Sample records for air pressure wind

  1. Investigation of the spatial variability and possible origins of wind-induced air pressure fluctuations responsible for pressure pumping

    NASA Astrophysics Data System (ADS)

    Mohr, Manuel; Laemmel, Thomas; Maier, Martin; Zeeman, Matthias; Longdoz, Bernard; Schindler, Dirk

    2017-04-01

    The exchange of greenhouse gases between the soil and the atmosphere is highly relevant for the climate of the Earth. Recent research suggests that wind-induced air pressure fluctuations can alter the soil gas transport and therefore soil gas efflux significantly. Using a newly developed method, we measured soil gas transport in situ in a well aerated forest soil. Results from these measurements showed that the commonly used soil gas diffusion coefficient is enhanced up to 30% during periods of strong wind-induced air pressure fluctuations. The air pressure fluctuations above the forest floor are only induced at high above-canopy wind speeds (> 5 m s-1) and lie in the frequency range 0.01-0.1 Hz. Moreover, the amplitudes of air pressure fluctuations in this frequency range show a clear quadratic dependence on mean above-canopy wind speed. However, the origin of these wind-induced pressure fluctuations is still unclear. Airflow measurements and high-precision air pressure measurements were conducted at three different vegetation-covered sites (conifer forest, deciduous forest, grassland) to investigate the spatial variability of dominant air pressure fluctuations, their origin and vegetation-dependent characteristics. At the conifer forest site, a vertical profile of air pressure fluctuations was measured and an array consisting of five pressure sensors were installed at the forest floor. At the grassland site, the air pressure measurements were compared with wind observations made by ground-based LIDAR and spatial temperature observations from a fibre-optic sensing network (ScaleX Campaign 2016). Preliminary results show that at all sites the amplitudes of relevant air pressure fluctuations increase with increasing wind speed. Data from the array measurements reveal that there are no time lags between the air pressure signals of different heights, but a time lag existed between the air pressure signals of the sensors distributed laterally on the forest floor

  2. Vandenberg Air Force Base Pressure Gradient Wind Study

    NASA Technical Reports Server (NTRS)

    Shafer, Jaclyn A.

    2013-01-01

    Warning category winds can adversely impact day-to-day space lift operations at Vandenberg Air Force Base (VAFB) in California. NASA's Launch Services Program and other programs at VAFB use wind forecasts issued by the 30 Operational Support Squadron Weather Flight (30 OSSWF) to determine if they need to limit activities or protect property such as a launch vehicle. The 30 OSSWF tasked the AMU to develop an automated Excel graphical user interface that includes pressure gradient thresholds between specific observing stations under different synoptic regimes to aid forecasters when issuing wind warnings. This required the AMU to determine if relationships between the variables existed.

  3. Influence of wind-induced air pressure fluctuations on topsoil gas concentrations within a Scots pine forest

    NASA Astrophysics Data System (ADS)

    Mohr, Manuel; Laemmel, Thomas; Maier, Martin; Schindler, Dirk

    2017-04-01

    Commonly it is assumed that soil gas transport is dominated by molecular diffusion. Few recent studies indicate that the atmosphere above the soil triggers non-diffusive gas transport processes in the soil, which can enhance soil gas transport and therefore soil gas efflux significantly. During high wind speed conditions, the so called pressure pumping effect has been observed: the enhancement of soil gas transport through dynamic changes in the air pressure field above the soil. However, the amplitudes and frequencies of the air pressure fluctuations responsible for pressure pumping are still uncertain. Moreover, an in situ observation of the pressure pumping effect is still missing. To investigate the pressure pumping effect, airflow measurements above and below the canopy of a Scots pine forest and high-precision relative air pressure measurements were conducted in the below-canopy space and in the soil over a measurement period of 16 weeks. To monitor the soil gas transport, a newly developed gas measurement system was used. The gas measurement system continuously injects helium as a tracer gas into the soil until a diffusive steady state is reached. With the steady state concentration profile of the tracer gas, it is possible to inversely model the gas diffusion coefficient profile of the soil. If the gas diffusion coefficient profile differed from steady state, we deduced that the soil gas transport is not only diffusive, but also influenced by non-diffusive processes. Results show that the occurrence of small air pressure fluctuations is strongly dependent on the mean above-canopy wind speed. The wind-induced air pressure fluctuations have mean amplitudes up to 10 Pa and lie in the frequency range 0.01-0.1 Hz. To describe the pumping motion of the air pressure field, the pressure pumping coefficient (PPC) was defined as the mean change in pressure per second. The PPC shows a clear quadratic dependence on mean above-canopy wind speed. Empirical modelling of

  4. Investigation on wind energy-compressed air power system.

    PubMed

    Jia, Guang-Zheng; Wang, Xuan-Yin; Wu, Gen-Mao

    2004-03-01

    Wind energy is a pollution free and renewable resource widely distributed over China. Aimed at protecting the environment and enlarging application of wind energy, a new approach to application of wind energy by using compressed air power to some extent instead of electricity put forward. This includes: explaining the working principles and characteristics of the wind energy-compressed air power system; discussing the compatibility of wind energy and compressor capacity; presenting the theoretical model and computational simulation of the system. The obtained compressor capacity vs wind power relationship in certain wind velocity range can be helpful in the designing of the wind power-compressed air system. Results of investigations on the application of high-pressure compressed air for pressure reduction led to conclusion that pressure reduction with expander is better than the throttle regulator in energy saving.

  5. An evaluation of Shuttle Entry Air Data System (SEADS) flight pressures - Comparisons with wind tunnel and theoretical predictions

    NASA Technical Reports Server (NTRS)

    Henry, M. W.; Wolf, H.; Siemers, Paul M., III

    1988-01-01

    The SEADS pressure data obtained from the Shuttle flight 61-C are analyzed in conjunction with the preflight database. Based on wind tunnel data, the sensitivity of the Shuttle Orbiter stagnation region pressure distribution to angle of attack and Mach number is demonstrated. Comparisons are made between flight and wind tunnel SEADS orifice pressure distributions at several points throughout the re-entry. It is concluded that modified Newtonian theory provides a good tool for the design of a flush air data system, furnishing data for determining orifice locations and transducer sizing. Ground-based wind tunnel facilities are capable of providing the correction factors necessary for the derivation of accurate air data parameters from pressure data.

  6. Multi-hole pressure probes to wind tunnel experiments and air data systems

    NASA Astrophysics Data System (ADS)

    Shevchenko, A. M.; Shmakov, A. S.

    2017-10-01

    The problems to develop a multihole pressure system to measure flow angularity, Mach number and dynamic head for wind tunnel experiments or air data systems are discussed. A simple analytical model with separation of variables is derived for the multihole spherical pressure probe. The proposed model is uniform for small subsonic and supersonic speeds. An error analysis was performed. The error functions are obtained, allowing to estimate the influence of the Mach number, the pitch angle, the location of the pressure ports on the uncertainty of determining the flow parameters.

  7. A large volume 2000 MPA air source for the radiatively driven hypersonic wind tunnel

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

    Constantino, M

    1999-07-14

    An ultra-high pressure air source for a hypersonic wind tunnel for fluid dynamics and combustion physics and chemistry research and development must provide a 10 kg/s pure air flow for more than 1 s at a specific enthalpy of more than 3000 kJ/kg. The nominal operating pressure and temperature condition for the air source is 2000 MPa and 900 K. A radial array of variable radial support intensifiers connected to an axial manifold provides an arbitrarily large total high pressure volume. This configuration also provides solutions to cross bore stress concentrations and the decrease in material strength with temperature. [hypersonic,more » high pressure, air, wind tunnel, ground testing]« less

  8. Air pressures in wood frame walls

    Treesearch

    Anton TenWolde; Charles G. Carll; Vyto Malinauskas

    1998-01-01

    Wind pressures can play an important role in the wetting of exterior walls (driving rain). In response, the rain screen concept, including compartmentalization and air spaces, has been developed to provide pressure equalization and limit water entry into the wall. However, conventional construction such as wood lap siding has not been evaluated as to its ability to...

  9. Direct monitoring of wind-induced pressure-pumping on gas transport in soil

    NASA Astrophysics Data System (ADS)

    Laemmel, Thomas; Mohr, Manuel; Schindler, Dirk; Schack-Kirchner, Helmer; Maier, Martin

    2017-04-01

    Gas exchange between soil and atmosphere is important for the biogeochemistry of soils and is commonly assumed to be governed by molecular diffusion. Yet a few previous field studies identified other gas transport processes such as wind-induced pressure-pumping to enhance soil-atmosphere fluxes significantly. However, since these wind-induced non-diffusive gas transport processes in soil often occur intermittently, the quantification of their contribution to soil gas emissions is challenging. To quantify the effects of wind-induced pressure-pumping on soil gas transport, we developed a method for in situ monitoring of soil gas transport. The method includes the use of Helium (He) as a tracer gas which was continuously injected into the soil. The resulting He steady-state concentration profile was monitored. Gas transport parameters of the soil were inversely modelled. We used our method during a field campaign in a well-aerated forest soil over three months. During periods of low wind speed, soil gas transport was modelled assuming diffusion as transport process. During periods of high wind speed, the previously steady diffusive He concentration profile showed temporary concentration decreases in the topsoil, indicating an increase of the effective gas transport rate in the topsoil up to 30%. The enhancement of effective topsoil soil gas diffusivity resulted from wind-induced air pressure fluctuations which are referred to as pressure-pumping. These air pressure fluctuations had frequencies between 0.1 and 0.01 Hz and amplitudes up to 10 Pa and occurred at above-canopy wind speeds greater than 5 m s-1. We could show the importance of the enhancement of the gas transport rate in relation with the wind intensity and corresponding air pressure fluctuations characteristics. We directly detected and quantified the pressure-pumping effect on gas transport in soil in a field study for the first time, and could thus validate and underpin the importance of this non

  10. Wind Tunnel Tests for Wind Pressure Distribution on Gable Roof Buildings

    PubMed Central

    2013-01-01

    Gable roof buildings are widely used in industrial buildings. Based on wind tunnel tests with rigid models, wind pressure distributions on gable roof buildings with different aspect ratios were measured simultaneously. Some characteristics of the measured wind pressure field on the surfaces of the models were analyzed, including mean wind pressure, fluctuating wind pressure, peak negative wind pressure, and characteristics of proper orthogonal decomposition results of the measured wind pressure field. The results show that extremely high local suctions often occur in the leading edges of longitudinal wall and windward roof, roof corner, and roof ridge which are the severe damaged locations under strong wind. The aspect ratio of building has a certain effect on the mean wind pressure coefficients, and the effect relates to wind attack angle. Compared with experimental results, the region division of roof corner and roof ridge from AIJ2004 is more reasonable than those from CECS102:2002 and MBMA2006.The contributions of the first several eigenvectors to the overall wind pressure distributions become much bigger. The investigation can offer some basic understanding for estimating wind load distribution on gable roof buildings and facilitate wind-resistant design of cladding components and their connections considering wind load path. PMID:24082851

  11. Wind tunnel tests for wind pressure distribution on gable roof buildings.

    PubMed

    Jing, Xiao-kun; Li, Yuan-qi

    2013-01-01

    Gable roof buildings are widely used in industrial buildings. Based on wind tunnel tests with rigid models, wind pressure distributions on gable roof buildings with different aspect ratios were measured simultaneously. Some characteristics of the measured wind pressure field on the surfaces of the models were analyzed, including mean wind pressure, fluctuating wind pressure, peak negative wind pressure, and characteristics of proper orthogonal decomposition results of the measured wind pressure field. The results show that extremely high local suctions often occur in the leading edges of longitudinal wall and windward roof, roof corner, and roof ridge which are the severe damaged locations under strong wind. The aspect ratio of building has a certain effect on the mean wind pressure coefficients, and the effect relates to wind attack angle. Compared with experimental results, the region division of roof corner and roof ridge from AIJ2004 is more reasonable than those from CECS102:2002 and MBMA2006.The contributions of the first several eigenvectors to the overall wind pressure distributions become much bigger. The investigation can offer some basic understanding for estimating wind load distribution on gable roof buildings and facilitate wind-resistant design of cladding components and their connections considering wind load path.

  12. Subsonic tests of an all-flush-pressure-orifice air data system

    NASA Technical Reports Server (NTRS)

    Larson, T. J.; Siemers, P. M., III

    1981-01-01

    The use of an all-flush-pressure-orifice array as a subsonic air data system was evaluated in flight and wind tunnel tests. Two orifice configurations were investigated. Both used orifices arranged in a cruciform pattern on the airplane nose. One configuration also used orifices on the sides of the fuselage for a source of static pressure. The all-nose-orifice configuration was similar to the shuttle entry air data system (SEADS). The flight data were obtained with a KC-135A airplane. The wind tunnel data were acquired with a 0.035-scale model of the KC-135A airplane. With proper calibration, several orifices on the vertical centerline of the vehicle's nose were found to be satisfactory for the determination of total pressure and angle of attack. Angle of sideslip could be accurately determined from pressure measurements made on the horizontal centerline of the aircraft. Orifice pairs were also found that provided pressure ratio relationships suitable for the determination of Mach number. The accuracy that can be expected for the air data determined with SEADS during subsonic orbiter flight is indicated.

  13. Thermodynamic characteristics of a novel wind-solar-liquid air energy storage system

    NASA Astrophysics Data System (ADS)

    Ji, W.; Zhou, Y.; Sun, Y.; Zhang, W.; Pan, C. Z.; Wang, J. J.

    2017-12-01

    Due to the nature of fluctuation and intermittency, the utilization of wind and solar power will bring a huge impact to the power grid management. Therefore a novel hybrid wind-solar-liquid air energy storage (WS-LAES) system was proposed. In this system, wind and solar power are stored in the form of liquid air by cryogenic liquefaction technology and thermal energy by solar thermal collector, respectively. Owing to the high density of liquid air, the system has a large storage capacity and no geographic constraints. The WS-LAES system can store unstable wind and solar power for a stable output of electric energy and hot water. Moreover, a thermodynamic analysis was carried out to investigate the best system performance. The result shows that the increases of compressor adiabatic efficiency, turbine inlet pressure and inlet temperature all have a beneficial effect.

  14. Multi-hole pressure probes to air data system for subsonic small-scale air vehicles

    NASA Astrophysics Data System (ADS)

    Shevchenko, A. M.; Berezin, D. R.; Puzirev, L. N.; Tarasov, A. Z.; Kharitonov, A. M.; Shmakov, A. S.

    2016-10-01

    A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi-hole pressure probe technique of measuring of a 3D flow to use in the air data system. Two multi-hole pressure probes with spherical and hemispherical head to air-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. The probes were calibrated in the wind tunnel, one of them is in-flight tested.

  15. Low-level wind response to mesoscale pressure systems

    NASA Astrophysics Data System (ADS)

    Garratt, J. R.; Physick, W. L.

    1983-09-01

    Observations are presented which show a strong correlation between low-level wind behaviour (e.g., rotation near the surface) and the passage of mesoscale pressure systems. The latter are associated with frontal transition zones, are dominated by a pressure-jump line and a mesoscale high pressure area, and produce locally large horizontal pressure gradients. The wind observations are simulated by specifying a time sequence of perturbation pressure gradient and subsequently solving the vertically-integrated momentum equations with appropriate initial conditions. Very good agreement is found between observed and calculated winds; in particular, (i) a 360 ° rotation in wind on passage of the mesoscale high; (ii) wind-shift lines produced dynamically by the pressure-jump line; (iii) rapid linear increase in wind speed on passage of the pressure jump.

  16. Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft. [conducted in a Langley 8 foot transonic pressure tunnel

    NASA Technical Reports Server (NTRS)

    Larson, T. J.; Flechner, S. G.; Siemers, P. M., III

    1980-01-01

    The results of a wind tunnel investigation on an all flush orifice air data system for use on a KC-135A aircraft are presented. The investigation was performed to determine the applicability of fixed all flush orifice air data systems that use only aircraft surfaces for orifices on the nose of the model (in a configuration similar to that of the shuttle entry air data system) provided the measurements required for the determination of stagnation pressure, angle of attack, and angle of sideslip. For the measurement of static pressure, additional flush orifices in positions on the sides of the fuselage corresponding to those in a standard pitot-static system were required. An acceptable but less accurate system, consisting of orifices only on the nose of the model, is defined and discussed.

  17. Low Pressure Seeder Development for PIV in Large Scale Open Loop Wind Tunnels

    NASA Astrophysics Data System (ADS)

    Schmit, Ryan

    2010-11-01

    A low pressure seeding techniques have been developed for Particle Image Velocimetry (PIV) in large scale wind tunnel facilities was performed at the Subsonic Aerodynamic Research Laboratory (SARL) facility at Wright-Patterson Air Force Base. The SARL facility is an open loop tunnel with a 7 by 10 foot octagonal test section that has 56% optical access and the Mach number varies from 0.2 to 0.5. A low pressure seeder sprayer was designed and tested in the inlet of the wind tunnel. The seeder sprayer was designed to produce an even and uniform distribution of seed while reducing the seeders influence in the test section. ViCount Compact 5000 using Smoke Oil 180 was using as the seeding material. The results show that this low pressure seeder does produce streaky seeding but excellent PIV images are produced.

  18. Field Calibration of XAD-Based Passive Air Sampler on the Tibetan Plateau: Wind Influence and Configuration Improvement.

    PubMed

    Gong, Ping; Wang, Xiaoping; Liu, Xiande; Wania, Frank

    2017-05-16

    The passive air sampler based on XAD-2 resin (XAD-PAS) has proven useful for collecting atmospheric persistent organic pollutants (POPs) in remote regions. Whereas laboratory studies have shown that, due to the open bottom of its housing, the passive sampling rate (PSR) of the XAD-PAS is susceptible to wind and other processes causing air turbulence, the sampler has not been calibrated in the field at sites experiencing high winds. In this study, the PSRs of the XAD-PAS were calibrated at three sites on the Tibetan Plateau, covering a wide range in temperature (T), pressure (P) and wind speed (v). At sites with low wind speeds (i.e., in a forest and an urban site), the PSRs are proportional to the ratio T 1.75 / P; at windy sites with an average wind speed above 3 m/s, the influence of v on PSRs cannot be ignored. Moreover, the open bottom of the XAD-PAS housing causes the PSRs to be influenced by wind angle and air turbulence caused by sloped terrain. Field calibration, wind speed measurements, and computational fluid dynamics (CFD) simulations indicate that a modified design incorporating an air spoiler consisting of 4 metal sheets dampens the turbulence caused by wind angle and sloped terrain and caps the PSR at ∼5 m 3 /day, irrespective of ambient wind. Therefore, the original XAD-PAS with an open bottom is suitable for deployment in urban areas and other less windy places, the modified design is preferable in mountain regions and other places where air circulation is complicated and strong.

  19. [Comfort of crew and passengers and atmospheric pressure, noise, wind speed in high-speed train of Shijiazhuang-Taiyuan passenger dedicated line].

    PubMed

    Zhai, Yi-biao; Huo, Wei; Liu, Qiao-ying; Chen, Bao-shan; Zhang, Jin-long; Shi, Lei

    2012-11-01

    To explore the crew and passengers' comfort on the Shijiazhuang-Taiyuan passenger dedicated line and physical factors, such as air pressure, noise, wind speed. Comfort investigation of all the crew (n = 244) and passengers (n = 377) on the Shijiazhuang-Taiyuan passenger dedicated line at speed of 250 km/h and 200 km/h and the detection of the air pressure, noise and wind speed were performed in 2011. Significantly higher ratio of comfortable feeling, lower ratio of seriously discomfortable feeling were observed in crew and passengers at 200 km/h compared with those at 250 km/h (P < 0.05), as well as rapid disappearance of discomfortable feeling in crew (P < 0.05) and significantly higher ratio of lightly discomfortable feeling and lower ratios of tinnitus and eardrum discomfort induced by air pressure and noise in passengers at 200 km/h. No significant difference was observed in ear discomfort induced by air pressure and noise among crew, and the duration of disappearance of discomfortable feeling among passengers between 200 km/h and 250 km/h. The noise in carriages exceeded the related standard when the high-speed train passing through the tunnels. The individuals feel more comfortable at 200 km/h than 250 km/h in this line., which may be related with rapid variation of wind speed and noise when the train passes through the tunnels with high speed.

  20. Space Shuttle Pressure Data Model in the 10- by 10-Foot Supersonic Wind Tunnel

    NASA Image and Video Library

    1978-04-21

    Technicians examine a scale model of the space shuttle used to obtain pressure data during tests in the 10- by 10-Foot Supersonic Wind Tunnel at the National Aeronautics and Space Administration (NASA) Lewis Research Center. Lewis researchers used the 10- by 10 tunnel extensively in the 1970s to study shuttle configurations in order to forecast conditions during an actual flight. These tests included analysis of the solid rocket boosters’ aerodynamics, orbiter forebody angle -of -attack and air speed, base heating for entire shuttle, and engine-out loads. The test seen in this photograph used a 3.5- percent scale aluminum alloy model of the entire launch configuration. The program was designed to obtain aerodynamic pressure data. The tests were part of a larger program to study possible trouble areas for the shuttle’s new Advanced Flexible Reusable Surface Insulation. The researchers obtained aeroacoustic data and pressure distributions from five locations on the model. Over 100 high-temperature pressure transducers were attached to the model. Other portions of the test program were conducted at Lewis’ 8- by 6-Foot Supersonic Wind Tunnel and the 11- by 11-Foot Transonic Wind Tunnel at Ames Research Center.

  1. Importance of air-sea interaction on wind waves, storm surge and hurricane simulations

    NASA Astrophysics Data System (ADS)

    Chen, Yingjian; Yu, Xiping

    2017-04-01

    It was reported from field observations that wind stress coefficient levels off and even decreases when the wind speed exceeds 30-40 m/s. We propose a wave boundary layer model (WBLM) based on the momentum and energy conservation equations. Taking into account the physical details of the air-sea interaction process as well as the energy dissipation due to the presence of sea spray, this model successfully predicts the decreasing tendency of wind stress coefficient. Then WBLM is embedded in the current-wave coupled model FVCOM-SWAVE to simulate surface waves and storm surge under the forcing of hurricane Katrina. Numerical results based on WBLM agree well with the observed data of NDBC buoys and tide gauges. Sensitivity analysis of different wind stress evaluation methods also shows that large anomalies of significant wave height and surge elevation are captured along the passage of hurricane core. The differences of the local wave height are up to 13 m, which is in accordance with the general knowledge that the ocean dynamic processes under storm conditions are very sensitive to the amount of momentum exchange at the air-sea interface. In the final part of the research, the reduced wind stress coefficient is tested in the numerical forecast of hurricane Katrina. A parabolic formula fitted to WBLM is employed in the atmosphere-ocean coupled model COAWST. Considering the joint effects of ocean cooling and reduced wind drag, the intensity metrics - the minimum sea level pressure and the maximum 10 m wind speed - are in good inconsistency with the best track result. Those methods, which predict the wind stress coefficient that increase or saturate in extreme wind condition, underestimate the hurricane intensity. As a whole, we unify the evaluation methods of wind stress in different numerical models and yield reasonable results. Although it is too early to conclude that WBLM is totally applicable or the drag coefficient does decrease for high wind speed, our current

  2. Winds over Japan.

    NASA Astrophysics Data System (ADS)

    Plumley, William J.

    1994-01-01

    Before World War II, weather forecasters had little knowledge of upper-air wind patterns above 20000 feet. Data were seldom avai able at these heights, and the need was not great because commercial aircraft seldom flew at these altitudes. The war in the Pacific changed all that. Wind forecasts for 30000 feet plus became urgent to support the XXI Bomber Command in its bombing mission over Japan.The U.S. Army Air Force Pacific Ocean Area (AAFPOA) placed a Weather Central in the Marianas Islands in 1944 (Saipan in 1944 and Guam in 1945) to provide forecasting support for this mission. A forecasting procedure was put into operation that combined the elements known as "single-station forecasting" and an advanced procedure that used "altirmeter corrections" to analyze upper-airdata and make prognoses. Upper-air charts were drawn for constant pressure surfaces rather than constant height surfaces. The constant pressure surfaces were tied together by means of the atmospheric temperature field represented by specific temperature anomalies between pressure surfaces. Wind forecasts over the Marianas-Japan route made use of space cross sections that provided the data to forecast winds at each 5000-ft level to 35000 ft along the mission flight path. The new procedures allowed the forecaster to construct internally consistent meteorological charts in three dimensions in regions of sparse data.Army air force pilots and their crews from the Marianas were among the first to experience the extreme wind conditions now known as the "jet stream". Air force forecasters demonstrated that, with experience, such winds could reasonably be forecast under difficult operational conditions.

  3. Evaluation of wind-induced internal pressure in low-rise buildings: A multi scale experimental and numerical approach

    NASA Astrophysics Data System (ADS)

    Tecle, Amanuel Sebhatu

    Hurricane is one of the most destructive and costly natural hazard to the built environment and its impact on low-rise buildings, particularity, is beyond acceptable. The major objective of this research was to perform a parametric evaluation of internal pressure (IP) for wind-resistant design of low-rise buildings and wind-driven natural ventilation applications. For this purpose, a multi-scale experimental, i.e. full-scale at Wall of Wind (WoW) and small-scale at Boundary Layer Wind Tunnel (BLWT), and a Computational Fluid Dynamics (CFD) approach was adopted. This provided new capability to assess wind pressures realistically on internal volumes ranging from small spaces formed between roof tiles and its deck to attic to room partitions. Effects of sudden breaching, existing dominant openings on building envelopes as well as compartmentalization of building interior on the IP were systematically investigated. Results of this research indicated: (i) for sudden breaching of dominant openings, the transient overshooting response was lower than the subsequent steady state peak IP and internal volume correction for low-wind-speed testing facilities was necessary. For example a building without volume correction experienced a response four times faster and exhibited 30--40% lower mean and peak IP; (ii) for existing openings, vent openings uniformly distributed along the roof alleviated, whereas one sided openings aggravated the IP; (iii) larger dominant openings exhibited a higher IP on the building envelope, and an off-center opening on the wall exhibited (30--40%) higher IP than center located openings; (iv) compartmentalization amplified the intensity of IP and; (v) significant underneath pressure was measured for field tiles, warranting its consideration during net pressure evaluations. The study aimed at wind driven natural ventilation indicated: (i) the IP due to cross ventilation was 1.5 to 2.5 times higher for Ainlet/Aoutlet>1 compared to cases where Ainlet

  4. Physical understanding of the tropical cyclone wind-pressure relationship.

    PubMed

    Chavas, Daniel R; Reed, Kevin A; Knaff, John A

    2017-11-08

    The relationship between the two common measures of tropical cyclone intensity, the central pressure deficit and the peak near-surface wind speed, is a long-standing problem in tropical meteorology that has been approximated empirically yet lacks physical understanding. Here we provide theoretical grounding for this relationship. We first demonstrate that the central pressure deficit is highly predictable from the low-level wind field via gradient wind balance. We then show that this relationship reduces to a dependence on two velocity scales: the maximum azimuthal-mean azimuthal wind speed and half the product of the Coriolis parameter and outer storm size. This simple theory is found to hold across a hierarchy of models spanning reduced-complexity and Earth-like global simulations and observations. Thus, the central pressure deficit is an intensity measure that combines maximum wind speed, storm size, and background rotation rate. This work has significant implications for both fundamental understanding and risk analysis, including why the central pressure better explains historical economic damages than does maximum wind speed.

  5. Weather and climate needs for Lidar observations from space and concepts for their realization. [wind, temperature, moisture, and pressure data needs

    NASA Technical Reports Server (NTRS)

    Atlas, D.; Korb, C. L.

    1980-01-01

    The spectrum of weather and climate needs for Lidar observations from space is discussed with emphasis on the requirements for wind, temperature, moisture, and pressure data. It is shown that winds are required to realistically depict all atmospheric scales in the tropics and the smaller scales at higher latitudes, where both temperature and wind profiles are necessary. The need for means to estimate air-sea exchanges of sensible and latent heat also is noted. A concept for achieving this through a combination of Lidar cloud top heights and IR cloud top temperatures of cloud streets formed during cold air outbreaks over the warmer ocean is outlined. Recent theoretical feasibility studies concerning the profiling of temperatures, pressure, and humidity by differential absorption Lidar (DIAL) from space and expected accuracies are reviewed. An alternative approach to Doppler Lidar wind measurements also is presented. The concept involves the measurement of the displacement of the aerosol backscatter pattern, at constant heights, between two successive scans of the same area, one ahead of the spacecraft and the other behind it a few minutes later. Finally, an integrated space Lidar system capable of measuring temperature, pressure, humidity, and winds which combines the DIAL methods with the aerosol pattern displacement concept is described.

  6. Development and testing of a portable wind sensitive directional air sampler

    NASA Technical Reports Server (NTRS)

    Deyo, J.; Toma, J.; King, R. B.

    1975-01-01

    A portable wind sensitive directional air sampler was developed as part of an air pollution source identification system. The system is designed to identify sources of air pollution based on the directional collection of field air samples and their analysis for TSP and trace element characteristics. Sources can be identified by analyzing the data on the basis of pattern recognition concepts. The unit, designated Air Scout, receives wind direction signals from an associated wind vane. Air samples are collected on filter slides using a standard high volume air sampler drawing air through a porting arrangement which tracks the wind direction and permits collection of discrete samples. A preset timer controls the length of time each filter is in the sampling position. At the conclusion of the sampling period a new filter is automatically moved into sampling position displacing the previous filter to a storage compartment. Thus the Air Scout may be set up at a field location, loaded with up to 12 filter slides, and left to acquire air samples automatically, according to the wind, at any timer interval desired from 1 to 30 hours.

  7. On Blockage Corrections for Two-dimensional Wind Tunnel Tests Using the Wall-pressure Signature Method

    NASA Technical Reports Server (NTRS)

    Allmaras, S. R.

    1986-01-01

    The Wall-Pressure Signature Method for correcting low-speed wind tunnel data to free-air conditions has been revised and improved for two-dimensional tests of bluff bodies. The method uses experimentally measured tunnel wall pressures to approximately reconstruct the flow field about the body with potential sources and sinks. With the use of these sources and sinks, the measured drag and tunnel dynamic pressure are corrected for blockage effects. Good agreement is obtained with simpler methods for cases in which the blockage corrections were about 10% of the nominal drag values.

  8. Influence of Wind Pressure on the Carbonation of Concrete

    PubMed Central

    Zou, Dujian; Liu, Tiejun; Du, Chengcheng; Teng, Jun

    2015-01-01

    Carbonation is one of the major deteriorations that accelerate steel corrosion in reinforced concrete structures. Many mathematical/numerical models of the carbonation process, primarily diffusion-reaction models, have been established to predict the carbonation depth. However, the mass transfer of carbon dioxide in porous concrete includes molecular diffusion and convection mass transfer. In particular, the convection mass transfer induced by pressure difference is called penetration mass transfer. This paper presents the influence of penetration mass transfer on the carbonation. A penetration-reaction carbonation model was constructed and validated by accelerated test results under high pressure. Then the characteristics of wind pressure on the carbonation were investigated through finite element analysis considering steady and fluctuating wind flows. The results indicate that the wind pressure on the surface of concrete buildings results in deeper carbonation depth than that just considering the diffusion of carbon dioxide. In addition, the influence of wind pressure on carbonation tends to increase significantly with carbonation depth. PMID:28793462

  9. Influence of Wind Pressure on the Carbonation of Concrete.

    PubMed

    Zou, Dujian; Liu, Tiejun; Du, Chengcheng; Teng, Jun

    2015-07-24

    Carbonation is one of the major deteriorations that accelerate steel corrosion in reinforced concrete structures. Many mathematical/numerical models of the carbonation process, primarily diffusion-reaction models, have been established to predict the carbonation depth. However, the mass transfer of carbon dioxide in porous concrete includes molecular diffusion and convection mass transfer. In particular, the convection mass transfer induced by pressure difference is called penetration mass transfer. This paper presents the influence of penetration mass transfer on the carbonation. A penetration-reaction carbonation model was constructed and validated by accelerated test results under high pressure. Then the characteristics of wind pressure on the carbonation were investigated through finite element analysis considering steady and fluctuating wind flows. The results indicate that the wind pressure on the surface of concrete buildings results in deeper carbonation depth than that just considering the diffusion of carbon dioxide. In addition, the influence of wind pressure on carbonation tends to increase significantly with carbonation depth.

  10. Multivariate optimum interpolation of surface pressure and winds over oceans

    NASA Technical Reports Server (NTRS)

    Bloom, S. C.

    1984-01-01

    The observations of surface pressure are quite sparse over oceanic areas. An effort to improve the analysis of surface pressure over oceans through the development of a multivariate surface analysis scheme which makes use of surface pressure and wind data is discussed. Although the present research used ship winds, future versions of this analysis scheme could utilize winds from additional sources, such as satellite scatterometer data.

  11. 6. VIEW OF FIVEFOOT WIND TUNNEL WITH AIR STRAIGHTENER AND ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    6. VIEW OF FIVE-FOOT WIND TUNNEL WITH AIR STRAIGHTENER AND OPERATOR STATION IN FOREGROUND (1991). - Wright-Patterson Air Force Base, Area B, Building No. 19, Five-Foot Wind Tunnel, Dayton, Montgomery County, OH

  12. Wind tunnel pressurization and recovery system

    NASA Technical Reports Server (NTRS)

    Pejack, Edwin R.; Meick, Joseph; Ahmad, Adnan; Lateh, Nordin; Sadeq, Omar

    1988-01-01

    The high density, low toxicity characteristics of refrigerant-12 (dichlorofluoromethane) make it an ideal gas for wind tunnel testing. Present limitations on R-12 emissions, set to slow the rate of ozone deterioration, pose a difficult problem in recovery and handling of large quantities of R-12. This preliminary design is a possible solution to the problem of R-12 handling in wind tunnel testing. The design incorporates cold temperature condensation with secondary purification of the R-12/air mixture by adsorption. Also discussed is the use of Freon-22 as a suitable refrigerant for the 12 foot wind tunnel.

  13. Association between lower air pressure and the onset of ischemic colitis: a case-control study.

    PubMed

    Kimura, Takefumi; Shinji, Akihiro; Tanaka, Naoki; Koinuma, Masayoshi; Yamaura, Maki; Nagaya, Tadanobu; Joshita, Satoru; Komatsu, Michiharu; Umemura, Takeji; Horiuchi, Akira; Wada, Shuichi; Tanaka, Eiji

    2017-09-01

    Ischemic colitis (IC) often affects the elderly. Proarteriosclerotic factors, such as hypertension and smoking, and cardiovascular disease are considered major contributors to IC. Although a possible link between certain cerebrocardiovascular disorders and meteorological phenomena has been reported, the relationship between IC onset and weather changes remains uninvestigated. This study examined whether specific meteorological factors were associated with the occurrence of IC. We retrospectively enrolled 303 patients who had been diagnosed with IC between January 2003 and June 2010 at Suwa Red Cross Hospital in Nagano Prefecture, Japan. The meteorological data of the days on which IC patients visited the hospital (IC+ days) were compared with those of the days on which IC patients did not (IC- days). Univariate analysis indicated that IC+ days had significantly lower air pressure (P<0.001), depressed air pressure from the previous day (P<0.001), and fewer daylight hours (P<0.001), as well as higher air temperature (P=0.017), air humidity (P=0.004), wind velocity (P<0.001), and rainfall (P=0.012) compared with IC- days. Multivariate logistic regression analysis of the meteorological data showed that air pressure (odds ratio: 0.935, P<0.001) and change in air pressure from the previous day (odds ratio: 0.934, P<0.001) were related to onset of IC. Lower air pressure and decrease in air pressure from the previous day are possible novel factors associated with the development of IC.

