlt">heat</span> flow capacity.In September 2007, a workshop was convened in Salt Lake City with sponsorship from the U.S. National Science Foundation (NSF) and participation by scientists and engineers from North America, Europe, and Asia. The primary goals of the workshop were to (1) assess <span class="hlt">high</span>-priority scientific and technical needs and (2) to evaluate options for developing and maintaining essential capabilities in marine <span class="hlt">heat</span> flow for the U.S. scientific community.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JGRA..123.3646S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JGRA..123.3646S"><span>A Distributed Lag Autoregressive Model of Geostationary Relativistic <span class="hlt">Electron</span> <span class="hlt">Fluxes</span>: Comparing the Influences of Waves, Seed and Source <span class="hlt">Electrons</span>, and Solar Wind Inputs</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Simms, Laura; Engebretson, Mark; Clilverd, Mark; Rodger, Craig; Lessard, Marc; Gjerloev, Jesper; Reeves, Geoffrey</p> <p>2018-05-01</p> <p>Relativistic <span class="hlt">electron</span> <span class="hlt">flux</span> at geosynchronous orbit depends on enhancement and loss processes driven by ultralow frequency (ULF) Pc5, chorus, and electromagnetic ion cyclotron (EMIC) waves, seed <span class="hlt">electron</span> <span class="hlt">flux</span>, magnetosphere compression, the "Dst effect," and substorms, while solar wind inputs such as velocity, number density, and interplanetary magnetic field Bz drive these factors and thus correlate with <span class="hlt">flux</span>. Distributed lag regression models show the time delay of highest influence of these factors on log10 <span class="hlt">high</span>-energy <span class="hlt">electron</span> <span class="hlt">flux</span> (0.7-7.8 MeV, Los Alamos National Laboratory satellites). Multiple regression with an autoregressive term (<span class="hlt">flux</span> persistence) allows direct comparison of the magnitude of each effect while controlling other correlated parameters. <span class="hlt">Flux</span> enhancements due to ULF Pc5 and chorus waves are of equal importance. The direct effect of substorms on <span class="hlt">high</span>-energy <span class="hlt">electron</span> <span class="hlt">flux</span> is strong, possibly due to injection of <span class="hlt">high</span>-energy <span class="hlt">electrons</span> by the substorms themselves. Loss due to electromagnetic ion cyclotron waves is less influential. Southward Bz shows only moderate influence when correlated processes are accounted for. Adding covariate compression effects (pressure and interplanetary magnetic field magnitude) allows wave-driven enhancements to be more clearly seen. Seed <span class="hlt">electrons</span> (270 keV) are most influential at lower relativistic energies, showing that such a population must be available for acceleration. However, they are not accelerated directly to the highest energies. Source <span class="hlt">electrons</span> (31.7 keV) show no direct influence when other factors are controlled. Their action appears to be indirect via the chorus waves they generate. Determination of specific effects of each parameter when studied in combination will be more helpful in furthering modeling work than studying them individually.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19740027928&hterms=1091&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3D%2526%25231091','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19740027928&hterms=1091&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3D%2526%25231091"><span>Anode power deposition in quasi-steady MPD arcs. [accelerator anode <span class="hlt">heat</span> <span class="hlt">flux</span> measurement</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Saber, A. J.; Jahn, R. G.</p> <p>1973-01-01</p> <p>The power deposited in the anode of a quasi-steady MPD accelerator has been measured directly by thermocouples attached to the inside surface of a shell anode which provide a local measurement of anode <span class="hlt">heat</span> <span class="hlt">flux</span>. The results over a range of arc currents from 5.5 to 44 kiloamperes and argon mass flows from 1 g/sec to 48 g/sec show that the fraction of the total input power deposited in the anode decreases drastically from 50% at an arc power of 200 kW to 10% at 20 MW, and that anode power is not uniformly deposited in the anode. A theoretical model of the anode <span class="hlt">heat</span> transfer, including effects of anode work function, <span class="hlt">electron</span> thermal energy, and anode sheath, can be brought into reasonable agreement with the measurements, provided the effective range of the conduction <span class="hlt">electrons</span> from within the discharge plasma to the anode surface is properly acknowledged.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1356713-analysis-edge-stability-models-heat-flux-width','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1356713-analysis-edge-stability-models-heat-flux-width"><span>Analysis of edge stability for models of <span class="hlt">heat</span> <span class="hlt">flux</span> width</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Makowski, Michael A.; Lasnier, Charles J.; Leonard, Anthony W.; ...</p> <p>2017-05-12</p> <p>Detailed measurements of the n e, and T e, and T i profiles in the vicinity of the separatrix of ELMing H-mode discharges have been used to examine plasma stability at the extreme edge of the plasma and assess stability dependent models of the <span class="hlt">heat</span> <span class="hlt">flux</span> width. The results are strongly contrary to the critical gradient model, which posits that a ballooning instability determines a gradient scale length related to the <span class="hlt">heat</span> <span class="hlt">flux</span> width. The results of this analysis are not sensitive to the choice of location to evaluate stability. Significantly, it is also found that the results are completelymore » consistent with the heuristic drift model for the <span class="hlt">heat</span> <span class="hlt">flux</span> width. Here the edge pressure gradient scales with plasma density and is proportional to the pressure gradient inferred from the equilibrium in accordance with the predictions of that theory.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910009750','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910009750"><span>Development of a laser-induced <span class="hlt">heat</span> <span class="hlt">flux</span> technique for measurement of convective <span class="hlt">heat</span> transfer coefficients in a supersonic flowfield</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Porro, A. Robert; Keith, Theo G., Jr.; Hingst, Warren R.; Chriss, Randall M.; Seablom, Kirk D.</p> <p>1991-01-01</p> <p>A technique is developed to measure the local convective <span class="hlt">heat</span> transfer coefficient on a model surface in a supersonic flow field. The technique uses a laser to apply a discrete local <span class="hlt">heat</span> <span class="hlt">flux</span> at the model test surface, and an infrared camera system determines the local temperature distribution due to <span class="hlt">heating</span>. From this temperature distribution and an analysis of the <span class="hlt">heating</span> process, a local convective <span class="hlt">heat</span> transfer coefficient is determined. The technique was used to measure the load surface convective <span class="hlt">heat</span> transfer coefficient distribution on a flat plate at nominal Mach numbers of 2.5, 3.0, 3.5, and 4.0. The flat plate boundary layer initially was laminar and became transitional in the measurement region. The experimental results agreed reasonably well with theoretical predictions of convective <span class="hlt">heat</span> transfer of flat plate laminar boundary layers. The results indicate that this non-intrusive optical measurement technique has the potential to obtain <span class="hlt">high</span> quality surface convective <span class="hlt">heat</span> transfer measurements in <span class="hlt">high</span> speed flowfields.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..DPPPI2005M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..DPPPI2005M"><span>Analysis of a Multi-Machine Database on Divertor <span class="hlt">Heat</span> <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Makowski, M. A.</p> <p>2011-10-01</p> <p>A coordinated effort to measure divertor <span class="hlt">heat</span> <span class="hlt">flux</span> characteristics in fully attached, similarly shaped H-mode plasmas on C-Mod, DIII-D and NSTX was carried out in 2010 in order to construct a predictive scaling relation applicable to next step devices including ITER, FNSF, and DEMO. Few published scaling laws are available and those that have been published were obtained under widely varying conditions and divertor geometries, leading to conflicting predictions for this critically important quantity. This study was designed to overcome these deficiencies. Corresponding plasma parameters were systematically varied in each tokamak, resulting in a combined data set in which Ip varies by a factor 3, Bt varies by a factor of 14.5, and major radius varies by a factor of 2.6. The derived scaling relation consistently predicts narrower <span class="hlt">heat</span> <span class="hlt">flux</span> widths than relations currently in use. Analysis of the combined data set reveals that the primary dependence of the parallel <span class="hlt">heat</span> <span class="hlt">flux</span> width is robustly inverse with Ip. All three tokamaks independently demonstrate this dependence. The midplane SOL profiles in DIII-D are also found to steepen with higher Ip, similar to the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> profiles. Weaker dependencies on the toroidal field and normalized Greenwald density, fGW, are also found, but vary across devices and with the measure of the <span class="hlt">heat</span> <span class="hlt">flux</span> width used, either FWHM or integral width. In the combined data set, the strongest size scaling is with minor radius resulting in an approximately linear dependence on a /Ip . This suggests a scaling correlated with the inverse of the poloidal field, as would be expected for critical gradient or drift-based transport. Supported by the US DOE under DE-AC52-07NA27344 and DE-FC02-04ER54698.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/11874138','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/11874138"><span>Methodology for estimation of time-dependent surface <span class="hlt">heat</span> <span class="hlt">flux</span> due to cryogen spray cooling.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tunnell, James W; Torres, Jorge H; Anvari, Bahman</p> <p>2002-01-01</p> <p>Cryogen spray cooling (CSC) is an effective technique to protect the epidermis during cutaneous laser therapies. Spraying a cryogen onto the skin surface creates a time-varying <span class="hlt">heat</span> <span class="hlt">flux</span>, effectively cooling the skin during and following the cryogen spurt. In previous studies mathematical models were developed to predict the human skin temperature profiles during the cryogen spraying time. However, no studies have accounted for the additional cooling due to residual cryogen left on the skin surface following the spurt termination. We formulate and solve an inverse <span class="hlt">heat</span> conduction (IHC) problem to predict the time-varying surface <span class="hlt">heat</span> <span class="hlt">flux</span> both during and following a cryogen spurt. The IHC formulation uses measured temperature profiles from within a medium to estimate the surface <span class="hlt">heat</span> <span class="hlt">flux</span>. We implement a one-dimensional sequential function specification method (SFSM) to estimate the surface <span class="hlt">heat</span> <span class="hlt">flux</span> from internal temperatures measured within an in vitro model in response to a cryogen spurt. Solution accuracy and experimental errors are examined using simulated temperature data. <span class="hlt">Heat</span> <span class="hlt">flux</span> following spurt termination appears substantial; however, it is less than that during the spraying time. The estimated time-varying <span class="hlt">heat</span> <span class="hlt">flux</span> can subsequently be used in forward <span class="hlt">heat</span> conduction models to estimate temperature profiles in skin during and following a cryogen spurt and predict appropriate timing for onset of the laser pulse.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_20 --> <div id="page_21" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="401"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930032422&hterms=thin+film+fabrication&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dthin%2Bfilm%2Bfabrication','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930032422&hterms=thin+film+fabrication&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dthin%2Bfilm%2Bfabrication"><span>Fabrication of thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensors</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Will, Herbert</p> <p>1991-01-01</p> <p>Thin-film <span class="hlt">heat-flux</span> sensors have been constructed in the form of arrays of thermocouples on upper and lower surfaces of an insulating layer, so that <span class="hlt">flux</span> values are proportional to the temperature difference across the upper and lower surface of the insulation material. The sensor thermocouples are connected in thermopile arrangement, and the structure is patterned with photolithographic techniques. Both chromel-alumel and Pt-Pt/Rh thermocouples have been devised; the later produced 28 microvolts when exposed to the radiation of a 1000 C furnace.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/34711','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/34711"><span>Fine fuel <span class="hlt">heating</span> by radiant <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>David Frankman; Brent W. Webb; Bret W. Butler; Don J. Latham</p> <p>2010-01-01</p> <p>Experiments were conducted wherein wood shavings and Ponderosa pine needles in quiescent air were subjected to a steady radiation <span class="hlt">heat</span> <span class="hlt">flux</span> from a planar ceramic burner. The internal temperature of these particles was measured using fine diameter (0.076mm diameter) type K thermocouples. A narrow angle radiometer was used to determine the emissive power generated by the...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/813610','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/813610"><span>Infrared Camera Diagnostic for <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements on NSTX</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>D. Mastrovito; R. Maingi; H.W. Kugel</p> <p>2003-03-25</p> <p>An infrared imaging system has been installed on NSTX (National Spherical Torus Experiment) at the Princeton Plasma Physics Laboratory to measure the surface temperatures on the lower divertor and center stack. The imaging system is based on an Indigo Alpha 160 x 128 microbolometer camera with 12 bits/pixel operating in the 7-13 {micro}m range with a 30 Hz frame rate and a dynamic temperature range of 0-700 degrees C. From these data and knowledge of graphite thermal properties, the <span class="hlt">heat</span> <span class="hlt">flux</span> is derived with a classic one-dimensional conduction model. Preliminary results of <span class="hlt">heat</span> <span class="hlt">flux</span> scaling are reported.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030062138','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030062138"><span>Microsample Characterization of Coatings for Grcop-84 for <span class="hlt">High</span> <span class="hlt">Heat</span> <span class="hlt">Flux</span> Applications</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hemker, Kevin</p> <p>2003-01-01</p> <p>A multidisciplinary Johns Hopkins University-NASA Glenn team is undertaking a collaborative research program to elucidate and model the thermal stability and mechanical integrity of candidate coatings for GRCop-84. GRCop-84 is a <span class="hlt">high</span> conductivity, <span class="hlt">high</span> strength copper alloy that was recently developed at NASA Glenn for use in <span class="hlt">high</span> temperature, <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> applications. With potential applications in rocket motor combustion chamber liners, nozzle ramps and other actively cooled structures, this new material offers great potential for decreasing weight and increasing reliability of third generation reusable launch vehicles. Current emphasis has turned toward the development of environmentally resistant and thermal barrier coatings for this alloy. Metallic coatings such as NiCrAlY and Cu-8-30%Cr have shown promise in: prohibiting blanching, reducing dog-house failures, increasing operating temperatures and decreasing cooling requirements. The focus of this research program is to develop a fundamental understanding of the substrate-coating interactions that occur during thermal cycling (inter-diffusion, viscoplasticity, morphological evolution, crack formation, etc.) and to derive a science-based protocol for future coating selection, optimization and reliability assurance. The microsample tensile testing approach adopted for this study allows us to characterize small-scale and <span class="hlt">highly</span> scale-specific coatings and properties in a way not possible by conventional means. In addition to providing much needed design data, the integration of microsample testing with detailed microstructural observations provides a mechanistic foundation for coating optimization and life prediction modeling.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22663622-sunward-propagating-solar-energetic-electrons-inside-multiple-interplanetary-flux-ropes','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22663622-sunward-propagating-solar-energetic-electrons-inside-multiple-interplanetary-flux-ropes"><span>Sunward-propagating Solar Energetic <span class="hlt">Electrons</span> inside Multiple Interplanetary <span class="hlt">Flux</span> Ropes</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Gómez-Herrero, Raúl; Hidalgo, Miguel A.; Carcaboso, Fernando</p> <p>2017-05-10</p> <p>On 2013 December 2 and 3, the SEPT and STE instruments on board STEREO-A observed two solar energetic <span class="hlt">electron</span> events with unusual sunward-directed <span class="hlt">fluxes</span>. Both events occurred during a time interval showing typical signatures of interplanetary coronal mass ejections (ICMEs). The <span class="hlt">electron</span> timing and anisotropies, combined with extreme-ultraviolet solar imaging and radio wave spectral observations, are used to confirm the solar origin and the injection times of the energetic <span class="hlt">electrons</span>. The solar source of the ICME is investigated using remote-sensing observations and a three-dimensional reconstruction technique. In situ plasma and magnetic field data combined with energetic <span class="hlt">electron</span> observations and amore » <span class="hlt">flux</span>-rope model are used to determine the ICME magnetic topology and the interplanetary <span class="hlt">electron</span> propagation path from the Sun to 1 au. Two consecutive <span class="hlt">flux</span> ropes crossed the STEREO-A location and each <span class="hlt">electron</span> event occurred inside a different <span class="hlt">flux</span> rope. In both cases, the <span class="hlt">electrons</span> traveled from the solar source to 1 au along the longest legs of the <span class="hlt">flux</span> ropes still connected to the Sun. During the December 2 event, energetic <span class="hlt">electrons</span> propagated along the magnetic field, while during the December 3 event they were propagating against the field. As found by previous studies, the energetic <span class="hlt">electron</span> propagation times are consistent with a low number of field line rotations N < 5 of the <span class="hlt">flux</span> rope between the Sun and 1 au. The <span class="hlt">flux</span> rope model used in this work suggests an even lower number of rotations.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011E%26PSL.306..205Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011E%26PSL.306..205Z"><span><span class="hlt">Heat</span> <span class="hlt">fluxes</span> at the Earth's surface and core-mantle boundary since Pangea formation and their implications for the geomagnetic superchrons</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Nan; Zhong, Shijie</p> <p>2011-06-01</p> <p>The Earth's surface and core-mantle boundary (CMB) <span class="hlt">heat</span> <span class="hlt">fluxes</span> are controlled by mantle convection and have important influences on Earth's thermal evolution and geodynamo processes in the core. However, the long-term variations of the surface and CMB <span class="hlt">heat</span> <span class="hlt">fluxes</span> remain poorly understood, particularly in response to the supercontinent Pangea — likely the most significant global tectonic event in the last 500 Ma. In this study, we reconstruct temporal evolution of the surface and CMB <span class="hlt">heat</span> <span class="hlt">fluxes</span> since the Paleozoic by formulating three-dimensional spherical models of mantle convection with plate motion history for the last 450 Ma that includes the assembly and break-up of supercontinent Pangea. Our models reproduce well present-day observations of the surface <span class="hlt">heat</span> <span class="hlt">flux</span> and seafloor age distribution. Our models show that the present-day CMB <span class="hlt">heat</span> <span class="hlt">flux</span> is low below the central Pacific and Africa but <span class="hlt">high</span> elsewhere due to subducted slabs, particularly when chemically dense piles are present above the CMB. We show that while the surface <span class="hlt">heat</span> <span class="hlt">flux</span> may not change significantly in response to Pangea assembly, it increases by ~ 16% from 200 to 120 Ma ago as a result of Pangea breakup and then decreases for the last 120 Ma to approximately the pre-200 Ma value. As consequences of the assembly and breakup of Pangea, equatorial CMB <span class="hlt">heat</span> <span class="hlt">flux</span> reaches minimum at ~ 270 Ma and again at ~ 100 Ma ago, while global CMB <span class="hlt">heat</span> <span class="hlt">flux</span> is a maximum at ~ 100 Ma ago. These extrema in CMB <span class="hlt">heat</span> <span class="hlt">fluxes</span> coincide with the Kiaman (316-262 Ma) and Cretaceous (118-83 Ma) Superchrons, respectively, and may be responsible for the Superchrons.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APJAS..49..443P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APJAS..49..443P"><span><span class="hlt">Heat</span> <span class="hlt">flux</span> variations over sea ice observed at the coastal area of the Sejong Station, Antarctica</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Park, Sang-Jong; Choi, Tae-Jin; Kim, Seong-Joong</p> <p>2013-08-01</p> <p>This study presents variations of sensible <span class="hlt">heat</span> <span class="hlt">flux</span> and latent <span class="hlt">heat</span> <span class="hlt">flux</span> over sea ice observed in 2011 from the 10-m <span class="hlt">flux</span> tower located at the coast of the Sejong Station on King George Island, Antarctica. A period from July to September was selected as a sea ice period based on daily record of sea state and hourly photos looking at the Marian Cove in front of the Sejong Station. For the sea ice period, mean sensible <span class="hlt">heat</span> <span class="hlt">flux</span> is about -11 Wm-2, latent <span class="hlt">heat</span> <span class="hlt">flux</span> is about +2 W m-2, net radiation is -12 W m-2, and residual energy is -3 W m-2 with clear diurnal variations. Estimated mean values of surface exchange coefficients for momentum, <span class="hlt">heat</span> and moisture are 5.15 × 10-3, 1.19 × 10-3, and 1.87 × 10-3, respectively. The observed exchange coefficients of <span class="hlt">heat</span> shows clear diurnal variations while those of momentum and moisture do not show diurnal variation. The parameterized exchange coefficients of <span class="hlt">heat</span> and moisture produces <span class="hlt">heat</span> <span class="hlt">fluxes</span> which compare well with the observed diurnal variations of <span class="hlt">heat</span> <span class="hlt">fluxes</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820009925','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820009925"><span>Sensitivity of a climatologically-driven sea ice model to the ocean <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Parkinson, C. L.; Good, M. R.</p> <p>1982-01-01</p> <p>Ocean <span class="hlt">heat</span> <span class="hlt">flux</span> sensitivity was studied on a numerical model of sea ice covering the Weddell Sea region of the southern ocean. The model is driven by mean monthly climatological atmospheric variables. For each model run, the ocean <span class="hlt">heat</span> <span class="hlt">flux</span> is uniform in both space and time. Ocean <span class="hlt">heat</span> <span class="hlt">fluxes</span> below 20 W m to the minus 2 power do not provide sufficient energy to allow the ice to melt to its summertime thicknesses and concentrations by the end of the 14 month simulation, whereas ocean <span class="hlt">heat</span> <span class="hlt">fluxes</span> of 30 W m to the minus 2 power and above result in too much ice melt, producing the almost total disappearance of ice in the Weddell Sea by the end of the 14 months. These results are dependent on the atmospheric forcing fields.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100005642','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100005642"><span>Fabrication and Testing of a Thin-Film <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensor for a Stirling Convertor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wilson, Scott D.; Fralick, Gus c.; Wrbanek, John D.; Sayir, Ali</p> <p>2010-01-01</p> <p>The NASA Glenn Research Center (GRC) has been testing <span class="hlt">high</span>-efficiency free-piston Stirling convertors for potential use in radioisotope power systems since 1999. Stirling convertors are being operated for many years to demonstrate a radioisotope power system capable of providing reliable power for potential multiyear missions. Techniques used to monitor the convertors for change in performance include measurements of temperature, pressure, energy addition, and energy rejection. Micro-porous bulk insulation is used in the Stirling convertor test setup to minimize the loss of thermal energy from the electric <span class="hlt">heat</span> source to the environment. The insulation is characterized before extended operation, enabling correlation of the net thermal energy addition to the convertor. Aging micro-porous bulk insulation changes insulation efficiency, introducing errors in the correlation for net thermal energy addition. A thin-film <span class="hlt">heat</span> <span class="hlt">flux</span> sensor was designed and fabricated to directly measure the net thermal energy addition to the Stirling convertor. The fabrication techniques include slipcasting and using Physical Vapor Deposition (PVD). One-micron-thick noble metal thermocouples measure temperature on the surface of an alumina ceramic disk and <span class="hlt">heat</span> <span class="hlt">flux</span> is calculated. Fabrication, integration, and test results of a thin-film <span class="hlt">heat</span> <span class="hlt">flux</span> sensor are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JGRC..122..726R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JGRC..122..726R"><span>Surface <span class="hlt">flux</span> and ocean <span class="hlt">heat</span> transport convergence contributions to seasonal and interannual variations of ocean <span class="hlt">heat</span> content</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Roberts, C. D.; Palmer, M. D.; Allan, R. P.; Desbruyeres, D. G.; Hyder, P.; Liu, C.; Smith, D.</p> <p>2017-01-01</p> <p>We present an observation-based <span class="hlt">heat</span> budget analysis for seasonal and interannual variations of ocean <span class="hlt">heat</span> content (H) in the mixed layer (Hmld) and full-depth ocean (Htot). Surface <span class="hlt">heat</span> <span class="hlt">flux</span> and ocean <span class="hlt">heat</span> content estimates are combined using a novel Kalman smoother-based method. Regional contributions from ocean <span class="hlt">heat</span> transport convergences are inferred as a residual and the dominant drivers of Hmld and Htot are quantified for seasonal and interannual time scales. We find that non-Ekman ocean <span class="hlt">heat</span> transport processes dominate Hmld variations in the equatorial oceans and regions of strong ocean currents and substantial eddy activity. In these locations, surface temperature anomalies generated by ocean dynamics result in turbulent <span class="hlt">flux</span> anomalies that drive the overlying atmosphere. In addition, we find large regions of the Atlantic and Pacific oceans where <span class="hlt">heat</span> transports combine with local air-sea <span class="hlt">fluxes</span> to generate mixed layer temperature anomalies. In all locations, except regions of deep convection and water mass transformation, interannual variations in Htot are dominated by the internal rearrangement of <span class="hlt">heat</span> by ocean dynamics rather than the loss or addition of <span class="hlt">heat</span> at the surface. Our analysis suggests that, even in extratropical latitudes, initialization of ocean dynamical processes could be an important source of skill for interannual predictability of Hmld and Htot. Furthermore, we expect variations in Htot (and thus thermosteric sea level) to be more predictable than near surface temperature anomalies due to the increased importance of ocean <span class="hlt">heat</span> transport processes for full-depth <span class="hlt">heat</span> budgets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140016851','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140016851"><span>Impacts of Soil-aquifer <span class="hlt">Heat</span> and Water <span class="hlt">Fluxes</span> on Simulated Global Climate</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Krakauer, N.Y.; Puma, Michael J.; Cook, B. I.</p> <p>2013-01-01</p> <p>Climate models have traditionally only represented <span class="hlt">heat</span> and water <span class="hlt">fluxes</span> within relatively shallow soil layers, but there is increasing interest in the possible role of <span class="hlt">heat</span> and water exchanges with the deeper subsurface. Here, we integrate an idealized 50m deep aquifer into the land surface module of the GISS ModelE general circulation model to test the influence of aquifer-soil moisture and <span class="hlt">heat</span> exchanges on climate variables. We evaluate the impact on the modeled climate of aquifer-soil <span class="hlt">heat</span> and water <span class="hlt">fluxes</span> separately, as well as in combination. The addition of the aquifer to ModelE has limited impact on annual-mean climate, with little change in global mean land temperature, precipitation, or evaporation. The seasonal amplitude of deep soil temperature is strongly damped by the soil-aquifer <span class="hlt">heat</span> <span class="hlt">flux</span>. This not only improves the model representation of permafrost area but propagates to the surface, resulting in an increase in the seasonal amplitude of surface air temperature of >1K in the Arctic. The soil-aquifer water and <span class="hlt">heat</span> <span class="hlt">fluxes</span> both slightly decrease interannual variability in soil moisture and in landsurface temperature, and decrease the soil moisture memory of the land surface on seasonal to annual timescales. The results of this experiment suggest that deepening the modeled land surface, compared to modeling only a shallower soil column with a no-<span class="hlt">flux</span> bottom boundary condition, has limited impact on mean climate but does affect seasonality and interannual persistence.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/491560','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/491560"><span>Critical <span class="hlt">heat</span> <span class="hlt">flux</span> (CHF) phenomenon on a downward facing curved surface</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Cheung, F.B.; Haddad, K.H.; Liu, Y.C.</p> <p>1997-06-01</p> <p>This report describes a theoretical and experimental study of the boundary layer boiling and critical <span class="hlt">heat</span> <span class="hlt">flux</span> phenomena on a downward facing curved <span class="hlt">heating</span> surface, including both hemispherical and toroidal surfaces. A subscale boundary layer boiling (SBLB) test facility was developed to measure the spatial variation of the critical <span class="hlt">heat</span> <span class="hlt">flux</span> and observe the underlying mechanisms. Transient quenching and steady-state boiling experiments were performed in the SBLB facility under both saturated and subcooled conditions to obtain a complete database on the critical <span class="hlt">heat</span> <span class="hlt">flux</span>. To complement the experimental effort, an advanced hydrodynamic CHF model was developed from the conservation lawsmore » along with sound physical arguments. The model provides a clear physical explanation for the spatial variation of the CHF observed in the SBLB experiments and for the weak dependence of the CHF data on the physical size of the vessel. Based upon the CHF model, a scaling law was established for estimating the local critical <span class="hlt">heat</span> <span class="hlt">flux</span> on the outer surface of a <span class="hlt">heated</span> hemispherical vessel that is fully submerged in water. The scaling law, which compares favorably with all the available local CHF data obtained for various vessel sizes, can be used to predict the local CHF limits on large commercial-size vessels. This technical information represents one of the essential elements that is needed in assessing the efficacy of external cooling of core melt by cavity flooding as a severe accident management strategy. 83 figs., 3 tabs.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920018134','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920018134"><span>Turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> measurements in a transitional boundary layer</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Sohn, K. H.; Zaman, K. B. M. Q.; Reshotko, E.</p> <p>1992-01-01</p> <p>During an experimental investigation of the transitional boundary layer over a <span class="hlt">heated</span> flat plate, an unexpected result was encountered for the turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> (bar-v't'). This quantity, representing the correlation between the fluctuating normal velocity and the temperature, was measured to be negative near the wall under certain conditions. The result was unexpected as it implied a counter-gradient <span class="hlt">heat</span> transfer by the turbulent fluctuations. Possible reasons for this anomalous result were further investigated. The possible causes considered for this negative bar-v't' were: (1) plausible measurement error and peculiarity of the flow facility, (2) large probe size effect, (3) 'streaky structure' in the near wall boundary layer, and (4) contributions from other terms usually assumed negligible in the energy equation including the Reynolds <span class="hlt">heat</span> <span class="hlt">flux</span> in the streamwise direction (bar-u't'). Even though the energy balance has remained inconclusive, none of the items (1) to (3) appear to be contributing directly to the anomaly.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JInst..12C2045T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JInst..12C2045T"><span>Characterisation of Redlen <span class="hlt">high-flux</span> CdZnTe</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Thomas, B.; Veale, M. C.; Wilson, M. D.; Seller, P.; Schneider, A.; Iniewski, K.</p> <p>2017-12-01</p> <p>CdZnTe is a promising material for the current generation of free <span class="hlt">electron</span> laser light sources and future laser-driven γ-ray sources which require detectors capable of <span class="hlt">high</span> <span class="hlt">flux</span> imaging at X-ray and γ-ray energies (> 10 keV) . However, at <span class="hlt">high</span> <span class="hlt">fluxes</span> CdZnTe has been shown to polarise due to hole trapping, leading to poor performance. Novel Redlen CdZnTe material with improved hole transport properties has been designed for <span class="hlt">high</span> <span class="hlt">flux</span> applications. Small pixel CdZnTe detectors were fabricated by Redlen Technologies and flip-chip bonded to PIXIE ASICs. An XIA Digital Gamma Finder PIXIE-16 system was used to digitise each of the nine analogue signals with a timing resolution of 10 ns. Pulse shape analysis was used to extract the rise times and amplitude of signals. These were measured as a function of applied bias voltage and used to calculate the mobility (μ) and mobility-lifetime (μτ) of <span class="hlt">electrons</span> and holes in the material for three identical detectors. The measured values of the transport properties of <span class="hlt">electrons</span> in the <span class="hlt">high-flux</span>-capable material was lower than previously reported for Redlen CdZnTe material (μeτe ~ 1 × 10-3 cm2V-1 and μe ~ 1000 cm2V-1s-1) while the hole transport properties were found to have improved (μhτh ~ 3 × 10-4 cm2V-1 and μh ~ 100 cm2V-1s-1).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19850046194&hterms=magnetic+cooling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dmagnetic%2Bcooling','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19850046194&hterms=magnetic+cooling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dmagnetic%2Bcooling"><span>On the <span class="hlt">heating</span> mechanism of magnetic <span class="hlt">flux</span> loops in the solar atmosphere</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Song, M. T.; Wu, S. T.</p> <p>1984-01-01</p> <p>An investigation is conducted of physical <span class="hlt">heating</span> mechanisms due to the ponderomotive forces exerted by turbulent waves along the solar atmosphere's curved magnetic <span class="hlt">flux</span> loops. Results indicate that the temperature difference between the inside and outside of the <span class="hlt">flux</span> loop can be classified into three parts, two of which represent the cooling or <span class="hlt">heating</span> effect exerted by the ponderomotive force, while the third is the <span class="hlt">heating</span> effect due to turbulent energy conversion from the localized plasma. This <span class="hlt">heating</span> mechanism is used to illustrate solar atmospheric <span class="hlt">heating</span> by means of an example that leads to the formulation of plages.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AIPC.1770b0011A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AIPC.1770b0011A"><span>Physical mechanisms of longitudinal vortexes formation, appearance of zones with <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> and early transition in hypersonic flow over delta wing with blunted leading edges</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Alexandrov, S. V.; Vaganov, A. V.; Shalaev, V. I.</p> <p>2016-10-01</p> <p>Processes of vortex structures formation and they interactions with the boundary layer in the hypersonic flow over delta wing with blunted leading edges are analyzed on the base of experimental investigations and numerical solutions of Navier-Stokes equations. Physical mechanisms of longitudinal vortexes formation, appearance of abnormal zones with <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> and early laminar turbulent transition are studied. These phenomena were observed in many <span class="hlt">high</span>-speed wind tunnel experiments; however they were understood only using the detailed analysis of numerical modeling results with the <span class="hlt">high</span> resolution. Presented results allowed explaining experimental phenomena. ANSYS CFX code (the DAFE MIPT license) on the grid with 50 million nodes was used for the numerical modeling. The numerical method was verified by comparison calculated <span class="hlt">heat</span> <span class="hlt">flux</span> distributions on the wing surface with experimental data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28410347','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28410347"><span>Accuracy of Zero-<span class="hlt">Heat-Flux</span> Cutaneous Temperature in Intensive Care Adults.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dahyot-Fizelier, Claire; Lamarche, Solène; Kerforne, Thomas; Bénard, Thierry; Giraud, Benoit; Bellier, Rémy; Carise, Elsa; Frasca, Denis; Mimoz, Olivier</p> <p>2017-07-01</p> <p>To compare accuracy of a continuous noninvasive cutaneous temperature using zero-<span class="hlt">heat-flux</span> method to esophageal temperature and arterial temperature. Prospective study. ICU and NeuroICU, University Hospital. Fifty-two ICU patients over a 4-month period who required continuous temperature monitoring were included in the study, after informed consent. All patients had esophageal temperature probe and a noninvasive cutaneous device to monitor their core temperature continuously. In seven patients who required cardiac output monitoring, continuous iliac arterial temperature was collected. Simultaneous core temperatures were recorded from 1 to 5 days. Comparison to the esophageal temperature, considered as the reference in this study, used the Bland and Altman method with adjustment for multiple measurements per patient. The esophageal temperature ranged from 33°C to 39.7°C, 61,298 pairs of temperature using zero-<span class="hlt">heat-flux</span> and esophageal temperature were collected and 1,850 triple of temperature using zero-<span class="hlt">heat-flux</span>, esophageal temperature, and arterial temperature. Bias and limits of agreement for temperature using zero-<span class="hlt">heat-flux</span> were 0.19°C ± 0.53°C compared with esophageal temperature with an absolute difference of temperature pairs equal to or lower than 0.5°C of 92.6% (95% CI, 91.9-93.4%) of cases and equal to or lower than 1°C for 99.9% (95% CI, 99.7-100.0%) of cases. Compared with arterial temperature, bias and limits of agreement were -0.00°C ± 0.36°C with an absolute difference of temperature pairs equal to or lower than 0.5°C of 99.8% (95% CI, 95.3-100%) of cases. All absolute difference of temperature pairs between temperature using zero-<span class="hlt">heat-flux</span> and arterial temperature and between arterial temperature and esophageal temperature were equal to or lower than 1°C. No local or systemic serious complication was observed. These results suggest a comparable reliability of the cutaneous sensor using the zero-<span class="hlt">heat-flux</span> method compared with esophageal or</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381797','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381797"><span>Darcy-Forchheimer flow with Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> and homogeneous-heterogeneous reactions</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Hayat, Tasawar; Haider, Farwa; Alsaedi, Ahmed</p> <p>2017-01-01</p> <p>Here Darcy-Forchheimer flow of viscoelastic fluids has been analyzed in the presence of Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> and homogeneous-heterogeneous reactions. Results for two viscoelastic fluids are obtained and compared. A linear stretching surface has been used to generate the flow. Flow in porous media is characterized by considering the Darcy-Forchheimer model. Modified version of Fourier's law through Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> is employed. Equal diffusion coefficients are employed for both reactants and auto catalyst. Optimal homotopy scheme is employed for solutions development of nonlinear problems. Solutions expressions of velocity, temperature and concentration fields are provided. Skin friction coefficient and <span class="hlt">heat</span> transfer rate are computed and analyzed. Here the temperature and thermal boundary layer thickness are lower for Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> model in comparison to classical Fourier's law of <span class="hlt">heat</span> conduction. Moreover, the homogeneous and heterogeneous reactions parameters have opposite behaviors for concentration field. PMID:28380014</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16711925','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16711925"><span>Effect of <span class="hlt">heat</span> <span class="hlt">flux</span> on differential rotation in turbulent convection.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kleeorin, Nathan; Rogachevskii, Igor</p> <p>2006-04-01</p> <p>We studied the effect of the turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> on the Reynolds stresses in a rotating turbulent convection. To this end we solved a coupled system of dynamical equations which includes the equations for the Reynolds stresses, the entropy fluctuations, and the turbulent <span class="hlt">heat</span> <span class="hlt">flux</span>. We used a spectral tau approximation in order to close the system of dynamical equations. We found that the ratio of the contributions to the Reynolds stresses caused by the turbulent <span class="hlt">heat</span> <span class="hlt">flux</span> and the anisotropic eddy viscosity is of the order of approximately 10(L rho/l0)2, where l0 is the maximum scale of turbulent motions and L rho is the fluid density variation scale. This effect is crucial for the formation of the differential rotation and should be taken into account in the theories of the differential rotation of the Sun, stars, and planets. In particular, we demonstrated that this effect may cause the differential rotation which is comparable with the typical solar differential rotation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1996APS..DPP..9P42S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1996APS..DPP..9P42S"><span>Shock wave as a probe of <span class="hlt">flux</span>-dimited thermal transport in laser-<span class="hlt">heated</span> solids</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Smith, K.; Forsman, A.; Chiu, G.</p> <p>1996-11-01</p> <p>Laser-generated shock waves in solids result from the ablation of the target material. Where radiation transport is negligible, the ablation process is dominated by <span class="hlt">electron</span> thermal conduction. This offers an opportunity to probe the degree of transport inhibition (compared with classical <span class="hlt">heat</span> flow) for steep temperature gradients in a dense plasma. Using a 1-dimensional hydrodynamic code, we have examined the effect of <span class="hlt">flux</span>-limited thermal conduction on the amplitude of the resulting shock wave.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_21 --> <div id="page_22" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="421"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19870006083','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19870006083"><span>Comparison of measured and modeled radiation, <span class="hlt">heat</span> and water vapor <span class="hlt">fluxes</span>: FIFE pilot study</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Blad, Blaine L.; Hubbard, Kenneth G.; Verma, Shashi B.; Starks, Patrick; Norman, John M.; Walter-Shea, Elizabeth</p> <p>1987-01-01</p> <p>The feasibility of using radio frequency receivers to collect data from automated weather stations to model <span class="hlt">fluxes</span> of latent <span class="hlt">heat</span>, sensible <span class="hlt">heat</span>, and radiation using routine weather data collected by automated weather stations was tested and the estimated <span class="hlt">fluxes</span> were compared with <span class="hlt">fluxes</span> measured over wheat. The model Cupid was used to model the <span class="hlt">fluxes</span>. Two or more automated weather stations, interrogated by radio frequency and other means, were utilized to examine some of the climatic variability of the First ISLSCP (International Satellite Land-Surface Climatology Project) Field Experiment (FIFE) site, to measure and model reflected and emitted radiation streams from various locations at the site and to compare modeled latent and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> with measured values. Some bidirectional reflected and emitted radiation data were collected from 23 locations throughout the FIFE site. Analysis of these data along with analysis of the measured sensible and latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> is just beginning.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005JGRA..110.4201V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005JGRA..110.4201V"><span>Solar, interplanetary, and magnetospheric parameters for the radiation belt energetic <span class="hlt">electron</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vassiliadis, D.; Fung, S. F.; Klimas, A. J.</p> <p>2005-04-01</p> <p>In developing models of the radiation belt energetic <span class="hlt">electron</span> <span class="hlt">flux</span>, it is important to include the states of the interplanetary medium and the magnetosphere, as well as the solar activity. In this study we choose the log <span class="hlt">flux</span> je(t;L;E) at 2-6 MeV, as measured by the Proton-<span class="hlt">Electron</span> Telescope (PET) on SAMPEX in the period 1993-2002, as a representative <span class="hlt">flux</span> variable and evaluate the usefulness of 17 interplanetary and magnetospheric (IP/MS) parameters in its specification. The reference parameter is the solar wind velocity, chosen because of its known <span class="hlt">high</span> geoeffectiveness. We use finite impulse response filters to represent the effective coupling of the individual parameters to the log <span class="hlt">flux</span>. We measure the temporal and spatial scales of the coupling using the impulse response function and the input's geoeffectiveness using the data-model correlation. The correlation profile as a function of L is complex, and we identify its peaks in reference to the radial regions P0 (L = 3.1-4.0, inner edge of the outer belt), P1 (4.1-7.5, main outer belt), and P2 (>7.5, quasi-trapped population), whose boundaries are determined from a radial correlative analysis (Vassiliadis et al., 2003b). Using the profiles, we classify the IP/MS parameters in four categories: (1) For the solar wind velocity and pressure the correlation is <span class="hlt">high</span> and largely independent of L across P0 and P1, reaching its maximum in L = 4.8-6.1, or the central part of P1. (2) The IMF BSouth component and related IP/MS parameters have a bimodal correlation function, with peaks in region P0 (L = 3.0-4.1) and the geosynchronous orbit region within P1. (3) The IMF BNorth and four other interplanetary or solar irradiance parameters have a minimum correlation in P1, while the highest correlation is in the slot-outer belt boundary (L = 2.5). (4) Finally, the solar wind density has a unique correlation profile, which is anticorrelated with that of the solar wind velocity for certain L shells. We verify this</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EPJB...90..260A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EPJB...90..260A"><span><span class="hlt">Electron</span>-phonon <span class="hlt">heat</span> exchange in quasi-two-dimensional nanolayers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Anghel, Dragos-Victor; Cojocaru, Sergiu</p> <p>2017-12-01</p> <p>We study the <span class="hlt">heat</span> power P transferred between <span class="hlt">electrons</span> and phonons in thin metallic films deposited on free-standing dielectric membranes. The temperature range is typically below 1 K, such that the wavelengths of the excited phonon modes in the system is large enough so that the picture of a quasi-two-dimensional phonon gas is applicable. Moreover, due to the quantization of the components of the <span class="hlt">electron</span> wavevectors perpendicular to the metal film's surface, the <span class="hlt">electrons</span> spectrum forms also quasi two-dimensional sub-bands, as in a quantum well (QW). We describe in detail the contribution to the <span class="hlt">electron</span>-phonon energy exchange of different <span class="hlt">electron</span> scattering channels, as well as of different types of phonon modes. We find that <span class="hlt">heat</span> <span class="hlt">flux</span> oscillates strongly with thickness of the film d while having a much smoother variation with temperature (Te for the <span class="hlt">electrons</span> temperature and Tph for the phonons temperature), so that one obtains a ridge-like landscape in the two coordinates, (d, Te) or (d, Tph), with crests and valleys aligned roughly parallel to the temperature axis. For the valley regions we find P ∝ Te3.5 - Tph3.5. From valley to crest, P increases by more than one order of magnitude and on the crests P cannot be represented by a simple power law. The strong dependence of P on d is indicative of the formation of the QW state and can be useful in controlling the <span class="hlt">heat</span> transfer between <span class="hlt">electrons</span> and crystal lattice in nano-<span class="hlt">electronic</span> devices. Nevertheless, due to the small value of the Fermi wavelength in metals, the surface imperfections of the metallic films can reduce the magnitude of the oscillations of P vs. d, so this effect might be easier to observe experimentally in doped semiconductors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050209932','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050209932"><span>Benchmark Wall <span class="hlt">Heat</span> <span class="hlt">Flux</span> Data for a GO2/GH2 Single Element Combustor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Marshall, William M.; Pal, Sibtosh; Woodward, Roger d.; Santoro, Robert J.