  14. Surface wind, pressure and temperature fields near tornadic and non-tornadic narrow cold-frontal rainbands

    NASA Astrophysics Data System (ADS)

    Clark, Matthew; Parker, Douglas

    2014-05-01

    Narrow cold frontal rainbands (NCFRs) occur frequently in the UK and other parts of northwest Europe. At the surface, the passage of an NCFR is often marked by a sharp wind veer, abrupt pressure increase and a rapid temperature decrease. Tornadoes and other instances of localised wind damage sometimes occur in association with meso-gamma-scale vortices (sometimes called misocyclones) that form along the zone of abrupt horizontal wind veer (and associated vertical vorticity) at the leading edge of the NCFR. Using one-minute-resolution data from a mesoscale network of automatic weather stations, surface pressure, wind and temperature fields in the vicinity of 12 NCFRs (five of which were tornadic) have been investigated. High-resolution surface analyses were obtained by mapping temporal variations in the observed parameters to equivalent spatial variations, using a system velocity determined by analysis of the radar-observed movement of NCFR precipitation segments. Substantial differences were found in the structure of surface wind and pressure fields close to tornadic and non-tornadic NCFRs. Tornadic NCFRs exhibited a large wind veer (near 90°) and strong pre- and post-frontal winds. These attributes were associated with large vertical vorticity and horizontal convergence across the front. Tornadoes typically occurred where vertical vorticity and horizontal convergence were increasing. Here, we present surface analyses from selected cases, and draw comparisons between the tornadic and non-tornadic NCFRs. Some Doppler radar observations will be presented, illustrating the development of misocyclones along parts of the NCFR that exhibit strong, and increasing, vertical vorticity stretching. The influence of the stability of the pre-frontal air on the likelihood of tornadoes will also be discussed.

  15. Solar wind control of magnetospheric pressure (CDAW 6)

    NASA Technical Reports Server (NTRS)

    Fairfield, D. H.

    1985-01-01

    The CDAW 6 data base is used to compare solar wind and magnetospheric pressures. The flaring angle of the tail magnetopause is determined by assuming that the component of solar wind pressure normal to the tail boundary is equal to the total pressure within the tail. Results indicate an increase in the tail flaring angle from 18 deg to 32 deg prior to the 1055 substorm onset and a decrease to 25 deg after the onset. This behavior supports the concept of tail energy storage before the substorm and subsequent release after the onset.

  16. Calculations of air cooler for new subsonic wind tunnel

    NASA Astrophysics Data System (ADS)

    Rtishcheva, A. S.

    2017-10-01

    As part of the component development of TsAGI’s new subsonic wind tunnel where the air flow velocity in the closed test section is up to 160 m/sec hydraulic and thermal characteristics of air cooler are calculated. The air cooler is one of the most important components due to its highest hydraulic resistance in the whole wind tunnel design. It is important to minimize its hydraulic resistance to ensure the energy efficiency of wind tunnel fans and the cost-cutting of tests. On the other hand the air cooler is to assure the efficient cooling of air flow in such a manner as to maintain the temperature below 40 °C for seamless operation of measuring equipment. Therefore the relevance of this project is driven by the need to develop the air cooler that would demonstrate low hydraulic resistance of air and high thermal effectiveness of heat exchanging surfaces; insofar as the cooling section must be given up per unit time with the amount of heat Q=30 MW according to preliminary evaluations. On basis of calculation research some variants of air cooler designs are proposed including elliptical tubes, round tubes, and lateral plate-like fins. These designs differ by the number of tubes and plates, geometrical characteristics and the material of finned surfaces (aluminium or cooper). Due to the choice of component configurations a high thermal effectiveness is achieved for finned surfaces. The obtained results form the basis of R&D support in designing the new subsonic wind tunnel.

  17. Tornado type wind turbines

    DOEpatents

    Hsu, Cheng-Ting

    1984-01-01

    A tornado type wind turbine has a vertically disposed wind collecting tower with spaced apart inner and outer walls and a central bore. The upper end of the tower is open while the lower end of the structure is in communication with a wind intake chamber. An opening in the wind chamber is positioned over a turbine which is in driving communication with an electrical generator. An opening between the inner and outer walls at the lower end of the tower permits radially flowing air to enter the space between the inner and outer walls while a vertically disposed opening in the wind collecting tower permits tangentially flowing air to enter the central bore. A porous portion of the inner wall permits the radially flowing air to interact with the tangentially flowing air so as to create an intensified vortex flow which exits out of the top opening of the tower so as to create a low pressure core and thus draw air through the opening of the wind intake chamber so as to drive the turbine.

  18. Middle Ear Pressures in Wind Instrument Musicians.

    PubMed

    Osborne, Max Sallis; Morris, Simon; Clark, Matthew P; Begg, Philip

    2018-05-22

    This study aimed to assess if playing wind instruments leads to a measurable increase in middle ear pressure during note generation and to provide evidence to clinicians to advise musicians undergoing middle ear surgery. An observational cohort study of 40 volunteers in 7 different wind instrument categories underwent tympanometry at rest and during note production. Community. Recreational musicians aged over 18 years recruited from the student body attending Birmingham University, UK. None. Tympanometry is used as a noninvasive measure of middle ear pressure. The pressure at which peak compliance occurred was taken as an indirect measure of middle ear pressure. The data produced at rest and during note production was statistically analysed with paired t testing and significance set at a p value less than 0.01. Overall a statistically significant increase in middle ear pressure change of 0.63 mm Hg (p = 0.0001) during note production was identified. Musicians playing the oboe and trumpet demonstrate the largest increase in middle ear pressure of 1.46 mm Hg (p = 0.0053) and 0.78 mm Hg (p = 0.0005) respectively. The data provided by this study gives evidence for the first time that playing wind instruments does increase middle ear pressure. Although the clinical significance of this is yet to be determined the authors would advise that musicians who undergo otological procedures should refrain from playing their instruments until full recovery has been achieved as advised by their clinician following direct microscopic review.

  19. A Full-Envelope Air Data Calibration and Three-Dimensional Wind Estimation Method Using Global Output-Error Optimization and Flight-Test Techniques

    NASA Technical Reports Server (NTRS)

    Taylor, Brian R.

    2012-01-01

    A novel, efficient air data calibration method is proposed for aircraft with limited envelopes. This method uses output-error optimization on three-dimensional inertial velocities to estimate calibration and wind parameters. Calibration parameters are based on assumed calibration models for static pressure, angle of attack, and flank angle. Estimated wind parameters are the north, east, and down components. The only assumptions needed for this method are that the inertial velocities and Euler angles are accurate, the calibration models are correct, and that the steady-state component of wind is constant throughout the maneuver. A two-minute maneuver was designed to excite the aircraft over the range of air data calibration parameters and de-correlate the angle-of-attack bias from the vertical component of wind. Simulation of the X-48B (The Boeing Company, Chicago, Illinois) aircraft was used to validate the method, ultimately using data derived from wind-tunnel testing to simulate the un-calibrated air data measurements. Results from the simulation were accurate and robust to turbulence levels comparable to those observed in flight. Future experiments are planned to evaluate the proposed air data calibration in a flight environment.

  20. Hurricane Isabel, AIRS Infrared and SeaWinds Scatterometer Data Combined

    NASA Image and Video Library

    2003-09-20

    These two images show Hurricane Isabel as viewed by AIRS and SeaWinds scatterometers on NASA ADEOS-2 and QuikScat satellites in September, 2003. AIRS data are used to create global three-dimensional maps of temperature, humidity and clouds, while scatterometers measure surface wind speed and direction. http://photojournal.jpl.nasa.gov/catalog/PIA00429

  1. Impacts of wind farms on surface air temperatures

    PubMed Central

    Baidya Roy, Somnath; Traiteur, Justin J.

    2010-01-01

    Utility-scale large wind farms are rapidly growing in size and numbers all over the world. Data from a meteorological field campaign show that such wind farms can significantly affect near-surface air temperatures. These effects result from enhanced vertical mixing due to turbulence generated by wind turbine rotors. The impacts of wind farms on local weather can be minimized by changing rotor design or by siting wind farms in regions with high natural turbulence. Using a 25-y-long climate dataset, we identified such regions in the world. Many of these regions, such as the Midwest and Great Plains in the United States, are also rich in wind resources, making them ideal candidates for low-impact wind farms. PMID:20921371

  2. Investigation of air flow in open-throat wind tunnels

    NASA Technical Reports Server (NTRS)

    Jacobs, Eastman N

    1930-01-01

    Tests were conducted on the 6-inch wind tunnel of the National Advisory Committee for Aeronautics to form a part of a research on open-throat wind tunnels. The primary object of this part of the research was to study a type of air pulsation which has been encountered in open-throat tunnels, and to find the most satisfactory means of eliminating such pulsations. In order to do this it was necessary to study the effects of different variable on all of the important characteristics of the tunnel. This paper gives not only the results of the study of air pulsations and methods of eliminating them, but also the effects of changing the exit-cone diameter and flare and the effects of air leakage from the return passage. It was found that the air pulsations in the 6-inch wind tunnel could be practically eliminated by using a moderately large flare on the exit cone in conjunction with leakage introduced by cutting holes in the exit cone somewhat aft of its minimum diameter.

  3. Determination of tropical cyclone surface pressure and winds from satellite microwave data

    NASA Technical Reports Server (NTRS)

    Kidder, S. Q.

    1979-01-01

    An approach to the problem of deducing wind speed and pressure around tropical cyclones is presented. The technique, called the Surface Wind Inference from Microwave data (SWIM technique, uses satellites microwave sounder data to measure upper tropospheric temperature anomalies which may then be related to surface pressure anomalies through the hydrostatic and radiative transfer equations. Surface pressure gradients outside of the radius of maximum wind are estimated for the first time. Future instruments may be able to estimate central pressure with + or - 0/1 kPa accuracy.

  4. Galactic Disk Winds Driven by Cosmic Ray Pressure

    NASA Astrophysics Data System (ADS)

    Mao, S. Alwin; Ostriker, Eve C.

    2018-02-01

    Cosmic ray pressure gradients transfer energy and momentum to extraplanar gas in disk galaxies, potentially driving significant mass loss as galactic winds. This may be particularly important for launching high-velocity outflows of “cool” (T ≲ 104 K) gas. We study cosmic ray-driven disk winds using a simplified semi-analytic model assuming streamlines follow the large-scale gravitational potential gradient. We consider scaled Milky Way–like potentials including a disk, bulge, and halo with a range of halo velocities V H = 50–300 km s-1 and streamline footpoints with radii in the disk R 0 = 1–16 kpc at a height of 1 kpc. Our solutions cover a wide range of footpoint gas velocity u 0, magnetic–to–cosmic ray pressure ratio, gas–to–cosmic ray pressure ratio, and angular momentum. Cosmic ray streaming at the Alfvén speed enables the effective sound speed C eff to increase from the footpoint to a critical point where C eff,c = u c ∼ V H; this differs from thermal winds, in which C eff decreases outward. The critical point is typically at a height of 1–6 kpc from the disk, increasing with V H, and the asymptotic wind velocity exceeds the escape speed of the halo. Mass-loss rates are insensitive to the footpoint values of the magnetic field and angular momentum. In addition to numerical parameter space exploration, we develop and compare to analytic scaling relations. We show that winds have mass-loss rates per unit area up to \\dot{Σ}∼ Π0VH-5/3u02/3, where Π0 is the footpoint cosmic ray pressure and u 0 is set by the upwelling of galactic fountains. The predicted wind mass-loss rate exceeds the star formation rate for V H ≲ 200 km s-1 and u 0 = 50 km s-1, a typical fountain velocity.

  5. Laser plasma at low air pressure

    NASA Astrophysics Data System (ADS)

    Vas'kovskii, Iu. M.; Moiseev, V. N.; Rovinskii, R. E.; Tsenina, I. S.

    1993-01-01

    The ambient-pressure dependences of the dynamic and optical characteristics of a laser plasma generated by CO2-laser irradiation of an obstacle are investigated experimentally. The change of the sample's surface roughness after irradiation is investigated as a function of air pressure. It is concluded that the transition from the air plasma to the erosion plasma takes place at an air pressure of about 1 mm Hg. The results confirm the existing theory of plasma formation near the surface of an obstacle under the CO2-laser pulse effect in air.

  6. Simulation of air-droplet mixed phase flow in icing wind-tunnel

    NASA Astrophysics Data System (ADS)

    Mengyao, Leng; Shinan, Chang; Menglong, Wu; Yunhang, Li

    2013-07-01

    Icing wind-tunnel is the main ground facility for the research of aircraft icing, which is different from normal wind-tunnel for its refrigeration system and spraying system. In stable section of icing wind-tunnel, the original parameters of droplets and air are different, for example, to keep the nozzles from freezing, the droplets are heated while the temperature of air is low. It means that complex mass and heat transfer as well as dynamic interactive force would happen between droplets and air, and the parameters of droplet will acutely change along the passageway. Therefore, the prediction of droplet-air mixed phase flow is necessary in the evaluation of icing researching wind-tunnel. In this paper, a simplified droplet-air mixed phase flow model based on Lagrangian method was built. The variation of temperature, diameter and velocity of droplet, as well as the air flow field, during the flow process were obtained under different condition. With calculating three-dimensional air flow field by FLUENT, the droplet could be traced and the droplet distribution could also be achieved. Furthermore, the patterns about how initial parameters affect the parameters in test section were achieved. The numerical simulation solving the flow and heat and mass transfer characteristics in the mixing process is valuable for the optimization of experimental parameters design and equipment adjustment.

  7. Numerical investigation of air flow in a supersonic wind tunnel

    NASA Astrophysics Data System (ADS)

    Drozdov, S. M.; Rtishcheva, A. S.

    2017-11-01

    In the framework of TsAGI’s supersonic wind tunnel modernization program aimed at improving flow quality and extending the range of test regimes it was required to design and numerically validate a new test section and a set of shaped nozzles: two flat nozzles with flow Mach number at nozzle exit M=4 and M=5 and two axisymmetric nozzles with M=5 and M=6. Geometric configuration of the nozzles, the test section (an Eiffel chamber) and the diffuser was chosen according to the results of preliminary calculations of two-dimensional air flow in the wind tunnel circuit. The most important part of the work are three-dimensional flow simulation results obtained using ANSYS Fluent software. The following flow properties were investigated: Mach number, total and static pressure, total and static temperature and turbulent viscosity ratio distribution, heat flux density at wind tunnel walls (for high-temperature flow regimes). It is demonstrated that flow perturbations emerging from the junction of the nozzle with the test section and spreading down the test section behind the boundaries of characteristic rhomb’s reverse wedge are nearly impossible to eliminate. Therefore, in order to perform tests under most uniform flow conditions, the model’s center of rotation and optical window axis should be placed as close to the center of the characteristic rhomb as possible. The obtained results became part of scientific and technical basis of supersonic wind tunnel design process and were applied to a generalized class of similar wind tunnels.

  8. An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-Foot Wind Tunnel: Pressure-Distribution Tests

    NASA Technical Reports Server (NTRS)

    Hunton, Lynn W.; James, Harry A.

    1948-01-01

    Pressure measurements were made during wind-tunnel tests of the McDonnell XP-85 parasite fighter. Static-pressure orifices were located over the fuselage nose, over the canopy, along the wing root, and along the upper and lower stabilizer roots. A total-pressure and static-pressure rake was located in the turbojet engine air-intake duct. It was installed at the station where the compressor face would be located. Pressure data were obtained for two airplane conditions, clean and with skyhook extended, through a range of angle of attack and a range of yaw.

  9. The Use of Red Green Blue (RGB) Air Mass Imagery to Investigate the Role of Stratospheric Air in a Non-Convective Wind Event

    NASA Technical Reports Server (NTRS)

    Berndt, Emily; Zavodsky, Bradley; Molthan, Andrew; Jedlovec, Gary

    2013-01-01

    AIRS ozone and model PV analysis confirm the stratospheric air in RGB Air Mass imagery. Trajectories confirm winds south of the low were distinct from CCB driven winds. Cross sections connect the tropopause fold, downward motion, and high nearsurface winds. Comparison to conceptual models show Shapiro-Keyser features and sting jet characteristics were observed in a storm that impacted the U.S. East Coast. RGB Air Mass imagery can be used to identify stratospheric air and regions susceptible to tropopause folding and attendant non-convective winds.

  10. Three-dimensional vapor intrusion modeling approach that combines wind and stack effects on indoor, atmospheric, and subsurface domains.

    PubMed

    Shirazi, Elham; Pennell, Kelly G

    2017-12-13

    Vapor intrusion (IV) exposure risks are difficult to characterize due to the role of atmospheric, building and subsurface processes. This study presents a three-dimensional VI model that extends the common subsurface fate and transport equations to incorporate wind and stack effects on indoor air pressure, building air exchange rate (AER) and indoor contaminant concentration to improve VI exposure risk estimates. The model incorporates three modeling programs: (1) COMSOL Multiphysics to model subsurface fate and transport processes, (2) CFD0 to model atmospheric air flow around the building, and (3) CONTAM to model indoor air quality. The combined VI model predicts AER values, zonal indoor air pressures and zonal indoor air contaminant concentrations as a function of wind speed, wind direction and outdoor and indoor temperature. Steady state modeling results for a single-story building with a basement demonstrate that wind speed, wind direction and opening locations in a building play important roles in changing the AER, indoor air pressure, and indoor air contaminant concentration. Calculated indoor air pressures ranged from approximately -10 Pa to +4 Pa depending on weather conditions and building characteristics. AER values, mass entry rates and indoor air concentrations vary depending on weather conditions and building characteristics. The presented modeling approach can be used to investigate the relationship between building features, AER, building pressures, soil gas concentrations, indoor air concentrations and VI exposure risks.

  11. The impact of changing wind speeds on gas transfer and its effect on global air-sea CO2 fluxes

    NASA Astrophysics Data System (ADS)

    Wanninkhof, R.; Triñanes, J.