</p> <p>2005-01-01</p> <p>Wall <span class="hlt">heat</span> <span class="hlt">flux</span> measurements in a 1.5 in. diameter circular cross-section rocket chamber for a uni-element shear coaxial injector element operating on gaseous oxygen (GOz)/gaseous hydrogen (GH,) propellants are presented. The wall <span class="hlt">heat</span> <span class="hlt">flux</span> measurements were made using arrays of Gardon type <span class="hlt">heat</span> <span class="hlt">flux</span> gauges and coaxial thermocouple instrumentation. Wall <span class="hlt">heat</span> <span class="hlt">flux</span> measurements were made for two cases. For the first case, GOZ/GHz oxidizer-rich (O/F=l65) and fuel-rich preburners (O/F=1.09) integrated with the main chamber were utilized to provide vitiated hot fuel and oxidizer to the study shear coaxial injector element. For the second case, the preburners were removed and ambient temperature gaseous oxygen/gaseous hydrogen propellants were supplied to the study injector. Experiments were conducted at four chamber pressures of 750, 600, 450 and 300psia for each case. The overall mixture ratio for the preburner case was 6.6, whereas for the ambient propellant case, the mixture ratio was 6.0. Total propellant flow was nominally 0.27-0.29 Ibm/s for the 750 psia case with flowrates scaled down linearly for lower chamber pressures. The axial <span class="hlt">heat</span> <span class="hlt">flux</span> profile results for both the preburner and ambient propellant cases show peak <span class="hlt">heat</span> <span class="hlt">flux</span> levels a t axial locations between 2.0 and 3.0 in. from the injector face. The maximum <span class="hlt">heat</span> <span class="hlt">flux</span> level was about two times greater for the preburner case. This is attributed to the higher injector fuel-to-oxidizer momentum <span class="hlt">flux</span> ratio that promotes mixing and higher initial propellant temperature for the preburner case which results in a shorter reaction zone. The axial <span class="hlt">heat</span> <span class="hlt">flux</span> profiles were also scaled with respect to the chamber pressure to the power 0.8. The results at the four chamber pressures for both cases collapsed to a single profile indicating that at least to first approximation, the basic fluid dynamic structures in the flow field are pressure independent as long as the chamber/njector/nozzle geometry and injection velocities</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1321430-nonlinear-fluid-simulation-particle-heat-fluxes-during-burst-elms-diii-bout++-code-fluid-simulation-particle-heat-fluxes-during-burst-elms-diid-bout++-code','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1321430-nonlinear-fluid-simulation-particle-heat-fluxes-during-burst-elms-diii-bout++-code-fluid-simulation-particle-heat-fluxes-during-burst-elms-diid-bout++-code"><span>Nonlinear fluid simulation of particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> during burst of ELMs on DIII-D with BOUT++ code [Fluid Simulation of Particle and <span class="hlt">Heat</span> <span class="hlt">Fluxes</span> during Burst of ELMs on DIID with BOUT++ code</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Xia, T. Y.; Xu, X. Q.</p> <p>2015-09-01</p> <p>In order to study the distribution and evolution of the transient particle and <span class="hlt">heat</span> <span class="hlt">fluxes</span> during edge-localized mode (ELM) bursts, a BOUT++ six-field two-fluid model based on the Braginskii equations with non-ideal physics effects is used to simulate pedestal collapse in divertor geometry. We used the profiles from the DIII-D H-mode discharge #144382 with fast target <span class="hlt">heat</span> <span class="hlt">flux</span> measurements as the initial conditions for the simulations. Moreover, a <span class="hlt">flux</span>-limited parallel thermal conduction is used with three values of the <span class="hlt">flux</span>-limiting coefficientmore » $${{\\alpha}_{j}}$$ , free streaming model with $${{\\alpha}_{j}}=1$$ , sheath-limit with $${{\\alpha}_{j}}=0.05$$ , and one value in between. The studies show that a 20 times increase in $${{\\alpha}_{j}}$$ leads to ~6 times increase in the <span class="hlt">heat</span> <span class="hlt">flux</span> amplitude to both the inner and outer targets, and the widths of the <span class="hlt">fluxes</span> are also expanded. The sheath-limit model of <span class="hlt">flux</span>-limiting coefficient is found to be the most appropriate one, which shows ELM sizes close to the measurements. The evolution of the density profile during the burst of ELMs of DIII-D discharge #144382 is simulated, and the collapse in width and depth of $${{n}_{\\text{e}}}$$ are reproduced at different time steps. The growing process of the profiles for the <span class="hlt">heat</span> <span class="hlt">flux</span> at divertor targets during the burst of ELMs measured by IRTV (infrared television) is also reproduced by this model. The widths of <span class="hlt">heat</span> <span class="hlt">fluxes</span> towards targets are a little narrower, and the peak amplitudes are twice the measurements possibly due to the lack of a model of divertor radiation which can effectively reduce the <span class="hlt">heat</span> <span class="hlt">fluxes</span>. The magnetic flutter combined with parallel thermal conduction is found to be able to increase the total <span class="hlt">heat</span> loss by around 33% since the magnetic flutter terms provide the additional conductive <span class="hlt">heat</span> transport in the radial direction. Finally, the <span class="hlt">heat</span> <span class="hlt">flux</span> profile at both the inner and outer targets is obviously broadened by magnetic flutter. The</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1430128-tunable-electron-heating-induced-giant-magnetoresistance-high-mobility-gaas-algaas-electron-system','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1430128-tunable-electron-heating-induced-giant-magnetoresistance-high-mobility-gaas-algaas-electron-system"><span>Tunable <span class="hlt">electron</span> <span class="hlt">heating</span> induced giant magnetoresistance in the <span class="hlt">high</span> mobility GaAs/AlGaAs 2D <span class="hlt">electron</span> system</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Wang, Zhuo; Samaraweera, R. L.; Reichl, C.; ...</p> <p>2016-12-07</p> <p><span class="hlt">Electron-heating</span> induced by a tunable, supplementary dc-current (I dc) helps to vary the observed magnetoresistance in the <span class="hlt">high</span> mobility GaAs/AlGaAs 2D <span class="hlt">electron</span> system. The magnetoresistance at B = 0.3 T is shown to progressively change from positive to negative with increasing Idc, yielding negative giant-magnetoresistance at the lowest temperature and highest I dc. A two-term Drude model successfully fits the data at all Idc and T. The results indicate that carrier <span class="hlt">heating</span> modifies a conductivity correction σ 1, which undergoes sign reversal from positive to negative with increasing I dc, and this is responsible for the observed crossover from positive-more » to negative- magnetoresistance, respectively, at the highest B.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JNuM..463.1252T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JNuM..463.1252T"><span><span class="hlt">High</span> <span class="hlt">heat-flux</span> self-rotating plasma-facing component: Concept and loading test in TEXTOR</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Terra, A.; Sergienko, G.; Hubeny, M.; Huber, A.; Mertens, Ph.; Philipps, V.; The Textor Team</p> <p>2015-08-01</p> <p>This contribution reports on the concept of a circular self-rotating and temperature self-stabilising plasma-facing component (PFC), and test of a related prototype in TEXTOR tokamak. This PFC uses the Lorentz force induced by plasma current and magnet field (J × B) to create a torque applied on metallic discs which produce a rotational movement. Additional thermionic current, present at <span class="hlt">high</span> operation temperatures, brings additional temperature stabilisation ability. This self-rotating disk limiter was exposed to plasma in the TEXTOR tokamak under different radial positions to vary the <span class="hlt">heat</span> <span class="hlt">flux</span>. This disk structure shows the interesting ability to stabilise its maximum temperature through the fact that the self-induced rotation is modulated by the thermal emission current. It was observed that the rotation speed increased following both the current collected by the limiter, and the temperature of the tungsten disks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1434406-high-flux-femtosecond-ray-emission-from-electron-hose-instability-laser-wakefield-accelerators','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1434406-high-flux-femtosecond-ray-emission-from-electron-hose-instability-laser-wakefield-accelerators"><span><span class="hlt">High</span> <span class="hlt">flux</span> femtosecond x-ray emission from the <span class="hlt">electron</span>-hose instability in laser wakefield accelerators</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Dong, C. F.; Zhao, T. Z.; Behm, K.</p> <p></p> <p>Here, bright and ultrashort duration x-ray pulses can be produced by through betatron oscillations of <span class="hlt">electrons</span> during laser wakefield acceleration (LWFA). Our experimental measurements using the Hercules laser system demonstrate a dramatic increase in x-ray <span class="hlt">flux</span> for interaction distances beyond the depletion/dephasing lengths, where the initial <span class="hlt">electron</span> bunch injected into the first wake bucket catches up with the laser pulse front and the laser pulse depletes. A transition from an LWFA regime to a beam-driven plasma wakefield acceleration regime consequently occurs. The drive <span class="hlt">electron</span> bunch is susceptible to the <span class="hlt">electron</span>-hose instability and rapidly develops large amplitude oscillations in its tail,more » which leads to greatly enhanced x-ray radiation emission. We measure the x-ray <span class="hlt">flux</span> as a function of acceleration length using a variable length gas cell. 3D particle-in-cell simulations using a Monte Carlo synchrotron x-ray emission algorithm elucidate the time-dependent variations in the radiation emission processes.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvS..21d1303D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvS..21d1303D"><span><span class="hlt">High</span> <span class="hlt">flux</span> femtosecond x-ray emission from the <span class="hlt">electron</span>-hose instability in laser wakefield accelerators</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dong, C. F.; Zhao, T. Z.; Behm, K.; Cummings, P. G.; Nees, J.; Maksimchuk, A.; Yanovsky, V.; Krushelnick, K.; Thomas, A. G. R.</p> <p>2018-04-01</p> <p>Bright and ultrashort duration x-ray pulses can be produced by through betatron oscillations of <span class="hlt">electrons</span> during laser wakefield acceleration (LWFA). Our experimental measurements using the Hercules laser system demonstrate a dramatic increase in x-ray <span class="hlt">flux</span> for interaction distances beyond the depletion/dephasing lengths, where the initial <span class="hlt">electron</span> bunch injected into the first wake bucket catches up with the laser pulse front and the laser pulse depletes. A transition from an LWFA regime to a beam-driven plasma wakefield acceleration regime consequently occurs. The drive <span class="hlt">electron</span> bunch is susceptible to the <span class="hlt">electron</span>-hose instability and rapidly develops large amplitude oscillations in its tail, which leads to greatly enhanced x-ray radiation emission. We measure the x-ray <span class="hlt">flux</span> as a function of acceleration length using a variable length gas cell. 3D particle-in-cell simulations using a Monte Carlo synchrotron x-ray emission algorithm elucidate the time-dependent variations in the radiation emission processes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1434406-high-flux-femtosecond-ray-emission-from-electron-hose-instability-laser-wakefield-accelerators','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1434406-high-flux-femtosecond-ray-emission-from-electron-hose-instability-laser-wakefield-accelerators"><span><span class="hlt">High</span> <span class="hlt">flux</span> femtosecond x-ray emission from the <span class="hlt">electron</span>-hose instability in laser wakefield accelerators</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Dong, C. F.; Zhao, T. Z.; Behm, K.; ...</p> <p>2018-04-24</p> <p>Here, bright and ultrashort duration x-ray pulses can be produced by through betatron oscillations of <span class="hlt">electrons</span> during laser wakefield acceleration (LWFA). Our experimental measurements using the Hercules laser system demonstrate a dramatic increase in x-ray <span class="hlt">flux</span> for interaction distances beyond the depletion/dephasing lengths, where the initial <span class="hlt">electron</span> bunch injected into the first wake bucket catches up with the laser pulse front and the laser pulse depletes. A transition from an LWFA regime to a beam-driven plasma wakefield acceleration regime consequently occurs. The drive <span class="hlt">electron</span> bunch is susceptible to the <span class="hlt">electron</span>-hose instability and rapidly develops large amplitude oscillations in its tail,more » which leads to greatly enhanced x-ray radiation emission. We measure the x-ray <span class="hlt">flux</span> as a function of acceleration length using a variable length gas cell. 3D particle-in-cell simulations using a Monte Carlo synchrotron x-ray emission algorithm elucidate the time-dependent variations in the radiation emission processes.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28063826','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28063826"><span>Evaluation of <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurement as a New Process Analytical Technology Monitoring Tool in Freeze Drying.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Vollrath, Ilona; Pauli, Victoria; Friess, Wolfgang; Freitag, Angelika; Hawe, Andrea; Winter, Gerhard</p> <p>2017-05-01</p> <p>This study investigates the suitability of <span class="hlt">heat</span> <span class="hlt">flux</span> measurement as a new technique for monitoring product temperature and critical end points during freeze drying. The <span class="hlt">heat</span> <span class="hlt">flux</span> sensor is tightly mounted on the shelf and measures non-invasively (no contact with the product) the <span class="hlt">heat</span> transferred from shelf to vial. <span class="hlt">Heat</span> <span class="hlt">flux</span> data were compared to comparative pressure measurement, thermocouple readings, and Karl Fischer titration as current state of the art monitoring techniques. The whole freeze drying process including freezing (both by ramp freezing and controlled nucleation) and primary and secondary drying was considered. We found that direct measurement of the transferred <span class="hlt">heat</span> enables more insights into thermodynamics of the freezing process. Furthermore, a vial <span class="hlt">heat</span> transfer coefficient can be calculated from <span class="hlt">heat</span> <span class="hlt">flux</span> data, which ultimately provides a non-invasive method to monitor product temperature throughout primary drying. The end point of primary drying determined by <span class="hlt">heat</span> <span class="hlt">flux</span> measurements was in accordance with the one defined by thermocouples. During secondary drying, <span class="hlt">heat</span> <span class="hlt">flux</span> measurements could not indicate the progress of drying as monitoring the residual moisture content. In conclusion, <span class="hlt">heat</span> <span class="hlt">flux</span> measurements are a promising new non-invasive tool for lyophilization process monitoring and development using energy transfer as a control parameter. Copyright © 2017 American Pharmacists Association®. Published by Elsevier Inc. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NucFu..57h6030B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NucFu..57h6030B"><span>Surface <span class="hlt">heat</span> <span class="hlt">flux</span> feedback controlled impurity seeding experiments with Alcator C-Mod’s <span class="hlt">high</span>-Z vertical target plate divertor: performance, limitations and implications for fusion power reactors</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Brunner, D.; Wolfe, S. M.; LaBombard, B.; Kuang, A. Q.; Lipschultz, B.; Reinke, M. L.; Hubbard, A.; Hughes, J.; Mumgaard, R. T.; Terry, J. L.; Umansky, M. V.; The Alcator C-Mod Team</p> <p>2017-08-01</p> <p>The Alcator C-Mod team has recently developed a feedback system to measure and control surface <span class="hlt">heat</span> <span class="hlt">flux</span> in real-time. The system uses real-time measurements of surface <span class="hlt">heat</span> <span class="hlt">flux</span> from surface thermocouples and a pulse-width modulated piezo valve to inject low-Z impurities (typically N2) into the private <span class="hlt">flux</span> region. It has been used in C-Mod to mitigate peak surface <span class="hlt">heat</span> fluxes  >40 MW m-2 down to  <10 MW m-2 while maintaining excellent core confinement, H 98  >  1. While the system works quite well under relatively steady conditions, use of it during transients has revealed important limitations on feedback control of impurity seeding in conventional vertical target plate divertors. In some cases, the system is unable to avoid plasma reattachment to the divertor plate or the formation of a confinement-damaging x-point MARFE. This is due to the small operational window for mitigated <span class="hlt">heat</span> <span class="hlt">flux</span> in the parameters of incident plasma <span class="hlt">heat</span> <span class="hlt">flux</span>, plasma density, and impurity density as well as the relatively slow response of the impurity gas injection system compared to plasma transients. Given the severe consequences for failure of such a system to operate reliably in a reactor, there is substantial risk that the conventional vertical target plate divertor will not provide an adequately controllable system in reactor-class devices. These considerations motivate the need to develop passively stable, <span class="hlt">highly</span> compliant divertor configurations and experimental facilities that can test such possible solutions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AIPC.1959e0009D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AIPC.1959e0009D"><span>Investigation of <span class="hlt">heat</span> <span class="hlt">flux</span> on aerodynamic body in supersonic gas flow with local energy deposition</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dobrov, Y. V.; Lashkov, V. A.; Mashek, I. Ch.; Khoronzhuk, R. S.</p> <p>2018-05-01</p> <p>Existence and intensive growth of <span class="hlt">heat</span> <span class="hlt">flux</span> on a vehicle is one of the main problems in hypersonic flight. Experimental study of <span class="hlt">heat</span> <span class="hlt">flux</span> in the stagnation point of a blunt cylinder in supersonic flow was made using gradient <span class="hlt">heat</span> <span class="hlt">flux</span> sensor. It was found that a transfer function of the measuring system should be used for obtaining data at fast-changing <span class="hlt">heat</span> <span class="hlt">flux</span> measurements. It was established that it was possible to produce a short-term <span class="hlt">heat</span> transfer from the surface of streamlined body with the help of microwave discharge. Numerical simulation showed that it is possible to change nature of the flow by means of local energy deposition in case of streamlined wedge.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20170003172&hterms=Ali&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DAli','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20170003172&hterms=Ali&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DAli"><span><span class="hlt">Electron</span> Energetics in the Martian Dayside Ionosphere: Model Comparisons with MAVEN Data</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Sakai, Shotaro; Andersson, Laila; Cravens, Thomas E.; Mitchell, David L.; Mazelle, Christian; Rahmati, Ali; Fowler, Christopher M.; Bougher, Stephen W.; Thiemann, Edward M. B.; Epavier, Francis G.; <a style="text-decoration: none; " href="javascript:void(0); " onClick="displayelement('author_20170003172'); toggleEditAbsImage('author_20170003172_show'); toggleEditAbsImage('author_20170003172_hide'); "> <img style="display:inline; width:12px; height:12px; " src="images/arrow-up.gif" width="12" height="12" border="0" alt="hide" id="author_20170003172_show"> <img style="width:12px; height:12px; display:none; " src="images/arrow-down.gif" width="12" height="12" border="0" alt="hide" id="author_20170003172_hide"></p> <p>2016-01-01</p> <p>This paper presents a study of the energetics of the dayside ionosphere of Mars using models and data from several instruments on board the Mars Atmosphere and Volatile EvolutioN spacecraft. In particular, calculated photoelectron <span class="hlt">fluxes</span> are compared with suprathermal <span class="hlt">electron</span> <span class="hlt">fluxes</span> measured by the Solar Wind <span class="hlt">Electron</span> Analyzer, and calculated <span class="hlt">electron</span> temperatures are compared with temperatures measured by the Langmuir Probe and Waves experiment. The major <span class="hlt">heat</span> source for the thermal <span class="hlt">electrons</span> is Coulomb <span class="hlt">heating</span> from the suprathermal <span class="hlt">electron</span> population, and cooling due to collisional rotational and vibrational CO2 dominates the energy loss. The models used in this study were largely able to reproduce the observed <span class="hlt">high</span> topside ionosphere <span class="hlt">electron</span> temperatures (e.g., 3000 K at 300 km altitude) without using a topside <span class="hlt">heat</span> <span class="hlt">flux</span> when magnetic field topologies consistent with the measured magnetic field were adopted. Magnetic topology affects both suprathermal <span class="hlt">electron</span> transport and thermal <span class="hlt">electron</span> <span class="hlt">heat</span> conduction. The effects of using two different solar irradiance models were also investigated. In particular, photoelectron <span class="hlt">fluxes</span> and <span class="hlt">electron</span> temperatures found using the Heliospheric Environment Solar Spectrum Radiation irradiance were higher than those with the Flare Irradiance Spectrum Model-Mars. The <span class="hlt">electron</span> temperature is shown to affect the O2(+) dissociative recombination rate coefficient, which in turn affects photochemical escape of oxygen from Mars.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20060047645','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20060047645"><span>Local <span class="hlt">Heat</span> <span class="hlt">Flux</span> Measurements with Single Element Coaxial Injectors</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jones, Gregg; Protz, Christopher; Bullard, Brad; Hulka, James</p> <p>2006-01-01</p> <p>To support the mission for the NASA Vision for Space Exploration, the NASA Marshall Space Flight Center conducted a program in 2005 to improve the capability to predict local thermal compatibility and <span class="hlt">heat</span> transfer in liquid propellant rocket engine combustion devices. The ultimate objective was to predict and hence reduce the local peak <span class="hlt">heat</span> <span class="hlt">flux</span> due to injector design, resulting in a significant improvement in overall engine reliability and durability. Such analyses are applicable to combustion devices in booster, upper stage, and in-space engines, as well as for small thrusters with few elements in the injector. In this program, single element and three-element injectors were hot-fire tested with liquid oxygen and ambient temperature gaseous hydrogen propellants at The Pennsylvania State University Cryogenic Combustor Laboratory from May to August 2005. Local <span class="hlt">heat</span> <span class="hlt">fluxes</span> were measured in a 1-inch internal diameter <span class="hlt">heat</span> sink combustion chamber using Medtherm coaxial thermocouples and Gardon <span class="hlt">heat</span> <span class="hlt">flux</span> gauges. Injectors were tested with shear coaxial and swirl coaxial elements, including recessed, flush and scarfed oxidizer post configurations, and concentric and non-concentric fuel annuli. This paper includes general descriptions of the experimental hardware, instrumentation, and results of the hot-fire testing for three of the single element injectors - recessed-post shear coaxial with concentric fuel, flush-post swirl coaxial with concentric fuel, and scarfed-post swirl coaxial with concentric fuel. Detailed geometry and test results will be published elsewhere to provide well-defined data sets for injector development and model validatation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT....54.1669P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT....54.1669P"><span>Upward and downward facing <span class="hlt">high</span> mass <span class="hlt">flux</span> spray cooling with additives: A novel technique to enhance the <span class="hlt">heat</span> removal rate at <span class="hlt">high</span> initial surface temperature</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pati, A. R.; Kumar, A.; Mohapatra, S. S.</p> <p>2018-06-01</p> <p>The objective of the current work is to enhance the spray cooling by changing the orientation of the nozzle with different additives (acetone, methanol, ethanol, benzene, n-hexane, tween 20 and salt) in water. The experiments are carried out by upward, downward and both upward and downward facing sprays. The optimization result depicts that the spray produced by upward facing spray gives higher <span class="hlt">heat</span> <span class="hlt">flux</span> than the downward facing spray and also cooling by both the upward and downward facing spray simultaneously produces better result than the individual. Further experiments with both upward and downward facing spray by using different coolants reveal that in case of cooling by ethanol (500 ppm) + water mixture, the maximum enhancement of surface <span class="hlt">heat</span> <span class="hlt">flux</span> ( 2.57 MW/m2) and cooling rate (204 °C/s) is observed. However, the minimum surface <span class="hlt">heat</span> <span class="hlt">flux</span> is achieved in case of methanol (100 ppm) + water due to higher contact angle (710) among all the considered coolants.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.A53G2359A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.A53G2359A"><span>Multi Seasonal and Diurnal Characterization of Sensible <span class="hlt">Heat</span> <span class="hlt">Flux</span> in an Arid Land Environment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Al-Mashharawi, S.; Aragon, B.; McCabe, M.</p> <p>2017-12-01</p> <p>In sparsely vegetated arid and semi-arid regions, the available energy is transformed primarily into sensible <span class="hlt">heat</span>, with little to no energy partitioned into latent <span class="hlt">heat</span>. The characterization of bare soil arid environments are rather poorly understood in the context of both local, regional and global energy budgets. Using data from a long-term surface layer scintillometer and co-located meteorological installation, we examine the diurnal and seasonal patterns of sensible <span class="hlt">heat</span> <span class="hlt">flux</span> and the net radiation to soil <span class="hlt">heat</span> <span class="hlt">flux</span> ratio. We do this over a bare desert soil located adjacent to an irrigated agricultural field in the central region of Saudi Arabia. The results of this exploratory analysis can be used to inform upon remote sensing techniques for surface <span class="hlt">flux</span> estimation, to derive and monitor soil <span class="hlt">heat</span> <span class="hlt">flux</span> dynamics, estimate the <span class="hlt">heat</span> transfer resistance and the thermal roughness length over bare soils, and to better inform efforts that model the advective effects that complicate the accurate representation of agricultural energy budgets in the arid zone.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AcAau.138..168H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AcAau.138..168H"><span>Drag and <span class="hlt">heat</span> <span class="hlt">flux</span> reduction mechanism of blunted cone with aerodisks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huang, Wei; Li, Lang-quan; Yan, Li; Zhang, Tian-tian</p> <p>2017-09-01</p> <p>The major challenge among a number of design requirements for hypersonic vehicles is the reduction of drag and aerodynamic <span class="hlt">heating</span>. Of all these techniques of drag and <span class="hlt">heat</span> <span class="hlt">flux</span> reduction, application of forward facing aerospike conceived in 1950s is an effective and simpler technique to reduce the drag as well as the <span class="hlt">heat</span> transfer rate for blunt nosed bodies at hypersonic Mach numbers. In this paper, the flow fields around a blunt cone with and without aerodisk flying at hypersonic Mach numbers are computed numerically, and the numerical simulations are conducted by specifying the freestream velocity, static pressure and static temperatures at the inlet of the computational domain with a three-dimensional, steady, Reynolds-averaged Navier-Stokes equation. An aerodisk is attached to the tip of the rod to reduce the drag and <span class="hlt">heat</span> <span class="hlt">flux</span> further. The influences of the length of rod and the diameter of aerodisk on the drag and <span class="hlt">heat</span> <span class="hlt">flux</span> reduction mechanism are analyzed comprehensively, and eight configurations are taken into consideration in the current study. The obtained results show that for all aerodisks, the reduction in drag of the blunt body is proportional to the extent of the recirculation dead air region. For long rods, the aerodisk is found not that beneficial in reducing the drag, and an aerodisk is more effective than an aerospike. The spike produces a region of recirculation separated flow that shields the blunt-nosed body from the incoming flow, and the recirculation region is formed around the root of the spike up to the reattachment point of the flow at the shoulder of the blunt body. The dynamic pressure in the recirculation area is <span class="hlt">highly</span> reduced and thus leads to the decrease in drag and <span class="hlt">heat</span> load on the surface of the blunt body. Because of the reattachment of the shear layer on the shoulder of the blunt body, the pressure near that point becomes large.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25045862','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25045862"><span>An evaluation of a zero-<span class="hlt">heat-flux</span> cutaneous thermometer in cardiac surgical patients.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Eshraghi, Yashar; Nasr, Vivian; Parra-Sanchez, Ivan; Van Duren, Albert; Botham, Mark; Santoscoy, Thomas; Sessler, Daniel I</p> <p>2014-09-01</p> <p>Although core temperature can be measured invasively, there are currently no widely available, reliable, noninvasive thermometers for its measurement. We thus compared a prototype zero-<span class="hlt">heat-flux</span> thermometer with simultaneous measurements from a pulmonary artery catheter. Specifically, we tested the hypothesis that zero-<span class="hlt">heat-flux</span> temperatures are sufficiently accurate for routine clinical use. Core temperature was measured from the thermistor of a standard pulmonary artery catheter and with a prototype zero-<span class="hlt">heat-flux</span> deep-tissue thermometer in 105 patients having nonemergent cardiac surgery. Zero-<span class="hlt">heat-flux</span> probes were positioned on the lateral forehead and lateral neck. Skin surface temperature probes were attached to the forehead just adjacent to the zero-<span class="hlt">heat-flux</span> probe. Temperatures were recorded at 1-minute intervals, excluding the period of cardiopulmonary bypass, and for the first 4 postoperative hours. Zero-<span class="hlt">heat-flux</span> and pulmonary artery temperatures were compared with bias analysis; differences exceeding 0.5°C were considered to be potentially clinically important. The mean duration in the operating room was 279 ± 75 minutes, and the mean cross-clamp time was 118 ± 50 minutes. All subjects were monitored for an additional 4 hours in the intensive care unit. The average overall difference between forehead zero-<span class="hlt">heat-flux</span> and pulmonary artery temperatures (i.e., forehead minus pulmonary artery) was -0.23°C (95% limits of agreement of ±0.82); 78% of the differences were ≤0.5°C. The average intraoperative temperature difference was -0.08°C (95% limits of agreement of ±0.88); 84% of the differences were ≤0.5°C. The average postoperative difference was -0.32°C (95% limits of agreement of ±0.75); 84% of the differences were ≤0.5°C. Bias and precision values for neck site were similar to the forehead values. Uncorrected forehead skin temperature showed an increasing negative bias as core temperature decreased. Core temperature can be noninvasively</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AGUFM.B11D0379L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AGUFM.B11D0379L"><span>A Semi-parametric Multivariate Gap-filling Model for Eddy Covariance Latent <span class="hlt">Heat</span> <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, M.; Chen, Y.</p> <p>2010-12-01</p> <p>Quantitative descriptions of latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> are important to study the water and energy exchanges between terrestrial ecosystems and the atmosphere. The eddy covariance approaches have been recognized as the most reliable technique for measuring surface <span class="hlt">fluxes</span> over time scales ranging from hours to years. However, unfavorable micrometeorological conditions, instrument failures, and applicable measurement limitations may cause inevitable <span class="hlt">flux</span> gaps in time series data. Development and application of suitable gap-filling techniques are crucial to estimate long term <span class="hlt">fluxes</span>. In this study, a semi-parametric multivariate gap-filling model was developed to fill latent <span class="hlt">heat</span> <span class="hlt">flux</span> gaps for eddy covariance measurements. Our approach combines the advantages of a multivariate statistical analysis (principal component analysis, PCA) and a nonlinear interpolation technique (K-nearest-neighbors, KNN). The PCA method was first used to resolve the multicollinearity relationships among various hydrometeorological factors, such as radiation, soil moisture deficit, LAI, and wind speed. The KNN method was then applied as a nonlinear interpolation tool to estimate the <span class="hlt">flux</span> gaps as the weighted sum latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> with the K-nearest distances in the PCs’ domain. Two years, 2008 and 2009, of eddy covariance and hydrometeorological data from a subtropical mixed evergreen forest (the Lien-Hua-Chih Site) were collected to calibrate and validate the proposed approach with artificial gaps after standard QC/QA procedures. The optimal K values and weighting factors were determined by the maximum likelihood test. The results of gap-filled latent <span class="hlt">heat</span> <span class="hlt">fluxes</span> conclude that developed model successful preserving energy balances of daily, monthly, and yearly time scales. Annual amounts of evapotranspiration from this study forest were 747 mm and 708 mm for 2008 and 2009, respectively. Nocturnal evapotranspiration was estimated with filled gaps and results are comparable with other studies</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_22 --> <div id="page_23" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="441"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930019430','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930019430"><span>Small hydrogen/oxygen rocket flowfield behavior from <span class="hlt">heat</span> <span class="hlt">flux</span> measurements</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Reed, Brian D.</p> <p>1993-01-01</p> <p>The mixing and <span class="hlt">heat</span> transfer phenomena in small rocket flow fields with fuel film cooling is not well understood. An instrumented, water-cooled chamber with a gaseous hydrogen/gaseous oxygen injector was used to gather steady-state inner and outer wall temperature profiles. The chamber was tested at 414 kPa (60 psia) chamber pressure, from mixture ratios of 3.41 to 8.36. Sixty percent of the fuel was used for film cooling. These temperature profiles were used as boundary conditions in a finite element analysis program, MSC/NASTRAN, to calculate the local radial and axial <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the chamber wall. The normal <span class="hlt">heat</span> <span class="hlt">fluxes</span> were then calculated and used as a diagnostic of the rocket's flow field behavior. The normal <span class="hlt">heat</span> <span class="hlt">fluxes</span> determined were on the order of 1.0 to 3.0 MW/meters squared (0.6 to 1.8 Btu/sec-inches squared). In the cases where mixture ratio was 5 or above, there was a sharp local <span class="hlt">heat</span> <span class="hlt">flux</span> maximum in the barrel section of the chamber. This local maximum seems to indicate a reduction or breakdown of the fuel film cooling layer, possibly due to increased mixing in the shear layer between the film and core flows. However, the flow was thought to be completely laminar, as the throat Reynolds numbers were below 50,000 for all the cases. The increased mixing in the shear layer in the higher mixture ratio cases appeared not to be due to the transition of the flow from laminar to turbulent, but rather due to increased reactions between the hydrogen film and oxidizer-rich core flows.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/7377945','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/7377945"><span>Wheelchair cushion effect on skin temperature, <span class="hlt">heat</span> <span class="hlt">flux</span>, and relative humidity.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Stewart, S F; Palmieri, V; Cochran, G V</p> <p>1980-05-01</p> <p>For patients subject to decubitus ulcers, wheelchair cushions should be prescribed with knowledge of the cushion's effect on the thermal as well as mechanical environment of the skin. To define thermal effects that may be encountered during routine use, tests werr made on 24 commercially available cushions. Skin temperature, <span class="hlt">heat</span> <span class="hlt">flux</span> and relative humidity were measured under the ischial tuberosities of a normal 24-year-old man during a 1-hour period of sitting on each cushion. After 1 hour, skin temperatures increased by means of 3.4 C and 2.8 C on foams and viscoelastic foams and there were slight decreases in <span class="hlt">heat</span> <span class="hlt">flux</span> as compared with control values in air. On gels, skin temperatures remained constant and <span class="hlt">heat</span> <span class="hlt">flux</span> increased, while water "floatation" pads caused a mean skin temperature decreased of 2.7 C along with a marked increase in <span class="hlt">heat</span> <span class="hlt">flux</span>. Relative humidity at the skin cushion interface increased by 10.4%, 22.8% and 19.8% on foams, gels and water floatation pads, as compared with room air values. Representative cushions from each of the general types (foam, viscoelastic foam, gel and water floatation) also were subjected to 2-hour tests which indicated the measured parameters continued to change asymptotically.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19890001997','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19890001997"><span>Comparison of measured and modeled radiation, <span class="hlt">heat</span> and water vapor <span class="hlt">fluxes</span>: FIFE pilot study</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Blad, Blaine L.; Verma, Shashi B.; Hubbard, Kenneth G.; Starks, Patrick; Hays, Cynthia; Norman, John M.; Waltershea, Elizabeth</p> <p>1988-01-01</p> <p>The primary objectives of the 1985 study were to test the feasibility of using radio frequency receivers to collect data from automated weather stations and to evaluate the use of the data collected by the automated weather stations for modeling the <span class="hlt">fluxes</span> of latent <span class="hlt">heat</span>, sensible <span class="hlt">heat</span>, and radiation over wheat. The model Cupid was used to calculate these <span class="hlt">fluxes</span> which were compared with <span class="hlt">fluxes</span> of these entities measured using micrometeorological techniques. The primary objectives of the 1986 study were to measure and model reflected and emitted radiation streams at a few locations within the First International Satellite Land-Surface Climatology Project Field Experiment (FIFE) site and to compare modeled and measured latent <span class="hlt">heat</span> and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> from the prairie vegetation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950024426','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950024426"><span>Diamond thin film temperature and <span class="hlt">heat-flux</span> sensors</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Aslam, M.; Yang, G. S.; Masood, A.; Fredricks, R.</p> <p>1995-01-01</p> <p>Diamond film temperature and <span class="hlt">heat-flux</span> sensors are developed using a technology compatible with silicon integrated circuit processing. The technology involves diamond nucleation, patterning, doping, and metallization. Multi-sensor test chips were designed and fabricated to study the thermistor behavior. The minimum feature size (device width) for 1st and 2nd generation chips are 160 and 5 micron, respectively. The p-type diamond thermistors on the 1st generation test chip show temperature and response time ranges of 80-1270 K and 0.29-25 microseconds, respectively. An array of diamond thermistors, acting as <span class="hlt">heat</span> <span class="hlt">flux</span> sensors, was successfully fabricated on an oxidized Si rod with a diameter of 1 cm. Some problems were encountered in the patterning of the Pt/Ti ohmic contacts on the rod, due mainly to the surface roughness of the diamond film. The use of thermistors with a minimum width of 5 micron (to improve the spatial resolution of measurement) resulted in lithographic problems related to surface roughness of diamond films. We improved the mean surface roughness from 124 nm to 30 nm by using an ultra <span class="hlt">high</span> nucleation density of 10(exp 11)/sq cm. To deposit thermistors with such small dimensions on a curved surface, a new 3-D diamond patterning technique is currently under development. This involves writing a diamond seed pattern directly on the curved surface by a computer-controlled nozzle.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014APS..DPPGI1003A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014APS..DPPGI1003A"><span>Broadening of the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> footprint with increasing number of ELM filaments in NSTX</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ahn, Joon-Wook</p> <p>2014-10-01</p> <p>We report on the broadening (narrowing) of the ELM <span class="hlt">heat</span> <span class="hlt">flux</span> footprint with increasing (decreasing) number of filamentary striations from in-depth thermography measurements in NSTX. Edge localized modes (ELMs) represent a challenge to future fusion devices, due to the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> on plasma facing surfaces. One ameliorating factor has been that the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> characteristic profile width (λq) has been observed to broaden with the size of ELM, as compared with the inter-ELM λq, which keeps the peak <span class="hlt">heat</span> <span class="hlt">flux</span> (qpeak) from increasing. In contrast, λq has been observed to narrow during ELMs under certain conditions in NSTX, for both naturally occurring and 3-D fields triggered ELMs. Fast thermographic measurements and detailed analysis demonstrate that the ELM λq increases with the number of observed filamentary striations, i . e . , profile narrowing (broadening) occurs when the number of striations is smaller (larger) than 3-4. With profile narrowing, qpeak at ELM peak times is inversely related (proportional) to λq (the ELM size), exacerbating the <span class="hlt">heat</span> <span class="hlt">flux</span> problem. Edge stability analysis shows that NSTX ELMs almost always lie on the current-driven kink/peeling mode side with low toroidal mode number (n = 1--5), consistent with the typical numbers of striations in NSTX (0-8) in comparison 10--15 striations are normally observed in intermediate-n peeling-ballooning ELMs, e.g., from JET. The NSTX characteristics may translate directly to ITER, which is also projected to lie on the low-n kink/peeling stability boundary. This work was supported by the U.S. DOE, Contract DE-AC05-00OR22725 (ORNL) and DE-AC02-09CH11466 (PPPL).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160007102','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160007102"><span>Estimation of Surface Temperature and <span class="hlt">Heat</span> <span class="hlt">Flux</span> by Inverse <span class="hlt">Heat</span> Transfer Methods Using Internal Temperatures Measured While Radiantly <span class="hlt">Heating</span> a Carbon/Carbon Specimen up to 1920 F</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pizzo, Michelle; Daryabeigi, Kamran; Glass, David</p> <p>2015-01-01</p> <p>The ability to solve the <span class="hlt">heat</span> conduction equation is needed when designing materials to be used on vehicles exposed to extremely <span class="hlt">high</span> temperatures; e.g. vehicles used for atmospheric entry or hypersonic flight. When using test and flight data, computational methods such as finite difference schemes may be used to solve for both the direct <span class="hlt">heat</span> conduction problem, i.e., solving between internal temperature measurements, and the inverse <span class="hlt">heat</span> conduction problem, i.e., using the direct solution to march forward in space to the surface of the material to estimate both surface temperature and <span class="hlt">heat</span> <span class="hlt">flux</span>. The completed research first discusses the methods used in developing a computational code to solve both the direct and inverse <span class="hlt">heat</span> transfer problems using one dimensional, centered, implicit finite volume schemes and one dimensional, centered, explicit space marching techniques. The developed code assumed the boundary conditions to be specified time varying temperatures and also considered temperature dependent thermal properties. The completed research then discusses the results of analyzing temperature data measured while radiantly <span class="hlt">heating</span> a carbon/carbon specimen up to 1920 F. The temperature was measured using thermocouple (TC) plugs (small carbon/carbon material specimens) with four embedded TC plugs inserted into the larger carbon/carbon specimen. The purpose of analyzing the test data was to estimate the surface <span class="hlt">heat</span> <span class="hlt">flux</span> and temperature values from the internal temperature measurements using direct and inverse <span class="hlt">heat</span> transfer methods, thus aiding in the thermal and structural design and analysis of <span class="hlt">high</span> temperature vehicles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20120003896&hterms=max+planck&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dmax%2Bplanck','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20120003896&hterms=max+planck&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dmax%2Bplanck"><span>Global Intercomparison of 12 Land Surface <span class="hlt">Heat</span> <span class="hlt">Flux</span> Estimates</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jimenez, C.; Prigent, C.; Mueller, B.; Seneviratne, S. I.; McCabe, M. F.; Wood, E. F.; Rossow, W. B.; Balsamo, G.; Betts, A. K.; Dirmeyer, P. A.; <a style="text-decoration: none; " href="javascript:void(0); " onClick="displayelement('author_20120003896'); toggleEditAbsImage('author_20120003896_show'); toggleEditAbsImage('author_20120003896_hide'); "> <img style="display:inline; width:12px; height:12px; " src="images/arrow-up.gif" width="12" height="12" border="0" alt="hide" id="author_20120003896_show"> <img style="width:12px; height:12px; display:none; " src="images/arrow-down.gif" width="12" height="12" border="0" alt="hide" id="author_20120003896_hide"></p> <p>2011-01-01</p> <p>A global intercomparison of 12 monthly mean land surface <span class="hlt">heat</span> <span class="hlt">flux</span> products for the period 1993-1995 is presented. The intercomparison includes some of the first emerging global satellite-based products (developed at Paris Observatory, Max Planck Institute for Biogeochemistry, University of California Berkeley, University of Maryland, and Princeton University) and examples of <span class="hlt">fluxes</span> produced by reanalyses (ERA-Interim, MERRA, NCEP-DOE) and off-line land surface models (GSWP-2, GLDAS CLM/ Mosaic/Noah). An intercomparison of the global latent <span class="hlt">heat</span> <span class="hlt">flux</span> (Q(sub le)) annual means shows a spread of approx 20 W/sq m (all-product global average of approx 45 W/sq m). A similar spread is observed for the sensible (Q(sub h)) and net radiative (R(sub n)) <span class="hlt">fluxes</span>. In general, the products correlate well with each other, helped by the large seasonal variability and common forcing data for some of the products. Expected spatial distributions related to the major climatic regimes and geographical features are reproduced by all products. Nevertheless, large Q(sub le)and Q(sub h) absolute differences are also observed. The <span class="hlt">fluxes</span> were spatially averaged for 10 vegetation classes. The larger Q(sub le) differences were observed for the rain forest but, when normalized by mean <span class="hlt">fluxes</span>, the differences were comparable to other classes. In general, the correlations between Q(sub le) and R(sub n) were higher for the satellite-based products compared with the reanalyses and off-line models. The <span class="hlt">fluxes</span> were also averaged for 10 selected basins. The seasonality was generally well captured by all products, but large differences in the <span class="hlt">flux</span> partitioning were observed for some products and basins.