    2017-06-01

    An increase in global wind speeds over time is affecting the global uptake of CO2 by the ocean. We determine the impact of changing winds on gas transfer and CO2 uptake by using the recently updated, global high-resolution, cross-calibrated multiplatform wind product (CCMP-V2) and a fixed monthly pCO2 climatology. In particular, we assess global changes in the context of regional wind speed changes that are attributed to large-scale climate reorganizations. The impact of wind on global CO2 gas fluxes as determined by the bulk formula is dependent on several factors, including the functionality of the gas exchange-wind speed relationship and the regional and seasonal differences in the air-water partial pressure of CO2 gradient (ΔpCO2). The latter also controls the direction of the flux. Fluxes out of the ocean are influenced more by changes in the low-to-intermediate wind speed range, while ingassing is impacted more by changes in higher winds because of the regional correlations between wind and ΔpCO2. Gas exchange-wind speed parameterizations with a quadratic and third-order polynomial dependency on wind, each of which meets global constraints, are compared. The changes in air-sea CO2 fluxes resulting from wind speed trends are greatest in the equatorial Pacific and cause a 0.03-0.04 Pg C decade-1 increase in outgassing over the 27 year time span. This leads to a small overall decrease of 0.00 to 0.02 Pg C decade-1 in global net CO2 uptake, contrary to expectations that increasing winds increase net CO2 uptake.Plain Language SummaryThe effects of changing <span class="hlt">winds</span> are isolated from the total change in trends in global <span class="hlt">air</span>-sea CO2 fluxes over the last 27 years. The overall effect of increasing <span class="hlt">winds</span> over time has a smaller impact than expected as the impact in regions of outgassing is greater than for the regions acting as a CO2 sink.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/53692','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/53692"><span><span class="hlt">Wind</span> <span class="hlt">pressure</span> testing of tornado safe room components made from wood</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Robert Falk; Deepak Shrestha</p> <p>2016-01-01</p> <p>To evaluate the ability of a wood tornado safe room to resist <span class="hlt">wind</span> <span class="hlt">pressures</span> produced by a tornado, two safe room com-ponents were tested for <span class="hlt">wind</span> <span class="hlt">pressure</span> strength. A tornado safe room ceiling panel and door were static-<span class="hlt">pressure</span>-tested according to ASTM E 330 using a vacuum test system. Re-sults indicate that the panels had load capacities from 2.4 to 3.5 times that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSM11B2312S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSM11B2312S"><span>Vortex, ULF wave and Aurora Observation after Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Change</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shi, Q.</p> <p>2017-12-01</p> <p>Here we will summarize our recent study and show some new results on the Magnetosphere and Ionosphere Response to Dynamic <span class="hlt">Pressure</span> Change/disturbances in the Solar <span class="hlt">Wind</span> and foreshock regions. We study the step function type solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> change (increase/decrease) interaction with the magnetosphere using THEMIS satellites at both dayside and nightside in different geocentric distances. Vortices generated by the dynamic <span class="hlt">pressure</span> change passing along the magnetopause are found and compared with model predictions. ULF waves and vortices are excited in the dayside and nightside plasma sheet when dynamic <span class="hlt">pressure</span> change hit the magnetotail. The related ionospheric responses, such as aurora and TCVs, are also investigated. We compare Global MHD simulations with the observations. We will also show some new results that dayside magnetospheric FLRs might be caused by foreshock structures.Shi, Q. Q. et al. (2013), THEMIS observations of ULF wave excitation in the nightside plasma sheet during sudden impulse events, J. Geophys. Res. Space Physics, 118, doi:10.1029/2012JA017984. Shi, Q. Q. et al. (2014), Solar <span class="hlt">wind</span> <span class="hlt">pressure</span> pulse-driven magnetospheric vortices and their global consequences, J. Geophys. Res. Space Physics, 119, doi:10.1002/2013JA019551. Tian, A.M. et al.(2016), Dayside magnetospheric and ionospheric responses to solar <span class="hlt">wind</span> <span class="hlt">pressure</span> increase: Multispacecraft and ground observations, J. Geophys. Res., 121, doi:10.1002/2016JA022459. Shen, X.C. et al.(2015), Magnetospheric ULF waves with increasing amplitude related to solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> changes: THEMIS observations, J. Geophys. Res., 120, doi:10.1002/2014JA020913Zhao, H. Y. et al. (2016), Magnetospheric vortices and their global effect after a solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> decrease, J. Geophys. Res. Space Physics, 121, doi:10.1002/2015JA021646. Shen, X. C., et al. (2017), Dayside magnetospheric ULF wave frequency modulated by a solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> negative impulse, J. Geophys. Res</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20070019877','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20070019877"><span>Brain <span class="hlt">Pressure</span> Monitoring</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>1977-01-01</p> <p>A transducer originally used to measure <span class="hlt">air</span> <span class="hlt">pressure</span> in aircraft <span class="hlt">wind</span> tunnel tests is the basis for a development important in diagnosis and treatment of certain types of brain damage. A totally implantable device, tbe intracranial <span class="hlt">pressure</span> monitor measures and reports brain <span class="hlt">pressure</span> by telemetry.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JGRA..122.6635D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JGRA..122.6635D"><span>Trajectories of thermospheric <span class="hlt">air</span> parcels flowing over Alaska, reconstructed from ground-based <span class="hlt">wind</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>Dhadly, Manbharat; Conde, Mark</p> <p>2017-06-01</p> <p>It is widely presumed that the convective stability and enormous kinematic viscosity of Earth's upper thermosphere hinders development of both horizontal and vertical <span class="hlt">wind</span> shears and other gradients. Any strong local structure (over scale sizes of several hundreds of kilometers) that might somehow form would be expected to dissipate rapidly. <span class="hlt">Air</span> flow in such an atmosphere should be relatively simple, and transport effects only slowly disperse and mix <span class="hlt">air</span> masses. However, our observations show that <span class="hlt">wind</span> fields in Earth's thermosphere have much more local-scale structure than usually predicated by current modeling techniques, at least at auroral latitudes; they complicate <span class="hlt">air</span> parcel trajectories enormously, relative to typical expectations. For tracing <span class="hlt">air</span> parcels, we used <span class="hlt">wind</span> measurements of an all-sky Scanning Doppler Fabry-Perot interferometer and reconstructed time-resolved two-dimensional maps of the horizontal vector <span class="hlt">wind</span> field to infer forward and backward <span class="hlt">air</span> parcel trajectories over time. This is the first comprehensive study to visualize the complex motions of thermospheric <span class="hlt">air</span> parcels carried through the actual observed local-scale structures in the high-latitude <span class="hlt">winds</span>. Results show that thermospheric <span class="hlt">air</span> parcel transport is a very difficult observational problem, because the trajectories followed are very sensitive to the detailed features of the driving <span class="hlt">wind</span> field. To reconstruct the actual motion of a given <span class="hlt">air</span> parcel requires <span class="hlt">wind</span> measurements everywhere along the trajectory followed, with spatial resolutions of 100 km or less, and temporal resolutions of a few minutes or better. Understanding such transport is important, for example, in predicting the global-scale impacts of aurorally generated composition perturbations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=4&id=EJ522892','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=4&id=EJ522892"><span>Intraoral <span class="hlt">Air</span> <span class="hlt">Pressure</span> of Alaryngeal Speakers during a No-<span class="hlt">Air</span> Insufflation Maneuver.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Gorham, Mary M.; And Others</p> <p>1996-01-01</p> <p>Intraoral <span class="hlt">air</span> <span class="hlt">pressure</span> was recorded during the production of consonant cognate pairs by 8 esophageal speakers (mean age 67 years) under 2 experimental conditions: after the insufflation of <span class="hlt">air</span> and without <span class="hlt">air</span> insufflation. Results revealed that peak intraoral <span class="hlt">air</span> <span class="hlt">pressure</span> magnitudes were significantly greater following the insufflation of <span class="hlt">air</span> than…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16563580','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16563580"><span>Polyurethane foam (PUF) disks passive <span class="hlt">air</span> samplers: <span class="hlt">wind</span> effect on sampling rates.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tuduri, Ludovic; Harner, Tom; Hung, Hayley</p> <p>2006-11-01</p> <p>Different passive sampler housings were evaluated for their <span class="hlt">wind</span> dampening ability and how this might translate to variability in sampler uptake rates. Polyurethane foam (PUF) disk samplers were used as the sampling medium and were exposed to a PCB-contaminated atmosphere in a <span class="hlt">wind</span> tunnel. The effect of outside <span class="hlt">wind</span> speed on PUF disk sampling rates was evaluated by exposing polyurethane foam (PUF) disks to a PCB-contaminated <span class="hlt">air</span> stream in a <span class="hlt">wind</span> tunnel over <span class="hlt">air</span> velocities in the range 0 to 1.75 m s-1. PUF disk sampling rates increased gradually over the range 0-0.9 m s-1 at approximately 4.5-14.6 m3 d-1 and then increased sharply to approximately 42 m3 d-1 at approximately 1.75 m s-1 (sum of PCBs). The results indicate that for most field deployments the conventional 'flying saucer' housing adequately dampens the <span class="hlt">wind</span> effect and will yield approximately time-weighted <span class="hlt">air</span> concentrations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352660p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352660p/"><span>10. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). WrightPatterson <span class="hlt">Air</span> ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>10. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). - Wright-Patterson <span class="hlt">Air</span> Force Base, Area B, Buildings 25 & 24,10-foot & 20-foot <span class="hlt">Wind</span> Tunnel Complex, Northeast side of block bounded by K, G, Third, & Fifth Streets, Dayton, Montgomery County, OH</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352659p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352659p/"><span>9. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). WrightPatterson <span class="hlt">Air</span> ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>9. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). - Wright-Patterson <span class="hlt">Air</span> Force Base, Area B, Buildings 25 & 24,10-foot & 20-foot <span class="hlt">Wind</span> Tunnel Complex, Northeast side of block bounded by K, G, Third, & Fifth Streets, Dayton, Montgomery County, OH</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352661p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/oh1691.photos.352661p/"><span>11. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). WrightPatterson <span class="hlt">Air</span> ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>11. INTERIOR VIEW OF <span class="hlt">WIND</span> TUNNEL (1991). - Wright-Patterson <span class="hlt">Air</span> Force Base, Area B, Buildings 25 & 24,10-foot & 20-foot <span class="hlt">Wind</span> Tunnel Complex, Northeast side of block bounded by K, G, Third, & Fifth Streets, Dayton, Montgomery County, OH</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_1");'>1</a></li> <li><a href="#" onclick='return showDiv("page_2");'>2</a></li> <li class="active"><span>3</span></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_3 --> <div id="page_4" 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_2");'>2</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li class="active"><span>4</span></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</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="61"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMOS31A1997S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMOS31A1997S"><span>Comparison of Sea-<span class="hlt">Air</span> CO2 Flux Estimates Using Satellite-Based Versus Mooring <span class="hlt">Wind</span> Speed Data</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sutton, A. J.; Sabine, C. L.; Feely, R. A.; Wanninkhof, R. H.</p> <p>2016-12-01</p> <p>The global ocean is a major sink of anthropogenic CO2, absorbing approximately 27% of CO2 emissions since the beginning of the industrial revolution. Any variation or change in the ocean CO2 sink has implications for future climate. Observations of sea-<span class="hlt">air</span> CO2 flux have relied primarily on ship-based underway measurements of partial <span class="hlt">pressure</span> of CO2 (pCO2) combined with satellite, model, or multi-platform <span class="hlt">wind</span> products. Direct measurements of ΔpCO2 (seawater - <span class="hlt">air</span> pCO2) and <span class="hlt">wind</span> speed from moored platforms now allow for high-resolution CO2 flux time series. Here we present a comparison of CO2 flux calculated from moored ΔpCO2 measured on four moorings in different biomes of the Pacific Ocean in combination with: 1) Cross-Calibrated Multi-Platform (CCMP) <span class="hlt">winds</span> or 2) <span class="hlt">wind</span> speed measurements made on ocean reference moorings excluded from the CCMP dataset. Preliminary results show using CCMP <span class="hlt">winds</span> overestimates CO2 flux on average by 5% at the Kuroshio Extension Observatory, Ocean Station Papa, WHOI Hawaii Ocean Timeseries Station, and Stratus. In general, CO2 flux seasonality follows patterns of seawater pCO2 and SST with periods of CO2 outgassing during summer and CO2 uptake during winter at these locations. Any offsets or seasonal biases in CCMP <span class="hlt">winds</span> could impact global ocean sink estimates using this data product. Here we present patterns and trends between the two CO2 flux estimates and discuss the potential implications for tracking variability and change in global ocean CO2 uptake.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/791325','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/791325"><span>Ultra-High <span class="hlt">Pressure</span> Driver and Nozzle Survivability in the RDHWT/MARIAH II Hypersonic <span class="hlt">Wind</span> Tunnel</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>Costantino, M.; Brown, G.; Raman, K.</p> <p>2000-06-02</p> <p>An ultra-high <span class="hlt">pressure</span> device provides a high enthalpy (> 2500 kJ/kg), low entropy (< 5 kJ/kg-K) <span class="hlt">air</span> source for the RDHWT/MARIAH II Program Medium Scale Hypersonic <span class="hlt">Wind</span> Tunnel. The design uses stagnation conditions of 2300 MPa (330,000 Psi) and 750 K (900 F) in a radial configuration of intensifiers around an axial manifold to deliver pure <span class="hlt">air</span> at 100 kg/s mass flow rates for run times suitable for aerodynamic, combustion, and test and evaluation applications. Helium injection upstream of the nozzle throat reduces the throat wall recovery temperature to about 1200 K and reduces the oxygen concentration at the nozzlemore » wall.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA434397','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA434397"><span>An Evaluation of <span class="hlt">Wind</span> Turbine Technology at Peterson <span class="hlt">Air</span> Force Base</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2005-03-01</p> <p>by the <span class="hlt">wind</span> speed. Darrieus turbines are ordinarily inexpensive and are used for electricity generation and irrigation. One advantage to a...AN EVALUATION OF <span class="hlt">WIND</span> TURBINE TECHNOLOGY...02 AN EVALUATION OF <span class="hlt">WIND</span> TURBINE TECHNOLOGY AT PETERSON <span class="hlt">AIR</span> FORCE BASE THESIS Presented to the Faculty Department of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800023881','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800023881"><span>Use of nose cap and fuselage <span class="hlt">pressure</span> orifices for determination of <span class="hlt">air</span> data for space shuttle orbiter below supersonic speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Larson, T. J.; Siemers, P. M., III</p> <p>1980-01-01</p> <p><span class="hlt">Wind</span> tunnel <span class="hlt">pressure</span> measurements were acquired from orifices on a 0.1 scale forebody model of the space shuttle orbiter that were arranged in a preliminary configuration of the shuttle entry <span class="hlt">air</span> data system (SEADS). <span class="hlt">Pressures</span> from those and auxiliary orifices were evaluated for their ability to provide <span class="hlt">air</span> data at subsonic and transonic speeds. The orifices were on the vehicle's nose cap and on the sides of the forebody forward of the cabin. The investigation covered a Mach number range of 0.25 to 1.40 and an angle of attack range from 4 deg. to 18 deg. An <span class="hlt">air</span> data system consisting of nose cap and forebody fuselage orifices constitutes a complete and accurate <span class="hlt">air</span> data system at subsonic and transonic speeds. For Mach numbers less than 0.80 orifices confined to the nose cap can be used as a complete and accurate <span class="hlt">air</span> data system. <span class="hlt">Air</span> data systems that use only flush <span class="hlt">pressure</span> orifices can be used to determine basic <span class="hlt">air</span> data on other aircraft at subsonic and transonic speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040033375','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040033375"><span>Persistence Characteristics of <span class="hlt">Wind</span>-Tunnel <span class="hlt">Pressure</span> Signatures From Two Similar Models</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mack, Robert J.</p> <p>2004-01-01</p> <p><span class="hlt">Pressure</span> signatures generated by two sonic-boom <span class="hlt">wind</span>-tunnel models and measured at Mach 2 are presented, analyzed, and discussed. The two <span class="hlt">wind</span>-tunnel models differed in length and span by a factor of fourteen, but were similar in wing-body planform shape. The geometry of the larger model had been low-boom tailored to generate a flat top ground <span class="hlt">pressure</span> signature, and the nacelles-off <span class="hlt">pressure</span> signatures from this model became more flattop in shape as the model-probe separation distances increased from 0.94 to 4.4 span lengths. The geometry of the smaller model had not been low-boom tailored, yet its measured <span class="hlt">pressure</span> signatures had non-N-wave shapes that persisted as model-probe separation distances increased from 26.0 to 104.2 span lengths. Since the overall planforms of the two <span class="hlt">wind</span>-tunnel models were so similar, it was concluded that the shape-persistence trends in the <span class="hlt">pressure</span> signatures of the smaller, non-low-boom tailored model would also be present at very large distances in the <span class="hlt">pressure</span> signatures of the larger, low-boom-tailored model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA116347','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA116347"><span>United States <span class="hlt">Air</span> Force Academy (USAFA) Vertical Axis <span class="hlt">Wind</span> Turbine.</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1980-09-01</p> <p>Rotors, SAND76-0131. Albuquerque: July 1977. 10. Oliver, R.C. and P.R. Nixon. "Design Procedure for Coupling Savonius and Darrieus <span class="hlt">Wind</span> Turbines ", <span class="hlt">Air</span>...May 17-20, 1976. -65- 16. Blackwell, B.F., R.E. Sheldahl, and L.V. Feltz. <span class="hlt">Wind</span> Tunnel Performance Data for the Darrieus <span class="hlt">Wind</span> Turbine with NACA 0012...a 5.8 m/s (13 mph) <span class="hlt">wind</span> . At 100 rpm, the Darrieus turbine would be fully self-sustaining and acceleration would continue to an operating tip speed</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013AGUFMSH43A..03W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013AGUFMSH43A..03W"><span>Turbulent Heating and Wave <span class="hlt">Pressure</span> in Solar <span class="hlt">Wind</span> Acceleration Modeling: New Insights to Empirical Forecasting of the Solar <span class="hlt">Wind</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Woolsey, L. N.; Cranmer, S. R.</p> <p>2013-12-01</p> <p>The study of solar <span class="hlt">wind</span> acceleration has made several important advances recently due to improvements in modeling techniques. Existing code and simulations test the competing theories for coronal heating, which include reconnection/loop-opening (RLO) models and wave/turbulence-driven (WTD) models. In order to compare and contrast the validity of these theories, we need flexible tools that predict the emergent solar <span class="hlt">wind</span> properties from a wide range of coronal magnetic field structures such as coronal holes, pseudostreamers, and helmet streamers. ZEPHYR (Cranmer et al. 2007) is a one-dimensional magnetohydrodynamics code that includes Alfven wave generation and reflection and the resulting turbulent heating to accelerate solar <span class="hlt">wind</span> in open flux tubes. We present the ZEPHYR output for a wide range of magnetic field geometries to show the effect of the magnetic field profiles on <span class="hlt">wind</span> properties. We also investigate the competing acceleration mechanisms found in ZEPHYR to determine the relative importance of increased gas <span class="hlt">pressure</span> from turbulent heating and the separate <span class="hlt">pressure</span> source from the Alfven waves. To do so, we developed a code that will become publicly available for solar <span class="hlt">wind</span> prediction. This code, TEMPEST, provides an outflow solution based on only one input: the magnetic field strength as a function of height above the photosphere. It uses correlations found in ZEPHYR between the magnetic field strength at the source surface and the temperature profile of the outflow solution to compute the <span class="hlt">wind</span> speed profile based on the increased gas <span class="hlt">pressure</span> from turbulent heating. With this initial solution, TEMPEST then adds in the Alfven wave <span class="hlt">pressure</span> term to the modified Parker equation and iterates to find a stable solution for the <span class="hlt">wind</span> speed. This code, therefore, can make predictions of the <span class="hlt">wind</span> speeds that will be observed at 1 AU based on extrapolations from magnetogram data, providing a useful tool for empirical forecasting of the sol! ar <span class="hlt">wind</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19870057832&hterms=Pressure+switch&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DPressure%2Bswitch','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870057832&hterms=Pressure+switch&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DPressure%2Bswitch"><span>An electronic scanner of <span class="hlt">pressure</span> for <span class="hlt">wind</span> tunnel models</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kauffman, Ronald C.; Coe, Charles F.</p> <p>1986-01-01</p> <p>An electronic scanner of <span class="hlt">pressure</span> (ESOP) has been developed by NASA Ames Research Center for installation in <span class="hlt">wind</span> tunnel models. An ESOP system consists of up to 20 <span class="hlt">pressure</span> modules (PMs), each with 48 <span class="hlt">pressure</span> transducers and a heater, an analog-to-digital (A/D) converter module, a microprocessor, a data controller, a monitor unit, a control and processing unit, and a heater controller. The PMs and the A/D converter module are sized to be installed in the models tested in the Ames Aerodynamics Division <span class="hlt">wind</span> tunnels. A unique feature of the <span class="hlt">pressure</span> module is the lack of moving parts such as a pneumatic switch used in other systems for in situ calibrations. This paper describes the ESOP system and the results of the initial testing of the system. The initial results indicate the system meets the original design goal of 0.15 percent accuracy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22034605-roles-radiation-ram-pressure-driving-galactic-winds','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22034605-roles-radiation-ram-pressure-driving-galactic-winds"><span>THE ROLES OF RADIATION AND RAM <span class="hlt">PRESSURE</span> IN DRIVING GALACTIC <span class="hlt">WINDS</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>Sharma, Mahavir; Nath, Biman B., E-mail: mahavir@rri.res.in, E-mail: biman@rri.res.in</p> <p></p> <p>We study gaseous outflows from disk galaxies driven by the combined effects of ram <span class="hlt">pressure</span> on cold gas clouds and radiation <span class="hlt">pressure</span> on dust grains. Taking into account the gravity due to disk, bulge, and dark matter halo, and assuming continuous star formation in the disk, we show that radiation or ram <span class="hlt">pressure</span> alone is not sufficient to drive escaping <span class="hlt">winds</span> from disk galaxies and that both processes contribute. We show that in the parameter space of star formation rate (SFR) and rotation speed of galaxies the <span class="hlt">wind</span> speed in galaxies with rotation speeds v{sub c} {<=} 200 km s{supmore » -1} and SFR {<=} 100 M{sub Sun} yr{sup -1} has a larger contribution from ram <span class="hlt">pressure</span>, and that in high-mass galaxies with large SFR radiation from the disk has a greater role in driving galactic <span class="hlt">winds</span>. The ratio of <span class="hlt">wind</span> speed to circular speed can be approximated as v{sub w} / v{sub c} {approx} 10{sup 0.7}, [SFR/50{sub Sun }yr{sup -1}]{sup 0.4} [v{sub c}/120 km s{sup -1}]{sup -1.25}. We show that this conclusion is borne out by observations of galactic <span class="hlt">winds</span> at low and high redshift and also of circumgalactic gas. We also estimate the mass loading factors under the combined effect of ram and radiation <span class="hlt">pressure</span>, and show that the ratio of mass-loss rate to SFR scales roughly as v{sup -1}{sub c}{Sigma}{sub g}{sup -1}, where {Sigma}{sub g} is the gas column density in the disk.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993wais.work...44B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993wais.work...44B"><span>Surface <span class="hlt">winds</span> over West Antarctica</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bromwich, David</p> <p>1993-07-01</p> <p>Five winter months (April-August 1988) of thermal infrared satellite images were examined to investigate the occurrence of dark (warm) signatures across the Ross Ice Shelf in the Antarctic continent. These features are inferred to be generated by katabatic <span class="hlt">winds</span> that descend from southern Marie Byrd Land and then blow horizontally across the ice shelf. Significant mass is added to this airstream by katabatic <span class="hlt">winds</span> blowing from the major glaciers that flow through the Transantarctic Mountains from East Antarctica. These negatively buoyant katabatic <span class="hlt">winds</span> can reach the northwestern edge of the shelf - a horizontal propagation distance of up to 1,000 km - 14 percent of the time. Where the airstream crosses from the ice shelf to the ice-covered Ross Sea, a prominent coastal polynya is formed. Because the downslope buoyancy force is near zero over the Ross Ice Shelf, the northwestward propagation of the katabatic <span class="hlt">air</span> mass requires <span class="hlt">pressure</span> gradient support. The study shows that the extended horizontal propagation of this atmospheric density current occurred in conjunction with the passage of synoptic cyclones over the southern Amundsen Sea. These cyclones can strengthen the <span class="hlt">pressure</span> gradient in the interior of West Antarctica and make the <span class="hlt">pressure</span> field favorable for northwestward movement of the katabatic <span class="hlt">winds</span> from West Antarctica across the ice shelf in a geostrophic direction. The glacier <span class="hlt">winds</span> from East Antarctica are further accelerated by the synoptic <span class="hlt">pressure</span> gradient, usually undergo abrupt adjustment beyond the exit to the glacier valley, and merge into the mountain-parallel katabatic <span class="hlt">air</span> mass.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010EGUGA..1210133Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010EGUGA..1210133Z"><span><span class="hlt">Air</span>-sea fluxes of momentum and mass in the presence of <span class="hlt">wind</span> waves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zülicke, Christoph</p> <p>2010-05-01</p> <p>An <span class="hlt">air</span>-sea interaction model (ASIM) is developed including the effect of <span class="hlt">wind</span> waves on momentum and mass transfer. This includes the derivation of profiles of dissipation rate, flow speed and concentration from a certain height to a certain depth. Simplified assumptions on the turbulent closure, skin - bulk matching and the spectral wave model allow for an analytic treatment. Particular emphasis was put on the inclusion of primary (gravity) waves and secondary (capillary-gravity) waves. The model was tuned to match wall-flow theory and data on wave height and slope. Growing waves reduce the <span class="hlt">air</span>-side turbulent stress and lead to an increasing drag coefficient. In the sea, breaking waves inject turbulent kinetic energy and accelerate the transfer. Cross-reference with data on wave-related momentum and energy flux, dissipation rate and transfer velocity was sufficient. The evaluation of ASIM allowed for the analytical calculation of bulk formulae for the <span class="hlt">wind</span>-dependent gas transfer velocity including information on the <span class="hlt">air</span>-side momentum transfer (drag coefficient) and the sea-side gas transfer (Dalton number). The following regimes have been identified: the smooth waveless regime with a transfer velocity proportional to (<span class="hlt">wind</span>) × (diffusion)2-3, the primary wave regime with a <span class="hlt">wind</span> speed dependence proportional to (<span class="hlt">wind</span>)1-4 × (diffusion)1-2-(waveage)1-4 and the secondary wave regime including a more-than-linear <span class="hlt">wind</span> speed dependence like (<span class="hlt">wind</span>)15-8 × (diffusion)1-2 × (waveage)5-8. These findings complete the current understanding of <span class="hlt">air</span>-sea interaction for medium <span class="hlt">winds</span> between 2 and 20 m s^-1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20020090258','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20020090258"><span>The Breath of Planet Earth: Atmospheric Circulation. Assimilation of Surface <span class="hlt">Wind</span> Observations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Atlas, Robert; Bloom, Stephen; Otterman, Joseph</p> <p>2000-01-01</p> <p>Differences in <span class="hlt">air</span> <span class="hlt">pressure</span> are a major cause of atmospheric circulation. Because heat excites the movement of atoms, warm temperatures cause, <span class="hlt">air</span> molecules to expand. Because those molecules now occupy a larger space, the <span class="hlt">pressure</span> that their weight exerts is decreased. <span class="hlt">Air</span> from surrounding high-<span class="hlt">pressure</span> areas is pushed toward the low-<span class="hlt">pressure</span> areas, creating circulation. This process causes a major pattern of global atmosphere movement known as meridional circulation. In this form of convection, or vertical <span class="hlt">air</span> movement, heated equatorial <span class="hlt">air</span> rises and travels through the upper atmosphere toward higher latitudes. <span class="hlt">Air</span> just above the equator heads toward the North Pole, and <span class="hlt">air</span> just below the equator moves southward. This <span class="hlt">air</span> movement fills the gap created where increased <span class="hlt">air</span> <span class="hlt">pressure</span> pushes down cold <span class="hlt">air</span>. The ,cold <span class="hlt">air</span> moves along the surface back toward the equator, replacing the <span class="hlt">air</span> masses that rise there. Another influence on atmospheric. circulation is the Coriolis force. Because of the Earth's rotation, large-scale <span class="hlt">wind</span> currents move in the direction of this axial spin around low-<span class="hlt">pressure</span> areas. <span class="hlt">Wind</span> rotates counterclockwise in the Northern Hemisphere and clockwise in the Southern Hemisphere. just as the Earth's rotation affects airflow, so too does its surface. In the phenomenon of orographic lifting, elevated topographic features such as mountain ranges lift <span class="hlt">air</span> as it moves up their surface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27036282','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27036282"><span><span class="hlt">Wind</span> turbine sound <span class="hlt">pressure</span> level calculations at dwellings.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Keith, Stephen E; Feder, Katya; Voicescu, Sonia A; Soukhovtsev, Victor; Denning, Allison; Tsang, Jason; Broner, Norm; Leroux, Tony; Richarz, Werner; van den Berg, Frits</p> <p>2016-03-01</p> <p>This paper provides calculations of outdoor sound <span class="hlt">pressure</span> levels (SPLs) at dwellings for 10 <span class="hlt">wind</span> turbine models, to support Health Canada's Community Noise and Health Study. Manufacturer supplied and measured <span class="hlt">wind</span> turbine sound power levels were used to calculate outdoor SPL at 1238 dwellings using ISO [(1996). ISO 9613-2-Acoustics] and a Swedish noise propagation method. Both methods yielded statistically equivalent results. The A- and C-weighted results were highly correlated over the 1238 dwellings (Pearson's linear correlation coefficient r > 0.8). Calculated <span class="hlt">wind</span> turbine SPLs were compared to ambient SPLs from other sources, estimated using guidance documents from the United States and Alberta, Canada.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26398125','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26398125"><span>Noncontact Monitoring of Respiration by Dynamic <span class="hlt">Air-Pressure</span> Sensor.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Takarada, Tohru; Asada, Tetsunosuke; Sumi, Yoshihisa; Higuchi, Yoshinori</p> <p>2015-01-01</p> <p>We have previously reported that a dynamic <span class="hlt">air-pressure</span> sensor system allows respiratory status to be visually monitored for patients in minimally clothed condition. The dynamic <span class="hlt">air-pressure</span> sensor measures vital information using changes in <span class="hlt">air</span> <span class="hlt">pressure</span>. To utilize this device in the field, we must clarify the influence of clothing conditions on measurement. The present study evaluated use of the dynamic <span class="hlt">air-pressure</span> sensor system as a respiratory monitor that can reliably detect change in breathing patterns irrespective of clothing. Twelve healthy volunteers reclined on a dental chair positioned horizontally with the sensor pad for measuring <span class="hlt">air-pressure</span> signals corresponding to respiration placed on the seat back of the dental chair in the central lumbar region. Respiratory measurements were taken under 2 conditions: (a) thinly clothed (subject lying directly on the sensor pad); and (b) thickly clothed (subject lying on the sensor pad covered with a <span class="hlt">pressure</span>-reducing sheet). <span class="hlt">Air-pressure</span> signals were recorded and time integration values for <span class="hlt">air</span> <span class="hlt">pressure</span> during each expiration were calculated. This information was compared with expiratory tidal volume measured simultaneously by a respirometer connected to the subject via face mask. The dynamic <span class="hlt">air-pressure</span> sensor was able to receive the signal corresponding to respiration regardless of clothing conditions. A strong correlation was identified between expiratory tidal volume and time integration values for <span class="hlt">air</span> <span class="hlt">pressure</span> during each expiration for all subjects under both clothing conditions (0.840-0.988 for the thinly clothed condition and 0.867-0.992 for the thickly clothed condition). These results show that the dynamic <span class="hlt">air-pressure</span> sensor is useful for monitoring respiratory physiology irrespective of clothing.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1412658-converting-wind-energy-ammonia-lower-pressure','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1412658-converting-wind-energy-ammonia-lower-pressure"><span>Converting <span class="hlt">Wind</span> Energy to Ammonia at Lower <span class="hlt">Pressure</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>Malmali, Mahdi; Reese, Michael; McCormick, Alon V.</p> <p></p> <p>Renewable <span class="hlt">wind</span> energy can be used to make ammonia. However, <span class="hlt">wind</span>-generated ammonia costs about twice that made from a traditional fossil-fuel driven process. To reduce the production cost, we replace the conventional ammonia condensation with a selective absorber containing metal halides, e.g., calcium chloride, operating at near synthesis temperatures. With this reaction-absorption process, ammonia can be synthesized at 20 bar from <span class="hlt">air</span>, water, and <span class="hlt">wind</span>-generated electricity, with rates comparable to the conventional process running at 150–300 bar. In our reaction-absorption process, the rate of ammonia synthesis is now controlled not by the chemical reaction but largely by the pump usedmore » to recycle the unreacted gases. The results suggest an alternative route to distributed ammonia manufacture which can locally supply nitrogen fertilizer and also a method to capture stranded <span class="hlt">wind</span> energy as a carbon-neutral liquid fuel.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1412658-converting-wind-energy-ammonia-lower-pressure','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1412658-converting-wind-energy-ammonia-lower-pressure"><span>Converting <span class="hlt">Wind</span> Energy to Ammonia at Lower <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Malmali, Mahdi; Reese, Michael; McCormick, Alon V.; ...</p> <p>2017-11-07</p> <p>Renewable <span class="hlt">wind</span> energy can be used to make ammonia. However, <span class="hlt">wind</span>-generated ammonia costs about twice that made from a traditional fossil-fuel driven process. To reduce the production cost, we replace the conventional ammonia condensation with a selective absorber containing metal halides, e.g., calcium chloride, operating at near synthesis temperatures. With this reaction-absorption process, ammonia can be synthesized at 20 bar from <span class="hlt">air</span>, water, and <span class="hlt">wind</span>-generated electricity, with rates comparable to the conventional process running at 150–300 bar. In our reaction-absorption process, the rate of ammonia synthesis is now controlled not by the chemical reaction but largely by the pump usedmore » to recycle the unreacted gases. The results suggest an alternative route to distributed ammonia manufacture which can locally supply nitrogen fertilizer and also a method to capture stranded <span class="hlt">wind</span> energy as a carbon-neutral liquid fuel.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.P53C2655T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.P53C2655T"><span>Effects of the Solar <span class="hlt">Wind</span> <span class="hlt">Pressure</span> on Mercury's Exosphere: Hybrid Simulations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Travnicek, P. M.; Schriver, D.; Orlando, T. M.; Hellinger, P.</p> <p>2017-12-01</p> <p>We study effects of the changed solar <span class="hlt">wind</span> <span class="hlt">pressure</span> on the precipitation of hydrogen on the Mercury's surface and on the formation of Mercury's magnetosphere. We carry out a set of global hybrid simulations of the Mercury's magnetosphere with the interplanetary magnetic field oriented in the equatorial plane. We change the solar <span class="hlt">wind</span> <span class="hlt">pressure</span> by changing the velocity of injected solar <span class="hlt">wind</span> plasma (vsw = 2 vA,sw; vsw = 4 vA,sw; vsw = 6 vA,sw). For each of the cases we examine proton and electron precipitation on Mercury's surface and calculate yields of heavy ions released from Mercury's surface via various processes (namely: Photo-Stimulated Desorption, Solar <span class="hlt">Wind</span> Sputtering, and Electron Stimulated Desorption). We study circulation of the released ions within the Mercury's magnetosphere for the three cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17476384','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17476384"><span>Microfluidic <span class="hlt">pressure</span> sensing using trapped <span class="hlt">air</span> compression.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Srivastava, Nimisha; Burns, Mark A</p> <p>2007-05-01</p> <p>We have developed a microfluidic method for measuring the fluid <span class="hlt">pressure</span> head experienced at any location inside a microchannel. The principal component is a microfabricated sealed chamber with a single inlet and no exit; the entrance to the single inlet is positioned at the location where <span class="hlt">pressure</span> is to be measured. The <span class="hlt">pressure</span> measurement is then based on monitoring the movement of a liquid-<span class="hlt">air</span> interface as it compresses <span class="hlt">air</span> trapped inside the microfabricated sealed chamber and calculating the <span class="hlt">pressure</span> using the ideal gas law. The method has been used to measure the <span class="hlt">pressure</span> of the <span class="hlt">air</span> stream and continuous liquid flow inside microfluidic channels (d approximately 50 microm). Further, a <span class="hlt">pressure</span> drop has also been measured using multiple microfabricated sealed chambers. For <span class="hlt">air</span> <span class="hlt">pressure</span>, a resolution of 700 Pa within a full-scale range of 700-100 kPa was obtained. For liquids, <span class="hlt">pressure</span> drops as low as 70 Pa were obtained in an operating range from 70 Pa to 10 kPa. Since the method primarily uses a microfluidic sealed chamber, it does not require additional fabrication steps and may easily be incorporated in several lab-on-a-chip fluidic applications for laminar as well as turbulent flow conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=2935205','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=2935205"><span>Microfluidic <span class="hlt">pressure</span> sensing using trapped <span class="hlt">air</span> compression</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Srivastava, Nimisha; Burns, Mark A.