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120016444','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120016444"><span>Fabrication and Testing of a Thin-Film <span class="hlt">Heat</span> <span class="hlt">Flux</span> Sensor for a Stirling Convertor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wilson, Scott D.; Fralick, Gustave; Wrbanek, John; Sayir, Ali</p> <p>2009-01-01</p> <p>The NASA Glenn Research Center (GRC) has been testing <span class="hlt">high</span> efficiency free-piston Stirling convertors for potential use in radioisotope power systems since 1999. Stirling convertors are being operated for many years to demonstrate a radioisotope power system capable of providing reliable power for potential multi-year missions. Techniques used to monitor the convertors for change in performance include measurements of temperature, pressure, energy addition, and energy rejection. Micro-porous bulk insulation is used in the Stirling convertor test set up to minimize the loss of thermal energy from the electric <span class="hlt">heat</span> source to the environment. The insulation is characterized before extended operation, enabling correlation of the net thermal energy addition to the convertor. Aging microporous bulk insulation changes insulation efficiency, introducing errors in the correlation for net thermal energy addition. A thin-mm <span class="hlt">heat</span> <span class="hlt">flux</span> sensor was designed and fabricated to directly measure the net thermal energy addition to the Stirling convertor. The fabrication techniques include slip casting and using Physical Vapor Deposition (PVD). One micron thick noble metal thermocouples measure temperature on the surface of an Alumina ceramic disc and <span class="hlt">heat</span> <span class="hlt">flux</span> is calculated. Fabrication, integration, and test results of a thin film <span class="hlt">heat</span> <span class="hlt">flux</span> sensor are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100002217','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100002217"><span><span class="hlt">Heat</span> <span class="hlt">Flux</span> and Wall Temperature Estimates for the NASA Langley HIFiRE Direct Connect Rig</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cuda, Vincent, Jr.; Hass, Neal E.</p> <p>2010-01-01</p> <p>An objective of the Hypersonic International Flight Research Experimentation (HIFiRE) Program Flight 2 is to provide validation data for <span class="hlt">high</span> enthalpy scramjet prediction tools through a single flight test and accompanying ground tests of the HIFiRE Direct Connect Rig (HDCR) tested in the NASA LaRC Arc <span class="hlt">Heated</span> Scramjet Test Facility (AHSTF). The HDCR is a full-scale, copper <span class="hlt">heat</span> sink structure designed to simulate the isolator entrance conditions and isolator, pilot, and combustor section of the HIFiRE flight test experiment flowpath and is fully instrumented to assess combustion performance over a range of operating conditions simulating flight from Mach 5.5 to 8.5 and for various fueling schemes. As part of the instrumentation package, temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> sensors were provided along the flowpath surface and also imbedded in the structure. The purpose of this paper is to demonstrate that the surface <span class="hlt">heat</span> <span class="hlt">flux</span> and wall temperature of the Zirconia coated copper wall can be obtained with a water-cooled <span class="hlt">heat</span> <span class="hlt">flux</span> gage and a sub-surface temperature measurement. An algorithm was developed which used these two measurements to reconstruct the surface conditions along the flowpath. Determinations of the surface conditions of the Zirconia coating were conducted for a variety of conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EPJC...77..251S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EPJC...77..251S"><span>Dynamics of charged bulk viscous collapsing cylindrical source with <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shah, S. M.; Abbas, G.</p> <p>2017-04-01</p> <p>In this paper, we have explored the effects of dissipation on the dynamics of charged bulk viscous collapsing cylindrical source which allows the out-flow of <span class="hlt">heat</span> <span class="hlt">flux</span> in the form of radiations. The Misner-Sharp formalism has been implemented to drive the dynamical equation in terms of proper time and radial derivatives. We have investigated the effects of charge and bulk viscosity on the dynamics of collapsing cylinder. To determine the effects of radial <span class="hlt">heat</span> <span class="hlt">flux</span>, we have formulated the <span class="hlt">heat</span> transport equations in the context of Müller-Israel-Stewart theory by assuming that thermodynamics viscous/<span class="hlt">heat</span> coupling coefficients can be neglected within some approximations. In our discussion, we have introduced the viscosity by the standard (non-causal) thermodynamics approach. The dynamical equations have been coupled with the <span class="hlt">heat</span> transport equation; the consequences of the resulting coupled <span class="hlt">heat</span> equation have been analyzed in detail.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ResPh...8..569I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ResPh...8..569I"><span>Three dimensional rotating flow of Powell-Eyring nanofluid with non-Fourier's <span class="hlt">heat</span> <span class="hlt">flux</span> and non-Fick's mass <span class="hlt">flux</span> theory</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ibrahim, Wubshet</p> <p>2018-03-01</p> <p>This article numerically examines three dimensional boundary layer flow of a rotating Powell-Eyring nanofluid. In modeling <span class="hlt">heat</span> transfer processes, non-Fourier <span class="hlt">heat</span> <span class="hlt">flux</span> theory and for mass transfer non-Fick's mass <span class="hlt">flux</span> theory are employed. This theory is recently re-initiated and it becomes the active research area to resolves some drawback associated with the famous Fourier <span class="hlt">heat</span> <span class="hlt">flux</span> and mass <span class="hlt">flux</span> theory. The mathematical model of the flow problem is a system of non-linear partial differential equations which are obtained using the boundary layer analysis. The non-linear partial differential equations have been transformed into non-linear <span class="hlt">high</span> order ordinary differential equations using similarity transformation. Employing bvp4c algorithm from matlab software routine, the numerical solution of the transformed ordinary differential equations is obtained. The governing equations are constrained by parameters such as rotation parameter λ , the non-Newtonian parameter N, dimensionless thermal relaxation and concentration relaxation parameters δt and δc . The impacts of these parameters have been discussed thoroughly and illustrated using graphs and tables. The findings show that thermal relaxation time δt reduces the thermal and concentration boundary layer thickness. Further, the results reveal that the rotational parameter λ has the effect of decreasing the velocity boundary layer thickness in both x and y directions. Further examination pinpoints that the skin friction coefficient along x-axis is an increasing and skin friction coefficient along y-axis is a decreasing function of rotation parameter λ . Furthermore, the non-Newtonian fluid parameter N has the characteristic of reducing the amount of local Nusselt numbers -f″ (0) and -g″ (0) both in x and y -directions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20170007784&hterms=electrons&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Delectrons','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20170007784&hterms=electrons&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Delectrons"><span><span class="hlt">Electron</span> <span class="hlt">Heating</span> at Kinetic Scales in Magnetosheath Turbulence</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chasapis, Alexandros; Matthaeus, W. H.; Parashar, T. N.; Lecontel, O.; Retino, A.; Breuillard, H.; Khotyaintsev, Y.; Vaivads, A.; Lavraud, B.; Eriksson, E.; <a style="text-decoration: none; " href="javascript:void(0); " onClick="displayelement('author_20170007784'); toggleEditAbsImage('author_20170007784_show'); toggleEditAbsImage('author_20170007784_hide'); "> <img style="display:inline; width:12px; height:12px; " src="images/arrow-up.gif" width="12" height="12" border="0" alt="hide" id="author_20170007784_show"> <img style="width:12px; height:12px; display:none; " src="images/arrow-down.gif" width="12" height="12" border="0" alt="hide" id="author_20170007784_hide"></p> <p>2017-01-01</p> <p>We present a statistical study of coherent structures at kinetic scales, using data from the Magnetospheric Multiscale mission in the Earths magnetosheath. We implemented the multi-spacecraft partial variance of increments (PVI) technique to detect these structures, which are associated with intermittency at kinetic scales. We examine the properties of the <span class="hlt">electron</span> <span class="hlt">heating</span> occurring within such structures. We find that, statistically, structures with a <span class="hlt">high</span> PVI index are regions of significant <span class="hlt">electron</span> <span class="hlt">heating</span>. We also focus on one such structure, a current sheet, which shows some signatures consistent with magnetic reconnection. Strong parallel <span class="hlt">electron</span> <span class="hlt">heating</span> coincides with whistler emissions at the edges of the current sheet.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017SPIE10444E..1PN','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017SPIE10444E..1PN"><span>Satellite data based approach for the estimation of anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> over urban areas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nitis, Theodoros; Tsegas, George; Moussiopoulos, Nicolas; Gounaridis, Dimitrios; Bliziotis, Dimitrios</p> <p>2017-09-01</p> <p>Anthropogenic effects in urban areas influence the thermal conditions in the environment and cause an increase of the atmospheric temperature. The cities are sources of <span class="hlt">heat</span> and pollution, affecting the thermal structure of the atmosphere above them which results to the urban <span class="hlt">heat</span> island effect. In order to analyze the urban <span class="hlt">heat</span> island mechanism, it is important to estimate the anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> which has a considerable impact on the urban energy budget. The anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> is the result of man-made activities (i.e. traffic, industrial processes, <span class="hlt">heating</span>/cooling) and thermal releases from the human body. Many studies have underlined the importance of the Anthropogenic <span class="hlt">Heat</span> <span class="hlt">Flux</span> to the calculation of the urban energy budget and subsequently, the estimation of mesoscale meteorological fields over urban areas. Therefore, spatially disaggregated anthropogenic <span class="hlt">heat</span> <span class="hlt">flux</span> data, at local and city scales, are of major importance for mesoscale meteorological models. The main objectives of the present work are to improve the quality of such data used as input for mesoscale meteorological models simulations and to enhance the application potential of GIS and remote sensing in the fields of climatology and meteorology. For this reason, the Urban Energy Budget concept is proposed as the foundation for an accurate determination of the anthropogenic <span class="hlt">heat</span> discharge as a residual term in the surface energy balance. The methodology is applied to the cities of Athens and Paris using the Landsat ETM+ remote sensing data. The results will help to improve our knowledge on Anthropogenic <span class="hlt">Heat</span> <span class="hlt">Flux</span>, while the potential for further improvement of the methodology is also discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27176779','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27176779"><span>A Comparative Study for Flow of Viscoelastic Fluids with Cattaneo-Christov <span class="hlt">Heat</span> <span class="hlt">Flux</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hayat, Tasawar; Muhammad, Taseer; Alsaedi, Ahmed; Mustafa, Meraj</p> <p>2016-01-01</p> <p>This article examines the impact of Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> in flows of viscoelastic fluids. Flow is generated by a linear stretching sheet. Influence of thermal relaxation time in the considered <span class="hlt">heat</span> <span class="hlt">flux</span> is seen. Mathematical formulation is presented for the boundary layer approach. Suitable transformations lead to a nonlinear differential system. Convergent series solutions of velocity and temperature are achieved. Impacts of various influential parameters on the velocity and temperature are sketched and discussed. Numerical computations are also performed for the skin friction coefficient and <span class="hlt">heat</span> transfer rate. Our findings reveal that the temperature profile has an inverse relationship with the thermal relaxation parameter and the Prandtl number. Further the temperature profile and thermal boundary layer thickness are lower for Cattaneo-Christov <span class="hlt">heat</span> <span class="hlt">flux</span> model in comparison to the classical Fourier's law of <span class="hlt">heat</span> conduction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016HMT....52.2833K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016HMT....52.2833K"><span>Condensation <span class="hlt">heat</span> transfer and pressure drop of R-410A in a 7.0 mm O.D. microfin tube at low mass <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Nae-Hyun</p> <p>2016-12-01</p> <p>R-410A condensation <span class="hlt">heat</span> transfer and pressure drop data are provided for a 7.0 mm O.D. microfin tube at low mass <span class="hlt">fluxes</span> (50-250 kg/m2 s). The <span class="hlt">heat</span> transfer coefficient of the microfin tube shows a minimum behavior with the mass <span class="hlt">flux</span>. At a low mass <span class="hlt">flux</span>, where flow pattern is stratified, condensation induced by surface tension by microfins overwhelms condensation induced by shear, and the <span class="hlt">heat</span> transfer coefficient decreases as mass <span class="hlt">flux</span> increases. At a <span class="hlt">high</span> mass <span class="hlt">flux</span>, where flow pattern is annular, condensation induced by shear governs the <span class="hlt">heat</span> transfer, and the <span class="hlt">heat</span> transfer coefficient increases as mass <span class="hlt">flux</span> increases. The pressure drop of the microfin tube is larger than that of the smooth tube at the annular flow regime. On the contrary, the pressure drop of the smooth tube is larger than that of the microfin tube at the stratified flow regime.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20030062133&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DMagnetic%2BFlux','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20030062133&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DMagnetic%2BFlux"><span>Solar Coronal <span class="hlt">Heating</span> and the Magnetic <span class="hlt">Flux</span> Content of the Network</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Falconer, D. A.; Moore, R. L.; Porter, J. G.; Hathaway, D. H.</p> <p>2003-01-01</p> <p>We investigate the <span class="hlt">heating</span> of the quiet corona by measuring the increase of coronal luminosity with the amount of magnetic <span class="hlt">flux</span> in the underlying network at solar minimum when there were no active regions on the face of the Sun. The coronal luminosity is measured from Fe IX/X-Fe XII pairs of coronal images from SOHO/EIT. The network magnetic <span class="hlt">flux</span> content is measured from SOHO/MDI magnetograms. We find that the luminosity of the corona in our quiet regions increases roughly in proportion to the square root of the magnetic <span class="hlt">flux</span> content of the network and roughly in proportion to the length of the perimeter of the network magnetic <span class="hlt">flux</span> clumps. From (1) this result, (2) other observations of many fine-scale explosive events at the edges of network <span class="hlt">flux</span> clumps, and (3) a demonstration that it is energetically feasible for the <span class="hlt">heating</span> of the corona in quiet regions to be driven by explosions of granule-sized sheared-core magnetic bipoles embedded in the edges of network <span class="hlt">flux</span> clumps, we infer that in quiet regions that are not influenced by active regions the corona is mainly <span class="hlt">heated</span> by such magnetic activity in the edges of the network <span class="hlt">flux</span> clumps. Our observational results together with our feasibility analysis allow us to predict that (1) at the edges of the network <span class="hlt">flux</span> clumps there are many transient sheared-core bipoles of the size and lifetime of granules and having transverse field strengths > approx. 100 G, (2) approx. 30 of these bipoles are present per supergranule, and (3) most spicules are produced by explosions of these bipoles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20030062034&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DMagnetic%2BFlux','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20030062034&hterms=Magnetic+Flux&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DMagnetic%2BFlux"><span>Solar Coronal <span class="hlt">Heating</span> and the Magnetic <span class="hlt">Flux</span> Content of the Network</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moore, R. L.; Falconer, D. A.; Porter, J. G.; Hathaway, D. H.</p> <p>2003-01-01</p> <p>We investigate the <span class="hlt">heating</span> of the quiet corona by measuring the increase of coronal luminosity with the amount of magnetic <span class="hlt">flux</span> in the underlying network at solar minimum when there were no active regions on the face of the Sun. The coronal luminosity is measured from Fe IX/X-Fe XII pairs of coronal images from SOHO/EIT. The network magnetic <span class="hlt">flux</span> content is measured from SOHO/MDI magnetograms. We find that the luminosity of the corona in our quiet regions increases roughly in proportion to the square root of the magnetic <span class="hlt">flux</span> content of the network and roughly in proportion to the length of the perimeter of the network magnetic <span class="hlt">flux</span> clumps. From (1) this result, (2) other observations of many fine-scale explosive events at the edges of network <span class="hlt">flux</span> clumps, and (3) a demonstration that it is energetically feasible for the <span class="hlt">heating</span> of the corona in quiet regions to be driven by explosions of granule-sized sheared-core magnetic bipoles embedded in the edges of network <span class="hlt">flux</span> clumps, we infer that in quiet regions that are not influenced by active regions the corona is mainly <span class="hlt">heated</span> by such magnetic activity in the edges of the network <span class="hlt">flux</span> clumps. Our observational results together with our feasibility analysis allow us to predict that (1) at the edges of the network <span class="hlt">flux</span> clumps there are many transient sheared-core bipoles of the size and lifetime of granules and having transverse field strengths greater than approximately - 100 G, (2) approximately 30 of these bipoles are present per supergranule, and (3) most spicules are produced by explosions of these bipoles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EGUGA..16.6056N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EGUGA..16.6056N"><span>Laboratory experiments of <span class="hlt">heat</span> and moisture <span class="hlt">fluxes</span> through supraglacial debris</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nicholson, Lindsey; Mayer, Christoph; Wirbel, Anna</p> <p>2014-05-01</p> <p>Inspired by earlier work (Reznichenko et al., 2010), we have carried out experiments within a climate chamber to explore the best ways to measure the <span class="hlt">heat</span> and moisture <span class="hlt">fluxes</span> through supraglacial debris. Sample ice blocks were prepared with debris cover of varying lithology, grain size and thickness and were instrumented with a combination of Gemini TinyTag temperature/relative humidity sensors and Decagon soil moisture sensors in order to monitor the <span class="hlt">heat</span> and moisture <span class="hlt">fluxes</span> through the overlying debris material when the experiment is exposed to specified solar lamp radiation and laminar airflow within the temperature-controlled climate chamber. Experimental results can be used to determine the optimal set up for numerical models of <span class="hlt">heat</span> and moisture <span class="hlt">flux</span> through supraglacial debris and also indicate the performance limitations of such sensors that can be expected in field installations. Reznichenko, N., Davies, T., Shulmeister, J. and McSaveney, M. (2010) Effects of debris on ice-surface melting rates: an experimental study. Journal of Glaciology, Volume 56, Number 197, 384-394.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013EGUGA..1511209H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013EGUGA..1511209H"><span>Seasonal cycle of oceanic mixed layer and upper-ocean <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the Mediterranean Sea from in-situ observations.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Houpert, Loïc; Testor, Pierre; Durrieu de Madron, Xavier; Estournel, Claude; D'Ortenzio, Fabrizio</p> <p>2013-04-01</p> <p><span class="hlt">Heat</span> <span class="hlt">fluxes</span> across the ocean-atmosphere interface play a crucial role in the upper turbulent mixing. The depth reached by this turbulent mixing is indicated by an homogenization of seawater properties in the surface layer, and is defined as the Mixed Layer Depth (MLD). The thickness of the mixed layer determines also the <span class="hlt">heat</span> content of the layer that directly interacts with the atmosphere. The seasonal variability of these air-sea <span class="hlt">fluxes</span> is crucial in the calculation of <span class="hlt">heat</span> budget. An improvement in the estimate of these <span class="hlt">fluxes</span> is needed for a better understanding of the Mediterranean ocean circulation and climate, in particular in Regional Climate Models. There are few estimations of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> based on oceanic observations in the Mediterranean, and none of them are based on mixed layer observations. So, we proposed here new estimations of these upper-ocean <span class="hlt">heat</span> <span class="hlt">fluxes</span> based on mixed layer. We present <span class="hlt">high</span> resolution Mediterranean climatology (0.5°) of the mean MLD based on a comprehensive collection of temperature profiles of last 43 years (1969-2012). The database includes more than 150,000 profiles, merging CTD, XBT, ARGO Profiling floats, and gliders observations. This dataset is first used to describe the seasonal cycle of the mixed layer depth on the whole Mediterranean on a monthly climatological basis. Our analysis discriminates several regions with coherent behaviors, in particular the deep water formation sites, characterized by significant differences in the winter mixing intensity. <span class="hlt">Heat</span> storage rates (HSR) were calculated as the time rate of change of the <span class="hlt">heat</span> content integrated from the surface down to a specific depth that is defined as the MLD plus an integration constant. Monthly climatology of net <span class="hlt">heat</span> <span class="hlt">flux</span> (NHF) from ERA-Interim reanalysis was balanced by the 1°x1° resolution <span class="hlt">heat</span> storage rate climatology. Local <span class="hlt">heat</span> budget balance and seasonal variability in the horizontal <span class="hlt">heat</span> <span class="hlt">flux</span> are then discussed by taking into account</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19870053663&hterms=worlds+oceans&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dworlds%2Boceans','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870053663&hterms=worlds+oceans&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dworlds%2Boceans"><span>Mass, <span class="hlt">heat</span> and freshwater <span class="hlt">fluxes</span> in the South Indian Ocean</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fu, Lee-Lueng</p> <p>1986-01-01</p> <p>Six hydrographic sections were used to examine the circulation and property <span class="hlt">fluxes</span> in the South Indian Ocean from 10 to 32 deg S. The calculations were made by applying an inverse method to the data. In the interior of the South Indian Ocean, the geostrophic flow is generally northward. At 18 deg S, the northward interior mass <span class="hlt">flux</span> is balanced by the southward Ekman mass <span class="hlt">flux</span> at the surface, whereas at 32 deg S the northward interior mass <span class="hlt">flux</span> is balanced by the southward mass <span class="hlt">flux</span> of the Agulhas Current. There is a weak, southward mass <span class="hlt">flux</span> of 6 x 10 to the 9th kg/s in the Mozambique Channel. The rate of water exchange between the Pacific Ocean and the Indian Ocean is dependent on the choice of the initial reference level used in the inverse calculation. The choice of 1500 m, the depth of the deep oxygen minimum, has led to a <span class="hlt">flux</span> of water from the Pacific Ocean to the Indian Ocean at a rate of 6.6 x 10 to the 9th kg/s. <span class="hlt">Heat</span> <span class="hlt">flux</span> calculations indicate that the Indian Ocean is exporting <span class="hlt">heat</span> to the rest of the world's oceans at a rate of -0.69 x 10 to the 15th W at 18 deg S and -0.25 x 10 to the 15th W at 32 deg S (negative values being southward).</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_23 --> <div id="page_24" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="461"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1254752-fast-response-electron-scale-turbulence-auxiliary-heating-cessation-national-spherical-torus-experiment','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1254752-fast-response-electron-scale-turbulence-auxiliary-heating-cessation-national-spherical-torus-experiment"><span>Fast response of <span class="hlt">electron</span>-scale turbulence to auxiliary <span class="hlt">heating</span> cessation in National Spherical Torus Experiment</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Ren, Y.; Wang, W. X.; LeBlanc, B. P.; ...</p> <p>2015-11-03</p> <p>In this letter, we report the first observation of the fast response of <span class="hlt">electron</span>-scale turbulence to auxiliary <span class="hlt">heating</span> cessation in National Spherical Torus eXperiment [Ono et al., Nucl. Fusion 40, 557 (2000)]. The observation was made in a set of RF-<span class="hlt">heated</span> L-mode plasmas with toroidal magnetic field of 0.55 T and plasma current of 300 kA. It is observed that <span class="hlt">electron</span>-scale turbulence spectral power (measured with a <span class="hlt">high</span>-k collective microwave scattering system) decreases significantly following fast cessation of RF <span class="hlt">heating</span> that occurs in less than 200 μs. The large drop in the turbulence spectral power has a short time delaymore » of about 1–2 ms relative to the RF cessation and happens on a time scale of 0.5–1 ms, much smaller than the energy confinement time of about 10 ms. Power balance analysis shows a factor of about 2 decrease in <span class="hlt">electron</span> thermal diffusivity after the sudden drop of turbulence spectral power. Measured small changes in equilibrium profiles across the RF cessation are unlikely able to explain this sudden reduction in the measured turbulence and decrease in <span class="hlt">electron</span> thermal transport, supported by local linear stability analysis and both local and global nonlinear gyrokinetic simulations. Furthermore, the observations imply that nonlocal <span class="hlt">flux</span>-driven mechanism may be important for the observed turbulence and <span class="hlt">electron</span> thermal transport.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS1000a2013I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS1000a2013I"><span>Network Simulation solution of free convective flow from a vertical cone with combined effect of non- uniform surface <span class="hlt">heat</span> <span class="hlt">flux</span> and <span class="hlt">heat</span> generation or absorption</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Immanuel, Y.; Pullepu, Bapuji; Sambath, P.</p> <p>2018-04-01</p> <p>A two dimensional mathematical model is formulated for the transitive laminar free convective, incompressible viscous fluid flow over vertical cone with variable surface <span class="hlt">heat</span> <span class="hlt">flux</span> combined with the effects of <span class="hlt">heat</span> generation and absorption is considered . using a powerful computational method based on thermoelectric analogy called Network Simulation Method (NSM0, the solutions of governing nondimensionl coupled, unsteady and nonlinear partial differential conservation equations of the flow that are obtained. The numerical technique is always stable and convergent which establish <span class="hlt">high</span> efficiency and accuracy by employing network simulator computer code Pspice. The effects of velocity and temperature profiles have been analyzed for various factors, namely Prandtl number Pr, <span class="hlt">heat</span> <span class="hlt">flux</span> power law exponent n and <span class="hlt">heat</span> generation/absorption parameter Δ are analyzed graphically.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AIPC.1218.1546B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AIPC.1218.1546B"><span>Experimental Study of a Nitrogen Natural Circulation Loop at Low <span class="hlt">Heat</span> <span class="hlt">Flux</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Baudouy, B.</p> <p>2010-04-01</p> <p>A natural convection circulation loop in liquid nitrogen, i.e. an open thermosiphon flow configuration, has been investigated experimentally near atmospheric pressure. The experiments were conducted on a 2 m <span class="hlt">high</span> loop with a copper tube of 10 mm inner diameter uniformly <span class="hlt">heated</span> over a length of 0.95 m. Evolution of the total mass flow rate of the loop and the pressure difference along the tube are described. We also report the boiling curves where single phase and two-phase flows are identified with increasing <span class="hlt">heat</span> <span class="hlt">flux</span>. We focus our <span class="hlt">heat</span> transfer analysis on the single phase regime where mixed convection is encountered. A <span class="hlt">heat</span> transfer coefficient correlation is proposed. We also examine the boiling incipience as a function of the tube height.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19720018905','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19720018905"><span>Combined buoyancy and flow direction effects on saturated boiling critical <span class="hlt">heat</span> <span class="hlt">flux</span> in liquid nitrogen</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Papell, S. S.</p> <p>1972-01-01</p> <p>Buoyancy effects on the critical <span class="hlt">heat</span> <span class="hlt">flux</span> and general data trends for a liquid nitrogen internal flow system were determined by comparison of upflow and downflow data under identical test conditions. The test section had a 1.28 cm diameter flow passage and a 30.5 cm <span class="hlt">heated</span> length which was subjected to uniform <span class="hlt">heat</span> <span class="hlt">fluxes</span> through resistance <span class="hlt">heating</span>. Test conditions covered a range of pressures from 3.4 to 10.2 atm, inlet velocities from 0.23 to 3.51 m/sec, with the liquid nitrogen temperature at saturated inlet conditions. Data comparisons showed that the critical <span class="hlt">heat</span> <span class="hlt">flux</span> for downflow could be up to 36 percent lower than for upflow. A nonmonotonic relationship between the critical <span class="hlt">heat</span> <span class="hlt">flux</span> and velocity was determined for upflow but not for downflow. A limiting inlet velocity of 4.12 m/sec was determined to be the minimum velocity required to completely suppress the influence of buoyancy on the critical <span class="hlt">heat</span> <span class="hlt">flux</span> for this saturated inlet flow system. A correlation of this limiting fluid velocity is presented that was developed from previously published subcooled liquid nitrogen data and the saturated data of this investigation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23521268','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23521268"><span>How the propagation of <span class="hlt">heat-flux</span> modulations triggers E × B flow pattern formation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kosuga, Y; Diamond, P H; Gürcan, O D</p> <p>2013-03-08</p> <p>We propose a novel mechanism to describe E×B flow pattern formation based upon the dynamics of propagation of <span class="hlt">heat-flux</span> modulations. The E × B flows of interest are staircases, which are quasiregular patterns of strong, localized shear layers and profile corrugations interspersed between regions of avalanching. An analogy of staircase formation to jam formation in traffic flow is used to develop an extended model of <span class="hlt">heat</span> avalanche dynamics. The extension includes a <span class="hlt">flux</span> response time, during which the instantaneous <span class="hlt">heat</span> <span class="hlt">flux</span> relaxes to the mean <span class="hlt">heat</span> <span class="hlt">flux</span>, determined by symmetry constraints. The response time introduced here is the counterpart of the drivers' response time in traffic, during which drivers adjust their speed to match the background traffic flow. The finite response time causes the growth of mesoscale temperature perturbations, which evolve to form profile corrugations. The length scale associated with the maximum growth rate scales as Δ(2) ~ (v(thi)/λT(i))ρ(i)sqrt[χ(neo)τ], where λT(i) is a typical <span class="hlt">heat</span> pulse speed, χ(neo) is the neoclassical thermal diffusivity, and τ is the response time of the <span class="hlt">heat</span> <span class="hlt">flux</span>. The connection between the scale length Δ(2) and the staircase interstep scale is discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016amsf.conf..335Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016amsf.conf..335Y"><span>Effect of Na2O on Crystallisation Behaviour and <span class="hlt">Heat</span> Transfer of Fluorine-Free Mould <span class="hlt">Fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, Jian; Zhang, Jianqiang; Sasaki, Yasushi; Ostrovski, Oleg; Zhang, Chen; Cai, Dexiang; Kashiwaya, Yoshiaki</p> <p></p> <p>Most of the commercial mould <span class="hlt">fluxes</span> contain fluorides which bring about serious environmental problems. The major challenge in the application of fluorine-free mould <span class="hlt">fluxes</span> is to control the <span class="hlt">heat</span> transfer from the strand to copper mould which is closely related to crystallisation behaviour. In this study, the effects of Na2O on the crystallisation behaviour and <span class="hlt">heat</span> transfer of CaO-SiO2-Na2O-B2O3-TiO2-Al2O3-MgO-Li2O mould <span class="hlt">fluxes</span> were investigated using single /double hot thermocouple technique (SHTT/DHTT) and infrared emitter technique (IET), respectively. Continuous cooling transformation (CCT) and time-temperature transformation (TTT) diagrams constructed using SHTT showed that the increase of Na2O concentration led to higher critical cooling rate and shorter incubation time. The crystallisation behaviour in a thermal gradient was examined using DHTT. The <span class="hlt">heat</span> <span class="hlt">flux</span> measured by IET showed that the increase of Na2O concentration decreased the <span class="hlt">heat</span> <span class="hlt">flux</span> when Na2O was lower than 9 mass% but the further increase of Na2O raised the <span class="hlt">heat</span> <span class="hlt">flux</span>. The relationship between <span class="hlt">flux</span> crystallisation and <span class="hlt">heat</span> transfer was also discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3089965','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3089965"><span>In situ methods for measuring thermal properties and <span class="hlt">heat</span> <span class="hlt">flux</span> on planetary bodies</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Kömle, Norbert I.; Hütter, Erika S.; Macher, Wolfgang; Kaufmann, Erika; Kargl, Günter; Knollenberg, Jörg; Grott, Matthias; Spohn, Tilman; Wawrzaszek, Roman; Banaszkiewicz, Marek; Seweryn, Karoly; Hagermann, Axel</p> <p>2011-01-01</p> <p>The thermo-mechanical properties of planetary surface and subsurface layers control to a <span class="hlt">high</span> extent in which way a body interacts with its environment, in particular how it responds to solar irradiation and how it interacts with a potentially existing atmosphere. Furthermore, if the natural temperature profile over a certain depth can be measured in situ, this gives important information about the <span class="hlt">heat</span> <span class="hlt">flux</span> from the interior and thus about the thermal evolution of the body. Therefore, in most of the recent and planned planetary lander missions experiment packages for determining thermo-mechanical properties are part of the payload. Examples are the experiment MUPUS on Rosetta's comet lander Philae, the TECP instrument aboard NASA's Mars polar lander Phoenix, and the mole-type instrument HP3 currently developed for use on upcoming lunar and Mars missions. In this review we describe several methods applied for measuring thermal conductivity and <span class="hlt">heat</span> <span class="hlt">flux</span> and discuss the particular difficulties faced when these properties have to be measured in a low pressure and low temperature environment. We point out the abilities and disadvantages of the different instruments and outline the evaluation procedures necessary to extract reliable thermal conductivity and <span class="hlt">heat</span> <span class="hlt">flux</span> data from in situ measurements. PMID:21760643</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21760643','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21760643"><span>In situ methods for measuring thermal properties and <span class="hlt">heat</span> <span class="hlt">flux</span> on planetary bodies.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kömle, Norbert I; Hütter, Erika S; Macher, Wolfgang; Kaufmann, Erika; Kargl, Günter; Knollenberg, Jörg; Grott, Matthias; Spohn, Tilman; Wawrzaszek, Roman; Banaszkiewicz, Marek; Seweryn, Karoly; Hagermann, Axel</p> <p>2011-06-01</p> <p>The thermo-mechanical properties of planetary surface and subsurface layers control to a <span class="hlt">high</span> extent in which way a body interacts with its environment, in particular how it responds to solar irradiation and how it interacts with a potentially existing atmosphere. Furthermore, if the natural temperature profile over a certain depth can be measured in situ, this gives important information about the <span class="hlt">heat</span> <span class="hlt">flux</span> from the interior and thus about the thermal evolution of the body. Therefore, in most of the recent and planned planetary lander missions experiment packages for determining thermo-mechanical properties are part of the payload. Examples are the experiment MUPUS on Rosetta's comet lander Philae, the TECP instrument aboard NASA's Mars polar lander Phoenix, and the mole-type instrument HP(3) currently developed for use on upcoming lunar and Mars missions. In this review we describe several methods applied for measuring thermal conductivity and <span class="hlt">heat</span> <span class="hlt">flux</span> and discuss the particular difficulties faced when these properties have to be measured in a low pressure and low temperature environment. We point out the abilities and disadvantages of the different instruments and outline the evaluation procedures necessary to extract reliable thermal conductivity and <span class="hlt">heat</span> <span class="hlt">flux</span> data from in situ measurements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890052278&hterms=heat+exchange&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dheat%2Bexchange','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890052278&hterms=heat+exchange&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dheat%2Bexchange"><span>A study of oceanic surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the Greenland, Norwegian, and Barents Seas</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hakkinen, Sirpa; Cavalieri, Donald J.</p> <p>1989-01-01</p> <p>This study examines oceanic surface <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the Norwegian, Greenland, and Barents seas using the gridded Navy Fleet Numerical Oceanography Central surface analysis and the First GARP Global Experiment (FGGE) IIc cloudiness data bases. Monthly and annual means of net and turbulent <span class="hlt">heat</span> <span class="hlt">fluxes</span> are computed for the FGGE year 1979. The FGGE IIb data base consisting of individual observations provides particularly good data coverage in this region for a comparison with the gridded Navy winds and air temperatures. The standard errors of estimate between the Navy and FGGE IIb winds and air temperatures are 3.6 m/s and 2.5 C, respectively. The computations for the latent and sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> are based on bulk formulas with the same constant <span class="hlt">heat</span> exchange coefficient of 0.0015. The results show extremely strong wintertime <span class="hlt">heat</span> <span class="hlt">fluxes</span> in the northern Greenland Sea and especially in the Barents Sea in contrast to previous studies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70016282','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70016282"><span>Spectral estimates of net radiation and soil <span class="hlt">heat</span> <span class="hlt">flux</span></span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Daughtry, C.S.T.; Kustas, William P.; Moran, M.S.; Pinter, P. J.; Jackson, R. D.; Brown, P.W.; Nichols, W.D.; Gay, L.W.</p> <p>1990-01-01</p> <p>Conventional methods of measuring surface energy balance are point measurements and represent only a small area. Remote sensing offers a potential means of measuring outgoing <span class="hlt">fluxes</span> over large areas at the spatial resolution of the sensor. The objective of this study was to estimate net radiation (Rn) and soil <span class="hlt">heat</span> <span class="hlt">flux</span> (G) using remotely sensed multispectral data acquired from an aircraft over large agricultural fields. Ground-based instruments measured Rn and G at nine locations along the flight lines. Incoming <span class="hlt">fluxes</span> were also measured by ground-based instruments. Outgoing <span class="hlt">fluxes</span> were estimated using remotely sensed data. Remote Rn, estimated as the algebraic sum of incoming and outgoing <span class="hlt">fluxes</span>, slightly underestimated Rn measured by the ground-based net radiometers. The mean absolute errors for remote Rn minus measured Rn were less than 7%. Remote G, estimated as a function of a spectral vegetation index and remote Rn, slightly overestimated measured G; however, the mean absolute error for remote G was 13%. Some of the differences between measured and remote values of Rn and G are associated with differences in instrument designs and measurement techniques. The root mean square error for available energy (Rn - G) was 12%. Thus, methods using both ground-based and remotely sensed data can provide reliable estimates of the available energy which can be partitioned into sensible and latent <span class="hlt">heat</span> under nonadvective conditions. ?? 1990.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015NucFu..55c3003T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015NucFu..55c3003T"><span>Coupled interactions between tungsten surfaces and transient <span class="hlt">high-heat-flux</span> deuterium plasmas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Takamura, S.; Uesugi, Y.</p> <p>2015-03-01</p> <p>Fundamental studies on the interactions between transient deuterium-plasma <span class="hlt">heat</span> pulses and tungsten surfaces were carried out in terms of electrical, mechanical and thermal response in a compact plasma device AIT-PID (Aichi Institute of Technology-Plasma Irradiation Device). Firstly, <span class="hlt">electron</span>-emission-induced surface-temperature increase is discussed in the surface-temperature range near tungsten's melting point, which is accomplished by controlling the sheath voltage and power transmission factor. Secondly, anomalous penetration of tungsten atomic efflux into the surrounding plasma was observed in addition to a normal layered population; it is discussed in terms of the effect of substantial tungsten influx into the deuterium plasma, which causes dissipation of plasma <span class="hlt">electron</span> energy. Thirdly, a momentum input from pulsed plasma onto a tungsten target was observed visually. The force is estimated numerically by the accelerated ion flow to the target as well as the reaction of tungsten-vapour efflux. Finally, a discussion follows on the effects of the plasma <span class="hlt">heat</span> pulses on the morphology of tungsten surface (originally a helium-induced ‘fuzzy’ nanostructure). A kind of bifurcated effect is obtained: melting and annealing. Open questions remain for all the phenomena observed, although sheath-voltage-dependent plasma-<span class="hlt">heat</span> input may be a key parameter. Discussions on all these phenomena are provided by considering their implications to tokamak fusion devices.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740003624','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740003624"><span>Effect of gage size on the measurement of local <span class="hlt">heat</span> <span class="hlt">flux</span>. [formulas for determining gage averaging errors</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Baumeister, K. J.; Papell, S. S.</p> <p>1973-01-01</p> <p>General formulas are derived for determining gage averaging errors of strip-type <span class="hlt">heat</span> <span class="hlt">flux</span> meters used in the measurement of one-dimensional <span class="hlt">heat</span> <span class="hlt">flux</span> distributions. In addition, a correction procedure is presented which allows a better estimate for the true value of the local <span class="hlt">heat</span> <span class="hlt">flux</span>. As an example of the technique, the formulas are applied to the cases of <span class="hlt">heat</span> transfer to air slot jets impinging on flat and concave surfaces. It is shown that for many practical problems, the use of very small <span class="hlt">heat</span> <span class="hlt">flux</span> gages is often unnecessary.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19770042168&hterms=geophysique&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dgeophysique','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19770042168&hterms=geophysique&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dgeophysique"><span><span class="hlt">Heat</span> budget of ionospheric <span class="hlt">electrons</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Prasad, S. S.; Schneck, L. J.</p> <p>1976-01-01</p> <p><span class="hlt">Heat</span> input calculations were detached from solar extreme UV data and monatomic oxygen densities were derived from simultaneously measured data sets (ion composition 146-191 km) in a study of the <span class="hlt">heat</span> budget of ionosphere <span class="hlt">electrons</span>. Earlier inferences that cooling predominates over <span class="hlt">heating</span> are supported. A search for additional <span class="hlt">heat</span> sources or a revision of the cooling rates is recommended, by way of balancing the <span class="hlt">heat</span> budget. Importance is attached to <span class="hlt">electron</span> cooling by fine structure excitation of monatomic oxygen.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920045458&hterms=RPA&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DRPA','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920045458&hterms=RPA&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3DRPA"><span><span class="hlt">Electron</span> distributions upstream of the Comet Halley bow shock - Evidence for adiabatic <span class="hlt">heating</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Larson, D. E.; Anderson, K. A.; Lin, R. P.; Carlson, C. W.; Reme, H.; Glassmeier, K. H.; Neubauer, F. M.</p> <p>1992-01-01</p> <p>Three-dimensional plasma <span class="hlt">electron</span> (22 eV to 30 keV) observations upstream of Comet Halley bow shock, obtained by the RPA-1 COPERNIC (Reme Plasma Analyzer - Complete Positive Ion, <span class="hlt">Electron</span> and Ram Negative Ion Measurements near Comet Halley) experiment on the Giotto spacecraft are reported. Besides <span class="hlt">electron</span> distributions typical of the undisturbed solar wind and backstreaming <span class="hlt">electrons</span> observed when the magnetic field line intersects the cometary bow shock, a new type of distribution, characterized by enhanced low energy (less than 100 eV) <span class="hlt">flux</span> which peaks at 90-deg pitch angles is found. These are most prominent when the spacecraft is on field lines which pass close to but are not connected to the bow shock. The 90-deg pitch angle <span class="hlt">electrons</span> appear to have been adiabatically <span class="hlt">heated</span> by the increase in the magnetic field strength resulting from the compression of the upstream solar wind plasma by the cometary mass loading. A model calculation of this effect which agrees qualitatively with the observed 90-deg <span class="hlt">flux</span> enhancements is presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940023156','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940023156"><span>Numerical and experimental analyses of the radiant <span class="hlt">heat</span> <span class="hlt">flux</span> produced by quartz <span class="hlt">heating</span> systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Turner, Travis L.; Ash, Robert L.</p> <p>1994-01-01</p> <p>A method is developed for predicting the radiant <span class="hlt">heat</span> <span class="hlt">flux</span> distribution produced by tungsten filament, tubular fused-quartz envelope <span class="hlt">heating</span> systems with reflectors. The method is an application of Monte Carlo simulation, which takes the form of a random walk or ray tracing scheme. The method is applied to four systems of increasing complexity, including a single lamp without a reflector, a single lamp with a Hat reflector, a single lamp with a parabolic reflector, and up to six lamps in a six-lamp contoured-reflector <span class="hlt">heating</span> unit. The application of the Monte Carlo method to the simulation of the thermal radiation generated by these systems is discussed. The procedures for numerical implementation are also presented. Experiments were conducted to study these quartz <span class="hlt">heating</span> systems and to acquire measurements of the corresponding empirical <span class="hlt">heat</span> <span class="hlt">flux</span> distributions for correlation with analysis. The experiments were conducted such that several complicating factors could be isolated and studied sequentially. Comparisons of the experimental results with analysis are presented and discussed. Good agreement between the experimental and simulated results was obtained in all cases. This study shows that this method can be used to analyze very complicated quartz <span class="hlt">heating</span> systems and can account for factors such as spectral properties, specular reflection from curved surfaces, source enhancement due to reflectors and/or adjacent sources, and interaction with a participating medium in a straightforward manner.