</p> <p>2010-01-01</p> <p>We have developed a microfluidic method for measuring the fluid <span class="hlt">pressure</span> head experienced at any location inside a microchannel. The principal component is a microfabricated sealed chamber with a single inlet and no exit; the entrance to the single inlet is positioned at the location where <span class="hlt">pressure</span> is to be measured. The <span class="hlt">pressure</span> measurement is then based on monitoring the movement of a liquid–<span class="hlt">air</span> interface as it compresses <span class="hlt">air</span> trapped inside the microfabricated sealed chamber and calculating the <span class="hlt">pressure</span> using the ideal gas law. The method has been used to measure the <span class="hlt">pressure</span> of the <span class="hlt">air</span> stream and continuous liquid flow inside microfluidic channels (d ~ 50 μm). Further, a <span class="hlt">pressure</span> drop has also been measured using multiple microfabricated sealed chambers. For <span class="hlt">air</span> <span class="hlt">pressure</span>, a resolution of 700 Pa within a full-scale range of 700–100 kPa was obtained. For liquids, <span class="hlt">pressure</span> drops as low as 70 Pa were obtained in an operating range from 70 Pa to 10 kPa. Since the method primarily uses a microfluidic sealed chamber, it does not require additional fabrication steps and may easily be incorporated in several lab-on-a-chip fluidic applications for laminar as well as turbulent flow conditions. PMID:17476384</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013IJMPS..2460002Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013IJMPS..2460002Z"><span><span class="hlt">Air</span> <span class="hlt">Pressure</span> Controlled Mass Measurement System</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhong, Ruilin; Wang, Jian; Cai, Changqing; Yao, Hong; Ding, Jin'an; Zhang, Yue; Wang, Xiaolei</p> <p></p> <p>Mass measurement is influenced by <span class="hlt">air</span> <span class="hlt">pressure</span>, temperature, humidity and other facts. In order to reduce the influence, mass laboratory of National Institute of Metrology, China has developed an <span class="hlt">air</span> <span class="hlt">pressure</span> controlled mass measurement system. In this system, an automatic mass comparator is installed in an airtight chamber. The Chamber is equipped with a <span class="hlt">pressure</span> controller and associate valves, thus the <span class="hlt">air</span> <span class="hlt">pressure</span> can be changed and stabilized to the pre-set value, the preferred <span class="hlt">pressure</span> range is from 200 hPa to 1100 hPa. In order to keep the environment inside the chamber stable, the display and control part of the mass comparator are moved outside the chamber, and connected to the mass comparator by feed-throughs. Also a lifting device is designed for this system which can easily lift up the upper part of the chamber, thus weights can be easily put inside the mass comparator. The whole system is put on a marble platform, and the temperature and humidity of the laboratory is very stable. The temperature, humidity, and carbon dioxide content inside the chamber are measured in real time and can be used to get <span class="hlt">air</span> density. Mass measurement cycle from 1100 hPa to 200 hPa and back to 1100 hPa shows the effective of the system.</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_2");'>2</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li class="active"><span>4</span></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_4 --> <div id="page_5" 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_3");'>3</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li class="active"><span>5</span></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</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="81"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100014071','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100014071"><span>Water-Based <span class="hlt">Pressure</span>-Sensitive Paints</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jordan, Jeffrey D.; Watkins, A. Neal; Oglesby, Donald M.; Ingram, JoAnne L.</p> <p>2006-01-01</p> <p>Water-based <span class="hlt">pressure</span>-sensitive paints (PSPs) have been invented as alternatives to conventional organic-solvent-based <span class="hlt">pressure</span>-sensitive paints, which are used primarily for indicating distributions of <span class="hlt">air</span> <span class="hlt">pressure</span> on <span class="hlt">wind</span>-tunnel models. Typically, PSPs are sprayed onto aerodynamic models after they have been mounted in <span class="hlt">wind</span> tunnels. When conventional organic-solvent-based PSPs are used, this practice creates a problem of removing toxic fumes from inside the <span class="hlt">wind</span> tunnels. The use of water-based PSPs eliminates this problem. The waterbased PSPs offer high performance as <span class="hlt">pressure</span> indicators, plus all the advantages of common water-based paints (low toxicity, low concentrations of volatile organic compounds, and easy cleanup by use of water).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19730004','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19730004"><span>The relationships between <span class="hlt">air</span> exposure, negative <span class="hlt">pressure</span>, and hemolysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pohlmann, Joshua R; Toomasian, John M; Hampton, Claire E; Cook, Keith E; Annich, Gail M; Bartlett, Robert H</p> <p>2009-01-01</p> <p>The purpose of this study was to describe the hemolytic effects of both negative <span class="hlt">pressure</span> and an <span class="hlt">air</span>-blood interface independently and in combination in an in vitro static blood model. Samples of fresh ovine or human blood (5 ml) were subjected to a bubbling <span class="hlt">air</span> interface (0-100 ml/min) or negative <span class="hlt">pressure</span> (0-600 mm Hg) separately, or in combination, for controlled periods of time and analyzed for hemolysis. Neither negative <span class="hlt">pressure</span> nor an <span class="hlt">air</span> interface alone increased hemolysis. However, when <span class="hlt">air</span> and negative <span class="hlt">pressure</span> were combined, hemolysis increased as a function of negative <span class="hlt">pressure</span>, the <span class="hlt">air</span> interface, and time. Moreover, when blood samples were exposed to <span class="hlt">air</span> before initiating the test, hemolysis was four to five times greater than samples not preexposed to <span class="hlt">air</span>. When these experiments were repeated using freshly drawn human blood, the same phenomena were observed, but the hemolysis was significantly higher than that observed in sheep blood. In this model, hemolysis is caused by combined <span class="hlt">air</span> and negative <span class="hlt">pressure</span> and is unrelated to either factor alone.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3662481','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3662481"><span>The Relationships between <span class="hlt">Air</span> Exposure, Negative <span class="hlt">Pressure</span> and Hemolysis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Pohlmann, Joshua R.; Toomasian, John M.; Hampton, Claire E.; Cook, Keith E.; Annich, Gail M.; Bartlett, Robert H.</p> <p>2013-01-01</p> <p>The purpose of this study was to describe the hemolytic effects of both negative <span class="hlt">pressure</span> and an <span class="hlt">air</span>-blood interface independently and in combination in an in-vitro static blood model. Samples of fresh ovine or human blood (5 mL) were subjected to a bubbling <span class="hlt">air</span> interface (0–100 mL/min) or negative <span class="hlt">pressure</span> (0–600 mmHg) separately, or in combination, for controlled periods of time, and analyzed for hemolysis. Neither negative <span class="hlt">pressure</span> nor an <span class="hlt">air</span> interface alone increased hemolysis. However, when <span class="hlt">air</span> and negative <span class="hlt">pressure</span> were combined, hemolysis increased as a function of negative <span class="hlt">pressure</span>, the <span class="hlt">air</span> interface, and time. Moreover, when blood samples were exposed to <span class="hlt">air</span> prior to initiating the test, hemolysis was 4–5 times greater than samples not pre-exposed to <span class="hlt">air</span>. When these experiments were repeated using freshly drawn human blood the same phenomena were observed, but the hemolysis was significantly higher than that observed in sheep blood. In this model, hemolysis is caused by combined <span class="hlt">air</span> and negative <span class="hlt">pressure</span> and is unrelated to either factor alone. PMID:19730004</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19860033224&hterms=Multivariate+analysis&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DMultivariate%2Banalysis','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19860033224&hterms=Multivariate+analysis&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DMultivariate%2Banalysis"><span>Multivariate optimum interpolation of surface <span class="hlt">pressure</span> and surface <span class="hlt">wind</span> over oceans</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bloom, S. C.; Baker, W. E.; Nestler, M. S.</p> <p>1984-01-01</p> <p>The present multivariate analysis method for surface <span class="hlt">pressure</span> and <span class="hlt">winds</span> incorporates ship <span class="hlt">wind</span> observations into the analysis of surface <span class="hlt">pressure</span>. For the specific case of 0000 GMT, on February 3, 1979, the additional data resulted in a global rms difference of 0.6 mb; individual maxima as larse as 5 mb occurred over the North Atlantic and East Pacific Oceans. These differences are noted to be smaller than the analysis increments to the first-guess fields.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19830011423','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19830011423"><span>Corotating <span class="hlt">pressure</span> waves without streams in the solar <span class="hlt">wind</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Burlaga, L. F.</p> <p>1983-01-01</p> <p>Voyager 1 and 2 magnetic field and plasma data are presented which demonstrate the existence of large scale, corotating, non-linear <span class="hlt">pressure</span> waves between 2 AU and 4 AU that are not accompanied by fast streams. The <span class="hlt">pressure</span> waves are presumed to be generated by corotating streams near the Sun. For two of the three <span class="hlt">pressure</span> waves that are discussed, the absence of a stream is probably a real, physical effect, viz., a consequence of deceleration of the stream by the associated compression wave. For the third <span class="hlt">pressure</span> wave, the apparent absence of a stream may be a geometrical effect; it is likely that the stream was at latitudes just above those of the spacecraft, while the associated shocks and compression wave extended over a broader range of latitudes so that they could be observed by the spacecraft. It is suggested that the development of large-scale non-linear <span class="hlt">pressure</span> waves at the expense of the kinetic energy of streams produces a qualitative change in the solar <span class="hlt">wind</span> in the outer heliosphere. Within a few AU the quasi-stationary solar <span class="hlt">wind</span> structure is determined by corotating streams whose structure is determined by the boundary conditions near the Sun.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005IJCli..25.1203S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005IJCli..25.1203S"><span>Extreme <span class="hlt">pressure</span> differences at 0900 NZST and <span class="hlt">winds</span> across New Zealand</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Salinger, M. James; Griffiths, Georgina M.; Gosai, Ashmita</p> <p>2005-07-01</p> <p>Trends in extremes in station daily sea-level <span class="hlt">pressure</span> differences at 0900 NZST are examined, and extreme daily <span class="hlt">wind</span> gusts, across New Zealand, since the 1960s. Annual time series were examined (with indices of magnitude and frequency over threshold percentiles) from the daily indices selected. These follow from earlier indices of normalized monthly mean sea-level <span class="hlt">pressure</span> differences between station pairs, except the daily indices are not normalized. The frequency statistics quantify the number of extreme zonal (westerly and easterly), or extreme meridional (southerly or northerly), <span class="hlt">pressure</span> gradient events. The frequency and magnitude of extreme westerly episodes has increased slightly over New Zealand, with a significant increase in the westerly extremes to the south of New Zealand. In contrast, the magnitude and frequency of easterly extremes has decreased over New Zealand, but increased to the south, with some trends weakly significant. The frequency and magnitude of daily southerly extremes has decreased significantly in the region.Extreme daily <span class="hlt">wind</span> gust events at key climate stations in New Zealand and at Hobart, Australia, are highly likely to be associated with an extreme daily <span class="hlt">pressure</span> difference. The converse was less likely to hold: extreme <span class="hlt">wind</span> gusts were not always observed on days with extreme daily <span class="hlt">pressure</span> difference, probably due to the strong influence that topography has on localized station <span class="hlt">winds</span>. Significant correlations exist between the frequency indices and both annual-average mean sea-level <span class="hlt">pressures</span> around the Australasian region and annual-average sea surface temperature (SST) anomalies in the Southern Hemisphere. These correlations are generally stronger for indices of extreme westerly or extreme southerly airflows. Annual-average <span class="hlt">pressures</span> in the Tasman Sea or Southern Ocean are highly correlated to zonal indices (frequency of extreme westerlies). SST anomalies in the NINO3 region or on either side of the South Island are</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860008821','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860008821"><span>Aeorodynamic characteristics of an <span class="hlt">air</span>-exchanger system for the 40- by 80-foot <span class="hlt">wind</span> tunnel at Ames Research Center</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rossow, V. J.; Schmidt, G. I.; Meyn, L. A.; Ortner, K. R.; Holmes, R. E.</p> <p>1986-01-01</p> <p>A 1/50-scale model of the 40- by 80-Foot <span class="hlt">Wind</span> Tunnel at Ames Research Center was used to study various <span class="hlt">air</span>-exchange configurations. System components were tested throughout a range of parameters, and approximate analytical relationships were derived to explain the observed characteristics. It is found that the efficiency of the <span class="hlt">air</span> exchanger could be increased (1) by adding a shaped wall to smoothly turn the incoming <span class="hlt">air</span> downstream, (2) by changing to a contoured door at the inlet to control the flow rate, and (3) by increasing the size of the exhaust opening. The static <span class="hlt">pressures</span> inside the circuit then remain within the design limits at the higher tunnel speeds if the <span class="hlt">air</span>-exchange rate is about 5% or more. Since the model is much smaller than the full-scale facility, it is not possible to completely duplicate the tunnel, and it will be necessary to measure such characteristics as flow rate and tunnel <span class="hlt">pressures</span> during implementation of the remodeled facility. The aerodynamic loads estimated for the inlet door and for nearby walls are also presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140016490','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140016490"><span>The Use of Red Green Blue <span class="hlt">Air</span> Mass Imagery to Investigate the Role of Stratospheric <span class="hlt">Air</span> in a Non-Convective <span class="hlt">Wind</span> Event</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Berndt, E. B.; Zavodsky, B. T.; Moltham, A. L.; Folmer, M. J.; Jedlovec, G. J.</p> <p>2014-01-01</p> <p>The investigation of non-convective <span class="hlt">winds</span> associated with passing extratropical cyclones and the formation of the sting jet in North Atlantic cyclones that impact Europe has been gaining interest. Sting jet research has been limited to North Atlantic cyclones that impact Europe because it is known to occur in Shapiro-Keyser cyclones and theory suggests it does not occur in Norwegian type cyclones. The global distribution of sting jet cyclones is unknown and questions remain as to whether cyclones with Shapiro-Keyser characteristics that impact the United States develop features similar to the sting jet. Therefore unique National Aeronautics and Space Administration (NASA) products were used to analyze an event that impacted the Northeast United States on 09 February 2013. Moderate Resolution Imaging Spectroradiometer (MODIS) Red Green Blue (RGB) <span class="hlt">Air</span> Mass imagery and Atmospheric Infrared Sounder (<span class="hlt">AIRS</span>) ozone data were used in conjunction with NASA's global Modern Era-Retrospective Analysis for Research and Applications (MERRA) reanalysis and higher-resolution regional 13-km Rapid Refresh (RAP) data to analyze the role of stratospheric <span class="hlt">air</span> in producing high <span class="hlt">winds</span>. The RGB <span class="hlt">Air</span> Mass imagery and a new <span class="hlt">AIRS</span> ozone anomaly product were used to confirm the presence of stratospheric <span class="hlt">air</span>. Plan view and cross sectional plots of <span class="hlt">wind</span>, potential vorticity, relative humidity, omega, and frontogenesis were used to analyze the relationship between stratospheric <span class="hlt">air</span> and high surface <span class="hlt">winds</span> during the event. Additionally, the Hybrid Single Particle Lagrangian Integrated Trajectory (HYSPLIT) model was used to plot trajectories to determine the role of the conveyor belts in producing the high <span class="hlt">winds</span>. Analyses of new satellite products, such as the RGB <span class="hlt">Air</span> Mass imagery, show the utility of future GOES-R products in forecasting non-convective <span class="hlt">wind</span> events.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860009862','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860009862"><span><span class="hlt">Pressure</span> distributions obtained on a 0.10-scale model of the space shuttle Orbiter's forebody in the AEDC 16T propulsion <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Siemers, P. M., III; Henry, M. W.</p> <p>1986-01-01</p> <p><span class="hlt">Pressure</span> distribution test data obtained on a 0.10-scale model of the forward fuselage of the Space Shuttle Orbiter are presented without analysis. The tests were completed in the AEDC 16T Propulsion <span class="hlt">Wind</span> Tunnel. The 0.10-scale model was tested at angles of attack from -2 deg to 18 deg and angles of side slip from -6 to 6 deg at Mach numbers from 0.25 to 1/5 deg. The tests were conducted in support of the development of the Shuttle Entry <span class="hlt">Air</span> Data System (SEADS). In addition to modeling the 20 SEADS orifices, the <span class="hlt">wind</span>-tunnel model was also instrumented with orifices to match Development Flight Instrumentation (DFI) port locations that existed on the Space Shuttle Orbiter Columbia (OV-102) during the Orbiter Flight Test program. This DFI simulation has provided a means of comparisons between reentry flight <span class="hlt">pressure</span> data and <span class="hlt">wind</span>-tunnel and computational data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.C13C0978D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.C13C0978D"><span>The Breathing Snowpack: <span class="hlt">Pressure</span>-induced Vapor Flux of Temperate Snow</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Drake, S. A.; Selker, J. S.; Higgins, C. W.</p> <p>2017-12-01</p> <p>As surface <span class="hlt">air</span> <span class="hlt">pressure</span> increases, hydrostatic compression of the <span class="hlt">air</span> column forces atmospheric <span class="hlt">air</span> into snowpack pore space. Likewise, as surface <span class="hlt">air</span> <span class="hlt">pressure</span> decreases, the atmospheric <span class="hlt">air</span> column decompresses and saturated <span class="hlt">air</span> exits the snow. Alternating influx and efflux of <span class="hlt">air</span> can be thought of as a "breathing" process that produces an upward vapor flux when <span class="hlt">air</span> above the snow is not saturated. The impact of <span class="hlt">pressure</span>-induced vapor exchange is assumed to be small and is thus ignored in model parameterizations of surface processes over snow. Rationale for disregarding this process is that large amplitude <span class="hlt">pressure</span> changes as caused by synoptic weather patterns are too infrequent to credibly impact vapor flux. The amplitude of high frequency <span class="hlt">pressure</span> changes is assumed to be too small to affect vapor flux, however, the basis for this hypothesis relies on <span class="hlt">pressure</span> measurements collected over an agricultural field (rather than snow). Resolution of the impact of <span class="hlt">pressure</span> changes on vapor flux over seasonal cycles depends on an accurate representation of the magnitude of <span class="hlt">pressure</span> changes caused by changes in <span class="hlt">wind</span> as a function of the frequency of <span class="hlt">pressure</span> changes. High precision in situ <span class="hlt">pressure</span> measurements in a temperature snowpack allowed us to compute the spectra of <span class="hlt">pressure</span> changes vs. <span class="hlt">wind</span> forcing. Using a simplified model for vapor exchange we then computed the frequency of <span class="hlt">pressure</span> changes that maximize vapor exchange. We examine and evaluate the seasonal impact of <span class="hlt">pressure</span>-induced vapor exchange relative to other snow ablation processes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20179887','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20179887"><span>[Aerodynamics study on <span class="hlt">pressure</span> changes inside <span class="hlt">pressure</span>-type whole-body plethysmograph produced by flowing <span class="hlt">air</span>].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Wei-Hua; Shen, Hua-Hao</p> <p>2010-02-25</p> <p>When using <span class="hlt">pressure</span>-type plethysmography to test lung function of rodents, calculation of lung volume is always based on Boyle's law. The precondition of Boyle's law is that perfect <span class="hlt">air</span> is static. However, <span class="hlt">air</span> in the chamber is flowing continuously when a rodent breathes inside the chamber. Therefore, Boyle's law, a principle of <span class="hlt">air</span> statics, may not be appropriate for measuring <span class="hlt">pressure</span> changes of flowing <span class="hlt">air</span>. In this study, we deduced equations for <span class="hlt">pressure</span> changes inside <span class="hlt">pressure</span>-type plethysmograph and then designed three experiments to testify the theoretic deduction. The results of theoretic deduction indicated that increased <span class="hlt">pressure</span> was generated from two sources: one was based on Boyle's law, and the other was based on the law of conservation of momentum. In the first experiment, after injecting 0.1 mL, 0.2 mL, 0.4 mL of <span class="hlt">air</span> into the plethysmograph, the <span class="hlt">pressure</span> inside the chamber increased sharply to a peak value, then promptly decreased to horizontal <span class="hlt">pressure</span>. Peak values were significantly higher than the horizontal values (P<0.001). This observation revealed that flowing <span class="hlt">air</span> made an extra effect on <span class="hlt">air</span> <span class="hlt">pressure</span> in the plethysmograph. In the second experiment, the same volume of <span class="hlt">air</span> was injected into the plethysmograph at different frequencies (0, 0.5, 1, 2, 3 Hz) and <span class="hlt">pressure</span> changes inside were measured. The results showed that, with increasing frequencies, the <span class="hlt">pressure</span> changes in the chamber became significantly higher (P<0.001). In the third experiment, small animal ventilator and pipette were used to make two types of airflow with different functions of time. The <span class="hlt">pressure</span> changes produced by the ventilator were significantly greater than those produced by the pipette (P<0.001). Based on the data obtained, we draw the conclusion that, the flow of <span class="hlt">air</span> plays a role in <span class="hlt">pressure</span> changes inside the plethysmograph, and the faster the airflow is, the higher the <span class="hlt">pressure</span> changes reach. Furthermore, the type of airflow also influences the <span class="hlt">pressure</span> changes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AMTD....7.2585C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AMTD....7.2585C"><span>Calibrating airborne measurements of airspeed, <span class="hlt">pressure</span> and temperature using a Doppler laser <span class="hlt">air</span>-motion sensor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cooper, W. A.; Spuler, S. M.; Spowart, M.; Lenschow, D. H.; Friesen, R. B.</p> <p>2014-03-01</p> <p>A new laser <span class="hlt">air</span>-motion sensor measures the true airspeed with an uncertainty of less than 0.1 m s-1 (standard error) and so reduces uncertainty in the measured component of the relative <span class="hlt">wind</span> along the longitudinal axis of the aircraft to about the same level. The calculated <span class="hlt">pressure</span> expected from that airspeed at the inlet of a pitot tube then provides a basis for calibrating the measurements of dynamic and static <span class="hlt">pressure</span>, reducing standard-error uncertainty in those measurements to less than 0.3 hPa and the precision applicable to steady flight conditions to about 0.1 hPa. These improved measurements of <span class="hlt">pressure</span>, combined with high-resolution measurements of geometric altitude from the Global Positioning System, then indicate (via integrations of the hydrostatic equation during climbs and descents) that the offset and uncertainty in temperature measurement for one research aircraft are +0.3 ± 0.3 °C. For airspeed, <span class="hlt">pressure</span> and temperature these are significant reductions in uncertainty vs. those obtained from calibrations using standard techniques. Finally, it is shown that the new laser <span class="hlt">air</span>-motion sensor, combined with parametrized fits to correction factors for the measured dynamic and ambient <span class="hlt">pressure</span>, provides a measurement of temperature that is independent of any other temperature sensor.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.usgs.gov/of/2013/1063/','USGSPUBS'); return false;" href="https://pubs.usgs.gov/of/2013/1063/"><span><span class="hlt">Air</span> temperature, <span class="hlt">wind</span> speed, and <span class="hlt">wind</span> direction in the National Petroleum Reserve—Alaska and the Arctic National Wildlife Refuge, 1998–2011</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Urban, Frank E.; Clow, Gary D.</p> <p>2013-01-01</p> <p>This report provides <span class="hlt">air</span> temperature, <span class="hlt">wind</span> speed, and <span class="hlt">wind</span> direction data collected on Federal lands in Arctic Alaska over the period August 1998 to July 2011 by the U.S. Department of the Interior's climate monitoring array, part of the Global Terrestrial Network for Permafrost. In addition to presenting data, this report also describes monitoring, data collection, and quality control methodology. This array of 16 monitoring stations spans 68.5°N to 70.5°N and 142.5°W to 161°W, an area of roughly 150,000 square kilometers. Climate summaries are presented along with provisional quality-controlled data. Data collection is ongoing and includes several additional climate variables to be released in subsequent reports, including ground temperature and soil moisture, snow depth, rainfall, up- and downwelling shortwave radiation, and atmospheric <span class="hlt">pressure</span>. These data were collected by the U.S. Geological Survey in close collaboration with the Bureau of Land Management and the U.S. Fish and Wildlife Service.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19810000242&hterms=air+bags&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bbags','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19810000242&hterms=air+bags&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bbags"><span><span class="hlt">Air</span> Bag Applies Uniform Bonding <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gillespie, C. A.</p> <p>1982-01-01</p> <p><span class="hlt">Air</span>-bag box applies constant uniform <span class="hlt">pressure</span> to tiles and other objects undergoing adhesive bonding. Box is basically a compliant clamp with adjustable force and position. Can be used on irregular surfaces as well as on flat ones. <span class="hlt">Pressurized</span> <span class="hlt">air</span> is fed to bag through a tube so that it expands, filling the box and pressing against work. Bag adopts a contour that accommodates surface under open side of box.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930037655&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930037655&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure"><span>Influence of ambient <span class="hlt">air</span> <span class="hlt">pressure</span> on effervescent atomization</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chen, S. K.; Lefebvre, A. H.; Rollbuhler, J.</p> <p>1993-01-01</p> <p>The influence of ambient <span class="hlt">air</span> <span class="hlt">pressure</span> on the drop-size distributions produced in effervescent atomization is examined in this article. Also investigated are the effects on spray characteristics of variations in <span class="hlt">air</span>/liquid mass ratio, liquid-injection <span class="hlt">pressure</span>, and atomizer discharge-orifice diameter at different levels of ambient <span class="hlt">air</span> <span class="hlt">pressure</span>. It is found that continuous increase in <span class="hlt">air</span> <span class="hlt">pressure</span> above the normal atmospheric value causes the mean drop-size to first increase up to a maximum value and then decline. An explanation for this characteristic is provided in terms of the various contributing factors to the overall atomization process. It is also observed that changes in atomizer geometry and operating conditions have little effect on the distribution of drop-sizes in the spray.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820014341','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820014341"><span>Effects of axisymmetric and normal <span class="hlt">air</span> jet plumes and solid plume on cylindrical afterbody <span class="hlt">pressure</span> distributions at Mach numbers from 1.65 to 2.50</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Covell, P. F.</p> <p>1982-01-01</p> <p>A <span class="hlt">wind</span> tunnel investigation of the interference effects of axisymmetric nozzle <span class="hlt">air</span> plumes, a solid plume, and normal <span class="hlt">air</span> jet plumes on the afterbody <span class="hlt">pressure</span> distributions and base <span class="hlt">pressures</span> of a cylindrical afterbody model was conducted at Mach numbers from 1.65 to 2.50. The axisymmetric nozzles, which varied in exit lip Mach number from 1.7 to 2.7, and the normal <span class="hlt">air</span> jet nozzle were tested at jet <span class="hlt">pressure</span> ratios from 1 (jet off) to 615. The tests were conducted at an angle of attack of 0 deg and a Reynolds number per meter of 6.56 million. The results of the investigation show that the solid plume induces greater interference effects than those induced by the axisymmetric nozzle plumes at the selected underexpanded design conditions. A thrust coefficient parameter based on nozzle lip conditons was found to correlate the afterbody disturbance distance and the base <span class="hlt">pressure</span> between the different axisymmetric nozzles. The normal <span class="hlt">air</span> jet plume and the solid plume induce afterbody disturbance distances similar to those induced by the axisymmetric <span class="hlt">air</span> plumes when base <span class="hlt">pressure</span> is held constant.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018GeoRL..45..585L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018GeoRL..45..585L"><span>Prompt Disappearance and Emergence of Radiation Belt Magnetosonic Waves Induced by Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Variations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Nigang; Su, Zhenpeng; Zheng, Huinan; Wang, Yuming; Wang, Shui</p> <p>2018-01-01</p> <p>Magnetosonic waves are highly oblique whistler mode emissions transferring energy from the ring current protons to the radiation belt electrons in the inner magnetosphere. Here we present the first report of prompt disappearance and emergence of magnetosonic waves induced by the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> variations. The solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> reduction caused the magnetosphere expansion, adiabatically decelerated the ring current protons for the Bernstein mode instability, and produced the prompt disappearance of magnetosonic waves. On the contrary, because of the adiabatic acceleration of the ring current protons by the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement, magnetosonic waves emerged suddenly. In the absence of impulsive injections of hot protons, magnetosonic waves were observable even only during the time period with the enhanced solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>. Our results demonstrate that the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> is an essential parameter for modeling of magnetosonic waves and their effect on the radiation belt electrons.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NatEn...217134M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NatEn...217134M"><span>The climate and <span class="hlt">air</span>-quality benefits of <span class="hlt">wind</span> and solar power in the United States</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Millstein, Dev; Wiser, Ryan; Bolinger, Mark; Barbose, Galen</p> <p>2017-09-01</p> <p><span class="hlt">Wind</span> and solar energy reduce combustion-based electricity generation and provide <span class="hlt">air</span>-quality and greenhouse gas emission benefits. These benefits vary dramatically by region and over time. From 2007 to 2015, solar and <span class="hlt">wind</span> power deployment increased rapidly while regulatory changes and fossil fuel price changes led to steep cuts in overall power-sector emissions. Here we evaluate how <span class="hlt">wind</span> and solar climate and <span class="hlt">air</span>-quality benefits evolved during this time period. We find cumulative <span class="hlt">wind</span> and solar <span class="hlt">air</span>-quality benefits of 2015 US$29.7-112.8 billion mostly from 3,000 to 12,700 avoided premature mortalities, and cumulative climate benefits of 2015 US$5.3-106.8 billion. The ranges span results across a suite of <span class="hlt">air</span>-quality and health impact models and social cost of carbon estimates. We find that binding cap-and-trade pollutant markets may reduce these cumulative benefits by up to 16%. In 2015, based on central estimates, combined marginal benefits equal 7.3 ¢ kWh-1 (<span class="hlt">wind</span>) and 4.0 ¢ kWh-1 (solar).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDF24003Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDF24003Z"><span>Simultaneous velocity and <span class="hlt">pressure</span> quantification using <span class="hlt">pressure</span>-sensitive flow tracers in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Peng; Peterson, Sean; Porfiri, Maurizio</p> <p>2017-11-01</p> <p>Particle-based measurement techniques for assessing the velocity field of a fluid have advanced rapidly over the past two decades. Full-field <span class="hlt">pressure</span> measurement techniques have remained elusive, however. In this work, we aim to demonstrate the possibility of direct simultaneous planar velocity and <span class="hlt">pressure</span> measurement of a high speed aerodynamic flow by employing novel <span class="hlt">pressure</span>-sensitive tracer particles for particle image velocimetry (PIV). Specifically, the velocity and <span class="hlt">pressure</span> variations of an airflow through a converging-diverging channel are studied. Polystyrene microparticles embedded with a <span class="hlt">pressure</span>-sensitive phosphorescent dye-platinum octaethylporphyrin (PtOEP)-are used as seeding particles. Due to the oxygen quenching effect, the emission lifetime of PtOEP is highly sensitive to the oxygen concentration, that is, the partial <span class="hlt">pressure</span> of oxygen, in the <span class="hlt">air</span>. Since the partial <span class="hlt">pressure</span> of oxygen is linearly proportional to the <span class="hlt">air</span> <span class="hlt">pressure</span>, we can determine the <span class="hlt">air</span> <span class="hlt">pressure</span> through the phosphorescence emission lifetime of the dye. The velocity field is instead obtained using traditional PIV methods. The particles have a <span class="hlt">pressure</span> resolution on the order of 1 kPa, which may be improved by optimizing the particle size and dye concentration to suit specific flow scenarios. This work was supported by the National Science Foundation under Grant Number CBET-1332204.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMSH42A..08S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMSH42A..08S"><span>Regulation of <span class="hlt">pressure</span> anisotropy in the solar <span class="hlt">wind</span>: processes within inertial range of turbulence</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Strumik, M.; Schekochihin, A. A.; Squire, J.; Bale, S. D.</p> <p>2016-12-01</p> <p>Dynamics of weakly collisional plasmas may lead to thermal <span class="hlt">pressure</span> anisotropies that are driven by velocity shear, plasma expansion/compression or temperature gradients. The <span class="hlt">pressure</span> anisotropies can provide free energy for the growth of micro-scale instabilities, like the mirror of firehose instabilities, that are commonly believed to constrain the <span class="hlt">pressure</span> anisotropy in the solar <span class="hlt">wind</span> if appropriate thresholds are exceeded. We discuss possible alternative mechanisms of regulation of the <span class="hlt">pressure</span> anisotropy in the inertial range of solar <span class="hlt">wind</span> turbulence that provide β-dependent constraints on the amplitude of fluctuations of <span class="hlt">pressure</span> components and other quantities. In particular it is shown that double-adiabatic (CGL) closure for magnetohydrodynamic regime leads to 1/β scaling of the amplitude of the <span class="hlt">pressure</span> component fluctuations and the <span class="hlt">pressure</span> anisotropy. Both freely decaying and forced turbulence are discussed based on results of 3D numerical simulations and analytical theoretical predictions. The theoretical results are contrasted with <span class="hlt">WIND</span> spacecraft measurements.</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_3");'>3</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li class="active"><span>5</span></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_5 --> <div id="page_6" 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_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</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="101"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20100001491&hterms=Hurricane+Katrina&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DHurricane%2BKatrina','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20100001491&hterms=Hurricane+Katrina&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DHurricane%2BKatrina"><span>Evaluation of Vertically Resolved Water <span class="hlt">Winds</span> from <span class="hlt">AIRS</span> using Hurricane Katrina</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Aumann, Hartmut H.; Dobkowski, Edwin C.; Gregorich, David T.</p> <p>2005-01-01</p> <p>The knowledge of <span class="hlt">wind</span> velocity as a function of altitude is key to weather forecast improvements. The ability of hyperspectral sounders in principle to measure vertically resolved water <span class="hlt">winds</span>, which has long been recognized, has been tested with Atmospheric Infrared Sounder (<span class="hlt">AIRS</span>) data. <span class="hlt">AIRS</span> retrievals of total column water above 300 mb have been correlated with the radiosonde upper-tropospheric <span class="hlt">wind</span> velocity and moisture data. The excellent correlation is illustrated with results obtained from hurricane Katrina and from the western United States. <span class="hlt">AIRS</span> is a hyperspectral infrared sounder in low Earth orbit. It was launched in May 2002. We illustrate the use of <span class="hlt">AIRS</span> data for the measurement of upper tropospheric water by using the 2387/cm CO2 R-branch channel and the 1551/cm water vapor channel. The 2387/cm channel measures the temperature at 300 mb totally independent of water vapor. The weighting function of the 1551/cm channel peaks at 300 mb only under moist conditions; the peak shifts downward (higher temperature) for less water and upward (lower temperature) for more water. The difference between the brightness temperatures bt2387 and bt1551 cancels the local several degree weather related variability of the temperature and measures the component due to the water vapor at 300 mb.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AMT.....7.3215C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AMT.....7.3215C"><span>Calibrating airborne measurements of airspeed, <span class="hlt">pressure</span> and temperature using a Doppler laser <span class="hlt">air</span>-motion sensor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cooper, W. A.; Spuler, S. M.; Spowart, M.; Lenschow, D. H.; Friesen, R. B.</p> <p>2014-09-01</p> <p>A new laser <span class="hlt">air</span>-motion sensor measures the true airspeed with a standard uncertainty of less than 0.1 m s-1 and so reduces uncertainty in the measured component of the relative <span class="hlt">wind</span> along the longitudinal axis of the aircraft to about the same level. The calculated <span class="hlt">pressure</span> expected from that airspeed at the inlet of a pitot tube then provides a basis for calibrating the measurements of dynamic and static <span class="hlt">pressure</span>, reducing standard uncertainty in those measurements to less than 0.3 hPa and the precision applicable to steady flight conditions to about 0.1 hPa. These improved measurements of <span class="hlt">pressure</span>, combined with high-resolution measurements of geometric altitude from the global positioning system, then indicate (via integrations of the hydrostatic equation during climbs and descents) that the offset and uncertainty in temperature measurement for one research aircraft are +0.3 ± 0.3 °C. For airspeed, <span class="hlt">pressure</span> and temperature, these are significant reductions in uncertainty vs. those obtained from calibrations using standard techniques. Finally, it is shown that although the initial calibration of the measured static and dynamic <span class="hlt">pressures</span> requires a measured temperature, once calibrated these measured <span class="hlt">pressures</span> and the measurement of airspeed from the new laser <span class="hlt">air</span>-motion sensor provide a measurement of temperature that does not depend on any other temperature sensor.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730008202','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730008202"><span>High-<span class="hlt">pressure</span> combustor exhaust emissions with improved <span class="hlt">air</span>-atomizing and conventional <span class="hlt">pressure</span>-atomizing fuel nozzles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ingebo, R. D.; Norgren, C. T.</p> <p>1973-01-01</p> <p>A high-<span class="hlt">pressure</span> combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by 0.305 meter (6 by 12 in.) was tested with specially designed <span class="hlt">air</span>-atomizing and conventional <span class="hlt">pressure</span>-atomizing fuel nozzles at inlet-<span class="hlt">air</span> temperatures of 340 to 755 k (610 deg to 1360 R), reference velocities of 12.4 to 26.1 meters per second (41 to 86 ft/sec), and fuel-<span class="hlt">air</span> ratios of 0.008 to 0.020. Increasing inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> from 4 to 20 atmospheres generally increased smoke number and nitric oxide, but decreased carbon monoxide and unburned hydrocarbon concentrations with <span class="hlt">air</span>-atomizing and <span class="hlt">pressure</span>-atomizing nozzles. Emission indexes for carbon monoxide and unburned hydrocarbons were lower at 4, 10, and 20 atmospheres, and nitric oxide emission indexes were lower at 10 and 20 atmospheres with <span class="hlt">air</span>-atomizing than with <span class="hlt">pressure</span>-atomizing nozzles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19830029836&hterms=wind+monitor&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dwind%2Bmonitor','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19830029836&hterms=wind+monitor&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dwind%2Bmonitor"><span>A new electronic scanner of <span class="hlt">pressure</span> designed for installation in <span class="hlt">wind</span>-tunnel models</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Coe, C. T.; Parra, G. T.; Kauffman, R. C.</p> <p>1981-01-01</p> <p>A new electronic scanner of <span class="hlt">pressure</span> (ESOP) has been developed by NASA Ames Research Center for installation in <span class="hlt">wind</span>-tunnel models. An ESOP system includes up to 20 <span class="hlt">pressure</span> modules, each with 48 <span class="hlt">pressure</span> transducers, an A/D converter, a microprocessor, a data controller, a monitor unit, and a heater controller. The system is sized so that the <span class="hlt">pressure</span> modules and A/D converter module can be installed within an average-size model tested in the Ames Aerodynamics Division <span class="hlt">wind</span> tunnels. This paper describes the ESOP system, emphasizing the main element of the system - the <span class="hlt">pressure</span> module. The measured performance of the overall system is also presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006JCoAM.192...40D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006JCoAM.192...40D"><span>Numerical analysis of <span class="hlt">pressure</span> field on curved self-weighted metallic roofs due to the <span class="hlt">wind</span> effect by the finite element method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Del Coz Diaz, J. J.; Garcia Nieto, P. J.; Suarez Dominguez, F. J.</p> <p>2006-07-01</p> <p>In this paper, an evaluation of distribution of the <span class="hlt">air</span> <span class="hlt">pressure</span> is determined throughout the curved and open self-weighted metallic roof due to the <span class="hlt">wind</span> effect by the finite element method (FEM) [K. Bathe, Finite Element Procedures, Prentice-Hall, Englewood Cliffs, New York, 1996]. Data from experimental tests carried out in a <span class="hlt">wind</span> tunnel involving a reduced scale model of a roof was used for comparison. The nonlinearity is due to time-averaged Navier-Stokes equations [C.A.J. Fletcher, Computational Techniques for Fluid Dynamics, Springer, Berlin, 1991] that govern the turbulent flow. The calculation has been carried out keeping in mind the possibility of turbulent flow in the vicinities of the walls, and speeds of <span class="hlt">wind</span> have been analyzed between 30 and 40 m/s. Finally, the forces and moments are determined on the cover, as well as the distribution of <span class="hlt">pressures</span> on the same one, comparing the results obtained with the Spanish and European Standards rules, giving place to the conclusions that are exposed in the study.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDQ12005L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDQ12005L"><span>Drop impact on a solid surface at reduced <span class="hlt">air</span> <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Langley, Kenneth; Li, E. Q.; Tian, Y. S.; Hicks, P. D.; Thoroddsen, S. T.</p> <p>2017-11-01</p> <p>When a drop approaches a solid surface at atmospheric <span class="hlt">pressure</span>, the lubrication <span class="hlt">pressure</span> within the <span class="hlt">air</span> forms a dimple in the bottom of the drop resulting in the entrainment of an <span class="hlt">air</span> disc upon impact. Reducing the ambient <span class="hlt">air</span> <span class="hlt">pressure</span> below atmospheric has been shown to suppress splashing and the compression of the intervening <span class="hlt">air</span> could be significant on the <span class="hlt">air</span> disc formation; however, to date there have been no experimental studies showing how the entrainment of the <span class="hlt">air</span> disc is affected by reducing the ambient <span class="hlt">pressure</span>. Using ultra-high-speed interferometry, at up to 5 Mfps, we investigate droplet impacts onto dry solid surfaces in reduced ambient <span class="hlt">air</span> <span class="hlt">pressures</span> with particular interest in what happens as rarified gas effects become important, i.e. when the thickness of the <span class="hlt">air</span> layer is of the same magnitude as the mean free path of the <span class="hlt">air</span> molecules. Experimental data will be presented showing novel phenomena and comparisons will be drawn with theoretical models from the literature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100037123','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100037123"><span>An Analytical Explanation for the X-43A Flush <span class="hlt">Air</span> Data Sensing System <span class="hlt">Pressure</span> Mismatch Between Flight and Theory</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ellsworth, Joel C.</p> <p>2010-01-01</p> <p>Following the successful Mach 7 flight test of the X-43A, unexpectedly low <span class="hlt">pressures</span> were measured by the aft set of the onboard Flush <span class="hlt">Air</span> Data Sensing System s <span class="hlt">pressure</span> ports. These in-flight aft port readings were significantly lower below Mach 3.5 than was predicted by theory. The same lower readings were also seen in the Mach 10 flight of the X-43A and in <span class="hlt">wind</span>-tunnel data. The pre-flight predictions were developed based on 2-dimensional wedge flow, which fails to predict some of the significant 3-dimensional flow features in this geometry at lower Mach numbers. Using Volterra s solution to the wave equation as a starting point, a three-dimensional finite wedge approximation to flow over the X-43A forebody is presented. The surface <span class="hlt">pressures</span> from this approximation compare favorably with the measured <span class="hlt">wind</span> tunnel and flight data at speeds of Mach 2.5 and 3.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19750020019','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19750020019"><span>Investigation of space shuttle vehicle 140C configuration orbiter (model 16-0) wheel well <span class="hlt">pressure</span> loads in the Rockwell International 7.75 x 11 foot <span class="hlt">wind</span> tunnel (OA143)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mennell, R. C.</p> <p>1975-01-01</p> <p>Experimental aerodynamic investigations were conducted on a sting mounted .0405-scale representation of the 140C outer mold line space shuttle orbiter configuration in the Rockwell International 7.75 x 11.00 foot low speed <span class="hlt">wind</span> tunnel. The primary test objectives were to define the orbiter wheel well <span class="hlt">pressure</span> loading and its effects on landing gear thermal insulation and to investigate the <span class="hlt">pressure</span> environment experienced by both the horizontal flight nose probe and <span class="hlt">air</span> vent door probes. Steady state and dynamic <span class="hlt">pressure</span> values were recorded in the orbiter nose gear well, left main landing gear well, horizontal flight nose probe, and both left and right <span class="hlt">air</span> vent door probe. All steady state <span class="hlt">pressure</span> levels were measured by Statham differential <span class="hlt">pressure</span> transducers while dynamic <span class="hlt">pressure</span> levels were recorded by Kulite high frequency response <span class="hlt">pressure</span> sensors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820015360','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820015360"><span>Determination of <span class="hlt">wind</span> tunnel constraint effects by a unified <span class="hlt">pressure</span> signature method. Part 1: Applications to winged configurations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hackett, J. E.; Sampath, S.; Phillips, C. G.</p> <p>1981-01-01</p> <p>A new, fast, non-iterative version of the "Wall <span class="hlt">Pressure</span> Signature Method" is described and used to determine blockage and angle-of-attack <span class="hlt">wind</span> tunnel corrections for highly-powered jet-flap models. The correction method is complemented by the application of tangential blowing at the tunnel floor to suppress flow breakdown there, using feedback from measured floor <span class="hlt">pressures</span>. This tangential blowing technique was substantiated by subsequent flow investigations using an LV. The basic tests on an unswept, knee-blown, jet flapped wing were supplemented to include the effects of slat-removal, sweep and the addition of unflapped tips. C sub mu values were varied from 0 to 10 free-<span class="hlt">air</span> C sub l's in excess of 18 were measured in some cases. Application of the new methods yielded corrected data which agreed with corresponding large tunnel "free <span class="hlt">air</span>" resuls to within the limits of experimental accuracy in almost all cases. A program listing is provided, with sample cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22552108','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22552108"><span><span class="hlt">Pressure</span> ulcer incidence and progression in critically ill subjects: influence of low <span class="hlt">air</span> loss mattress versus a powered <span class="hlt">air</span> <span class="hlt">pressure</span> redistribution mattress.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Black, Joyce; Berke, Christine; Urzendowski, Gail</p> <p>2012-01-01</p> <p>The primary objective of this study was to compare facility-acquired <span class="hlt">pressure</span> ulcer incidence and progression of <span class="hlt">pressure</span> ulcers present on admission in critically ill patients, using 2 different support surfaces. We completed a comparison cohort study in a surgical intensive care unit (ICU). The study setting was a 12-bed cardiovascular ICU in a university-based hospital in the Midwestern United States. The sample comprised 52 critically ill patients; 31 were placed on low <span class="hlt">air</span> loss weight-based <span class="hlt">pressure</span> redistribution-microclimate management system beds and 21 were placed on integrated powered <span class="hlt">air</span> <span class="hlt">pressure</span> redistribution beds. Prior to the start of the study, 5 low airloss beds were placed in open rooms in the cardiovascular surgical ICU. Inclusion criteria were anticipated ICU stay of 3 days, and patients did not receive a speciality bed for pulmonary or wound issues. Initial assessment of the patients included risk assessment and prior events that would increase risk for <span class="hlt">pressure</span> ulcer development such as extended time in operating room, along with skin assessment for existing <span class="hlt">pressure</span> ulcers. Subjects in both groups had ongoing skin assessment every 3 to 4 days and a subjective evaluation of heel elevation and turning or repositioning by the researcher. Data were collected until the subjects were dismissed from the ICU. Patients admitted to the unit were assigned to open rooms following the usual protocols. The mean length of stay was 7.0 days, with an 8.1-day length of stay for subjects on "low <span class="hlt">air</span> loss with microclimate management" beds (LAL-MCM) and 6.6 days on the integrated power <span class="hlt">pressure</span> <span class="hlt">air</span> redistribution (IP-AR) beds (P = NS). The incidence of <span class="hlt">pressure</span> ulcers on the buttocks, sacrum, or coccyx was 0% (0/31) on the low <span class="hlt">air</span> loss bed and 18% (4/21) on the IP-AR bed (P = .046). Five subjects had 6 <span class="hlt">pressure</span> ulcers on admission. Two <span class="hlt">pressure</span> ulcers on 2 patients worsened on the integrated power <span class="hlt">air</span> redistribution beds, which required specialty bed rental</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930089515','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930089515"><span>A Balanced-<span class="hlt">pressure</span> Sliding Seal for Transfer of <span class="hlt">Pressurized</span> <span class="hlt">Air</span> Between Stationary and Rotating Parts</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Curren, Arthur N; Cochran, Reeves P</p> <p>1957-01-01</p> <p>A combination sliding-ring and <span class="hlt">pressure</span>-balancing seal capable of transferring <span class="hlt">pressurize</span> <span class="hlt">air</span> from stationary to rotating parts was developed and experimentally investigated at sliding velocities and cooling-<span class="hlt">air</span> <span class="hlt">pressures</span> up to 10,000 feet per minute and 38.3 pounds per square inch absolute, respectively. Leakage of cooling <span class="hlt">air</span> was completely eliminated with an expenditure of balance <span class="hlt">air</span> less than one-fourth the leakage loss of <span class="hlt">air</span> from labyrinth seals under the same conditions. Additional cooling of the carbon-base seal rings was required, and the maximum wear rate on the rings was about 0.0005 inch per hour.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..GECHT6073C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..GECHT6073C"><span>The effect of humidity on ionic <span class="hlt">wind</span> velocity in ambient <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, She; Nobelen, J. C. P. Y.; Nijdam, S.</p> <p>2016-09-01</p> <p>Due to the evolution of portable electronics and LED lightning system, advances in <span class="hlt">air</span> cooling technologies must also keep pace. Active cooling by ionic <span class="hlt">wind</span>, which is usually generated by corona discharge, can greatly reduce the noise and lifetime issues compared to the mechanical fans. The <span class="hlt">wind</span> is induced when a gas discharge is formed, and neutral molecules gain their energy by the momentum transfer of ion-neutral collisions. However, there is few discussion about the effect of gas composition such as humidity on the <span class="hlt">wind</span> generation and the physical mechanism is not clear. In the experiment, a positive 5-20 kV DC voltage is applied to the needle-cylinder electrodes with separation of 20 mm. The ionic <span class="hlt">wind</span> velocity is measured by hot wire anemometry. As the relative humidity (RH) in the ambient <span class="hlt">air</span> increases, the velocity is found to be severely inhibited. The current is also measured between the cylinder electrode and earth. The results show that the DC component of corona current decreases when RH increases. Since both the discharge current and the ion mobility are reduced when RH increases, their combined effects determine the ionic <span class="hlt">wind</span> velocity. This work is supported by STW project 13651.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050215488','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050215488"><span>Low-<span class="hlt">Pressure</span> Capability of NASA Glenn's 10- by 10-Foot Supersonic <span class="hlt">Wind</span> Tunnel Expanded</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Roeder, James W.</p> <p>2004-01-01</p> <p>Extremely low dynamic <span class="hlt">pressure</span> Q conditions are desired for space-related research including the testing of parachute designs and other decelerator concepts for future vehicles landing on Mars. Therefore, the low-<span class="hlt">pressure</span> operating capability of the Abe Silverstein 10- by 10-foot Supersonic <span class="hlt">Wind</span> Tunnel (10 10 SWT) at NASA Glenn Research Center was recently increased. Successful checkout tests performed in the fall of 2002 showed significantly reduced minimum operating <span class="hlt">pressures</span> in the <span class="hlt">wind</span> tunnel.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27351253','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27351253"><span>Experimental investigation of <span class="hlt">air</span> <span class="hlt">pressure</span> affecting filtration performance of fibrous filter sheet.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Bin; Yu, Xiao; Wu, Ya; Lin, Zhongping</p> <p>2017-03-01</p> <p>Understanding the effect of <span class="hlt">air</span> <span class="hlt">pressure</span> on their filtration performance is important for assessing the effectiveness of fibrous filters under different practical circumstances. The effectiveness of three classes of <span class="hlt">air</span> filter sheets were investigated in laboratory-based measurements at a wide range of <span class="hlt">air</span> <span class="hlt">pressures</span> (60-130 KPa). The filtration efficiency was found most sensitive to the <span class="hlt">air</span> <span class="hlt">pressure</span> change at smaller particle sizes. As the <span class="hlt">air</span> <span class="hlt">pressure</span> increased from 60 to 130 KPa, significant decrease in filtration efficiency (up to 15%) and increase in <span class="hlt">pressure</span> drop (up to 90 Pa) were observed. The filtration efficiency of the filter sheet with largest fiber diameter and smallest solid volume fraction was affected most, while the <span class="hlt">pressure</span> drop of the filter sheet with smallest fiber diameter and largest solid volume fraction was affected most. The effect of <span class="hlt">air</span> <span class="hlt">pressure</span> on the filtration efficiency was slightly larger at greater filter face <span class="hlt">air</span> velocity. However, the effect of <span class="hlt">air</span> <span class="hlt">pressure</span> on the <span class="hlt">pressure</span> drop was negligible. The filtration efficiency and <span class="hlt">pressure</span> drop were explicitly expressed as functions of the <span class="hlt">air</span> <span class="hlt">pressure</span>. Two coefficients were empirically derived and successfully accounted for the effects of <span class="hlt">air</span> <span class="hlt">pressure</span> on filtration efficiency and <span class="hlt">pressure</span> drop.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140008835','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140008835"><span>Within-Tunnel Variations in <span class="hlt">Pressure</span> Data for Three Transonic <span class="hlt">Wind</span> Tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>DeLoach, Richard</p> <p>2014-01-01</p> <p>This paper compares the results of <span class="hlt">pressure</span> measurements made on the same test article with the same test matrix in three transonic <span class="hlt">wind</span> tunnels. A comparison is presented of the unexplained variance associated with polar replicates acquired in each tunnel. The impact of a significance component of systematic (not random) unexplained variance is reviewed, and the results of analyses of variance are presented to assess the degree of significant systematic error in these representative <span class="hlt">wind</span> tunnel tests. Total uncertainty estimates are reported for 140 samples of <span class="hlt">pressure</span> data, quantifying the effects of within-polar random errors and between-polar systematic bias errors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920015848&hterms=foot+model&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dfoot%2Bmodel','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920015848&hterms=foot+model&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dfoot%2Bmodel"><span>The 12-foot <span class="hlt">pressure</span> <span class="hlt">wind</span> tunnel restoration project model support systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Sasaki, Glen E.</p> <p>1992-01-01</p> <p>The 12 Foot <span class="hlt">Pressure</span> <span class="hlt">Wind</span> Tunnel is a variable density, low turbulence <span class="hlt">wind</span> tunnel that operates at subsonic speeds, and up to six atmospheres total <span class="hlt">pressure</span>. The restoration of this facility is of critical importance to the future of the U.S. aerospace industry. As part of this project, several state of the art model support systems are furnished to provide an optimal balance between aerodynamic and operational efficiency parameters. Two model support systems, the Rear Strut Model Support, and the High Angle of Attack Model Support are discussed. This paper covers design parameters, constraints, development, description, and component selection.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ACP....13.1039M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ACP....13.1039M"><span>Where do <span class="hlt">winds</span> come from? A new theory on how water vapor condensation influences atmospheric <span class="hlt">pressure</span> and dynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Makarieva, A. M.; Gorshkov, V. G.; Sheil, D.; Nobre, A. D.; Li, B.-L.</p> <p>2013-01-01</p> <p>Phase transitions of atmospheric water play a ubiquitous role in the Earth's climate system, but their direct impact on atmospheric dynamics has escaped wide attention. Here we examine and advance a theory as to how condensation influences atmospheric <span class="hlt">pressure</span> through the mass removal of water from the gas phase with a simultaneous account of the latent heat release. Building from fundamental physical principles we show that condensation is associated with a decline in <span class="hlt">air</span> <span class="hlt">pressure</span> in the lower atmosphere. This decline occurs up to a certain height, which ranges from 3 to 4 km for surface temperatures from 10 to 30 °C. We then estimate the horizontal <span class="hlt">pressure</span> differences associated with water vapor condensation and find that these are comparable in magnitude with the <span class="hlt">pressure</span> differences driving observed circulation patterns. The water vapor delivered to the atmosphere via evaporation represents a store of potential energy available to accelerate <span class="hlt">air</span> and thus drive <span class="hlt">winds</span>. Our estimates suggest that the global mean power at which this potential energy is released by condensation is around one per cent of the global solar power - this is similar to the known stationary dissipative power of general atmospheric circulation. We conclude that condensation and evaporation merit attention as major, if previously overlooked, factors in driving atmospheric dynamics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19990052691&hterms=plague&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dplague','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19990052691&hterms=plague&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dplague"><span>Correlation of Fin Buffet <span class="hlt">Pressures</span> on an F/A-18 with Scaled <span class="hlt">Wind</span>-Tunnel Measurements</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moses, Robert W.; Shah, Gautam H.</p> <p>1999-01-01</p> <p>Buffeting is an aeroelastic phenomenon occurring at high angles of attack that plagues high performance aircraft, especially those with twin vertical tails. Previous <span class="hlt">wind</span>-tunnel and flight tests were conducted to characterize the buffet loads on the vertical tails by measuring surface <span class="hlt">pressures</span>, bending moments, and accelerations. Following these tests, buffeting responses were computed using the measured buffet <span class="hlt">pressures</span> and compared to the measured buffeting responses. The calculated results did not match the measured data because the assumed spatial correlation of the buffet <span class="hlt">pressures</span> was not correct. A better understanding of the partial (spatial) correlation of the differential buffet <span class="hlt">pressures</span> on the tail was necessary to improve the buffeting predictions. Several <span class="hlt">wind</span>-tunnel investigations were conducted for this purpose. When compared, the results of these tests show that the partial correlation scales with flight conditions. One of the remaining questions is whether the <span class="hlt">wind</span>-tunnel data is consistent with flight data. Presented herein, cross-spectra and coherence functions calculated from <span class="hlt">pressures</span> that were measured on the High Alpha Research Vehicle indicate that the partial correlation of the buffet <span class="hlt">pressures</span> in flight agrees with the partial correlation observed in the <span class="hlt">wind</span> tunnel.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018DSRI..132....6Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018DSRI..132....6Z"><span>Near 7-day response of ocean bottom <span class="hlt">pressure</span> to atmospheric surface <span class="hlt">pressure</span> and <span class="hlt">winds</span> in the northern South China Sea</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Kun; Zhu, Xiao-Hua; Zhao, Ruixiang</p> <p>2018-02-01</p> <p>Ocean bottom <span class="hlt">pressures</span>, observed by five <span class="hlt">pressure</span>-recording inverted echo sounders (PIESs) from October 2012 to July 2014, exhibit strong near 7-day variability in the northern South China Sea (SCS) where long-term in situ bottom <span class="hlt">pressure</span> observations are quite sparse. This variability was strongest in October 2013 during the near two years observation period. By joint analysis with European Center for Medium-Range Weather Forecasts (ECMWF) data, it is shown that the near 7-day ocean bottom <span class="hlt">pressure</span> variability is closely related to the local atmospheric surface <span class="hlt">pressure</span> and <span class="hlt">winds</span>. Within a period band near 7 days, there are high coherences, exceeding 95% significance level, of observed ocean bottom <span class="hlt">pressure</span> with local atmospheric surface <span class="hlt">pressure</span> and with both zonal and meridional components of the <span class="hlt">wind</span>. Ekman pumping/suction caused by the meridional component of the <span class="hlt">wind</span> in particular, is suggested as one driving mechanism. A Kelvin wave response to the near 7-day oscillation would propagate down along the continental slope, observed at the Qui Nhon in the Vietnam. By multiple and partial coherence analyses, we find that local atmospheric surface <span class="hlt">pressure</span> and Ekman pumping/suction show nearly equal influence on ocean bottom <span class="hlt">pressure</span> variability at near 7-day periods. A schematic diagram representing an idealized model gives us a possible mechanism to explain the relationship between ocean bottom <span class="hlt">pressure</span> and local atmospheric forcing at near 7-day periods in the northern SCS.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title21-vol8/pdf/CFR-2013-title21-vol8-sec880-5550.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title21-vol8/pdf/CFR-2013-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2013-04-01 2013-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</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_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_6 --> <div id="page_7" 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_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> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="121"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title21-vol8/pdf/CFR-2010-title21-vol8-sec880-5550.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title21-vol8/pdf/CFR-2010-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2010-04-01 2010-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title21-vol8/pdf/CFR-2014-title21-vol8-sec880-5550.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title21-vol8/pdf/CFR-2014-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2014-04-01 2014-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title21-vol8/pdf/CFR-2011-title21-vol8-sec880-5550.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title21-vol8/pdf/CFR-2011-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2011-04-01 2011-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title21-vol8/pdf/CFR-2012-title21-vol8-sec880-5550.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title21-vol8/pdf/CFR-2012-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2012-04-01 2012-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930094691','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930094691"><span>Attaining a steady <span class="hlt">air</span> stream in <span class="hlt">wind</span> tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Prandtl, L</p> <p>1933-01-01</p> <p>Many experimental arrangements of varying kind involve the problems of assuring a large, steady <span class="hlt">air</span> stream both as to volume and to time. For this reason a separate discussion of the methods by which this is achieved should prove of particular interest. Motors and blades receive special attention and a review of existent <span class="hlt">wind</span> tunnels is also provided.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=PIA00435&hterms=french+system&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dfrench%2Bsystem','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=PIA00435&hterms=french+system&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dfrench%2Bsystem"><span>Hurricane Frances as Observed by NASA's Spaceborne Atmospheric Infrared Sounder (<span class="hlt">AIRS</span>) and Sea<span class="hlt">Winds</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>2004-01-01</p> <p><p/> This image shows Hurricane Frances as captured by instruments onboard two different satellites: the <span class="hlt">AIRS</span> infrared instrument onboard Aqua, and the Sea<span class="hlt">Winds</span> scatterometer onboard QuikSCAT. Both are JPL-managed instruments. <span class="hlt">AIRS</span> data are used to create global three-dimensional maps of temperature, humidity and clouds, while scatterometers measure surface <span class="hlt">wind</span> speed and direction over the ocean. <p/> The red vectors in the image show Frances' surface <span class="hlt">winds</span> as measured by Sea<span class="hlt">Winds</span> on QuikSCAT. The background colors show the temperature of clouds and surface as viewed in the infrared by <span class="hlt">AIRS</span>, with cooler areas pushing to purple and warmer areas are pushing to red. The color scale on the right gives the temperatures in degrees Kelvin. (The top of the scale, 320 degrees Kelvin, corresponds to 117 degrees Fahrenheit, and the bottom, 180 degrees K is -135 degrees F.) The powerful circulation of this storm is evident from the combined data as well as the development of a clearly-defined central 'eye'. The infrared signal does not penetrate through clouds, so the light blue areas reveal the cold clouds tops associated with strong thunderstorms embedded within the storm. In cloud-free areas the infrared signal comes from Earth's surface, revealing warmer temperatures. <p/> The power of the Sea<span class="hlt">Winds</span> scatterometer data set lies in its ability to generate global maps of <span class="hlt">wind</span> speed and direction, giving us a snapshot of how the atmosphere is circulating. Weather prediction centers, including the Tropical Prediction Center - a branch of NOAA that monitors the creation of ocean-born storms, use scatterometer data to help it 'see' where these storms are brewing so that warnings can be issued and the storms, with often erratic motions, can be tracked. <p/> While the Sea<span class="hlt">Winds</span> instrument isn't designed to gather hurricane data, having difficulty seeing the surface in heavy rain, it's data can be used in combination with other data sets to give us an insight into these storms. In</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800004408','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800004408"><span><span class="hlt">Wind</span> study for high altitude platform design</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Strganac, T. W.</p> <p>1979-01-01</p> <p>An analysis of upper <span class="hlt">air</span> <span class="hlt">winds</span> was performed to define the <span class="hlt">wind</span> environment at potential operating altitudes for high altitude powered platform concepts. <span class="hlt">Wind</span> conditions of the continental United States, Pacific area (Alaska to Sea of Japan), and European area (Norwegian and Mediterranean Sea) were obtained using a representative network of sites selected based upon adequate high altitude sampling, geographic dispersion, and observed upper <span class="hlt">wind</span> patterns. A data base of twenty plus years of rawinsonde gathered <span class="hlt">wind</span> information was used in the analysis. Annual variations from surface to 10 mb <span class="hlt">pressure</span> altitude were investigated to encompass the practical operating range for the platform concepts. Parametric analysis for the United States and foreign areas was performed to provide a basis for vehicle system design tradeoffs. This analysis of <span class="hlt">wind</span> magnitudes indicates the feasibility of annual operation at a majority of sites and more selective seasonal operation for the extreme conditions between the <span class="hlt">pressure</span> altitudes of 100 to 25 mb based upon the assumed design speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993PhDT........49J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993PhDT........49J"><span>Gap <span class="hlt">Winds</span> in a Fjord: Howe Sound, British Columbia.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jackson, Peter L.</p> <p>1993-01-01</p> <p>Gap, outflow, or Squamish <span class="hlt">wind</span>, is the cold low level seaward flow of <span class="hlt">air</span> through fjords which dissect the coastal mountain barrier of northwestern North America. These flows, occurring mainly during winter, can be strong, threatening safety, economic activity and comfort. Howe Sound gap <span class="hlt">winds</span> were studied using a combination of observations and several types of models. Observations of <span class="hlt">winds</span> in Howe Sound showed that gap <span class="hlt">wind</span> strength varied considerably along the channel, across the channel and vertically. Generally, <span class="hlt">winds</span> increase down the channel, are strongest along the eastern side, and are below 1000 m depth. Observations were unable to answer all questions about gap <span class="hlt">winds</span> due to data sparseness, particularly in the vertical direction. Therefore, several modelling approaches were used. The modelling began with a complete 3-dimensional quasi-Boussinesq model (CSU RAMS) and ended with the creation and testing of models which are conceptually simpler, and more easily interpreted and manipulated. A gap <span class="hlt">wind</span> simulation made using RAMS was shown to be mostly successful by statistical evaluation compared to other mesoscale simulations, and by visual inspection of the fields. The RAMS output, which has very high temporal and spatial resolution, provided much additional information about the details of gap flow. In particular, RAMS results suggested a close analogy between gap <span class="hlt">wind</span> and hydraulic channel flow, with hydraulic features such as supercritical flow and hydraulic jumps apparent. These findings imply gap <span class="hlt">wind</span> flow could potentially be represented by much simpler models. The simplest possible models containing <span class="hlt">pressure</span> gradient, advection and friction but not incorporating hydraulic effects, were created, tested, and found lacking. A hydraulic model, which in addition incorporates varying gap <span class="hlt">wind</span> height and channel geometry, was created and shown to successfully simulate gap <span class="hlt">winds</span>. Force balance analysis from RAMS and the hydraulic model showed that <span class="hlt">pressure</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012TJSAI..10.Pa19M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012TJSAI..10.Pa19M"><span>Observation of Flame Stabilized at a Hydrogen-Turbojet-Engine Injector Installed into a Lab-Scale Combustion <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Michishita, Kazutaka; Nomura, Hiroshi; Ujiie, Yasushige; Okai, Keiichi</p> <p></p> <p>A lab-scale combustion <span class="hlt">wind</span> tunnel was developed for investigation of low-<span class="hlt">pressure</span> ignition and flame holding in a sub-scale pre-cooled turbojet engine with hydrogen fuel in order to make engine start at high altitudes sure. The combustion <span class="hlt">wind</span> tunnel is a blow-down type. A fuel injector of the sub-scale pre-cooled turbojet engine was installed into the combustion <span class="hlt">wind</span> tunnel. Conditions in which a flame can be stabilized at the fuel injector were examined. The combustor <span class="hlt">pressure</span> and equivalence ratio were varied from 10 to 40 kPa and from 0.4 to 0.8, respectively. The mean inlet <span class="hlt">air</span> velocity was varied from 2 to 48 m/s. Flames stabilized at 20 kPa in <span class="hlt">pressure</span> and 0.6 in equivalence ratio were observed. It was found that the decrease in the combustor <span class="hlt">pressure</span> narrows the mean inlet <span class="hlt">air</span> velocity range for successful flame holdings. Flame holding at lower combustor <span class="hlt">pressures</span> is realized at the equivalence ratio of 0.4 in the low mean inlet <span class="hlt">air</span> velocity range, and at the equivalence ratio of 0.6 in the high mean inlet <span class="hlt">air</span> velocity range. Flame luminosity is the largest near the fuel injector. The flame luminosity distribution becomes flatter as the increase in the mean inlet <span class="hlt">air</span> velocity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/42121','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/42121"><span>Persistent <span class="hlt">wind</span>-induced enhancement of diffusive CO2 transport in a mountain forest snowpack</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>D. R. Bowling; W. J. Massman</p> <p>2011-01-01</p> <p>Diffusion dominates the transport of trace gases between soil and the atmosphere. <span class="hlt">Pressure</span> gradients induced by atmospheric flow and <span class="hlt">wind</span> interacting with topographical features cause a small but persistent bulk flow of <span class="hlt">air</span> within soil or snow. This forcing, called <span class="hlt">pressure</span> pumping or <span class="hlt">wind</span> pumping, leads to a poorly quantified enhancement of gas transport beyond the...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air&pg=4&id=EJ920071','ERIC'); return false;" href="https://eric.ed.gov/?q=air&pg=4&id=EJ920071"><span>One-Component <span class="hlt">Pressure</span>-Temperature Phase Diagrams in the Presence of <span class="hlt">Air</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Andrade-Gamboa, Julio; Martire, Daniel O.; Donati, Edgardo R.</p> <p>2010-01-01</p> <p>One-component phase diagrams are good approximations to predict <span class="hlt">pressure</span>-temperature ("P-T") behavior of a substance in the presence of <span class="hlt">air</span>, provided <span class="hlt">air</span> <span class="hlt">pressure</span> is not much higher than the vapor <span class="hlt">pressure</span>. However, at any <span class="hlt">air</span> <span class="hlt">pressure</span>, and from the conceptual point of view, the use of a traditional "P-T" phase diagram is not strictly correct. In…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1027616','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1027616"><span>Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span> and Saline Filled Cuffs</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2017-01-31</p> <p>AFRL-SA-WP-SR-2017-0004 Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span>- and Saline -Filled...Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span>- and Saline -Filled Cuffs 5a. CONTRACT NUMBER FA8650-14...descending from altitude. When using saline in the ETT cuff, TW <span class="hlt">pressure</span> differences with the 7.5 high-volume, low-<span class="hlt">pressure</span> cuff and 8.0 TaperGuard</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19730030269&hterms=background+wind&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dbackground%2Bwind','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19730030269&hterms=background+wind&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dbackground%2Bwind"><span>Internal gravity wave-atmospheric <span class="hlt">wind</span> interaction - A cause of clear <span class="hlt">air</span> turbulence.</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bekofske, K.; Liu, V. C.</p> <p>1972-01-01</p> <p>The interaction between an internal gravity wave (IGW) and a vertical <span class="hlt">wind</span> shear is discussed as a possible cause in the production of clear <span class="hlt">air</span> turbulence in the free atmosphere. It is shown that under certain typical condition the interaction of an IGW with a background <span class="hlt">wind</span> shear near a critical level provides a mechanism for depositing sufficient momentum in certain regions of the atmosphere to significantly increase the local mean <span class="hlt">wind</span> shear and to lead to the production of turbulence.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28054663','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28054663"><span>Thermal separation of soil particles from thermal conductivity measurement under various <span class="hlt">air</span> <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lu, Sen; Ren, Tusheng; Lu, Yili; Meng, Ping; Zhang, Jinsong</p> <p>2017-01-05</p> <p>The thermal conductivity of dry soils is related closely to <span class="hlt">air</span> <span class="hlt">pressure</span> and the contact areas between solid particles. In this study, the thermal conductivity of two-phase soil systems was determined under reduced and increased <span class="hlt">air</span> <span class="hlt">pressures</span>. The thermal separation of soil particles, i.e., the characteristic dimension of the pore space (d), was then estimated based on the relationship between soil thermal conductivity and <span class="hlt">air</span> <span class="hlt">pressure</span>. Results showed that under both reduced and increased <span class="hlt">air</span> <span class="hlt">pressures</span>, d estimations were significantly larger than the geometrical mean separation of solid particles (D), which suggested that conductive heat transfer through solid particles dominated heat transfer in dry soils. The increased <span class="hlt">air</span> <span class="hlt">pressure</span> approach gave d values lower than that of the reduced <span class="hlt">air</span> <span class="hlt">pressure</span> method. With increasing <span class="hlt">air</span> <span class="hlt">pressure</span>, more collisions between gas molecules and solid surface occurred in micro-pores and intra-aggregate pores due to the reduction of mean free path of <span class="hlt">air</span> molecules. Compared to the reduced <span class="hlt">air</span> <span class="hlt">pressure</span> approach, the increased <span class="hlt">air</span> <span class="hlt">pressure</span> approach expressed more micro-pore structure attributes in heat transfer. We concluded that measuring thermal conductivity under increased <span class="hlt">air</span> <span class="hlt">pressure</span> procedures gave better-quality d values, and improved soil micro-pore structure estimation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1174722','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/1174722"><span><span class="hlt">Pressurized</span> solid oxide fuel cell integral <span class="hlt">air</span> accumular containment</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Gillett, James E.; Zafred, Paolo R.; Basel, Richard A.</p> <p>2004-02-10</p> <p>A fuel cell generator apparatus contains at least one fuel cell subassembly module in a module housing, where the housing is surrounded by a <span class="hlt">pressure</span> vessel such that there is an <span class="hlt">air</span> accumulator space, where the apparatus is associated with an <span class="hlt">air</span> compressor of a turbine/generator/<span class="hlt">air</span> compressor system, where <span class="hlt">pressurized</span> <span class="hlt">air</span> from the compressor passes into the space and occupies the space and then flows to the fuel cells in the subassembly module, where the <span class="hlt">air</span> accumulation space provides an accumulator to control any unreacted fuel gas that might flow from the module.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130009025','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130009025"><span><span class="hlt">Pressure</span>-Sensitive Paints Advance Rotorcraft Design Testing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>2013-01-01</p> <p>The rotors of certain helicopters can spin at speeds as high as 500 revolutions per minute. As the blades slice through the <span class="hlt">air</span>, they flex, moving into the <span class="hlt">wind</span> and back out, experiencing <span class="hlt">pressure</span> changes on the order of thousands of times a second and even higher. All of this makes acquiring a true understanding of rotorcraft aerodynamics a difficult task. A traditional means of acquiring aerodynamic data is to conduct <span class="hlt">wind</span> tunnel tests using a vehicle model outfitted with <span class="hlt">pressure</span> taps and other sensors. These sensors add significant costs to <span class="hlt">wind</span> tunnel testing while only providing measurements at discrete locations on the model's surface. In addition, standard sensor solutions do not work for pulling data from a rotor in motion. "Typical static <span class="hlt">pressure</span> instrumentation can't handle that," explains Neal Watkins, electronics engineer in Langley Research Center s Advanced Sensing and Optical Measurement Branch. "There are dynamic <span class="hlt">pressure</span> taps, but your costs go up by a factor of five to ten if you use those. In addition, recovery of the <span class="hlt">pressure</span> tap readings is accomplished through slip rings, which allow only a limited amount of sensors and can require significant maintenance throughout a typical rotor test." One alternative to sensor-based <span class="hlt">wind</span> tunnel testing is <span class="hlt">pressure</span> sensitive paint (PSP). A coating of a specialized paint containing luminescent material is applied to the model. When exposed to an LED or laser light source, the material glows. The glowing material tends to be reactive to oxygen, explains Watkins, which causes the glow to diminish. The more oxygen that is present (or the more <span class="hlt">air</span> present, since oxygen exists in a fixed proportion in <span class="hlt">air</span>), the less the painted surface glows. Imaged with a camera, the areas experiencing greater <span class="hlt">air</span> <span class="hlt">pressure</span> show up darker than areas of less <span class="hlt">pressure</span>. "The paint allows for a global <span class="hlt">pressure</span> map as opposed to specific points," says Watkins. With PSP, each pixel recorded by the camera becomes an optical <span class="hlt">pressure</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19750047374&hterms=oil+drilling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Doil%2Bdrilling','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19750047374&hterms=oil+drilling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Doil%2Bdrilling"><span>Underground storage systems for high-<span class="hlt">pressure</span> <span class="hlt">air</span> and gases</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Beam, B. H.; Giovannetti, A.