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19740030181&hterms=heat+insulation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dheat%2Binsulation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19740030181&hterms=heat+insulation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dheat%2Binsulation"><span>Solid motor aft closure insulation erosion. [<span class="hlt">heat</span> <span class="hlt">flux</span> correlation for rate analysis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stampfl, E.; Landsbaum, E. M.</p> <p>1973-01-01</p> <p>The erosion rate of aft closure insulation in a number of large solid propellant motors was empirically analyzed by correlating the average ablation rate with a number of variables that had previously been demonstrated to affect <span class="hlt">heat</span> <span class="hlt">flux</span>. The main correlating parameter was a <span class="hlt">heat</span> <span class="hlt">flux</span> based on the simplified Bartz <span class="hlt">heat</span> transfer coefficient corrected for two-dimensional effects. A multiplying group contained terms related to port-to-throat ratio, local wall angle, grain geometry and nozzle cant angle. The resulting equation gave a good correlation and is a useful design tool.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22663755-electron-heating-kinetic-scales-magnetosheath-turbulence','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22663755-electron-heating-kinetic-scales-magnetosheath-turbulence"><span><span class="hlt">Electron</span> <span class="hlt">Heating</span> at Kinetic Scales in Magnetosheath Turbulence</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Chasapis, Alexandros; Matthaeus, W. H.; Parashar, T. N.</p> <p>2017-02-20</p> <p>We present a statistical study of coherent structures at kinetic scales, using data from the Magnetospheric Multiscale mission in the Earth’s magnetosheath. We implemented the multi-spacecraft partial variance of increments (PVI) technique to detect these structures, which are associated with intermittency at kinetic scales. We examine the properties of the <span class="hlt">electron</span> <span class="hlt">heating</span> occurring within such structures. We find that, statistically, structures with a <span class="hlt">high</span> PVI index are regions of significant <span class="hlt">electron</span> <span class="hlt">heating</span>. We also focus on one such structure, a current sheet, which shows some signatures consistent with magnetic reconnection. Strong parallel <span class="hlt">electron</span> <span class="hlt">heating</span> coincides with whistler emissions at themore » edges of the current sheet.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPYI2005C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPYI2005C"><span>Progress towards modeling tokamak boundary plasma turbulence and understanding its role in setting divertor <span class="hlt">heat</span> <span class="hlt">flux</span> widths</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Bin</p> <p>2017-10-01</p> <p>QCMs (quasi-coherent modes) are well characterized in the edge of Alcator C-Mod, when operating in the Enhanced Dα (EDA) H-mode, a promising alternative regime for ELM (edge localized modes) suppressed operation. To improve the understanding of the physics behind the QCMs, three typical C-Mod EDA H-Mode discharges are simulated by BOUT + + using a six-field two-fluid model (based on the Braginskii equations). The simulated characteristics of the frequency versus wave number spectra of the modes is in reasonable agreement with phase contrast imaging data. The key simulation results are: 1) Linear spectrum analysis and the nonlinear phase relationship indicate the dominance of resistive-ballooning modes and drift-Alfven wave instabilities; 2) QCMs originate inside the separatrix; (3) magnetic flutter causes the mode spreading into the SOL; 4) the boundary electric field Er changes the turbulent characteristics of the QCMs and controls edge transport and the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> width; 5) the magnitude of the divertor <span class="hlt">heat</span> <span class="hlt">flux</span> depends on the physics models, such as sources and sinks, sheath boundary conditions, and parallel <span class="hlt">heat</span> <span class="hlt">flux</span> limiting coefficient. The BOUT + + simulations have also been performed for inter-ELM periods of DIII-D and EAST discharges, and similar quasi-coherent modes have been found. The parallel <span class="hlt">electron</span> <span class="hlt">heat</span> <span class="hlt">fluxes</span> projected onto the target from these BOUT + + simulations follow the experimental <span class="hlt">heat</span> <span class="hlt">flux</span> width scaling, in particular the inverse dependence of the width on the poloidal magnetic field with an outlier. Further turbulence statistics analysis shows that the blobs are generated near the pedestal peak gradient region inside the separatrix and contribute to the transport of the particle and <span class="hlt">heat</span> in the SOL region. To understand the Goldston heuristic drift-based model, results will also be presented from self-consistent transport simulations with the electric and magnetic drifts in BOUT + + and with the sheath potential included in the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014APS..DPPGP8086W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014APS..DPPGP8086W"><span>Exciting Alfven Waves using Modulated <span class="hlt">Electron</span> <span class="hlt">Heating</span> by <span class="hlt">High</span> Power Microwaves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Yuhou; Gekelman, Walter; Pribyl, Patrick; van Compernolle, Bart; Papadopoulos, Konstantinos</p> <p>2014-10-01</p> <p>Experiments exploring the physics of ionospheric modification with intense perpendicular propagating waves (k-> ⊥B->0) on the Large Plasma Device (LaPD) at UCLA have been upgraded with the addition of a <span class="hlt">high</span> power rapidly pulsed microwave source. The plasma is irradiated with ten pulses (250 kW X-band) near the upper-hybrid frequency. The pulses are modulated at a frequency of a fraction (0.1-1.0) of fci (ion cyclotron frequency). Based on a previous single-pulse experiment, the modulated <span class="hlt">electron</span> <span class="hlt">heating</span> may drive a large amplitude shear Alfvén wave (f <fci), making the plasma a virtual antenna. This wave driving mechanism may have important application in terrestrial radio communications by low frequency waves, which are difficult to launch directly due to their enormous wavelengths. Various <span class="hlt">heating</span> methods involving X-mode, O-mode, and <span class="hlt">electron</span> Bernstein mode are investigated in plasmas with controllable parameters (ne =108 ~1012 cm-3 ,Te = 0 . 1 ~ 6 eV ,Ti <<Te ,B0 = 100 ~ 3000 G). Mode-conversion between these waves and the subsequent structural changes of the plasma near the conversion region are also under investigation. This work is supported by an AFOSR MURI award, and conducted at the Basic Plasma Science Facility at UCLA funded by DoE and NSF.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017HMT....53.3241A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017HMT....53.3241A"><span>Characterization of a <span class="hlt">high</span> performance ultra-thin <span class="hlt">heat</span> pipe cooling module for mobile hand held <span class="hlt">electronic</span> devices</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ahamed, Mohammad Shahed; Saito, Yuji; Mashiko, Koichi; Mochizuki, Masataka</p> <p>2017-11-01</p> <p>In recent years, <span class="hlt">heat</span> pipes have been widely used in various hand held mobile <span class="hlt">electronic</span> devices such as smart phones, tablet PCs, digital cameras. With the development of technology these devices have different user friendly features and applications; which require very <span class="hlt">high</span> clock speeds of the processor. In general, a <span class="hlt">high</span> clock speed generates a lot of <span class="hlt">heat</span>, which needs to be spreaded or removed to eliminate the hot spot on the processor surface. However, it is a challenging task to achieve proper cooling of such <span class="hlt">electronic</span> devices mentioned above because of their confined spaces and concentrated <span class="hlt">heat</span> sources. Regarding this challenge, we introduced an ultra-thin <span class="hlt">heat</span> pipe; this <span class="hlt">heat</span> pipe consists of a special fiber wick structure named as "Center Fiber Wick" which can provide sufficient vapor space on the both sides of the wick structure. We also developed a cooling module that uses this kind of ultra-thin <span class="hlt">heat</span> pipe to eliminate the hot spot issue. This cooling module consists of an ultra-thin <span class="hlt">heat</span> pipe and a metal plate. By changing the width, the flattened thickness and the effective length of the ultra-thin <span class="hlt">heat</span> pipe, several experiments have been conducted to characterize the thermal properties of the developed cooling module. In addition, other experiments were also conducted to determine the effects of changes in the number of <span class="hlt">heat</span> pipes in a single module. Characterization and comparison of the module have also been conducted both experimentally and theoretically.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_24 --> <div id="page_25" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="481"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/872555','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/872555"><span>Method of fission <span class="hlt">heat</span> <span class="hlt">flux</span> determination from experimental data</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Paxton, Frank A.</p> <p>1999-01-01</p> <p>A method is provided for determining the fission <span class="hlt">heat</span> <span class="hlt">flux</span> of a prime specimen inserted into a specimen of a test reactor. A pair of thermocouple test specimens are positioned at the same level in the holder and a determination is made of various experimental data including the temperature of the thermocouple test specimens, the temperature of bulk water channels located in the test holder, the gamma scan count ratios for the thermocouple test specimens and the prime specimen, and the thicknesses of the outer clads, the fuel fillers, and the backclad of the thermocouple test specimen. Using this experimental data, the absolute value of the fission <span class="hlt">heat</span> <span class="hlt">flux</span> for the thermocouple test specimens and prime specimen can be calculated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhST..170a4001G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhST..170a4001G"><span>Results of <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> qualification tests of W monoblock components for WEST</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Greuner, H.; Böswirth, B.; Lipa, M.; Missirlian, M.; Richou, M.</p> <p>2017-12-01</p> <p>One goal of the WEST project (W Environment in Steady-state Tokamak) is the manufacturing, quality assessment and operation of ITER-like actively water-cooled divertor plasma facing components made of tungsten. Six W monoblock plasma facing units (PFUs) from different suppliers have been successfully evaluated in the <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span> test facility GLADIS at IPP. Each PFU is equipped with 35 W monoblocks of an ITER-like geometry. However, the W blocks are made of different tungsten grades and the suppliers applied different bonding techniques between tungsten and the inserted Cu-alloy cooling tubes. The intention of the HHF test campaign was to assess the manufacturing quality of the PFUs on the basis of a statistical analysis of the surface temperature evolution of the individual W monoblocks during thermal loading with 100 cycles at 10 MW m-2. These tests confirm the non-destructive examinations performed by the manufacturer and CEA prior to the installation of the WEST platform, and no defects of the components were detected.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009DPS....41.1409P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009DPS....41.1409P"><span>Solar <span class="hlt">Flux</span> Deposition And <span class="hlt">Heating</span> Rates In Jupiter's Atmosphere</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Perez-Hoyos, Santiago; Sánchez-Lavega, A.</p> <p>2009-09-01</p> <p>We discuss here the solar downward net <span class="hlt">flux</span> in the 0.25 - 2.5 µm range in the atmosphere of Jupiter and the associated <span class="hlt">heating</span> rates under a number of vertical cloud structure scenarios focusing in the effect of clouds and hazes. Our numerical model is based in the doubling-adding technique to solve the radiative transfer equation and it includes gas absorption by CH4, NH3 and H2, in addition to Rayleigh scattering by a mixture of H2 plus He. Four paradigmatic Jovian regions have been considered (hot-spots, belts, zones and Polar Regions). The hot-spots are the most transparent regions with downward net <span class="hlt">fluxes</span> of 2.5±0.5 Wm-2 at the 6 bar level. The maximum solar <span class="hlt">heating</span> is 0.04±0.01 K/day and occurs above 1 bar. Belts and zones characterization result in a maximum net downward <span class="hlt">flux</span> of 0.5 Wm-2 at 2 bar and 0.015 Wm-2 at 6 bar. <span class="hlt">Heating</span> is concentrated in the stratospheric and tropospheric hazes. Finally, Polar Regions are also explored and the results point to a considerable stratospheric <span class="hlt">heating</span> of 0.04±0.02 K/day. In all, these calculations suggest that the role of the direct solar forcing in the Jovian atmospheric dynamics is limited to the upper 1 - 2 bar of the atmosphere except in the hot-spot areas. Acknowledgments: This work has been funded by Spanish MEC AYA2006-07735 with FEDER support and Grupos Gobierno Vasco IT-464-07.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018GeoJI.214..265V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018GeoJI.214..265V"><span>Temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> scaling laws for isoviscous, infinite Prandtl number mixed <span class="hlt">heating</span> convection</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vilella, Kenny; Deschamps, Frédéric</p> <p>2018-07-01</p> <p>Thermal evolution of terrestrial planets is controlled by <span class="hlt">heat</span> transfer through their silicate mantles. A suitable framework for modelling this <span class="hlt">heat</span> transport is a system including bottom <span class="hlt">heating</span> (from the core) and internal <span class="hlt">heating</span>, for example, generated by secular cooling or by the decay of radioactive isotopes. The mechanism of <span class="hlt">heat</span> transfer depends on the physical properties of the system. In systems where convection is able to operate, two different regimes are possible depending on the relative amount of bottom and internal <span class="hlt">heating</span>. For moderate internal <span class="hlt">heating</span> rates, the system is composed of active hot upwellings and cold downwellings. For large internal <span class="hlt">heating</span> rates, the bottom <span class="hlt">heat</span> <span class="hlt">flux</span> becomes negative and the system is only composed of active cold downwellings. Here, we build theoretical scaling laws for both convective regimes following the approach of Vilella & Kaminski (2017), which links the surface <span class="hlt">heat</span> <span class="hlt">flux</span> and the temperature jump across both the top and the bottom thermal boundary layer (TBL) to the Rayleigh number and the dimensionless internal <span class="hlt">heating</span> rate. Theoretical predictions are then verified against numerical simulations performed in 2-D and 3-D Cartesiangeometry, and covering a large range of the parameter space. Our theoretical scaling laws are more successful in predicting the thermal structure of systems with large internal <span class="hlt">heating</span> rates than that of systems with no or moderate internal <span class="hlt">heating</span>. The differences between moderate and large internal <span class="hlt">heating</span> rates are interpreted as differences in the mechanisms generating thermal instabilities. We identified three mechanisms: conductive growth of the TBL, instability impacting, and TBL erosion, the last two being present only for moderate internal <span class="hlt">heating</span> rates, in which hot plumes are generated at the bottom of the system and are able to reach the surface. Finally, we apply our scaling laws to the evolution of the early Earth, proposing a new model for the cooling of the primordial</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018GeoJI.tmp..134V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018GeoJI.tmp..134V"><span>Temperature and <span class="hlt">heat</span> <span class="hlt">flux</span> scaling laws for isoviscous, infinite Prandtl number mixed <span class="hlt">heating</span> convection.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vilella, Kenny; Deschamps, Frederic</p> <p>2018-04-01</p> <p>Thermal evolution of terrestrial planets is controlled by <span class="hlt">heat</span> transfer through their silicate mantles. A suitable framework for modelling this <span class="hlt">heat</span> transport is a system including bottom <span class="hlt">heating</span> (from the core) and internal <span class="hlt">heating</span>, e.g., generated by secular cooling or by the decay of radioactive isotopes. The mechanism of <span class="hlt">heat</span> transfer depends on the physical properties of the system. In systems where convection is able to operate, two different regimes are possible depending on the relative amount of bottom and internal <span class="hlt">heating</span>. For moderate internal <span class="hlt">heating</span> rates, the system is composed of active hot upwellings and cold downwellings. For large internal <span class="hlt">heating</span> rates, the bottom <span class="hlt">heat</span> <span class="hlt">flux</span> becomes negative and the system is only composed of active cold downwellings. Here, we build theoretical scaling laws for both convective regimes following the approach of Vilella & Kaminski (2017), which links the surface <span class="hlt">heat</span> <span class="hlt">flux</span> and the temperature jump across both the top and bottom thermal boundary layer (TBL) to the Rayleigh number and the dimensionless internal <span class="hlt">heating</span> rate. Theoretical predictions are then verified against numerical simulations performed in 2D and 3D-Cartesian geometry, and covering a large range of the parameter space. Our theoretical scaling laws are more successful in predicting the thermal structure of systems with large internal <span class="hlt">heating</span> rates than that of systems with no or moderate internal <span class="hlt">heating</span>. The differences between moderate and large internal <span class="hlt">heating</span> rates are interpreted as differences in the mechanisms generating thermal instabilities. We identified three mechanisms: conductive growth of the TBL, instability impacting, and TBL erosion, the last two being present only for moderate internal <span class="hlt">heating</span> rates, in which hot plumes are generated at the bottom of the system and are able to reach the surface. Finally, we apply our scaling laws to the evolution of the early Earth, proposing a new model for the cooling of the primordial magma ocean</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JGRC..121.8419K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JGRC..121.8419K"><span>Reconciling estimates of the ratio of <span class="hlt">heat</span> and salt <span class="hlt">fluxes</span> at the ice-ocean interface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Keitzl, T.; Mellado, J. P.; Notz, D.</p> <p>2016-12-01</p> <p>The <span class="hlt">heat</span> exchange between floating ice and the underlying ocean is determined by the interplay of diffusive <span class="hlt">fluxes</span> directly at the ice-ocean interface and turbulent <span class="hlt">fluxes</span> away from it. In this study, we examine this interplay through direct numerical simulations of free convection. Our results show that an estimation of the interface <span class="hlt">flux</span> ratio based on direct measurements of the turbulent <span class="hlt">fluxes</span> can be difficult because the <span class="hlt">flux</span> ratio varies with depth. As an alternative, we present a consistent evaluation of the <span class="hlt">flux</span> ratio based on the total <span class="hlt">heat</span> and salt <span class="hlt">fluxes</span> across the boundary layer. This approach allows us to reconcile previous estimates of the ice-ocean interface conditions. We find that the ratio of <span class="hlt">heat</span> and salt <span class="hlt">fluxes</span> directly at the interface is 83-100 rather than 33 as determined by previous turbulence measurements in the outer layer. This can cause errors in the estimated ice-ablation rate from field measurements of up to 40% if they are based on the three-equation formulation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950065587&hterms=burning+plasma&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dburning%2Bplasma','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950065587&hterms=burning+plasma&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dburning%2Bplasma"><span>Measuring <span class="hlt">Fluxes</span> Of <span class="hlt">Heat</span> To A Plasma-Arc Anode</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Sankovic, John M.; Menart, James A.; Pfender, Emil; Heberlein, Joachim</p> <p>1995-01-01</p> <p>Three probes constructed to provide measurements indicative of conductive, convective, and radiative transfer of <span class="hlt">heat</span> from free-burning plasma arc to water-cooled copper anode used in generating arc. Each probe consists mainly of copper body with two thermocouples embedded at locations 4 mm apart along length. Thermocouples provide measure of rate of conduction of <span class="hlt">heat</span> along probe and transfers of <span class="hlt">heat</span> from plasma to sensing surface at tip of probe. Probes identical except sensing surface of one uncoated and other two coated with different materials to make them sensitive to different components of overall <span class="hlt">flux</span> of <span class="hlt">heat</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/111422','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/111422"><span>General correlation for prediction of critical <span class="hlt">heat</span> <span class="hlt">flux</span> ratio in water cooled channels</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Pernica, R.; Cizek, J.</p> <p>1995-09-01</p> <p>The paper present the general empirical Critical <span class="hlt">Heat</span> <span class="hlt">Flux</span> Ration (CHFR) correlation which is valid for vertical water upflow through tubes, internally <span class="hlt">heated</span> concentric annuli and rod bundles geometries with both wide and very tight square and triangular rods lattices. The proposed general PG correlation directly predicts the CHFR, it comprises axial and radial non-uniform <span class="hlt">heating</span>, and is valid in a wider range of thermal hydraulic conditions than previously published critical <span class="hlt">heat</span> <span class="hlt">flux</span> correlations. The PG correlation has been developed using the critical <span class="hlt">heat</span> <span class="hlt">flux</span> Czech data bank which includes more than 9500 experimental data on tubes, 7600 data onmore » rod bundles and 713 data on internally <span class="hlt">heated</span> concentric annuli. Accuracy of the CHFR prediction, statistically assessed by the constant dryout conditions approach, is characterized by the mean value nearing 1.00 and the standard deviation less than 0.06. Moverover, a subchannel form of the PG correlations is statistically verified on Westinghouse and Combustion Engineering rod bundle data bases, i.e. more than 7000 experimental CHF points of Columbia University data bank were used.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22402477-electronic-cooling-using-thermoelectric-devices','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22402477-electronic-cooling-using-thermoelectric-devices"><span><span class="hlt">Electronic</span> cooling using thermoelectric devices</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Zebarjadi, M., E-mail: m.zebarjadi@rutgers.edu; Institute of Advanced Materials, Devices, and Nanotechnology, Rutgers University, Piscataway, New Jersey 08854</p> <p>2015-05-18</p> <p>Thermoelectric coolers or Peltier coolers are used to pump <span class="hlt">heat</span> in the opposite direction of the natural <span class="hlt">heat</span> <span class="hlt">flux</span>. These coolers have also been proposed for <span class="hlt">electronic</span> cooling, wherein the aim is to pump <span class="hlt">heat</span> in the natural <span class="hlt">heat</span> <span class="hlt">flux</span> direction and from hot spots to the colder ambient temperature. In this manuscript, we show that for such applications, one needs to use thermoelectric materials with large thermal conductivity and large power factor, instead of the traditionally used <span class="hlt">high</span> ZT thermoelectric materials. We further show that with the known thermoelectric materials, the active cooling cannot compete with passive cooling, andmore » one needs to explore a new set of materials to provide a cooling solution better than a regular copper <span class="hlt">heat</span> sink. We propose a set of materials and directions for exploring possible materials candidates suitable for <span class="hlt">electronic</span> cooling. Finally, to achieve maximum cooling, we propose to use thermoelectric elements as fins attached to copper blocks.