</p> <p>1975-01-01</p> <p>This paper is a discussion of the safety and cost of underground high-<span class="hlt">pressure</span> <span class="hlt">air</span> and gas storage systems based on recent experience with a high-<span class="hlt">pressure</span> <span class="hlt">air</span> system installed at Moffett Field, California. The system described used threaded and coupled oil well casings installed vertically to a depth of 1200 ft. Maximum <span class="hlt">pressure</span> was 3000 psi and capacity was 500,000 lb of <span class="hlt">air</span>. A failure mode analysis is presented, and it is shown that underground storage offers advantages in avoiding catastrophic consequences from <span class="hlt">pressure</span> vessel failure. Certain problems such as corrosion, fatigue, and electrolysis are discussed in terms of the economic life of such vessels. A cost analysis shows that where favorable drilling conditions exist, the cost of underground high-<span class="hlt">pressure</span> storage is approximately one-quarter that of equivalent aboveground storage.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110004016','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110004016"><span>Thermal and <span class="hlt">Pressure</span> Characterization of a <span class="hlt">Wind</span> Tunnel Force Balance Using the Single Vector System. Experimental Design and Analysis Approach to Model <span class="hlt">Pressure</span> and Temperature Effects in Hypersonic <span class="hlt">Wind</span> Tunnel Research</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lynn, Keith C.; Commo, Sean A.; Johnson, Thomas H.; Parker, Peter A,</p> <p>2011-01-01</p> <p><span class="hlt">Wind</span> tunnel research at NASA Langley Research Center s 31-inch Mach 10 hypersonic facility utilized a 5-component force balance, which provided a <span class="hlt">pressurized</span> flow-thru capability to the test article. The goal of the research was to determine the interaction effects between the free-stream flow and the exit flow from the reaction control system on the Mars Science Laboratory aeroshell during planetary entry. In the <span class="hlt">wind</span> tunnel, the balance was exposed to aerodynamic forces and moments, steady-state and transient thermal gradients, and various internal balance cavity <span class="hlt">pressures</span>. Historically, these effects on force measurement accuracy have not been fully characterized due to limitations in the calibration apparatus. A statistically designed experiment was developed to adequately characterize the behavior of the balance over the expected <span class="hlt">wind</span> tunnel operating ranges (forces/moments, temperatures, and <span class="hlt">pressures</span>). The experimental design was based on a Taylor-series expansion in the seven factors for the mathematical models. Model inversion was required to calculate the aerodynamic forces and moments as a function of the strain-gage readings. Details regarding transducer on-board compensation techniques, experimental design development, mathematical modeling, and <span class="hlt">wind</span> tunnel data reduction are included in this paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4883286','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4883286"><span>Static and <span class="hlt">Wind</span>-on Performance of Polymer-Based <span class="hlt">Pressure</span>-Sensitive Paints Using Platinum and Ruthenium as the Luminophore</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lo, Kin Hing; Kontis, Konstantinos</p> <p>2016-01-01</p> <p>An experimental study has been conducted to investigate the static and <span class="hlt">wind</span>-on performance of two in-house-developed polymer-based <span class="hlt">pressure</span>-sensitive paints. Platinum tetrakis (pentafluorophenyl) porphyrin and tris-bathophenanthroline ruthenium II are used as the luminophores of these two polymer-based <span class="hlt">pressure</span>-sensitive paints. The <span class="hlt">pressure</span> and temperature sensitivity and the photo-degradation rate of these two <span class="hlt">pressure</span>-sensitive paints have been investigated. In the <span class="hlt">wind</span> tunnel test, it was observed that the normalised intensity ratio of both polymer-based <span class="hlt">pressure</span>-sensitive paints being studied decreases with increasing the number of <span class="hlt">wind</span> tunnel runs. The exact reason that leads to the occurrence of this phenomenon is unclear, but it is deduced that the luminophore is either removed or deactivated by the incoming flow during a <span class="hlt">wind</span> tunnel test. PMID:27128913</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/865745','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/865745"><span><span class="hlt">Air</span> separation with temperature and <span class="hlt">pressure</span> swing</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Cassano, Anthony A.</p> <p>1986-01-01</p> <p>A chemical absorbent <span class="hlt">air</span> separation process is set forth which uses a temperature swing absorption-desorption cycle in combination with a <span class="hlt">pressure</span> swing wherein the <span class="hlt">pressure</span> is elevated in the desorption stage of the process.</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://hdl.handle.net/2060/20140000733','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140000733"><span>Background <span class="hlt">Pressure</span> Profiles for Sonic Boom Vehicle Testing in the NASA Glenn 8- by 6-Foot Supersonic <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Castner, Raymond; Shaw, Stephen; Adamson, Eric; Simerly, Stephanie</p> <p>2013-01-01</p> <p>In an effort to identify test facilities that offer sonic boom measurement capabilities, an exploratory test program was initiated using <span class="hlt">wind</span> tunnels at NASA research centers. The subject of this report is the sonic boom <span class="hlt">pressure</span> rail data collected in the Glenn Research Center 8- by 6-Foot Supersonic <span class="hlt">Wind</span> Tunnel. The purpose is to summarize the lessons learned based on the test activity, specifically relating to collecting sonic boom data which has a large amount of spatial <span class="hlt">pressure</span> variation. The <span class="hlt">wind</span> tunnel background <span class="hlt">pressure</span> profiles are presented as well as data which demonstrated how both <span class="hlt">wind</span> tunnel Mach number and model support-strut position affected the <span class="hlt">wind</span> tunnel background <span class="hlt">pressure</span> profile. Techniques were developed to mitigate these effects and are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19818553','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19818553"><span>Temperature and <span class="hlt">pressure</span> influence on explosion <span class="hlt">pressures</span> of closed vessel propane-<span class="hlt">air</span> deflagrations.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razus, Domnina; Brinzea, Venera; Mitu, Maria; Oancea, Dumitru</p> <p>2010-02-15</p> <p>An experimental study on <span class="hlt">pressure</span> evolution during closed vessel explosions of propane-<span class="hlt">air</span> mixtures was performed, for systems with various initial concentrations and <span class="hlt">pressures</span> ([C(3)H(8)]=2.50-6.20 vol.%, p(0)=0.3-1.2 bar). The explosion <span class="hlt">pressures</span> and explosion times were measured in a spherical vessel (Phi=10 cm), at various initial temperatures (T(0)=298-423 K) and in a cylindrical vessel (Phi=10 cm; h=15 cm), at ambient initial temperature. The experimental values of explosion <span class="hlt">pressures</span> are examined against literature values and compared to adiabatic explosion <span class="hlt">pressures</span>, computed by assuming chemical equilibrium within the flame front. The influence of initial <span class="hlt">pressure</span>, initial temperature and fuel concentration on explosion <span class="hlt">pressures</span> and explosion times are discussed. At constant temperature and fuel/oxygen ratio, the explosion <span class="hlt">pressures</span> are linear functions of total initial <span class="hlt">pressure</span>, as reported for other fuel-<span class="hlt">air</span> mixtures. At constant initial <span class="hlt">pressure</span> and composition, both the measured and calculated (adiabatic) explosion <span class="hlt">pressures</span> are linear functions of reciprocal value of initial temperature. Such correlations are extremely useful for predicting the explosion <span class="hlt">pressures</span> of flammable mixtures at elevated temperatures and/or <span class="hlt">pressures</span>, when direct measurements are not available.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JPS...332..447H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JPS...332..447H"><span><span class="hlt">Pressurized</span> <span class="hlt">air</span> cathodes for enhanced stability and power generation by microbial fuel cells</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>He, Weihua; Yang, Wulin; Tian, Yushi; Zhu, Xiuping; Liu, Jia; Feng, Yujie; Logan, Bruce E.</p> <p>2016-11-01</p> <p>Large differences between the water and <span class="hlt">air</span> <span class="hlt">pressure</span> in microbial fuel cells (MFCs) can deform and damage cathodes. To avoid deformation, the cathode <span class="hlt">air</span> <span class="hlt">pressure</span> was controlled to balance <span class="hlt">pressure</span> differences between the <span class="hlt">air</span> and water. Raising the <span class="hlt">air</span> <span class="hlt">pressures</span> from 0 to 10 kPa at a set cathode potential of -0.3 V (versus Ag/AgCl) enhanced cathode performance by 17%, but <span class="hlt">pressures</span> ≥25 kPa decreased current and resulted in <span class="hlt">air</span> leakage into the solution. Matching the <span class="hlt">air</span> <span class="hlt">pressure</span> with the water <span class="hlt">pressure</span> avoided cathode deformation and improved performance. The maximum power density increased by 15%, from 1070 ± 20 to 1230 ± 70 mW m-2, with balanced <span class="hlt">air</span> and water <span class="hlt">pressures</span> of 10-25 kPa. Oxygen partial <span class="hlt">pressures</span> ≥12.5 kPa in the cathode compartment maintained the oxygen reduction rate to be within 92 ± 1% of that in ambient <span class="hlt">air</span>. The use of <span class="hlt">pressurized</span> <span class="hlt">air</span> flow through the cathode compartments can enable closer spacing of the cathodes compared to passive gas transfer systems, which could make the reactor design more compact. The energy cost of <span class="hlt">pressurizing</span> the cathodes was estimated to be smaller than the increase in power that resulted from the use of <span class="hlt">pressurized</span> cathodes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19238948','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19238948"><span><span class="hlt">Air</span> emissions due to <span class="hlt">wind</span> and solar power.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Katzenstein, Warren; Apt, Jay</p> <p>2009-01-15</p> <p>Renewables portfolio standards (RPS) encourage large-scale deployment of <span class="hlt">wind</span> and solar electric power. Their power output varies rapidly, even when several sites are added together. In many locations, natural gas generators are the lowest cost resource available to compensate for this variability, and must ramp up and down quickly to keep the grid stable, affecting their emissions of NOx and CO2. We model a <span class="hlt">wind</span> or solar photovoltaic plus gas system using measured 1-min time-resolved emissions and heat rate data from two types of natural gas generators, and power data from four <span class="hlt">wind</span> plants and one solar plant. Over a wide range of renewable penetration, we find CO2 emissions achieve approximately 80% of the emissions reductions expected if the power fluctuations caused no additional emissions. Using steam injection, gas generators achieve only 30-50% of expected NOx emissions reductions, and with dry control NOx emissions increase substantially. We quantify the interaction between state RPSs and NOx constraints, finding that states with substantial RPSs could see significant upward <span class="hlt">pressure</span> on NOx permit prices, if the gas turbines we modeled are representative of the plants used to mitigate <span class="hlt">wind</span> and solar power variability.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPS...364..280K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPS...364..280K"><span>Effects of oxygen partial <span class="hlt">pressure</span> on Li-<span class="hlt">air</span> battery performance</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwon, Hyuk Jae; Lee, Heung Chan; Ko, Jeongsik; Jung, In Sun; Lee, Hyun Chul; Lee, Hyunpyo; Kim, Mokwon; Lee, Dong Joon; Kim, Hyunjin; Kim, Tae Young; Im, Dongmin</p> <p>2017-10-01</p> <p>For application in electric vehicles (EVs), the Li-<span class="hlt">air</span> battery system needs an <span class="hlt">air</span> intake system to supply dry oxygen at controlled concentration and feeding rate as the cathode active material. To facilitate the design of such <span class="hlt">air</span> intake systems, we have investigated the effects of oxygen partial <span class="hlt">pressure</span> (≤1 atm) on the performance of the Li-<span class="hlt">air</span> cell, which has not been systematically examined. The amounts of consumed O2 and evolved CO2 from the Li-<span class="hlt">air</span> cell are measured with a custom in situ differential electrochemical gas chromatography-mass spectrometry (DEGC-MS). The amounts of consumed O2 suggest that the oxygen partial <span class="hlt">pressure</span> does not affect the reaction mechanism during discharge, and the two-electron reaction occurs under all test conditions. On the other hand, the charging behavior varies by the oxygen partial <span class="hlt">pressure</span>. The highest O2 evolution ratio is attained under 70% O2, along with the lowest CO2 evolution. The cell cycle life also peaks at 70% O2 condition. Overall, an oxygen partial <span class="hlt">pressure</span> of about 0.5-0.7 atm maximizes the Li-<span class="hlt">air</span> cell capacity and stability at 1 atm condition. The findings here indicate that the appropriate oxygen partial <span class="hlt">pressure</span> can be a key factor when developing practical Li-<span class="hlt">air</span> battery systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AIPC.1440..595R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AIPC.1440..595R"><span>Design and optimization of resistance wire electric heater for hypersonic <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rehman, Khurram; Malik, Afzaal M.; Khan, I. J.; Hassan, Jehangir</p> <p>2012-06-01</p> <p>The range of flow velocities of high speed <span class="hlt">wind</span> tunnels varies from Mach 1.0 to hypersonic order. In order to achieve such high speed flows, a high expansion nozzle is employed in the converging-diverging section of <span class="hlt">wind</span> tunnel nozzle. The <span class="hlt">air</span> for flow is compressed and stored in <span class="hlt">pressure</span> vessels at temperatures close to ambient conditions. The stored <span class="hlt">air</span> is dried and has minimum amount of moisture level. However, when this <span class="hlt">air</span> is expanded rapidly, its temperature drops significantly and liquefaction conditions can be encountered. <span class="hlt">Air</span> at near room temperature will liquefy due to expansion cooling at a flow velocity of more than Mach 4.0 in a <span class="hlt">wind</span> tunnel test section. Such liquefaction may not only be hazardous to the model under test and <span class="hlt">wind</span> tunnel structure; it may also affect the test results. In order to avoid liquefaction of <span class="hlt">air</span>, a pre-heater is employed in between the <span class="hlt">pressure</span> vessel and the converging-diverging section of a <span class="hlt">wind</span> tunnel. A number of techniques are being used for heating the flow in high speed <span class="hlt">wind</span> tunnels. Some of these include the electric arc heating, pebble bed electric heating, pebble bed natural gas fired heater, hydrogen burner heater, and the laser heater mechanisms. The most common are the pebble bed storage type heaters, which are inefficient, contaminating and time consuming. A well designed electrically heating system can be efficient, clean and simple in operation, for accelerating the <span class="hlt">wind</span> tunnel flow up to Mach 10. This paper presents CFD analysis of electric preheater for different configurations to optimize its design. This analysis has been done using ANSYS 12.1 FLUENT package while geometry and meshing was done in GAMBIT.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=cosmology&id=EJ1172650','ERIC'); return false;" href="https://eric.ed.gov/?q=cosmology&id=EJ1172650"><span>Toward an Educational Sphereology: <span class="hlt">Air</span>, <span class="hlt">Wind</span>, and Materialist Pedagogy</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Ford, Derek R.; Zhao, Weili</p> <p>2018-01-01</p> <p>It's not uncommon for people to make reference to atmospheres, including in relationship with educational spaces. In this article, we investigate educational atmospheres by turning to Western and Chinese literature on the <span class="hlt">air</span> and <span class="hlt">wind</span>. We pursue this task in three phases. First, we examine the Western literature to see the possible strings of…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790058385&hterms=1607&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3D%2526%25231607','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790058385&hterms=1607&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3D%2526%25231607"><span><span class="hlt">Wind</span> study for high altitude platform design</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Strganac, T. W.</p> <p>1979-01-01</p> <p>An analysis of upper <span class="hlt">air</span> <span class="hlt">winds</span> was performed to define the <span class="hlt">wind</span> environment at potential operating altitudes for high-altitude powered platform concepts. Expected <span class="hlt">wind</span> conditions of the contiguous United States, Pacific area (Alaska to Sea of Japan), and European area (Norwegian and Mediterranean Seas) were obtained using a representative network of sites selected based upon adequate high-altitude sampling, geographic dispersion, and observed upper <span class="hlt">wind</span> patterns. A data base of twenty plus years of rawinsonde gathered <span class="hlt">wind</span> information was used in the analysis. Annual variations from surface to 10 mb (approximately 31 km) <span class="hlt">pressure</span> altitude were investigated to encompass the practical operating range for the platform concepts. Parametric analysis for the United States and foreign areas was performed to provide a basis for vehicle system design tradeoffs. This analysis of <span class="hlt">wind</span> magnitudes indicates the feasibility of annual operation at a majority of sites and more selective seasonal operation for the extreme conditions between the <span class="hlt">pressure</span> altitudes of 100 to 25 mb based upon the assumed design speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011AtmEn..45.3352Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011AtmEn..45.3352Z"><span>Effect of real-time boundary <span class="hlt">wind</span> conditions on the <span class="hlt">air</span> flow and pollutant dispersion in an urban street canyon—Large eddy simulations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Yun-Wei; Gu, Zhao-Lin; Cheng, Yan; Lee, Shun-Cheng</p> <p>2011-07-01</p> <p><span class="hlt">Air</span> flow and pollutant dispersion characteristics in an urban street canyon are studied under the real-time boundary conditions. A new scheme for realizing real-time boundary conditions in simulations is proposed, to keep the upper boundary <span class="hlt">wind</span> conditions consistent with the measured time series of <span class="hlt">wind</span> data. The <span class="hlt">air</span> flow structure and its evolution under real-time boundary <span class="hlt">wind</span> conditions are simulated by using this new scheme. The induced effect of time series of ambient <span class="hlt">wind</span> conditions on the flow structures inside and above the street canyon is investigated. The flow shows an obvious intermittent feature in the street canyon and the flapping of the shear layer forms near the roof layer under real-time <span class="hlt">wind</span> conditions, resulting in the expansion or compression of the <span class="hlt">air</span> mass in the canyon. The simulations of pollutant dispersion show that the pollutants inside and above the street canyon are transported by different dispersion mechanisms, relying on the time series of <span class="hlt">air</span> flow structures. Large scale <span class="hlt">air</span> movements in the processes of the <span class="hlt">air</span> mass expansion or compression in the canyon exhibit obvious effects on pollutant dispersion. The simulations of pollutant dispersion also show that the transport of pollutants from the canyon to the upper <span class="hlt">air</span> flow is dominated by the shear layer turbulence near the roof level and the expansion or compression of the <span class="hlt">air</span> mass in street canyon under real-time boundary <span class="hlt">wind</span> conditions. Especially, the expansion of the <span class="hlt">air</span> mass, which features the large scale <span class="hlt">air</span> movement of the <span class="hlt">air</span> mass, makes more contribution to the pollutant dispersion in this study. Comparisons of simulated results under different boundary <span class="hlt">wind</span> conditions indicate that real-time boundary <span class="hlt">wind</span> conditions produces better condition for pollutant dispersion than the artificially-designed steady boundary <span class="hlt">wind</span> conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.A41D2318L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.A41D2318L"><span>A Method to Quantify the <span class="hlt">Wind</span> and Non-<span class="hlt">wind</span> Contribution to Year-to-year <span class="hlt">Air</span> Quality Variation and its Application in China</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>LI, Y.; Lau, A. K. H.; Wong, A.; Fung, J. C. H.</p> <p>2017-12-01</p> <p>Changes in emissions and <span class="hlt">wind</span> are often identified as the two dominant factors contributing to year-to-year variations in the concentration of primary pollutants. However, because changes in <span class="hlt">wind</span> and emissions are intertwined, it has been difficult to quantitatively differentiate their effects on <span class="hlt">air</span> quality directly from observed data. In particular, if the annual mean concentration of pollutants is higher than the previous year, it is difficult to identify whether the deterioration in <span class="hlt">air</span> quality is caused by <span class="hlt">wind</span> blowing from more polluted regions or an increase in contributing emissions. In this paper, based on <span class="hlt">wind</span> and pollution roses, we propose a method to differentiate the effects of <span class="hlt">wind</span> and non-<span class="hlt">wind</span> (e.g., emissions) changes using direct observation. An index (L) is first defined to quantify the validity of the linear decomposition. The method is then validated by idealized experiments, numerical experiments and a two-year observation dataset from an actual emissions control program. Finally, we demonstrate the proposed method by studying long-term PM10 variations in Hong Kong during 2000-2011. We find that for most of the period, the linear decomposition of the changes in annual PM10 is valid (up to 90% confidence) and is dominated by the change in non-<span class="hlt">wind</span> effects (e.g., emissions), whereas the average absolute effect from the <span class="hlt">wind</span> variability is about 20%. Sensitivity analyses also suggest that our method should work in any location as long as the observed <span class="hlt">wind</span> and pollution data have sufficient duration and resolution to resolve the corresponding <span class="hlt">wind</span> and pollution roses. The method is applied for estimating the control effectiveness of the intervention programs in the Shanghai Expo, the longest socioeconomic international event held in China. The results show that integrated effect of control policies taken for improving the <span class="hlt">air</span> quality in Shanghai are significantly effective for PM10 reduction and also effective for SO2 reduction, whereas the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3893195','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3893195"><span>Inverse Association between <span class="hlt">Air</span> <span class="hlt">Pressure</span> and Rheumatoid Arthritis Synovitis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Furu, Moritoshi; Nakabo, Shuichiro; Ohmura, Koichiro; Nakashima, Ran; Imura, Yoshitaka; Yukawa, Naoichiro; Yoshifuji, Hajime; Matsuda, Fumihiko; Ito, Hiromu; Fujii, Takao; Mimori, Tsuneyo</p> <p>2014-01-01</p> <p>Rheumatoid arthritis (RA) is a bone destructive autoimmune disease. Many patients with RA recognize fluctuations of their joint synovitis according to changes of <span class="hlt">air</span> <span class="hlt">pressure</span>, but the correlations between them have never been addressed in large-scale association studies. To address this point we recruited large-scale assessments of RA activity in a Japanese population, and performed an association analysis. Here, a total of 23,064 assessments of RA activity from 2,131 patients were obtained from the KURAMA (Kyoto University Rheumatoid Arthritis Management Alliance) database. Detailed correlations between <span class="hlt">air</span> <span class="hlt">pressure</span> and joint swelling or tenderness were analyzed separately for each of the 326 patients with more than 20 assessments to regulate intra-patient correlations. Association studies were also performed for seven consecutive days to identify the strongest correlations. Standardized multiple linear regression analysis was performed to evaluate independent influences from other meteorological factors. As a result, components of composite measures for RA disease activity revealed suggestive negative associations with <span class="hlt">air</span> <span class="hlt">pressure</span>. The 326 patients displayed significant negative mean correlations between <span class="hlt">air</span> <span class="hlt">pressure</span> and swellings or the sum of swellings and tenderness (p = 0.00068 and 0.00011, respectively). Among the seven consecutive days, the most significant mean negative correlations were observed for <span class="hlt">air</span> <span class="hlt">pressure</span> three days before evaluations of RA synovitis (p = 1.7×10−7, 0.00027, and 8.3×10−8, for swellings, tenderness and the sum of them, respectively). Standardized multiple linear regression analysis revealed these associations were independent from humidity and temperature. Our findings suggest that <span class="hlt">air</span> <span class="hlt">pressure</span> is inversely associated with synovitis in patients with RA. PMID:24454853</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110016348','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110016348"><span>Peak <span class="hlt">Wind</span> Forecasts for the Launch-Critical <span class="hlt">Wind</span> Towers on Kennedy Space Center/Cape Canaveral <span class="hlt">Air</span> Force Station, Phase IV</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crawford, Winifred</p> <p>2011-01-01</p> <p>This final report describes the development of a peak <span class="hlt">wind</span> forecast tool to assist forecasters in determining the probability of violating launch commit criteria (LCC) at Kennedy Space Center (KSC) and Cape Canaveral <span class="hlt">Air</span> Force Station (CCAFS). The peak <span class="hlt">winds</span> arc an important forecast clement for both the Space Shuttle and Expendable Launch Vehicle (ELV) programs. The LCC define specific peak <span class="hlt">wind</span> thresholds for each launch operation that cannot be exceeded in order to ensure the safety of the vehicle. The 45th Weather Squadron (45 WS) has found that peak <span class="hlt">winds</span> are a challenging parameter to forecast, particularly in the cool season months of October through April. Based on the importance of forecasting peak <span class="hlt">winds</span>, the 45 WS tasked the Applied Meteorology Unit (AMU) to update the statistics in the current peak-<span class="hlt">wind</span> forecast tool to assist in forecasting LCC violations. The tool includes onshore and offshore flow climatologies of the 5-minute mean and peak <span class="hlt">winds</span> and probability distributions of the peak <span class="hlt">winds</span> as a function of the 5-minute mean <span class="hlt">wind</span> speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3093244','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3093244"><span><span class="hlt">Air</span> <span class="hlt">Pressure</span> Responses to Sudden Vocal Tract <span class="hlt">Pressure</span> Bleeds During Production of Stop Consonants: New Evidence of Aeromechanical Regulation</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Zajac, David J.; Weissler, Mark C.</p> <p>2011-01-01</p> <p>Two studies were conducted to evaluate short-latency vocal tract <span class="hlt">air</span> <span class="hlt">pressure</span> responses to sudden <span class="hlt">pressure</span> bleeds during production of voiceless bilabial stop consonants. It was hypothesized that the occurrence of respiratory reflexes would be indicated by distinct patterns of responses as a function of bleed magnitude. In Study 1, 19 adults produced syllable trains of /pΛ/ using a mouthpiece coupled to a computer-controlled perturbator. The device randomly created bleed apertures that ranged from 0 to 40 mm2 during production of the 2nd or 4th syllable of an utterance. Although peak oral <span class="hlt">air</span> <span class="hlt">pressure</span> dropped in a linear manner across bleed apertures, it averaged 2 to 3 cm H2O at the largest bleed. While slope of oral <span class="hlt">pressure</span> also decreased in a linear trend, duration of the oral <span class="hlt">pressure</span> pulse remained relatively constant. The patterns suggest that respiratory reflexes, if present, have little effect on oral <span class="hlt">air</span> <span class="hlt">pressure</span> levels. In Study 2, both oral and subglottal <span class="hlt">air</span> <span class="hlt">pressure</span> responses were monitored in 2 adults while bleed apertures of 20 and 40 mm2 were randomly created. For 1 participant, peak oral <span class="hlt">air</span> <span class="hlt">pressure</span> dropped across bleed apertures, as in Study 1. Subglottal <span class="hlt">air</span> <span class="hlt">pressure</span> and slope, however, remained relatively stable. These patterns provide some support for the occurrence of respiratory reflexes to regulate subglottal <span class="hlt">air</span> <span class="hlt">pressure</span>. Overall, the studies indicate that the inherent physiologic processes of the respiratory system, which may involve reflexes, and passive aeromechanical resistance of the upper airway are capable of developing oral <span class="hlt">air</span> <span class="hlt">pressure</span> in the face of substantial <span class="hlt">pressure</span> bleeds. Implications for understanding speech production and the characteristics of individuals with velopharyngeal dysfunction are discussed. PMID:15324286</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110014594','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110014594"><span>Ocean <span class="hlt">Winds</span> and Turbulent <span class="hlt">Air</span>-Sea Fluxes Inferred From Remote Sensing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bourassa, Mark A.; Gille, Sarah T.; Jackson, Daren L.; Roberts, J. Brent; Wick, Gary A.</p> <p>2010-01-01</p> <p><span class="hlt">Air</span>-sea turbulent fluxes determine the exchange of momentum, heat, freshwater, and gas between the atmosphere and ocean. These exchange processes are critical to a broad range of research questions spanning length scales from meters to thousands of kilometers and time scales from hours to decades. Examples are discussed (section 2). The estimation of surface turbulent fluxes from satellite is challenging and fraught with considerable errors (section 3); however, recent developments in retrievals (section 3) will greatly reduce these errors. Goals for the future observing system are summarized in section 4. Surface fluxes are defined as the rate per unit area at which something (e.g., momentum, energy, moisture, or CO Z ) is transferred across the <span class="hlt">air</span>/sea interface. <span class="hlt">Wind</span>- and buoyancy-driven surface fluxes are called surface turbulent fluxes because the mixing and transport are due to turbulence. Examples of nonturbulent processes are radiative fluxes (e.g., solar radiation) and precipitation (Schmitt et al., 2010). Turbulent fluxes are strongly dependent on <span class="hlt">wind</span> speed; therefore, observations of <span class="hlt">wind</span> speed are critical for the calculation of all turbulent surface fluxes. <span class="hlt">Wind</span> stress, the vertical transport of horizontal momentum, also depends on <span class="hlt">wind</span> direction. Stress is very important for many ocean processes, including upper ocean currents (Dohan and Maximenko, 2010) and deep ocean currents (Lee et al., 2010). On short time scales, this horizontal transport is usually small compared to surface fluxes. For long-term processes, transport can be very important but again is usually small compared to surface fluxes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150003353','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150003353"><span>Method and Apparatus for Measuring Surface <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lin, Bing (Inventor); Hu, Yongxiang (Inventor)</p> <p>2014-01-01</p> <p>The present invention is directed to an apparatus and method for remotely measuring surface <span class="hlt">air</span> <span class="hlt">pressure</span>. In one embodiment, the method of the present invention utilizes the steps of transmitting a signal having multiple frequencies into the atmosphere, measuring the transmitted/reflected signal to determine the relative received power level of each frequency and then determining the surface <span class="hlt">air</span> <span class="hlt">pressure</span> based upon the attenuation of the transmitted frequencies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010093214','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010093214"><span><span class="hlt">Pressure</span> Probe Designs for Dynamic <span class="hlt">Pressure</span> Measurements in a Supersonic Flow Field. [conducted in the Glenn Supersonic <span class="hlt">Wind</span> Tunnel (SWT)</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</p> <p>2001-01-01</p> <p>A series of dynamic flow field <span class="hlt">pressure</span> probes were developed for use in large-scale supersonic <span class="hlt">wind</span> tunnels at NASA Glenn Research Center. These flow field probes include pitot, static, and five-hole conical <span class="hlt">pressure</span> probes that are capable of capturing fast acting flow field <span class="hlt">pressure</span> transients that occur on a millisecond time scale. The pitot and static probes can be used to determine local Mach number time histories during a transient event. The five-hole conical <span class="hlt">pressure</span> probes are used primarily to determine local flow angularity, but can also determine local Mach number. These probes were designed, developed, and tested at the NASA Glenn Research Center. They were also used in a NASA Glenn 10- by 10-Foot Supersonic <span class="hlt">Wind</span> Tunnel (SWT) test program where they successfully acquired flow field <span class="hlt">pressure</span> data in the vicinity of a propulsion system during an engine compressor stall and inlet unstart transient event. Details of the design, development, and subsequent use of these probes are discussed in this report.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23473519','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23473519"><span>[Effect of subglottic <span class="hlt">air</span> insufflation on subglottic <span class="hlt">pressure</span> during swallowing].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Clarett, M; Andreu, M F; Salvati, I G; Donnianni, M C; Montes, G S; Rodríguez, M G</p> <p>2014-04-01</p> <p>To determine whether there are differences between subglottic <span class="hlt">pressure</span> during swallowing with and without <span class="hlt">air</span> insufflation via a subglottic catheter in tracheostomized patients. A prospective, randomized cross-over study was made. Adult Intensive Care Units. Patients requiring mechanical ventilation and tracheostomy with a subglottic catheter, and with tolerance to deflation of the balloon and a speaking valve placed over the opening of the tracheostomy tube. Subglottic <span class="hlt">pressure</span> was measured during swallowing of a thickened solution with and without the delivery of airflow through the subglottic catheter. Subglottic <span class="hlt">pressure</span> during swallowing. Twelve out of 14 patients showed higher subglottic <span class="hlt">pressure</span> values during swallowing with <span class="hlt">air</span> insufflation. Two patients showed no differences between both conditions. Median (Med) values of subglottic <span class="hlt">pressure</span> for the first, second and third swallow were 5, 4 and 4.5 cmH2O (Med 4.5 cmH2O) without <span class="hlt">air</span> insufflation, and 8, 5.5 and 7.5 cmH2O (Med 5.5 cmH2O) with <span class="hlt">air</span> insufflation, respectively (Wilcoxon, Z=-3.078; p=.002). In a group of tracheostomized patients, <span class="hlt">air</span> insufflation via a subglottic catheter increased subglottic <span class="hlt">pressure</span> levels measured during swallowing. Copyright © 2012 Elsevier España, S.L. and SEMICYUC. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1170705','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1170705"><span>Define and Quantify the Physics of <span class="hlt">Air</span> Flow, <span class="hlt">Pressure</span> Drop and Aerosol Collection in Nuclear Grade HEPA Filters</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>Moore, Murray E.</p> <p></p> <p>Objective: Develop a set of peer-review and verified analytical methods to adjust HEPA filter performance to different flow rates, temperatures and altitudes. Experimental testing will measure HEPA filter flow rate, <span class="hlt">pressure</span> drop and efficiency to verify the analytical approach. Nuclear facilities utilize HEPA (High Efficiency Particulate <span class="hlt">Air</span>) filters to purify <span class="hlt">air</span> flow for workspace ventilation. However, the ASME AG-1 technical standard (Code on Nuclear <span class="hlt">Air</span> and Gas Treatment) does not adequately describe <span class="hlt">air</span> flow measurement units for HEPA filter systems. Specifically, the AG-1 standard does not differentiate between volumetric <span class="hlt">air</span> flow in ACFM (actual cubic feet per minute)compared to massmore » flow measured in SCFM (standard cubic feet per minute). More importantly, the AG-1 standard has an overall deficiency for using HEPA filter devices at different <span class="hlt">air</span> flow rates, temperatures, and altitudes. Technical Approach: The collection efficiency and <span class="hlt">pressure</span> drops of 18 different HEPA filters will be measured over a range of flow rates, temperatures and altitudes. The experimental results will be compared to analytical scoping calculations. Three manufacturers have allocated six HEPA filters each for this effort. The 18 filters will be tested at two different flow rates, two different temperatures and two different altitudes. The 36 total tests will be conducted at two different facilities: the ATI Test facilities (Baltimore MD) and the Los Alamos National Laboratory (Los Alamos NM). The Radiation Protection RP-SVS group at Los Alamos has an aerosol <span class="hlt">wind</span> tunnel that was originally designed to evaluate small <span class="hlt">air</span> samplers. In 2010, modifications were started to convert the <span class="hlt">wind</span> tunnel for HEPA filter testing. (Extensive changes were necessary for the required aerosol generators, HEPA test fixtures, temperature control devices and measurement capabilities.) To this date, none of these modification activities have been funded through a specific DOE or NNSA program</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20080014166&hterms=HTML&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DHTML','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20080014166&hterms=HTML&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DHTML"><span>Simulation of the Impact of New <span class="hlt">Air</span>-Based Ocean Surface <span class="hlt">Wind</span> Measurements on H*<span class="hlt">Wind</span> Analyses</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, Timothy; Atlas, Robert; Black, Peter; Case, Jonathan; Chen, Shuyi; Hood, Robbie; Jones, Linwood; Ruff, Chris; Uhlhorn, Eric</p> <p>2008-01-01</p> <p>The H'<span class="hlt">Wind</span> analysis, a product of the Hurricane Research Division of NOAA's Atlantic Oceanographic and Meteorological Laboratory, brings together <span class="hlt">wind</span> measurements from a variety of observation platforms into an objective analysis of the distribution of <span class="hlt">wind</span> speeds in a tropical cyclone. This product is designed to improve understanding of the extent and strength of the <span class="hlt">wind</span> field, and to improve the assessment of hurricane intensity. See http://www.aoml.noaa.gov/hrd/data sub/<span class="hlt">wind</span>.html. The Hurricane Imaging Radiometer (HIRad) is a new airborne microwave remote sensor for hurricane observations that is currently under development by NASA Marshall Space Flight Center, NOAA Hurricane Research Division, the University of Central Florida and the University of Michigan. HIRad is being designed to enhance the real-time airborne ocean surface <span class="hlt">winds</span> observation capabilities of NOAA and USAF Weather Squadron hurricane hunter aircraft using the operational airborne Stepped Frequency Microwave Radiometer (SFMR). Unlike SFMR, which measures <span class="hlt">wind</span> speed and rain rate along the ground track directly beneath the aircraft, HIRad will provide images of the surface <span class="hlt">wind</span> and rain field over a wide swath (approx. 3 x the aircraft altitude). The instrument is described in a paper presented to the Hurricanes and Tropical Meteorology Symposium. The present paper describes a set of Observing System Simulation Experiments (OSSEs) in which measurements from the new instrument as well as those from existing instruments (<span class="hlt">air</span>, surface, and space-based) are simulated from the output of a numerical model from the University of Miami and those results are used to construct H*<span class="hlt">Wind</span> analyses. Evaluations will be presented on the impact of the HIRad instrument on H'<span class="hlt">Wind</span> analyses, both in terms of adding it to the full suite of current measurements, as well as using it to replace instrument(s) that may not be functioning at the future tame the HIRad instrument is implemented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ACPD...1313285B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ACPD...1313285B"><span><span class="hlt">Air</span>/sea DMS gas transfer in the North Atlantic: evidence for limited interfacial gas exchange at high <span class="hlt">wind</span> speed</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bell, T. G.; De Bruyn, W.; Miller, S. D.; Ward, B.; Christensen, K.; Saltzman, E. S.</p> <p>2013-05-01</p> <p>Shipboard measurements of eddy covariance DMS <span class="hlt">air</span>/sea fluxes and seawater concentration were carried out in the North Atlantic bloom region in June/July 2011. Gas transfer coefficients (k660) show a linear dependence on mean horizontal <span class="hlt">wind</span> speed at <span class="hlt">wind</span> speeds up to 11 m s-1. At higher <span class="hlt">wind</span> speeds the relationship between k660 and <span class="hlt">wind</span> speed weakens. At high <span class="hlt">winds</span>, measured DMS fluxes were lower than predicted based on the linear relationship between <span class="hlt">wind</span> speed and interfacial stress extrapolated from low to intermediate <span class="hlt">wind</span> speeds. In contrast, the transfer coefficient for sensible heat did not exhibit this effect. The apparent suppression of <span class="hlt">air</span>/sea gas flux at higher <span class="hlt">wind</span> speeds appears to be related to sea state, as determined from shipboard wave measurements. These observations are consistent with the idea that long waves suppress near surface water side turbulence, and decrease interfacial gas transfer. This effect may be more easily observed for DMS than for less soluble gases, such as CO2, because the <span class="hlt">air</span>/sea exchange of DMS is controlled by interfacial rather than bubble-mediated gas transfer under high <span class="hlt">wind</span> speed conditions.</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('https://www.ncbi.nlm.nih.gov/pubmed/21233664','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21233664"><span>Hospital-acquired <span class="hlt">pressure</span> ulcer prevalence--evaluating low-<span class="hlt">air</span>-loss beds.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Johnson, Jane; Peterson, Darcie; Campbell, Betty; Richardson, Regina; Rutledge, Dana</p> <p>2011-01-01</p> <p>Higher-category <span class="hlt">pressure</span> redistribution mattresses are considered a critical component of a <span class="hlt">pressure</span> ulcer prevention program, but few studies have quantified the impact of specific preventive measures on the incidence or prevalence of hospital-acquired <span class="hlt">pressure</span> ulcers (HAPUs). Therefore, this study was undertaken to determine the impact of low-<span class="hlt">air</span>-loss beds on HAPU prevalence. This prospective, comparative cohort study monitored the prevalence of HAPU at our hospital and compared rates of matched medical-surgical units with and without low-<span class="hlt">air</span>-loss beds. Units without low-<span class="hlt">air</span>-loss beds used a variety of alternative <span class="hlt">pressure</span> redistribution devices for patients deemed at risk for <span class="hlt">pressure</span> ulceration. The prevalence of HAPU was operationally defined as the number of patients with HAPUs divided by numbers of patients observed. The prevalence of HAPU over 3 quarters in 2008 ranged from 1.0% to 3.3% (overall rate 2.4%). Eighty-three percent of patients with HAPUs were cared for on low-<span class="hlt">air</span>-loss beds. Of 12 patients with 16 HAPUs during this time, 75% were aged 70 years or older and 25% were managed in critical care units. Over half of patients who developed HAPUs had been hospitalized for 20 days or more. Half of the patients with HAPUs were scored as no-low risk on the Braden Scale.On the paired medical-surgical units, no statistically significant differences were found when patients with low-<span class="hlt">air</span>-loss beds were compared to standard hospital mattresses supplemented by a variety of <span class="hlt">pressure</span> redistribution devices. Seven of 11 HAPUs (63%) occurred in patients placed on low-<span class="hlt">air</span>-loss beds. The prevalence of HAPU in patients placed on low-<span class="hlt">air</span>-loss beds was no different from patients placed on standard hospital mattresses supplemented by a variety of <span class="hlt">pressure</span> redistribution devices. Further research is needed to determine the impact of specific strategies on prevention of HAPU.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3656658','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3656658"><span>Ambient <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> changes during pregnancy</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lee, Pei-Chen; Talbott, Evelyn O.; Roberts, James M.; Catov, Janet M.; Bilonick, Richard A.; Stone, Roslyn A.; Sharma, Ravi K.; Ritz, Beate</p> <p>2013-01-01</p> <p>Background Maternal exposure to ambient <span class="hlt">air</span> pollution has been associated with adverse birth outcomes such as preterm delivery. However, only one study to date has linked <span class="hlt">air</span> pollution to blood <span class="hlt">pressure</span> changes during pregnancy, a period of dramatic cardiovascular function changes. Objectives We examined whether maternal exposures to criteria <span class="hlt">air</span> pollutants, including particles of less than 10 µm (PM10) or 2.5 µm diameter (PM2.5), carbon monoxide (CO), nitrogen dioxide (NO2), sulfur dioxide (SO2), and ozone (O3), in each trimester of pregnancy are associated with magnitude of rise of blood <span class="hlt">pressure</span> between the first 20 weeks of gestation and late pregnancy in a prospectively followed cohort of 1684 pregnant women in Allegheny County, PA. Methods <span class="hlt">Air</span> pollution measures for maternal ZIP code areas were derived using Kriging interpolation. Using logistic regression analysis, we evaluated the associations between <span class="hlt">air</span> pollution exposures and blood <span class="hlt">pressure</span> changes between the first 20 weeks of gestation and late pregnancy. Results First trimester PM10 and ozone exposures were associated with blood <span class="hlt">pressure</span> changes between the first 20 weeks of gestation and late pregnancy, most strongly in non-smokers. Per interquartile increases in first trimester PM10 and O3 concentrations were associated with mean increases in systolic blood <span class="hlt">pressure</span> of 1.88 mmHg (95% CI = 0.84 to 2.93) and 1.84 (95% CI = 1.05 to 4.63), respectively, and in diastolic blood <span class="hlt">pressure</span> of 0.63 mmHg (95% CI= −0.50 to 1.76) and 1.13 (95% CI= −0.46 to 2.71) in non-smokers. Conclusions Our novel finding suggests that first trimester PM10 and O3 <span class="hlt">air</span> pollution exposures increase blood <span class="hlt">pressure</span> in the later stages of pregnancy. These changes may play a role in mediating the relationships between <span class="hlt">air</span> pollution and adverse birth outcomes. PMID:22835955</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940025146','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940025146"><span>Laminar Flow Supersonic <span class="hlt">Wind</span> Tunnel primary <span class="hlt">air</span> injector</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Smith, Brooke Edward</p> <p>1993-01-01</p> <p>This paper describes the requirements, design, and prototype testing of the flex-section and hinge seals for the Laminar Flow Supersonic <span class="hlt">Wind</span> Tunnel Primary Injector. The supersonic atmospheric primary injector operates between Mach 1.8 and Mach 2.2 with mass-flow rates of 62 to 128 lbm/s providing the necessary <span class="hlt">pressure</span> reduction to operate the tunnel in the desired Reynolds number (Re) range.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009PhDT.......168G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009PhDT.......168G"><span><span class="hlt">Pressure</span> distribution on the roof of a model low-rise building tested in a boundary layer <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Goliber, Matthew Robert</p> <p></p> <p>With three of the largest metropolitan areas in the United States along the Gulf coast (Houston, Tampa, and New Orleans), residential populations ever increasing due to the subtropical climate, and insured land value along the coast from Texas to the Florida panhandle greater than $500 billion, hurricane related knowledge is as important now as ever before. This thesis focuses on model low-rise building <span class="hlt">wind</span> tunnel tests done in connection with full-scale low-rise building tests. Mainly, <span class="hlt">pressure</span> data collection equipment and methods used in the <span class="hlt">wind</span> tunnel are compared to <span class="hlt">pressure</span> data collection equipment and methods used in the field. Although the focus of this report is on the testing of models in the <span class="hlt">wind</span> tunnel, the low-rise building in the field is located in Pensacola, Florida. It has a wall length of 48 feet, a width of 32 feet, a height of 10 feet, and a gable roof with a pitch of 1:3 and 68 <span class="hlt">pressure</span> ports strategically placed on the surface of the roof. Built by Forest Products Laboratory (FPL) in 2002, the importance of the test structure has been realized as it has been subjected to numerous hurricanes. In fact, the validity of the field data is so important that the following thesis was necessary. The first model tested in the Bill James <span class="hlt">Wind</span> Tunnel for this research was a rectangular box. It was through the testing of this box that much of the basic <span class="hlt">wind</span> tunnel and <span class="hlt">pressure</span> data collection knowledge was gathered. Knowledge gained from Model 1 tests was as basic as how to: mount <span class="hlt">pressure</span> tubes on a model, use a <span class="hlt">pressure</span> transducer, operate the <span class="hlt">wind</span> tunnel, utilize the pitot tube and reference <span class="hlt">pressure</span>, and measure <span class="hlt">wind</span> velocity. Model 1 tests also showed the importance of precise construction to produce precise <span class="hlt">pressure</span> coefficients. Model 2 was tested in the AABL <span class="hlt">Wind</span> Tunnel at Iowa State University. This second model was a 22 inch cube which contained a total of 11 rows of <span class="hlt">pressure</span> ports on its front and top faces. The purpose of Model 2 was to</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..307a2057C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..307a2057C"><span>The Influence of Shaping <span class="hlt">Air</span> <span class="hlt">Pressure</span> of Pneumatic Spray Gun</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Wenzhuo; Chen, Yan; Pan, Haiwei; Zhang, Weiming; Li, Bo</p> <p>2018-02-01</p> <p>The shaping <span class="hlt">air</span> <span class="hlt">pressure</span> is a very important parameter in the application of pneumatic spray gun, and studying its influence on spray flow field and film thickness distribution has practical values. In this paper, Euler-Lagrangian method is adopted to describe the two-phase spray flow of pneumatic painting process, and the <span class="hlt">air</span> flow fields, spray patterns and dynamic film thickness distributions were obtained with the help of the computational fluid dynamics code—ANSYS Fluent. Results show that with the increase of the shaping <span class="hlt">air</span> <span class="hlt">pressure</span>, the <span class="hlt">air</span> phase flow field spreads in the plane perpendicular to the shaping <span class="hlt">air</span> hole plane, the spray pattern becomes narrower and flatter, and the width of the dynamic film increases with the reduced maximum value of the film thickness. But the film thickness distribution seems to change little with the shaping <span class="hlt">air</span> <span class="hlt">pressure</span> decreasing from 0.6bar to 0.9bar.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19790012912','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19790012912"><span><span class="hlt">Wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wilson, E. M. (Inventor)</p> <p>1969-01-01</p> <p>A supersonic <span class="hlt">wind</span> <span class="hlt">wind</span> tunnel is described for testing several <span class="hlt">air</span> foils mounted in a row. A test section of a <span class="hlt">wind</span> tunnel contains means for mounting <span class="hlt">air</span> foil sections in a row, means for rotating each section about an axis so that the angle of attack of each section changes with the other sections, and means for rotating the row with respect to the <span class="hlt">air</span> stream so that the row forms an oblique angle with the <span class="hlt">air</span> stream.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009AIPC.1159...11A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009AIPC.1159...11A"><span>Integration of <span class="hlt">Wind</span> Turbines with Compressed <span class="hlt">Air</span> Energy Storage</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Arsie, I.; Marano, V.; Rizzo, G.; Moran, M.</p> <p>2009-08-01</p> <p>Some of the major limitations of renewable energy sources are represented by their low power density and intermittent nature, largely depending upon local site and unpredictable weather conditions. These problems concur to increase the unit costs of <span class="hlt">wind</span> power, so limiting their diffusion. By coupling storage systems with a <span class="hlt">wind</span> farm, some of the major limitations of <span class="hlt">wind</span> power, such as a low power density and an unpredictable nature, can be overcome. After an overview on storage systems, the Compressed <span class="hlt">Air</span> Energy Storage (CAES) is analyzed, and the state of art on such systems is discussed. A Matlab/Simulink model of a hybrid power plant consisting of a <span class="hlt">wind</span> farm coupled with CAES is then presented. The model has been successfully validated starting from the operating data of the McIntosh CAES Plant in Alabama. Time-series neural network-based <span class="hlt">wind</span> speed forecasting are employed to determine the optimal daily operation strategy for the storage system. A detailed economic analysis has been carried out: investment and maintenance costs are estimated based on literature data, while operational costs and revenues are calculated according to energy market prices. As shown in the paper, the knowledge of the expected available energy is a key factor to optimize the management strategies of the proposed hybrid power plant, allowing to obtain environmental and economic benefits.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=temperature+AND+influence+AND+HA&pg=2&id=EJ726716','ERIC'); return false;" href="https://eric.ed.gov/?q=temperature+AND+influence+AND+HA&pg=2&id=EJ726716"><span>The Effect of Venue and <span class="hlt">Wind</span> on the Distance of a Hammer Throw</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Hunter, Iain</p> <p>2005-01-01</p> <p>In track and field, gravity and <span class="hlt">air</span> resistance act on the hammer after it has been released. Both of these forces depend on altitude and latitude. In addition, <span class="hlt">air</span> resistance also depends on <span class="hlt">wind</span>, temperature, humidity, and barometric <span class="hlt">pressure</span>. Often, <span class="hlt">air</span> resistance and varying gravity throughout the earth are not considered when throwing…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860009863','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860009863"><span><span class="hlt">Pressure</span> distributions obtained on a 0.10-scale model of the Space Shuttle Orbiter's forebody in the Ames Unitary Plan <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Siemers, P. M., III; Henry, M. W.</p> <p>1986-01-01</p> <p><span class="hlt">Pressure</span> distribution test data obtained on a 0.10-scale model of the forward fuselage of the Space Shuttle Orbiter are presented without analysis. The tests were completed in the Ames Unitary <span class="hlt">Wind</span> Tunnel (UPWT). The UPWT tests were conducted in two different test sections operating in the continuous mode, the 8 x 7 feet and 9 x 7 feet test sections. Each test section has its own Mach number range, 1.6 to 2.5 and 2.5 to 3.5 for the 9 x 7 feet and 8 x 7 feet test section, respectively. The test Reynolds number ranged from 1.6 to 2.5 x 10 to the 6th power ft and 0.6 to 2.0 x 10 to the 6th power ft, respectively. The tests were conducted in support of the development of the Shuttle Entry <span class="hlt">Air</span> Data System (SEADS). In addition to modeling the 20 SEADS orifices, the <span class="hlt">wind</span>-tunnel model was also instrumented with orifices to match Development Flight Instrumentation (DFI) port locations that existed on the Space Shuttle Columbia (OV-102) during the Orbiter Flight test program. This DFI simulation has provided a means for comparisons between reentry flight <span class="hlt">pressure</span> data and <span class="hlt">wind</span>-tunnel and computational data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19780023720','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19780023720"><span>Analysis of vector <span class="hlt">wind</span> change with respect to time for Vandenberg <span class="hlt">Air</span> Force Base, California</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Adelfang, S. I.</p> <p>1978-01-01</p> <p>A statistical analysis of the temporal variability of <span class="hlt">wind</span> vectors at 1 km altitude intervals from 0 to 27 km altitude taken from a 10-year data sample of twice-daily rawinsode <span class="hlt">wind</span> measurements over Vandenberg <span class="hlt">Air</span> Force Base, California is presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17079636','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17079636"><span>Compressed <span class="hlt">air</span> injection technique to standardize block injection <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tsui, Ban C H; Li, Lisa X Y; Pillay, Jennifer J</p> <p>2006-11-01</p> <p>Presently, no standardized technique exists to monitor injection <span class="hlt">pressures</span> during peripheral nerve blocks. Our objective was to determine if a compressed <span class="hlt">air</span> injection technique, using an in vitro model based on Boyle's law and typical regional anesthesia equipment, could consistently maintain injection <span class="hlt">pressures</span> below a 1293 mmHg level associated with clinically significant nerve injury. Injection <span class="hlt">pressures</span> for 20 and 30 mL syringes with various needle sizes (18G, 20G, 21G, 22G, and 24G) were measured in a closed system. A set volume of <span class="hlt">air</span> was aspirated into a saline-filled syringe and then compressed and maintained at various percentages while <span class="hlt">pressure</span> was measured. The needle was inserted into the injection port of a <span class="hlt">pressure</span> sensor, which had attached extension tubing with an injection plug clamped "off". Using linear regression with all data points, the <span class="hlt">pressure</span> value and 99% confidence interval (CI) at 50% <span class="hlt">air</span> compression was estimated. The linearity of Boyle's law was demonstrated with a high correlation, r = 0.99, and a slope of 0.984 (99% CI: 0.967-1.001). The net <span class="hlt">pressure</span> generated at 50% compression was estimated as 744.8 mmHg, with the 99% CI between 729.6 and 760.0 mmHg. The various syringe/needle combinations had similar results. By creating and maintaining syringe <span class="hlt">air</span> compression at 50% or less, injection <span class="hlt">pressures</span> will be substantially below the 1293 mmHg threshold considered to be an associated risk factor for clinically significant nerve injury. This technique may allow simple, real-time and objective monitoring during local anesthetic injections while inherently reducing injection speed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=human+AND+body+AND+ratios&pg=2&id=EJ1015638','ERIC'); return false;" href="https://eric.ed.gov/?q=human+AND+body+AND+ratios&pg=2&id=EJ1015638"><span>Tongue-Palate Contact <span class="hlt">Pressure</span>, Oral <span class="hlt">Air</span> <span class="hlt">Pressure</span>, and Acoustics of Clear Speech</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Searl, Jeff; Evitts, Paul M.</p> <p>2013-01-01</p> <p>Purpose: The authors compared articulatory contact <span class="hlt">pressure</span> (ACP), oral <span class="hlt">air</span> <span class="hlt">pressure</span> (Po), and speech acoustics for conversational versus clear speech. They also assessed the relationship of these measures to listener perception. Method: Twelve adults with normal speech produced monosyllables in a phrase using conversational and clear speech.…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25570740','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25570740"><span>An alternating <span class="hlt">pressure</span> sequence proposal for an <span class="hlt">air</span>-cell cushion for preventing <span class="hlt">pressure</span> ulcers.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Arias, Sandra; Cardiel, Eladio; Rogeli, Pablo; Mori, Taketoshi; Nakagami, Gojiro; Noguchi, Hiroshi; Sanada, Hiromi</p> <p>2014-01-01</p> <p>The distribution and release of <span class="hlt">pressure</span> on ischial regions are two important parameters for evaluating the effectiveness of a cushion; especially the release of <span class="hlt">pressure</span> over time on ischial tuberosities, which is significant for preventing <span class="hlt">pressure</span> ulcers. The aim of this work is to evaluate the effect on interface <span class="hlt">pressure</span> through the application of a proposed alternating <span class="hlt">pressure</span> sequence for an <span class="hlt">air</span>-cell cushion. Six healthy volunteers were asked to sit on the <span class="hlt">air</span> cell cushion, in static and alternating modes, as well as on a typical foam cushion for 12 minutes. Interface <span class="hlt">pressure</span> was monitored with a matrix sensor system. Interface <span class="hlt">pressure</span> values on ischial tuberosities, user contact area and <span class="hlt">pressure</span> distribution were analyzed. Results showed that IP on IT tends to increase in both foam and static cushions, while in alternating cushion IP on IT tends to decrease. User contact area was significantly larger in alternating cushion than in static or foam cushions. Moreover, there is a better <span class="hlt">pressure</span> re-distribution with alternating cushion than with the other cushions. The goal of the alternating sequence is to redistribute <span class="hlt">pressure</span> and stimulate the ischial regions in order to promote blood flow and prevent <span class="hlt">pressure</span> occurring in wheelchair users.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018E%26ES..140a2125N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018E%26ES..140a2125N"><span><span class="hlt">Wind</span> load effects on high rise buildings in Peninsular Malaysia</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nizamani, Z.; Thang, K. C.; Haider, B.; Shariff, M.</p> <p>2018-04-01</p> <p><span class="hlt">Wind</span> is a randomly varying dynamic phenomenon composed of a multitude of eddies of varying sizes and rotational characteristics along a general stream of <span class="hlt">air</span> moving relative to the ground. These eddies give <span class="hlt">wind</span> its gustiness, creating fluctuation and results in a complex flow characteristics. The <span class="hlt">wind</span> vector at any point can be regarded as the sum of mean <span class="hlt">wind</span> vector and the fluctuation components. These components not only vary with height but also dependant on the approach terrain and topography. Prevailing <span class="hlt">wind</span> exerts <span class="hlt">pressure</span> onto the structural surfaces. The effects of <span class="hlt">wind</span> <span class="hlt">pressure</span> in the form of shear and bending moments are found to be a major problem in structural failure. This study aims to study the effects of <span class="hlt">wind</span> load on a fifteen-storey high rise building using EN 1991-1-4 code and MS1553:2002. The simulation results showed that by increasing the <span class="hlt">wind</span> speed, the storey resultant forces, namely storey shear and storey moment increases significantly. Furthermore, simulation results according to EN 1991-1-4 yield higher values compared to the simulation results according to MS1553:2002.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15487792','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15487792"><span>Passive <span class="hlt">air</span> sampling using semipermeable membrane devices at different <span class="hlt">wind</span>-speeds in situ calibrated by performance reference compounds.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Söderström, Hanna S; Bergqvist, Per-Anders</p> <p>2004-09-15</p> <p>Semipermeable membrane devices (SPMDs) are passive samplers used to measure the vapor phase of organic pollutants in <span class="hlt">air</span>. This study tested whether extremely high <span class="hlt">wind</span>-speeds during a 21-day sampling increased the sampling rates of polycyclic aromatic hydrocarbons (PAHs) and polychlorinated biphenyls (PCBs), and whether the release of performance reference compounds (PRCs) was related to the uptakes at different <span class="hlt">wind</span>-speeds. Five samplers were deployed in an indoor, unheated, and dark <span class="hlt">wind</span> tunnel with different <span class="hlt">wind</span>-speeds at each site (6-50 m s(-1)). In addition, one sampler was deployed outside the <span class="hlt">wind</span> tunnel and one outside the building. To test whether a sampler, designed to reduce the <span class="hlt">wind</span>-speeds, decreased the uptake and release rates, each sampler in the <span class="hlt">wind</span> tunnel included two SPMDs positioned inside a protective device and one unprotected SPMD outside the device. The highest amounts of PAHs and PCBs were found in the SPMDs exposed to the assumed highest <span class="hlt">wind</span>-speeds. Thus, the SPMD sampling rates increased with increasing <span class="hlt">wind</span>-speeds, indicating that the uptake was largely controlled by the boundary layer at the membrane-<span class="hlt">air</span> interface. The coefficient of variance (introduced by the 21-day sampling and the chemical analysis) for the <span class="hlt">air</span> concentrations of three PAHs and three PCBs, calculated using the PRC data, was 28-46%. Thus, the PRCs had a high ability to predict site effects of <span class="hlt">wind</span> and assess the actual sampling situation. Comparison between protected and unprotected SPMDs showed that the sampler design reduced the <span class="hlt">wind</span>-speed inside the devices and thereby the uptake and release rates.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990071195','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990071195"><span>NASA Glenn 1-by 1-Foot Supersonic <span class="hlt">Wind</span> Tunnel User Manual</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Seablom, Kirk D.; Soeder, Ronald H.; Stark, David E.; Leone, John F. X.; Henry, Michael W.</p> <p>1999-01-01</p> <p>This manual describes the NASA Glenn Research Center's 1 - by 1 -Foot Supersonic <span class="hlt">Wind</span> Tunnel and provides information for customers who wish to conduct experiments in this facility. Tunnel performance envelopes of total <span class="hlt">pressure</span>, total temperature, and dynamic <span class="hlt">pressure</span> as a function of test section Mach number are presented. For each Mach number, maps are presented of Reynolds number per foot as a function of the total <span class="hlt">air</span> temperature at the test section inlet for constant total <span class="hlt">air</span> <span class="hlt">pressure</span> at the inlet. General support systems-such as the service <span class="hlt">air</span>, combustion <span class="hlt">air</span>, altitude exhaust system, auxiliary bleed system, model hydraulic system, schlieren system, model <span class="hlt">pressure</span>-sensitive paint, and laser sheet system are discussed. In addition, instrumentation and data processing, acquisition systems are described, pretest meeting formats and schedules are outlined, and customer responsibilities and personnel safety are addressed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24320194','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24320194"><span>Development and evaluation of a self-regulating alternating <span class="hlt">pressure</span> <span class="hlt">air</span> cushion.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nakagami, Gojiro; Sanada, Hiromi; Sugama, Junko</p> <p>2015-03-01</p> <p>To investigate the effect of alternating <span class="hlt">air</span> cells of a newly developed dynamic cushion on interface <span class="hlt">pressure</span> and tissue oxygenation levels. This cross-over experimental study included 19 healthy volunteers. The dynamic cushion used has an automatic self-regulating alternating <span class="hlt">pressure</span> <span class="hlt">air</span>-cell system with 35 small and four large <span class="hlt">air</span> cells for maintaining posture while seated. This cushion also has 17 bottoming-out detectors that automatically inflate the <span class="hlt">air</span> cells to release a high interface <span class="hlt">pressure</span>. To assess the effect of this alternating system, participants sat on the new cushion with an alternating system or static system for 30 min and then performed push-ups. The interface <span class="hlt">pressure</span> was monitored by <span class="hlt">pressure</span>-sensitive and conductive ink film sensors and tissue oxygenation levels were monitored by near-infrared spectroscopy. A reactive hyperaemia indicator was calculated using tissue oxygenation levels as an outcome measure. The peak interface <span class="hlt">pressure</span> was not significantly different between the groups. The reactive hyperaemia indicator was significantly higher in the static group than in the alternating group. An alternating system has beneficial effects on blood oxygenation levels without increasing interface <span class="hlt">pressure</span>. Therefore, our new cushion is promising for preventing <span class="hlt">pressure</span> ulcers with patients with limited ability to perform push-ups. Implications for Rehabilitation A dynamic cushion was developed, which consists of a uniquely-designed <span class="hlt">air</span>-cell layout, detectors for bottoming out, and an alternating system with multiple <span class="hlt">air</span>-cell lines. The alternating system did not increase interface <span class="hlt">pressure</span> and it significantly reduced reactive hyperaemia after 30 min of sitting in healthy volunteers. This cushion is a new option for individuals who require stable posture but have limitations in performing scheduled push-ups for prevention of <span class="hlt">pressure</span> ulcers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC24F..06D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC24F..06D"><span>Using Analog Ensemble to generate spatially downscaled probabilistic <span class="hlt">wind</span> power forecasts</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Delle Monache, L.; Shahriari, M.; Cervone, G.</p> <p>2017-12-01</p> <p>We use the Analog Ensemble (AnEn) method to generate probabilistic 80-m <span class="hlt">wind</span> power forecasts. We use data from the NCEP GFS ( 28 km resolution) and NCEP NAM (12 km resolution). We use forecasts data from NAM and GFS, and analysis data from NAM which enables us to: 1) use a lower-resolution model to create higher-resolution forecasts, and 2) use a higher-resolution model to create higher-resolution forecasts. The former essentially increases computing speed and the latter increases forecast accuracy. An aggregated model of the former can be compared against the latter to measure the accuracy of the AnEn spatial downscaling. The AnEn works by taking a deterministic future forecast and comparing it with past forecasts. The model searches for the best matching estimates within the past forecasts and selects the predictand value corresponding to these past forecasts as the ensemble prediction for the future forecast. Our study is based on predicting <span class="hlt">wind</span> speed and <span class="hlt">air</span> density at more than 13,000 grid points in the continental US. We run the AnEn model twice: 1) estimating 80-m <span class="hlt">wind</span> speed by using predictor variables such as temperature, <span class="hlt">pressure</span>, geopotential height, U-component and V-component of <span class="hlt">wind</span>, 2) estimating <span class="hlt">air</span> density by using predictors such as temperature, <span class="hlt">pressure</span>, and relative humidity. We use the <span class="hlt">air</span> density values to correct the standard <span class="hlt">wind</span> power curves for different values of <span class="hlt">air</span> density. The standard deviation of the ensemble members (i.e. ensemble spread) will be used as the degree of difficulty to predict <span class="hlt">wind</span> power at different locations. The value of the correlation coefficient between the ensemble spread and the forecast error determines the appropriateness of this measure. This measure is prominent for <span class="hlt">wind</span> farm developers as building <span class="hlt">wind</span> farms in regions with higher predictability will reduce the real-time risks of operating in the electricity markets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140005778','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140005778"><span>The Use of Red Green Blue <span class="hlt">Air</span> Mass Imagery to Investigate the Role of Stratospheric <span class="hlt">Air</span> in a Non-convective <span class="hlt">Wind</span> Event</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Berndt, E. B.; Zavodsky, B. T.; Jedlovec, G. J.; Molthan, A. L.</p> <p>2013-01-01</p> <p>Non-convective <span class="hlt">wind</span> events commonly occur with passing extratropical cyclones and have significant societal and economic impacts. Since non-convective <span class="hlt">winds</span> often occur in the absence of specific phenomena such as a thunderstorm, tornado, or hurricane, the public are less likely to heed high <span class="hlt">wind</span> warnings and continue daily activities. Thus non-convective <span class="hlt">wind</span> events result in as many fatalities as straight line thunderstorm <span class="hlt">winds</span>. One physical explanation for non-convective <span class="hlt">winds</span> includes tropopause folds. Improved model representation of stratospheric <span class="hlt">air</span> and associated non-convective <span class="hlt">wind</span> events could improve non-convective <span class="hlt">wind</span> forecasts and associated warnings. In recent years, satellite data assimilation has improved skill in forecasting extratropical cyclones; however errors still remain in forecasting the position and strength of extratropical cyclones as well as the tropopause folding process. The goal of this study is to determine the impact of assimilating satellite temperature and moisture retrieved profiles from hyperspectral infrared (IR) sounders (i.e. Atmospheric Infrared Sounder (<span class="hlt">AIRS</span>), Cross-track Infrared and Microwave Sounding Suite (CrIMSS), and Infrared Atmospheric Sounding Interferometer (IASI)) on the model representation of the tropopause fold and an associated high <span class="hlt">wind</span> event that impacted the Northeast United States on 09 February 2013. Model simulations using the Advanced Research Weather Research and Forecasting Model (ARW) were conducted on a 12-km grid with cycled data assimilation mimicking the operational North American Model (NAM). The results from the satellite assimilation run are compared to a control experiment (without hyperspectral IR retrievals), Modern Era-Retrospective Analysis for Research and Applications (MERRA) reanalysis, and Rapid Refresh analyses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ACP....1311073B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ACP....1311073B"><span><span class="hlt">Air</span>-sea dimethylsulfide (DMS) gas transfer in the North Atlantic: evidence for limited interfacial gas exchange at high <span class="hlt">wind</span> speed</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bell, T. G.; De Bruyn, W.; Miller, S. D.; Ward, B.; Christensen, K.; Saltzman, E. S.</p> <p>2013-11-01</p> <p>Shipboard measurements of eddy covariance dimethylsulfide (DMS) <span class="hlt">air</span>-sea fluxes and seawater concentration were carried out in the North Atlantic bloom region in June/July 2011. Gas transfer coefficients (k660) show a linear dependence on mean horizontal <span class="hlt">wind</span> speed at <span class="hlt">wind</span> speeds up to 11 m s-1. At higher <span class="hlt">wind</span> speeds the relationship between k660 and <span class="hlt">wind</span> speed weakens. At high <span class="hlt">winds</span>, measured DMS fluxes were lower than predicted based on the linear relationship between <span class="hlt">wind</span> speed and interfacial stress extrapolated from low to intermediate <span class="hlt">wind</span> speeds. In contrast, the transfer coefficient for sensible heat did not exhibit this effect. The apparent suppression of <span class="hlt">air</span>-sea gas flux at higher <span class="hlt">wind</span> speeds appears to be related to sea state, as determined from shipboard wave measurements. These observations are consistent with the idea that long waves suppress near-surface water-side turbulence, and decrease interfacial gas transfer. This effect may be more easily observed for DMS than for less soluble gases, such as CO2, because the <span class="hlt">air</span>-sea exchange of DMS is controlled by interfacial rather than bubble-mediated gas transfer under high <span class="hlt">wind</span> speed conditions.</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('https://www.gpo.gov/fdsys/pkg/CFR-2012-title29-vol7/pdf/CFR-2012-title29-vol7-sec1915-172.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title29-vol7/pdf/CFR-2012-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... 29 Labor 7 2012-07-01 2012-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title29-vol7/pdf/CFR-2013-title29-vol7-sec1915-172.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title29-vol7/pdf/CFR-2013-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... 29 Labor 7 2013-07-01 2013-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title29-vol7/pdf/CFR-2014-title29-vol7-sec1915-172.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title29-vol7/pdf/CFR-2014-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... 29 Labor 7 2014-07-01 2014-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..19.6998W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..19.6998W"><span>Operational design and <span class="hlt">pressure</span> response of large-scale compressed <span class="hlt">air</span> energy storage in porous formations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Bo; Bauer, Sebastian</p> <p>2017-04-01</p> <p>With the rapid growth of energy production from intermittent renewable sources like <span class="hlt">wind</span> and solar power plants, large-scale energy storage options are required to compensate for fluctuating power generation on different time scales. Compressed <span class="hlt">air</span> energy storage (CAES) in porous formations is seen as a promising option for balancing short-term diurnal fluctuations. CAES is a power-to-power energy storage, which converts electricity to mechanical energy, i.e. highly <span class="hlt">pressurized</span> <span class="hlt">air</span>, and stores it in the subsurface. This study aims at designing the storage setup and quantifying the <span class="hlt">pressure</span> response of a large-scale CAES operation in a porous sandstone formation, thus assessing the feasibility of this storage option. For this, numerical modelling of a synthetic site and a synthetic operational cycle is applied. A hypothetic CAES scenario using a typical anticline structure in northern Germany was investigated. The top of the storage formation is at 700 m depth and the thickness is 20 m. The porosity and permeability were assumed to have a homogenous distribution with a value of 0.35 and 500 mD, respectively. According to the specifications of the Huntorf CAES power plant, a gas turbine producing 321 MW power with a minimum inlet <span class="hlt">pressure</span> of 43 bars at an <span class="hlt">air</span> mass flowrate of 417 kg/s was assumed. <span class="hlt">Pressure</span> loss in the gas wells was accounted for using an analytical solution, which defines a minimum bottom hole <span class="hlt">pressure</span> of 47 bars. Two daily extraction cycles of 6 hours each were set to the early morning and the late afternoon in order to bypass the massive solar energy production around noon. A two-year initial filling of the reservoir with <span class="hlt">air</span> and ten years of daily cyclic operation were numerically simulated using the Eclipse E300 reservoir simulator. The simulation results show that using 12 wells the storage formation with a permeability of 500 mD can support the required 6-hour continuous power output of 321MW, which corresponds an energy output of 3852 MWh per</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100014092','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100014092"><span>Fuel Cells Utilizing Oxygen From <span class="hlt">Air</span> at Low <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cisar, Alan; Boyer, Chris; Greenwald, Charles</p> <p>2006-01-01</p> <p>A fuel cell stack has been developed to supply power for a high-altitude aircraft with a minimum of <span class="hlt">air</span> handling. The fuel cell is capable of utilizing oxygen from ambient <span class="hlt">air</span> at low <span class="hlt">pressure</span> with no need for compression. For such an application, it is advantageous to take oxygen from the <span class="hlt">air</span> (in contradistinction to carrying a supply of oxygen onboard), but it is a challenging problem to design a fuel-cell stack of reasonable weight that can generate sufficient power while operating at reduced <span class="hlt">pressures</span>. The present fuel-cell design is a response to this challenge. The design features a novel bipolar plate structure in combination with a gas-diffusion structure based on a conductive metal core and a carbon gas-diffusion matrix. This combination makes it possible for the flow fields in the stack to have a large open fraction (ratio between open volume and total volume) to permit large volumes of <span class="hlt">air</span> to flow through with exceptionally low backpressure. Operations at reduced <span class="hlt">pressure</span> require a corresponding increase in the volume of <span class="hlt">air</span> that must be handled to deliver the same number of moles of oxygen to the anodes. Moreover, the increase in the open fraction, relative to that of a comparable prior fuel-cell design, reduces the mass of the stack. The fuel cell has been demonstrated to operate at a power density as high as 105 W/cm2 at an <span class="hlt">air</span> <span class="hlt">pressure</span> as low as 2 psia (absolute <span class="hlt">pressure</span> 14 kPa), which is the atmospheric <span class="hlt">pressure</span> at an altitude of about 50,000 ft ( 15.2 km). The improvements in the design of this fuel cell could be incorporated into designs of other fuel cells to make them lighter in weight and effective at altitudes higher than those of prior designs. Potential commercial applications for these improvements include most applications now under consideration for fuel cells.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.ars.usda.gov/research/publications/publication/?seqNo115=283989','TEKTRAN'); return false;" href="http://www.ars.usda.gov/research/publications/publication/?seqNo115=283989"><span>Application of the <span class="hlt">Wind</span> Erosion Prediction System in the AIRPACT regional <span class="hlt">air</span> quality modeling framework</span></a></p> <p><a target="_blank" href="https://www.ars.usda.gov/research/publications/find-a-publication/">USDA-ARS?s Scientific Manuscript database</a></p> <p></p> <p></p> <p><span class="hlt">Wind</span> erosion of soil is a major concern of the agricultural community as it removes the most fertile part of the soil and thus degrades soil productivity. Furthermore, dust emissions due to <span class="hlt">wind</span> erosion contribute to poor <span class="hlt">air</span> quality, reduce visibility, and cause perturbations to regional radiation ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009GeoRL..3621605V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009GeoRL..3621605V"><span>A generalized model for the <span class="hlt">air</span>-sea transfer of dimethyl sulfide at high <span class="hlt">wind</span> speeds</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vlahos, Penny; Monahan, Edward C.</p> <p>2009-11-01</p> <p>The <span class="hlt">air</span>-sea exchange of dimethyl sulfide (DMS) is an important component of ocean biogeochemistry and global climate models. Both laboratory experiments and field measurements of DMS transfer rates have shown that the <span class="hlt">air</span>-sea flux of DMS is analogous to that of other significant greenhouse gases such as CO2 at low <span class="hlt">wind</span> speeds (<10 m/s) but that these DMS transfer rates may diverge from other gases as <span class="hlt">wind</span> speeds increase. Herein we provide a mechanism that predicts the attenuation of DMS transfer rates at high <span class="hlt">wind</span> speeds. The model is based on the amphiphilic nature of DMS that leads to transfer delay at the water-bubble interface and becomes significant at <span class="hlt">wind</span> speeds above >10 m/s. The result is an attenuation of the dimensionless Henry's Law constant (H) where (Heff = H/(1 + (Cmix/Cw) ΦB) by a solubility enhancement Cmix/Cw, and the fraction of bubble surface area per m2 surface ocean.