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19880733','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19880733"><span>Transectional <span class="hlt">heat</span> transfer in thermoregulating bigeye tuna (Thunnus obesus) - a 2D <span class="hlt">heat</span> <span class="hlt">flux</span> model.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Boye, Jess; Musyl, Michael; Brill, Richard; Malte, Hans</p> <p>2009-11-01</p> <p>We developed a 2D <span class="hlt">heat</span> <span class="hlt">flux</span> model to elucidate routes and rates of <span class="hlt">heat</span> transfer within bigeye tuna Thunnus obesus Lowe 1839 in both steady-state and time-dependent settings. In modeling the former situation, we adjusted the efficiencies of <span class="hlt">heat</span> conservation in the red and the white muscle so as to make the output of the model agree as closely as possible with observed cross-sectional isotherms. In modeling the latter situation, we applied the <span class="hlt">heat</span> exchanger efficiencies from the steady-state model to predict the distribution of temperature and <span class="hlt">heat</span> <span class="hlt">fluxes</span> in bigeye tuna during their extensive daily vertical excursions. The simulations yielded a close match to the data recorded in free-swimming fish and strongly point to the importance of the <span class="hlt">heat</span>-producing and <span class="hlt">heat</span>-conserving properties of the white muscle. The best correspondence between model output and observed data was obtained when the countercurrent <span class="hlt">heat</span> exchangers in the blood flow pathways to the red and white muscle retained 99% and 96% (respectively) of the <span class="hlt">heat</span> produced in these tissues. Our model confirms that the ability of bigeye tuna to maintain elevated muscle temperatures during their extensive daily vertical movements depends on their ability to rapidly modulate <span class="hlt">heating</span> and cooling rates. This study shows that the differential cooling and <span class="hlt">heating</span> rates could be fully accounted for by a mechanism where blood flow to the swimming muscles is either exclusively through the <span class="hlt">heat</span> exchangers or completely shunted around them, depending on the ambient temperature relative to the body temperature. Our results therefore strongly suggest that such a mechanism is involved in the extensive physiological thermoregulatory abilities of endothermic bigeye tuna.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EGUGA..1615883R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EGUGA..1615883R"><span>Geothermal <span class="hlt">Heat</span> <span class="hlt">Flux</span>: Linking Deep Earth's Interior and the Dynamics of Large-Scale Ice Sheets</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rogozhina, Irina; Vaughan, Alan</p> <p>2014-05-01</p> <p>Regions covered by continental-scale ice sheets have the highest degree of uncertainty in composition and structure of the crust and lithospheric mantle, compounded by the poorest coverage on Earth of direct <span class="hlt">heat</span> flow measurements. In addition to challenging conditions that make direct measurements and geological survey difficult Greenland and Antarctica are known to be geologically complex. Antarctica in particular is marked by two lithospherically distinct zones. In contrast to young and thin lithosphere of West Antarctica, East Antarctica is a collage of thick Precambrian fragments of Gondwana and earlier supercontinents. However, recent observations and modeling studies have detected large systems of subglacial lakes extending beneath much of the East Antarctic ice sheet base that have been linked to anomalously elevated <span class="hlt">heat</span> flow. Outcrop samples from the rift margin with Australia (Prydz Bay) have revealed <span class="hlt">highly</span> radiogenic Cambrian granite intrusives that are implicated in regional increase of crustal <span class="hlt">heat</span> <span class="hlt">flux</span> by a factor of two to three compared to the estimated continental background. Taken together, these indicate <span class="hlt">high</span> variability of <span class="hlt">heat</span> flow and properties of rocks across Antarctica. Similar conclusions have been made based on direct measurements and observations of the Greenland ice sheet. Airborne ice-penetrating radar and deep ice core projects show very <span class="hlt">high</span> rates of basal melt for parts of the ice sheet in northern and central Greenland that have been explained by abnormally <span class="hlt">high</span> <span class="hlt">heat</span> <span class="hlt">flux</span>. Archaean in age, the Greenland lithosphere was significantly reworked during the Early Proterozoic. In this region, the interpretation of independent geophysical data is complicated by Proterozoic and Phanerozoic collision zones, compounded by strong thermochemical effects of rifting along the western and eastern continental margins between 80 and 25 million years ago. In addition, <span class="hlt">high</span> variability of <span class="hlt">heat</span> flow and thermal lithosphere structure in central</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22486409-frozen-flux-violation-electron-demagnetization-magnetic-reconnection','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22486409-frozen-flux-violation-electron-demagnetization-magnetic-reconnection"><span>Frozen <span class="hlt">flux</span> violation, <span class="hlt">electron</span> demagnetization and magnetic reconnection</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Scudder, J. D.; Karimabadi, H.; Roytershteyn, V.</p> <p>2015-10-15</p> <p>We argue that the analogue in collisionless plasma of the collisional diffusion region of magnetic reconnection is properly defined in terms of the demagnetization of the plasma <span class="hlt">electrons</span> that enable “frozen flux” slippage to occur. This condition differs from the violation of the “frozen-in” condition, which only implies that two fluid effects are involved, rather than the necessary slippage of magnetic <span class="hlt">flux</span> as viewed in the <span class="hlt">electron</span> frame. Using 2D Particle In Cell (PIC) simulations, this approach properly finds the saddle point region of the <span class="hlt">flux</span> function. Our demagnetization conditions are the dimensionless guiding center approximation expansion parameters for electronsmore » which we show are observable and determined locally by the ratio of non-ideal electric to magnetic field strengths. Proxies for frozen <span class="hlt">flux</span> slippage are developed that (a) are measurable on a single spacecraft, (b) are dimensionless with theoretically justified threshold values of significance, and (c) are shown in 2D simulations to recover distinctions theoretically possible with the (unmeasurable) <span class="hlt">flux</span> function. A new potentially observable dimensionless frozen <span class="hlt">flux</span> rate, Λ{sub Φ}, differentiates significant from anecdotal frozen <span class="hlt">flux</span> slippage. A single spacecraft observable, ϒ, is shown with PIC simulations to be essentially proportional to the unobservable local Maxwell frozen <span class="hlt">flux</span> rate. This relationship theoretically establishes <span class="hlt">electron</span> demagnetization in 3D as the general cause of frozen <span class="hlt">flux</span> slippage. In simple 2D cases with an isolated central diffusion region surrounded by separatrices, these diagnostics uniquely identify the traditional diffusion region (without confusing it with the two fluid “ion-diffusion” region) and clarify the role of the separatrices where frozen <span class="hlt">flux</span> violations do occur but are not substantial. In the more complicated guide and asymmetric 2D cases, substantial <span class="hlt">flux</span> slippage regions extend out along, but inside of, the preferred</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040161241','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040161241"><span>Effects of <span class="hlt">Heat</span> <span class="hlt">Flux</span>, Oxygen Concentration and Glass Fiber Volume Fraction on Pyrolysate Mass <span class="hlt">Flux</span> from Composite Solids</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rich, D. B.; Lautenberger, C. W.; Yuan, Z.; Fernandez-Pello, A. C.</p> <p>2004-01-01</p> <p>Experimental work on the effects of <span class="hlt">heat</span> <span class="hlt">flux</span>, oxygen concentration and glass fiber volume fraction on pyrolysate mass <span class="hlt">flux</span> from samples of polypropylene/glass fiber composite (PP/G) is underway. The research is conducted as part of a larger project to develop a test methodology for flammability of materials, particularly composites, in the microgravity and variable oxygen concentration environment of spacecraft and space structures. Samples of PP/G sized at 30 x 30 x 10 mm are flush mounted in a flow tunnel, which provides a flow of oxidizer over the surface of the samples at a fixed value of 1 m/s and oxygen concentrations varying between 18 and 30%. Each sample is exposed to a constant external radiant <span class="hlt">heat</span> <span class="hlt">flux</span> at a given value, which varies between tests from 10 to 24 kW/sq m. Continuous sample mass loss and surface temperature measurements are recorded for each test. Some tests are conducted with an igniter and some are not. In the former case, the research goal is to quantify the critical mass <span class="hlt">flux</span> at ignition for the various environmental and material conditions described above. The later case generates a wider range of mass <span class="hlt">flux</span> rates than those seen prior to ignition, providing an opportunity to examine the protective effects of blowing on oxidative pyrolysis and <span class="hlt">heating</span> of the surface. Graphs of surface temperature and sample mass loss vs. time for samples of 30% PPG at oxygen concentrations of 18 and 21% are presented in the figures below. These figures give a clear indication of the lower pyrolysis rate and extended time to ignition that accompany a lower oxygen concentration. Analysis of the mass <span class="hlt">flux</span> rate at the time of ignition gives good repeatability but requires further work to provide a clear indication of mass <span class="hlt">flux</span> trends accompanying changes in environmental and material properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040084193','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040084193"><span>Effects of <span class="hlt">Heat</span> <span class="hlt">Flux</span>, Oxygen Concentration and Glass Fiber Volume Fraction on Pyrolysate Mass <span class="hlt">Flux</span> from Composite Solids</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rich, D. B.; Lautenberger, C. W.; Yuan, Z.; Fernandez-Pello, A. C.</p> <p>2004-01-01</p> <p>Experimental work on the effects of <span class="hlt">heat</span> <span class="hlt">flux</span>, oxygen concentration and glass fiber volume fraction on pyrolysate mass <span class="hlt">flux</span> from samples of polypropylene/glass fiber composite (PP/G) is underway. The research is conducted as part of a larger project to develop a test methodology for flammability of materials, particularly composites, in the microgravity and variable oxygen concentration environment of spacecraft and space structures. Samples of PP/G sized at 30x30x10 mm are flush mounted in a flow tunnel, which provides a flow of oxidizer over the surface of the samples at a fixed value of 1 m/s and oxygen concentrations varying between 18 and 30%. Each sample is exposed to a constant external radiant <span class="hlt">heat</span> <span class="hlt">flux</span> at a given value, which varies between tests from 10 to 24 kW/m2. Continuous sample mass loss and surface temperature measurements are recorded for each test. Some tests are conducted with an igniter and some are not. In the former case, the research goal is to quantify the critical mass <span class="hlt">flux</span> at ignition for the various environmental and material conditions described above. The later case generates a wider range of mass <span class="hlt">flux</span> rates than those seen prior to ignition, providing an opportunity to examine the protective effects of blowing on oxidative pyrolysis and <span class="hlt">heating</span> of the surface. Graphs of surface temperature and sample mass loss vs. time for samples of 30% PPG at oxygen concentrations of 18 and 21% are presented in the figures below. These figures give a clear indication of the lower pyrolysis rate and extended time to ignition that accompany a lower oxygen concentration. Analysis of the mass <span class="hlt">flux</span> rate at the time of ignition gives good repeatability but requires further work to provide a clear indication of mass <span class="hlt">flux</span> trends accompanying changes in environmental and material properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ClDy...49.1531H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ClDy...49.1531H"><span>Revisiting the global surface energy budgets with maximum-entropy-production model of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huang, Shih-Yu; Deng, Yi; Wang, Jingfeng</p> <p>2017-09-01</p> <p>The maximum-entropy-production (MEP) model of surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>, based on contemporary non-equilibrium thermodynamics, information theory, and atmospheric turbulence theory, is used to re-estimate the global surface <span class="hlt">heat</span> <span class="hlt">fluxes</span>. The MEP model predicted surface <span class="hlt">fluxes</span> automatically balance the surface energy budgets at all time and space scales without the explicit use of near-surface temperature and moisture gradient, wind speed and surface roughness data. The new MEP-based global annual mean <span class="hlt">fluxes</span> over the land surface, using input data of surface radiation, temperature data from National Aeronautics and Space Administration-Clouds and the Earth's Radiant Energy System (NASA CERES) supplemented by surface specific humidity data from the Modern-Era Retrospective Analysis for Research and Applications (MERRA), agree closely with previous estimates. The new estimate of ocean evaporation, not using the MERRA reanalysis data as model inputs, is lower than previous estimates, while the new estimate of ocean sensible <span class="hlt">heat</span> <span class="hlt">flux</span> is higher than previously reported. The MEP model also produces the first global map of ocean surface <span class="hlt">heat</span> <span class="hlt">flux</span> that is not available from existing global reanalysis products.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AdSpR..61.2290Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AdSpR..61.2290Z"><span>Inter-satellite calibration of FengYun 3 medium energy <span class="hlt">electron</span> <span class="hlt">fluxes</span> with POES <span class="hlt">electron</span> measurements</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Yang; Ni, Binbin; Xiang, Zheng; Zhang, Xianguo; Zhang, Xiaoxin; Gu, Xudong; Fu, Song; Cao, Xing; Zou, Zhengyang</p> <p>2018-05-01</p> <p>We perform an L-shell dependent inter-satellite calibration of FengYun 3 medium energy <span class="hlt">electron</span> measurements with POES measurements based on rough orbital conjunctions within 5 min × 0.1 L × 0.5 MLT. By comparing <span class="hlt">electron</span> <span class="hlt">flux</span> data between the U.S. Polar Orbiting Environmental Satellites (POES) and Chinese sun-synchronous satellites including FY-3B and FY-3C for a whole year of 2014, we attempt to remove less reliable data and evaluate systematic uncertainties associated with the FY-3B and FY-3C datasets, expecting to quantify the inter-satellite calibration factors for the 150-350 keV energy channel at L = 2-7. Compared to the POES data, the FY-3B and FY-3C data generally exhibit a similar trend of <span class="hlt">electron</span> <span class="hlt">flux</span> variations but more or less underestimate them within a factor of 5 for the medium <span class="hlt">electron</span> energy 150-350 keV channel. Good consistency in the <span class="hlt">flux</span> conjunctions after the inter-calibration procedures gives us certain confidence to generalize our method to calibrate <span class="hlt">electron</span> <span class="hlt">flux</span> measurements from various satellite instruments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20170003242&hterms=comparative&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcomparative','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20170003242&hterms=comparative&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcomparative"><span>Comparative Analysis of NOAA REFM and SNB3GEO Tools for the Forecast of the <span class="hlt">Fluxes</span> of <span class="hlt">High</span>-Energy <span class="hlt">Electrons</span> at GEO</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Balikhin, M. A.; Rodriguez, J. V.; Boynton, R. J.; Walker, S. N.; Aryan, Homayon; Sibeck, D. G.; Billings, S. A.</p> <p>2016-01-01</p> <p>Reliable forecasts of relativistic <span class="hlt">electrons</span> at geostationary orbit (GEO) are important for the mitigation of their hazardous effects on spacecraft at GEO. For a number of years the Space Weather Prediction Center at NOAA has provided advanced online forecasts of the fluence of <span class="hlt">electrons</span> with energy >2 MeV at GEO using the Relativistic <span class="hlt">Electron</span> Forecast Model (REFM). The REFM forecasts are based on real-time solar wind speed observations at L1. The <span class="hlt">high</span> reliability of this forecasting tool serves as a benchmark for the assessment of other forecasting tools. Since 2012 the Sheffield SNB3GEO model has been operating online, providing a 24 h ahead forecast of the same <span class="hlt">fluxes</span>. In addition to solar wind speed, the SNB3GEO forecasts use solar wind density and interplanetary magnetic field B(sub z) observations at L1. The period of joint operation of both of these forecasts has been used to compare their accuracy. Daily averaged measurements of <span class="hlt">electron</span> <span class="hlt">fluxes</span> by GOES 13 have been used to estimate the prediction efficiency of both forecasting tools. To assess the reliability of both models to forecast infrequent events of very <span class="hlt">high</span> <span class="hlt">fluxes</span>, the Heidke skill score was employed. The results obtained indicate that SNB3GEO provides a more accurate 1 day ahead forecast when compared to REFM. It is shown that the correction methodology utilized by REFM potentially can improve the SNB3GEO forecast.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27642268','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27642268"><span>Comparative analysis of NOAA REFM and SNB3GEO tools for the forecast of the <span class="hlt">fluxes</span> of <span class="hlt">high</span>-energy <span class="hlt">electrons</span> at GEO.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Balikhin, M A; Rodriguez, J V; Boynton, R J; Walker, S N; Aryan, H; Sibeck, D G; Billings, S A</p> <p>2016-01-01</p> <p>Reliable forecasts of relativistic <span class="hlt">electrons</span> at geostationary orbit (GEO) are important for the mitigation of their hazardous effects on spacecraft at GEO. For a number of years the Space Weather Prediction Center at NOAA has provided advanced online forecasts of the fluence of <span class="hlt">electrons</span> with energy >2 MeV at GEO using the Relativistic <span class="hlt">Electron</span> Forecast Model (REFM). The REFM forecasts are based on real-time solar wind speed observations at L1. The <span class="hlt">high</span> reliability of this forecasting tool serves as a benchmark for the assessment of other forecasting tools. Since 2012 the Sheffield SNB 3 GEO model has been operating online, providing a 24 h ahead forecast of the same <span class="hlt">fluxes</span>. In addition to solar wind speed, the SNB 3 GEO forecasts use solar wind density and interplanetary magnetic field B z observations at L1.The period of joint operation of both of these forecasts has been used to compare their accuracy. Daily averaged measurements of <span class="hlt">electron</span> <span class="hlt">fluxes</span> by GOES 13 have been used to estimate the prediction efficiency of both forecasting tools. To assess the reliability of both models to forecast infrequent events of very <span class="hlt">high</span> <span class="hlt">fluxes</span>, the Heidke skill score was employed. The results obtained indicate that SNB 3 GEO provides a more accurate 1 day ahead forecast when compared to REFM. It is shown that the correction methodology utilized by REFM potentially can improve the SNB 3 GEO forecast.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC21D0969Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC21D0969Z"><span>Uncertainty analysis of scintillometers methods in measuring sensible <span class="hlt">heat</span> <span class="hlt">fluxes</span> of forest ecosystem</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zheng, N.</p> <p>2017-12-01</p> <p>Sensible <span class="hlt">heat</span> <span class="hlt">flux</span> (H) is one of the driving factors of surface turbulent motion and energy exchange. Therefore, it is particularly important to measure sensible <span class="hlt">heat</span> <span class="hlt">flux</span> accurately at the regional scale. However, due to the heterogeneity of the underlying surface, hydrothermal regime, and different weather conditions, it is difficult to estimate the represented <span class="hlt">flux</span> at the kilometer scale. The scintillometer have been developed into an effective and universal equipment for deriving <span class="hlt">heat</span> <span class="hlt">flux</span> at the regional-scale which based on the turbulence effect of light in the atmosphere since the 1980s. The parameter directly obtained by the scintillometer is the structure parameter of the refractive index of air based on the changes of light intensity fluctuation. Combine with parameters such as temperature structure parameter, zero-plane displacement, surface roughness, wind velocity, air temperature and the other meteorological data <span class="hlt">heat</span> <span class="hlt">fluxes</span> can be derived. These additional parameters increase the uncertainties of <span class="hlt">flux</span> because the difference between the actual feature of turbulent motion and the applicable conditions of turbulence theory. Most previous studies often focused on the constant <span class="hlt">flux</span> layers that are above the rough sub-layers and homogeneous flat surfaces underlying surfaces with suitable weather conditions. Therefore, the criteria and modified forms of key parameters are invariable. In this study, we conduct investment over the hilly area of northern China with different plants, such as cork oak, cedar-black and locust. On the basis of key research on the threshold and modified forms of saturation with different turbulence intensity, modified forms of Bowen ratio with different drying-and-wetting conditions, universal function for the temperature structure parameter under different atmospheric stability, the dominant sources of uncertainty will be determined. The above study is significant to reveal influence mechanism of uncertainty and explore influence</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160000481','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160000481"><span>Comparison of Turbulent <span class="hlt">Heat</span>-Transfer Results for Uniform Wall <span class="hlt">Heat</span> <span class="hlt">Flux</span> and Uniform Wall Temperature</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Siegel, R.; Sparrow, E. M.</p> <p>1960-01-01</p> <p>The purpose of this note is to examine in a more precise way how the Nusselt numbers for turbulent <span class="hlt">heat</span> transfer in both the fully developed and thermal entrance regions of a circular tube are affected by two different wall boundary conditions. The comparisons are made for: (a) Uniform wall temperature (UWT); and (b) uniform wall <span class="hlt">heat</span> <span class="hlt">flux</span> (UHF). Several papers which have been concerned with the turbulent thermal entrance region problem are given. 1 Although these analyses have all utilized an eigenvalue formulation for the thermal entrance region there were differences in the choices of eddy diffusivity expressions, velocity distributions, and methods for carrying out the numerical solutions. These differences were also found in the fully developed analyses. Hence when making a comparison of the analytical results for uniform wall temperature and uniform wall <span class="hlt">heat</span> <span class="hlt">flux</span>, it was not known if differences in the Nusselt numbers could be wholly attributed to the difference in wall boundary conditions, since all the analytical results were not obtained in a consistent way. To have results which could be directly compared, computations were carried out for the uniform wall temperature case, using the same eddy diffusivity, velocity distribution, and digital computer program employed for uniform wall <span class="hlt">heat</span> <span class="hlt">flux</span>. In addition, the previous work was extended to a lower Reynolds number range so that comparisons could be made over a wide range of both Reynolds and Prandtl numbers.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_25 --> <div class="footer-extlink text-muted" style="margin-bottom:1rem; text-align:center;">Some links on this page may take you to non-federal websites. 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