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA128761','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA128761"><span>A 20-KW <span class="hlt">Wind</span> Energy Conversion System (WECS) at the Marine Corps <span class="hlt">Air</span> Station, Kaneohe, Hawaii.</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1983-01-01</p> <p>of propellers and that vertical-axis <span class="hlt">wind</span> turbines would be more efficient. Several turbines such as the Darrieus and gyro-mill, of this type are... <span class="hlt">wind</span> turbines , <span class="hlt">wind</span> systems siting, alternate energy systems, remote site power generation. 20 ABSTRACT (Con!,,u,. - r r... .. do I(3 lI - d #,d e...Corps <span class="hlt">Air</span> Station (MCAS) Kaneohe Bay, Hawaii. The <span class="hlt">wind</span> turbine generator chosen for the evaluation was a horizontal-axis-propeller- downwind rotor</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AGUFMEP43D0770P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AGUFMEP43D0770P"><span><span class="hlt">Wind</span> driven vertical transport in a vegetated, wetland water column with <span class="hlt">air</span>-water gas exchange</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Poindexter, C.; Variano, E. A.</p> <p>2010-12-01</p> <p>Flow around arrays of cylinders at low and intermediate Reynolds numbers has been studied numerically, analytically and experimentally. Early results demonstrated that at flow around randomly oriented cylinders exhibits reduced turbulent length scales and reduced diffusivity when compared to similarly forced, unimpeded flows (Nepf 1999). While horizontal dispersion in flows through cylinder arrays has received considerable research attention, the case of vertical dispersion of reactive constituents has not. This case is relevant to the vertical transfer of dissolved gases in wetlands with emergent vegetation. We present results showing that the presence of vegetation can significantly enhance vertical transport, including gas transfer across the <span class="hlt">air</span>-water interface. Specifically, we study a <span class="hlt">wind</span>-sheared <span class="hlt">air</span>-water interface in which randomly arrayed cylinders represent emergent vegetation. <span class="hlt">Wind</span> is one of several processes that may govern physical dispersion of dissolved gases in wetlands. <span class="hlt">Wind</span> represents the dominant force for gas transfer across the <span class="hlt">air</span>-water interface in the ocean. Empirical relationships between <span class="hlt">wind</span> and the gas transfer coefficient, k, have been used to estimate spatial variability of CO2 exchange across the worlds’ oceans. Because wetlands with emergent vegetation are different from oceans, different model of <span class="hlt">wind</span> effects is needed. We investigated the vertical transport of dissolved oxygen in a scaled wetland model built inside a laboratory tank equipped with an open-ended <span class="hlt">wind</span> tunnel. Plastic tubing immersed in water to a depth of approximately 40 cm represented emergent vegetation of cylindrical form such as hard-stem bulrush (Schoenoplectus acutus). After partially removing the oxygen from the tank water via reaction with sodium sulfite, we used an optical probe to measure dissolved oxygen at mid-depth as the tank water re-equilibrated with the <span class="hlt">air</span> above. We used dissolved oxygen time-series for a range of mean <span class="hlt">wind</span> speeds to estimate the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016SPIE.9906E..2MK','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016SPIE.9906E..2MK"><span>The University of Tokyo Atacama Observatory 6.5m Telescope: enclosure design and <span class="hlt">wind</span> analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Konishi, Masahiro; Sako, Shigeyuki; Uchida, Takanori; Araya, Ryou; Kim, Koui; Yoshii, Yuzuru; Doi, Mamoru; Kohno, Kotaro; Miyata, Takashi; Motohara, Kentaro; Tanaka, Masuo; Minezaki, Takeo; Morokuma, Tomoki; Tamura, Yoichi; Tanabé, Toshihiko; Kato, Natsuko; Kamizuka, Takafumi; Takahashi, Hidenori; Aoki, Tsutomu; Soyano, Takao; Tarusawa, Ken'ichi</p> <p>2016-07-01</p> <p>We present results on the computational fluid dynamics (CFD) numerical simulations as well as the <span class="hlt">wind</span> tunnel experiments for the observation facilities of the University of Tokyo Atacama Observatory 6.5m Telescope being constructed at the summit of Co. Chajnantor in northern Chile. Main purpose of this study starting with the baseline design reported in 2014 is to analyze topographic effect on the <span class="hlt">wind</span> behavior, and to evaluate the <span class="hlt">wind</span> <span class="hlt">pressure</span>, the <span class="hlt">air</span> turbulence, and the <span class="hlt">air</span> change (ventilation) efficiency in the enclosure. The <span class="hlt">wind</span> velocity is found to be accelerated by a factor of 1.2 to reach the summit (78 m sec-1 expected at a maximum), and the resulting <span class="hlt">wind</span> <span class="hlt">pressure</span> (3,750 N m-2) is used for the framework design of the facilities. The CFD data reveals that the open space below the floor of the facilities works efficiently to drift away the <span class="hlt">air</span> turbulence near the ground level which could significantly affect the dome seeing. From comparisons of the <span class="hlt">wind</span> velocity field obtained from the CFD simulation for three configurations of the ventilation windows, we find that the windows at a level of the telescope secondary mirror have less efficiency of the <span class="hlt">air</span> change than those at lower levels. Considering the construction and maintenance costs, and operation procedures, we finally decide to allocate 13 windows at a level of the observing floor, 12 at a level of the primary mirror, and 2 at the level of the secondary mirror. The opening area by those windows accounts for about 14% of the total interior surface of the enclosure. Typical <span class="hlt">air</span> change rate of 20-30 per hour is expected at the <span class="hlt">wind</span> velocity of 1 m sec-1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790031066&hterms=air+pollution&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dair%2Bpollution','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790031066&hterms=air+pollution&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dair%2Bpollution"><span>Pattern recognition methods and <span class="hlt">air</span> pollution source identification. [based on <span class="hlt">wind</span> direction</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Leibecki, H. F.; King, R. B.</p> <p>1978-01-01</p> <p>Directional <span class="hlt">air</span> samplers, used for resolving suspended particulate matter on the basis of time and <span class="hlt">wind</span> direction were used to assess the feasibility of characterizing and identifying emission source types in urban multisource environments. Filters were evaluated for 16 elements and X-ray fluorescence methods yielded elemental concentrations for direction, day, and the interaction of direction and day. Large numbers of samples are necessary to compensate for large day-to-day variations caused by <span class="hlt">wind</span> perturbations and/or source changes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005AGUFM.P11C0128F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005AGUFM.P11C0128F"><span>Low-latitude Temperatures, <span class="hlt">Pressures</span>, and <span class="hlt">Winds</span> on Saturn from Cassini Radio Occultations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Flasar, F. M.; Schinder, P. J.; Kliore, A. J.; French, R. G.; Marouf, E. A.; Nagy, A.; Rappaport, N. J.; Anabtawi, A.; Asmar, S.; Barbinis, E.; Fleischman, D. U.; Goltz, G. L.; Johnston, D. V.; Rochblatt, D.; McGhee, C. A.</p> <p>2005-12-01</p> <p>We present results from 12 ingress and egress soundings done within 10 degrees of Saturn's equator. Above the 100-mbar level, near the tropopause, the vertical profiles of temperature are marked by undulatory structure that may be associated with vertically propagating waves. Below the 200-mbar level, in the upper troposphere, the vertical profiles are smoother, and the overall trend of temperatures is to increase away from the equator. This implies a decay of the zonal <span class="hlt">winds</span> with altitude. The zonal <span class="hlt">winds</span> can actually be inferred directly from the meridional gradient in <span class="hlt">pressure</span>, without the need of a boundary condition on the <span class="hlt">winds</span>. We summarize results of these calculations. This is of interest because recent cloud tracking studies have indicated lower equatorial <span class="hlt">winds</span> than found earlier, but whether this indicates a real change in the <span class="hlt">winds</span> at a given altitude or a change in the altitudes of the features tracked is controversial.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2004MeScT..15.2349M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2004MeScT..15.2349M"><span>Unsteady <span class="hlt">pressure</span> measurement instrumentation using anodized-aluminium PSP applied in a transonic <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mérienne, Marie-Claire; LeSant, Yves; Ancelle, Jacques; Soulevant, Didier</p> <p>2004-12-01</p> <p>The objective of this work is to demonstrate the feasibility of <span class="hlt">pressure</span> measurement instrumentation using anodized-aluminium <span class="hlt">pressure</span>-sensitive paint (or AA-PSP) for application in unsteady flows. An anodized procedure was applied to an aluminium tape that can be easily placed on a model even when it is mounted in a <span class="hlt">wind</span> tunnel. The response time of the PSP coating is assessed using a calibration rig that generates fast <span class="hlt">pressure</span> steps or sinusoidal <span class="hlt">pressure</span> fluctuations up to 1 kHz. A pointwise measurement system made with a Cassegrain telescope and a photomultiplier tube was designed to collect the PSP luminescence. The spot displacement on the model surface was carried out by using a 3D moving bench. A camera is used to identify the spot position according to the model geometry. An application in a <span class="hlt">wind</span> tunnel was performed on a forced shock wave oscillation test, generating amplitude variations up to 25 kPa. The calibration problem due to non-uniformity of the anodized properties did not allow quantitative data processing of <span class="hlt">pressure</span> levels. Nevertheless frequency analysis demonstrates that the coating is able to follow the <span class="hlt">pressure</span> fluctuations, as shown by comparison with standard <span class="hlt">pressure</span> transducers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=background+AND+wind&id=EJ322691','ERIC'); return false;" href="https://eric.ed.gov/?q=background+AND+wind&id=EJ322691"><span><span class="hlt">Air</span> on the Move.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>NatureScope, 1985</p> <p>1985-01-01</p> <p>Provides (1) background information on global <span class="hlt">winds</span>, <span class="hlt">air</span> masses, fronts, and <span class="hlt">pressure</span> systems; (2) five activities on this topic; and (3) a ready-to-copy coloring page and worksheet. Each activity includes an objective, list of materials needed, recommended age level(s), subject area(s), and instructional strategies. (JN)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PlST...19f4016W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PlST...19f4016W"><span>Experimental study of rotating <span class="hlt">wind</span> turbine breakdown characteristics in large scale <span class="hlt">air</span> gaps</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Yu; Qu, Lu; Si, Tianjun; Ni, Yang; Xu, Jianwei; Wen, Xishan</p> <p>2017-06-01</p> <p>When a <span class="hlt">wind</span> turbine is struck by lightning, its blades are usually rotating. The effect of blade rotation on a turbine’s ability to trigger a lightning strike is unclear. Therefore, an arching electrode was used in a <span class="hlt">wind</span> turbine lightning discharge test to investigate the difference in lightning triggering ability when blades are rotating and stationary. A negative polarity switching waveform of 250/2500 μs was applied to the arching electrode and the up-and-down method was used to calculate the 50% discharge voltage. Lightning discharge tests of a 1:30 scale <span class="hlt">wind</span> turbine model with 2, 4, and 6 m <span class="hlt">air</span> gaps were performed and the discharge process was observed. The experimental results demonstrated that when a 2 m <span class="hlt">air</span> gap was used, the breakdown voltage increased as the blade speed was increased, but when the gap length was 4 m or longer, the trend was reversed and the breakdown voltage decreased. The analysis revealed that the rotation of the blades changes the charge distribution in the blade-tip region, promotes upward leader development on the blade tip, and decreases the breakdown voltage. Thus, the blade rotation of a <span class="hlt">wind</span> turbine increases its ability to trigger lightning strikes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009AGUFM.A51E0162M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009AGUFM.A51E0162M"><span>Sea spray contributions to the <span class="hlt">air</span>-sea fluxes at moderate and hurricane <span class="hlt">wind</span> speeds</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mueller, J. A.; Veron, F.</p> <p>2009-12-01</p> <p>At sufficiently high <span class="hlt">wind</span> speed conditions, the surface of the ocean separates to form a substantial number of sea spray drops, which can account for a significant fraction of the total <span class="hlt">air</span>-sea surface area and thus make important contributions to the aggregate <span class="hlt">air</span>-sea momentum, heat and mass fluxes. Although consensus around the qualitative impacts of these drops has been building in recent years, the quantification of their impacts has remained elusive. Ultimately, the spray-mediated fluxes depend on three controlling factors: the number and size of drops formed at the surface, the duration of suspension within the atmospheric marine boundary layer, and the rate of momentum, heat and mass transfer between the drops and the atmosphere. While the latter factor can be estimated from an established, physically-based theory, the estimates for the former two are not well established. Using a recent, physically-based model of the sea spray source function along with the results from Lagrangian stochastic simulations of individual drops, we estimate the aggregate spray-mediated fluxes, finding reasonable agreement with existing models and estimates within the empirical range of <span class="hlt">wind</span> speed conditions. At high <span class="hlt">wind</span> speed conditions that are outside the empirical range, however, we find somewhat lower spray-mediated fluxes than previously reported in the literature, raising new questions about the relative <span class="hlt">air</span>-sea fluxes at high <span class="hlt">wind</span> speeds as well as the development and sustainment of hurricanes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860020620','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860020620"><span>Numerical and experimental studies of particle flow in a high-<span class="hlt">pressure</span> boundary-layer <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>White, B. R.</p> <p>1984-01-01</p> <p>The approach was to simulate the surface environment of Venus as closely as practicable and to conduct experiments to determine threshold <span class="hlt">wind</span> speeds, particle flux, particle velocities, and the characteristics of various aeolian bedforms. The Venus <span class="hlt">Wind</span> Tunnel (VWT) is described and the experimental procedures that were developed to make the high-<span class="hlt">pressure</span> <span class="hlt">wind</span> tunnel measurements are presented. In terrestrial simulations of aeolian activity, it is possible to conduct experiments under <span class="hlt">pressures</span> and temperatures found in natural environments. Because of the high <span class="hlt">pressures</span> and temperatures, Venusian simulations are difficult to achieve in this regard. Consequently, extrapolation of results to Venue potentially involves unknown factors. The experimental rationale was developed in the following way: The VWT enables the density of the Venusian atmosphere to be reproduced. Density is the principal atmospheric property for governing saltation threshold, particle flux, and the ballistics of airborne particles (equivalent density maintains dynamic similarity of gas flow). When operated at or near Earth's ambient temperature, VWT achieves Venusian atmospheric density at <span class="hlt">pressures</span> of about 30 bar, or about one third less than those on Venus, although still maintaining dynamic similarity to Venus.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28499454','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28499454"><span>Risk for intracranial <span class="hlt">pressure</span> increase related to enclosed <span class="hlt">air</span> in post-craniotomy patients during <span class="hlt">air</span> ambulance transport: a retrospective cohort study with simulation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Brändström, Helge; Sundelin, Anna; Hoseason, Daniela; Sundström, Nina; Birgander, Richard; Johansson, Göran; Winsö, Ola; Koskinen, Lars-Owe; Haney, Michael</p> <p>2017-05-12</p> <p>Post-craniotomy intracranial <span class="hlt">air</span> can be present in patients scheduled for <span class="hlt">air</span> ambulance transport to their home hospital. We aimed to assess risk for in-flight intracranial <span class="hlt">pressure</span> (ICP) increases related to observed intracranial <span class="hlt">air</span> volumes, hypothetical sea level pre-transport ICP, and different potential flight levels and cabin <span class="hlt">pressures</span>. A cohort of consecutive subdural hematoma evacuation patients from one University Medical Centre was assessed with post-operative intracranial <span class="hlt">air</span> volume measurements by computed tomography. Intracranial <span class="hlt">pressure</span> changes related to estimated intracranial <span class="hlt">air</span> volume effects of changing atmospheric <span class="hlt">pressure</span> (simulating flight and cabin <span class="hlt">pressure</span> changes up to 8000 ft) were simulated using an established model for intracranial <span class="hlt">pressure</span> and volume relations. Approximately one third of the cohort had post-operative intracranial <span class="hlt">air</span>. Of these, approximately one third had intracranial <span class="hlt">air</span> volumes less than 11 ml. The simulation estimated that the expected changes in intracranial <span class="hlt">pressure</span> during 'flight' would not result in intracranial hypertension. For intracranial <span class="hlt">air</span> volumes above 11 ml, the simulation suggested that it was possible that intracranial hypertension could develop 'inflight' related to cabin <span class="hlt">pressure</span> drop. Depending on the pre-flight intracranial <span class="hlt">pressure</span> and <span class="hlt">air</span> volume, this could occur quite early during the assent phase in the flight profile. DISCUSSION: These findings support the idea that there should be radiographic verification of the presence or absence of intracranial <span class="hlt">air</span> after craniotomy for patients planned for long distance <span class="hlt">air</span> transport. Very small amounts of <span class="hlt">air</span> are clinically inconsequential. Otherwise, <span class="hlt">air</span> transport with maintained ground-level cabin <span class="hlt">pressure</span> should be a priority for these patients.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSA31A2569C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSA31A2569C"><span>Ionospheric Scintillation Induced by Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Enhancements in the Southern Hemisphere</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Coppeans, T.; Zou, S.; Weatherwax, A. T.; Coster, A. J.</p> <p>2017-12-01</p> <p>Ionospheric scintillation is the random fluctuation in GPS signal radio waves passing through the ionosphere, a phenomenon that can result in the loss of GPS tracking, but can also reveal information about plasma structures in the ionosphere. Sudden compression of the Earth's magnetosphere by a solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement can cause dramatic changes in the E and F region ionospheric plasma. In this study, we investigate the possible ionospheric scintillation induced by solar <span class="hlt">wind</span> <span class="hlt">pressure</span> enhancements using ground-based scintillation receivers located at the McMurdo station and the South Pole station in Antarctica. Various studies of scintillation effects have been carried out, mainly in the northern hemisphere, while the southern hemisphere remains less studied. A pool of storm sudden commencements occurring between Jan. 2011 and Dec. 2014 were sorted based on solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement, background conditions, availability of data, and magnitude of scintillation response. Among the 89 events examined, 14 of them exhibited enhanced scintillation and were selected for detailed examination. Besides the scintillation receivers, other datasets have also been used to carry out the above study, including field-aligned currents from AMPERE, and global GPS TEC. Effects of FACs and TEC/TEC gradients on the generation of these scintillations are studied.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970023034','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970023034"><span>Radiation <span class="hlt">Pressure</span>-Driven Magnetic Disk <span class="hlt">Winds</span> in Broad Absorption Line Quasi-Stellar Objects</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>DeKool, Martin; Begelman, Mitchell C.</p> <p>1995-01-01</p> <p>We explore a model in which QSO broad absorption lines (BALS) are formed in a radiation <span class="hlt">pressure</span>-driven <span class="hlt">wind</span> emerging from a magnetized accretion disk. The magnetic field threading the disk material is dragged by the flow and is compressed by the radiation <span class="hlt">pressure</span> until it is dynamically important and strong enough to contribute to the confinement of the BAL clouds. We construct a simple self-similar model for such radiatively driven magnetized disk <span class="hlt">winds</span>, in order to explore their properties. It is found that solutions exist for which the entire magnetized flow is confined to a thin wedge over the surface of the disk. For reasonable values of the mass-loss rate, a typical magnetic field strength such that the magnetic <span class="hlt">pressure</span> is comparable to the inferred gas <span class="hlt">pressure</span> in BAL clouds, and a moderate amount of internal soft X-ray absorption, we find that the opening angle of the flow is approximately 0.1 rad, in good agreement with the observed covering factor of the broad absorption line region.</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('https://www.fs.usda.gov/treesearch/pubs/55840','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/55840"><span>Residential tornado safe room from commodity wood products – impact and <span class="hlt">wind</span> <span class="hlt">pressure</span> testing</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Robert H. Falk; James J. Bridwell; C. Adam Senalik; Marshall Begel</p> <p>2018-01-01</p> <p>A tornado safe room is a shelter designed to provide protection during a tornado and is specifically engineered to resist the high <span class="hlt">wind</span> <span class="hlt">pressures</span> and debris impact generated by these high <span class="hlt">wind</span> events. The required performance criteria of these shelters has been established and is found in the International Code Council Standard for the Design and Construction of Storm...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS.995a2051A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS.995a2051A"><span>Preliminary Investigation on the Behavior of Pore <span class="hlt">Air</span> <span class="hlt">Pressure</span> During Rainfall Infiltration</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ashraf Mohamad Ismail, Mohd; Min, Ng Soon; Hasliza Hamzah, Nur; Hazreek Zainal Abidin, Mohd; Madun, Aziman; Tajudin, Saiful Azhar Ahmad</p> <p>2018-04-01</p> <p>This paper focused on the preliminary investigation of pore <span class="hlt">air</span> <span class="hlt">pressure</span> behaviour during rainfall infiltration in order to substantiate the mechanism of rainfall induced slope failure. The actual behaviour or pore <span class="hlt">air</span> <span class="hlt">pressure</span> during infiltration is yet to be clearly understood as it is regularly assumed as atmospheric. Numerical modelling of one dimensional (1D) soil column was utilized in this study to provide a preliminary insight of this highlighted uncertainty. Parametric study was performed by using rainfall intensities of 1.85 x 10-3m/s and 1.16 x 10-4m/s applied on glass beads to simulate intense and modest rainfall conditions. Analysis results show that the high rainfall intensity causes more development of pore <span class="hlt">air</span> <span class="hlt">pressure</span> compared to low rainfall intensity. This is because at high rainfall intensity, the rainwater cannot replace the pore <span class="hlt">air</span> smoothly thus confining the pore <span class="hlt">air</span>. Therefore, the effect of pore <span class="hlt">air</span> <span class="hlt">pressure</span> has to be taken into consideration particularly during heavy rainfall.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvF...3f3701M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvF...3f3701M"><span>Electrohydrodynamic ionic <span class="hlt">wind</span>, force field, and ionic mobility in a positive dc wire-to-cylinders corona discharge in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Monrolin, Nicolas; Praud, Olivier; Plouraboué, Franck</p> <p>2018-06-01</p> <p>Ionic <span class="hlt">wind</span> refers to the acceleration of partially ionized <span class="hlt">air</span> between two high-voltage electrodes. We study the momentum transfer from ions to <span class="hlt">air</span>, resulting from ionic <span class="hlt">wind</span> created by two asymmetric electrodes and producing a net thrust. This electrohydrodynamic (EHD) thrust, has already been measured in previous studies with digital scales. In this study, we provide more insights into the electrohydrodynamic momentum transfer for a wire-to-cylinder(s) positive dc corona discharge. We provide a simple and general theoretical derivation for EHD thrust, which is proportional to the current/mobility ratio and also to an effective distance integrated on the surface of the electrodes. By considering various electrode configurations, our investigation brings out the physical origin of previously obtained optimal configurations, associated with a better tradeoff between Coulomb forcing, friction occurring at the collector, and wake interactions. By measuring two-dimensional velocity fields using particle image velocimetry (PIV), we are able to evaluate the resulting local net force, including the <span class="hlt">pressure</span> gradient. It is shown that the contribution of velocity fluctuations in the wake of the collecting electrode(s) must be taken into account to recover the net thrust. We confirm the proportionality between the EHD force and the current/mobility ratio experimentally, and evaluate the ion mobility from PIV measurements. A spectral analysis of the velocity fluctuations indicates a dominant frequency corresponding to a Strouhal number of 0.3 based on the ionic <span class="hlt">wind</span> velocity and the collector size. Finally, the effective mobility of charge carriers is estimated by a PIV based method inside the drift region.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890040288&hterms=experimental+survey&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dexperimental%2Bsurvey','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890040288&hterms=experimental+survey&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Dexperimental%2Bsurvey"><span>Miniaturized compact water-cooled pitot-<span class="hlt">pressure</span> probe for flow-field surveys in hypersonic <span class="hlt">wind</span> tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ashby, George C.</p> <p>1988-01-01</p> <p>An experimental investigation of the design of pitot probes for flowfield surveys in hypersonic <span class="hlt">wind</span> tunnels is reported. The results show that a pitot-<span class="hlt">pressure</span> probe can be miniaturized for minimum interference effects by locating the transducer in the probe support body and water-cooling it so that the <span class="hlt">pressure</span>-settling time and transducer temperature are compatible with hypersonic tunnel operation and flow conditions. Flowfield surveys around a two-to-one elliptical cone model in a 20-inch Mach 6 <span class="hlt">wind</span> tunnel using such a probe show that probe interference effects are essentially eliminated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-PIA00435.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-PIA00435.html"><span>Hurricane Frances as Observed by NASA Spaceborne Atmospheric Infrared Sounder <span class="hlt">AIRS</span> and Sea<span class="hlt">Winds</span> Scatterometer</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2004-08-30</p> <p>This image shows Hurricane Frances in August 2004 as captured by instruments onboard two different NASA satellites: the <span class="hlt">AIRS</span> infrared instrument onboard Aqua, and the Sea<span class="hlt">Winds</span> scatterometer onboard QuikSCAT. Both are JPL-managed instruments. <span class="hlt">AIRS</span> data are used to create global three-dimensional maps of temperature, humidity and clouds, while scatterometers measure surface <span class="hlt">wind</span> speed and direction over the ocean. The red vectors in the image show Frances' surface <span class="hlt">winds</span> as measured by Sea<span class="hlt">Winds</span> on QuikSCAT. The background colors show the temperature of clouds and surface as viewed in the infrared by <span class="hlt">AIRS</span>, with cooler areas pushing to purple and warmer areas are pushing to red. The color scale on the right gives the temperatures in degrees Kelvin. (The top of the scale, 320 degrees Kelvin, corresponds to 117 degrees Fahrenheit, and the bottom, 180 degrees K is -135 degrees F.) The powerful circulation of this storm is evident from the combined data as well as the development of a clearly-defined central "eye." The infrared signal does not penetrate through clouds, so the light blue areas reveal the cold clouds tops associated with strong thunderstorms embedded within the storm. In cloud-free areas the infrared signal comes from Earth's surface, revealing warmer temperatures. http://photojournal.jpl.nasa.gov/catalog/PIA00435</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091250','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091250"><span>The Resistance of Spheres in <span class="hlt">Wind</span> Tunnels and In <span class="hlt">Air</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bacon, D L; Reid, E G</p> <p>1924-01-01</p> <p>To supplement the standardization tests now in progress at several laboratories, a broad investigation of the resistance of spheres in <span class="hlt">wind</span> tunnels and free <span class="hlt">air</span> has been carried out by the National Advisory Committee for Aeronautics. The subject has been classed in aerodynamic research, and in consequence there is available a great mass of data from previous investigations. This material was given careful consideration in laying out the research, and explanation of practically all the disagreement between former experiments has resulted. A satisfactory confirmation of Reynolds law has been accomplished, the effect of means of support determined, the range of experiment greatly extended by work in the new variable density <span class="hlt">wind</span> tunnel, and the effects of turbulence investigated by work in the tunnels and by towing and dropping tests in free <span class="hlt">air</span>. It is concluded that the erratic nature of most of the previous work is due to support interference and differing turbulence conditions. While the question of support has been investigated thoroughly, a systematic and comprehensive study of the effects of scale and quality of turbulence will be necessary to complete the problem, as this phase was given only general treatment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ClDy..tmp...41C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ClDy..tmp...41C"><span>Mechanisms of the intensification of the upwelling-favorable <span class="hlt">winds</span> during El Niño 1997-1998 in the Peruvian upwelling system</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chamorro, Adolfo; Echevin, Vincent; Colas, François; Oerder, Vera; Tam, Jorge; Quispe-Ccalluari, Carlos</p> <p>2018-01-01</p> <p>The physical processes driving the <span class="hlt">wind</span> intensification in a coastal band of 100 km off Peru during the intense 1997-1998 El Niño (EN) event were studied using a regional atmospheric model. A simulation performed for the period 1994-2000 reproduced the coastal <span class="hlt">wind</span> response to local sea surface temperature (SST) forcing and large scale atmospheric conditions. The model, evaluated with satellite data, represented well the intensity, seasonal and interannual variability of alongshore (i.e. NW-SE) <span class="hlt">winds</span>. An alongshore momentum budget showed that the <span class="hlt">pressure</span> gradient was the dominant force driving the surface <span class="hlt">wind</span> acceleration. The <span class="hlt">pressure</span> gradient tended to accelerate the coastal <span class="hlt">wind</span>, while turbulent vertical mixing decelerated it. A quasi-linear relation between surface <span class="hlt">wind</span> and <span class="hlt">pressure</span> gradient anomalies was found. Alongshore <span class="hlt">pressure</span> gradient anomalies were caused by a greater increase in near-surface <span class="hlt">air</span> temperature off the northern coast than off the southern coast, associated with the inhomogeneous SST warming. Vertical profiles of <span class="hlt">wind</span>, mixing coefficient, and momentum trends showed that the surface <span class="hlt">wind</span> intensification was not caused by the increase of turbulence in the planetary boundary layer. Moreover, the temperature inversion in the vertical mitigated the development of <span class="hlt">pressure</span> gradient due to <span class="hlt">air</span> convection during part of the event. Sensitivity experiments allowed to isolate the respective impacts of the local SST forcing and large scale condition on the coastal <span class="hlt">wind</span> intensification. It was primarily driven by the local SST forcing whereas large scale variability associated with the South Pacific Anticyclone modulated its effects. Examination of other EN events using reanalysis data confirmed that intensifications of alongshore <span class="hlt">wind</span> off Peru were associated with SST alongshore gradient anomalies, as during the 1997-1998 event.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26282384','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26282384"><span>The influence of intraocular <span class="hlt">pressure</span> and <span class="hlt">air</span> jet <span class="hlt">pressure</span> on corneal contactless tonometry tests.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Simonini, Irene; Pandolfi, Anna</p> <p>2016-05-01</p> <p>The <span class="hlt">air</span> puff is a dynamic contactless tonometer test used in ophthalmology clinical practice to assess the biomechanical properties of the human cornea and the intraocular <span class="hlt">pressure</span> due to the filling fluids of the eye. The test is controversial, since the dynamic response of the cornea is governed by the interaction of several factors which cannot be discerned within a single measurement. In this study we describe a numerical model of the <span class="hlt">air</span> puff tests, and perform a parametric analysis on the major action parameters (jet <span class="hlt">pressure</span> and intraocular <span class="hlt">pressure</span>) to assess their relevance on the mechanical response of a patient-specific cornea. The particular cornea considered here has been treated with laser reprofiling to correct myopia, and the parametric study has been conducted on both the preoperative and postoperative geometries. The material properties of the cornea have been obtained by means of an identification procedure that compares the static biomechanical response of preoperative and postoperative corneas under the physiological IOP. The parametric study on the intraocular <span class="hlt">pressure</span> suggests that the displacement of the cornea׳s apex can be a reliable indicator for tonometry, and the one on the <span class="hlt">air</span> jet <span class="hlt">pressure</span> predicts the outcomes of two or more distinct measurements on the same cornea, which can be used in inverse procedures to estimate the material properties of the tissue. Copyright © 2015 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-LRC-2014-01133.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-LRC-2014-01133.html"><span>The Unitary Plan <span class="hlt">Wind</span> Tunnel(UPWT) Test 1891 Space Launch System</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2014-10-15</p> <p>Stage Separation Test of the Space Launch System(SLS) in the Langley Unitary Plan <span class="hlt">Wind</span> Tunnel (UPWT). The model used High <span class="hlt">Pressure</span> <span class="hlt">air</span> blown through the solid rocket boosters. (SRB) to simulate the booster separation motors (BSM) firing.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-LRC-2014-01142.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-LRC-2014-01142.html"><span>The Unitary Plan <span class="hlt">Wind</span> Tunnel(UPWT) Test 1891 Space Launch System</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2014-10-14</p> <p>Stage Separation Test of the Space Launch System(SLS) in the Langley Unitary Plan <span class="hlt">Wind</span> Tunnel (UPWT). The model used High <span class="hlt">Pressure</span> <span class="hlt">air</span> blown through the solid rocket boosters. (SRB) to simulate the booster separation motors (BSM) firing.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080008680','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080008680"><span>Method and apparatus for monitoring oxygen partial <span class="hlt">pressure</span> in <span class="hlt">air</span> masks</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kelly, Mark E. (Inventor); Pettit, Donald R. (Inventor)</p> <p>2006-01-01</p> <p>Method and apparatus are disclosed for monitoring an oxygen partial <span class="hlt">pressure</span> in an <span class="hlt">air</span> mask and providing a tactile warning to the user. The oxygen partial <span class="hlt">pressure</span> in the <span class="hlt">air</span> mask is detected using an electrochemical sensor, the output signal from which is provided to a comparator. The comparator compares the output signal with a preset reference value or range of values representing acceptable oxygen partial <span class="hlt">pressures</span>. If the output signal is different than the reference value or outside the range of values, the <span class="hlt">air</span> mask is vibrated by a vibrating motor to alert the user to a potentially hypoxic condition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25085005','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25085005"><span>Prosthetics socket that incorporates an <span class="hlt">air</span> splint system focusing on dynamic interface <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razak, Nasrul Anuar Abd; Osman, Noor Azuan Abu; Gholizadeh, Hossein; Ali, Sadeeq</p> <p>2014-08-01</p> <p>The interface <span class="hlt">pressure</span> between the residual limb and prosthetic socket has a significant effect on an amputee's satisfaction and comfort. This paper presents the design and performance of a new prosthetic socket that uses an <span class="hlt">air</span> splint system. The <span class="hlt">air</span> splint prosthetic socket system was implemented by combining the <span class="hlt">air</span> splint with a <span class="hlt">pressure</span> sensor that the transhumeral user controls through the use of a microcontroller. The modular construction of the system developed allows the FSR <span class="hlt">pressure</span> sensors that are placed inside the <span class="hlt">air</span> splint socket to determine the required size and fitting for the socket used. Fifteen transhumeral amputees participated in the study. The subject's dynamic <span class="hlt">pressure</span> on the socket that's applied while wearing the <span class="hlt">air</span> splint systems was recorded using F-socket transducers and microcontroller analysis. The values collected by the F-socket sensor for the <span class="hlt">air</span> splint prosthetic socket system were determined accordingly by comparing the dynamic <span class="hlt">pressure</span> applied using statically socket. The <span class="hlt">pressure</span> volume of the <span class="hlt">air</span> splint fluctuated and was recorded at an average of 38 kPa (2.5) to 41 kPa (1.3) over three hours. The <span class="hlt">air</span> splint socket might reduce the <span class="hlt">pressure</span> within the interface of residual limb. This is particularly important during the daily life activities and may reduce the pain and discomfort at the residual limb in comparison to the static socket. The potential development of an auto-adjusted socket that uses an <span class="hlt">air</span> splint system as the prosthetic socket will be of interest to researchers involved in rehabilitation engineering, prosthetics and orthotics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15716946','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15716946"><span>Solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> and electric field as the main factors controlling Saturn's aurorae.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Crary, F J; Clarke, J T; Dougherty, M K; Hanlon, P G; Hansen, K C; Steinberg, J T; Barraclough, B L; Coates, A J; Gérard, J-C; Grodent, D; Kurth, W S; Mitchell, D G; Rymer, A M; Young, D T</p> <p>2005-02-17</p> <p>The interaction of the solar <span class="hlt">wind</span> with Earth's magnetosphere gives rise to the bright polar aurorae and to geomagnetic storms, but the relation between the solar <span class="hlt">wind</span> and the dynamics of the outer planets' magnetospheres is poorly understood. Jupiter's magnetospheric dynamics and aurorae are dominated by processes internal to the jovian system, whereas Saturn's magnetosphere has generally been considered to have both internal and solar-<span class="hlt">wind</span>-driven processes. This hypothesis, however, is tentative because of limited simultaneous solar <span class="hlt">wind</span> and magnetospheric measurements. Here we report solar <span class="hlt">wind</span> measurements, immediately upstream of Saturn, over a one-month period. When combined with simultaneous ultraviolet imaging we find that, unlike Jupiter, Saturn's aurorae respond strongly to solar <span class="hlt">wind</span> conditions. But in contrast to Earth, the main controlling factor appears to be solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> and electric field, with the orientation of the interplanetary magnetic field playing a much more limited role. Saturn's magnetosphere is, therefore, strongly driven by the solar <span class="hlt">wind</span>, but the solar <span class="hlt">wind</span> conditions that drive it differ from those that drive the Earth's magnetosphere.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eosweb.larc.nasa.gov/project/narsto/narsto_epa_ss_st_louis_air_chem_pm_met_data_table','SCIGOV-ASDC'); return false;" href="https://eosweb.larc.nasa.gov/project/narsto/narsto_epa_ss_st_louis_air_chem_pm_met_data_table"><span>NARSTO EPA SS ST LOUIS <span class="hlt">AIR</span> CHEM PM MET DATA</span></a></p> <p><a target="_blank" href="http://eosweb.larc.nasa.gov/">Atmospheric Science Data Center </a></p> <p></p> <p>2018-04-09</p> <p>... <span class="hlt">Winds</span> Precipitation Amount Surface <span class="hlt">Pressure</span> Solar Radiation Surface <span class="hlt">Air</span> Temperature Particulates Trace Metals ... Earth Related Data:  Environmental Protection Agency Supersites St. Louis SCAR-B Block:  ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22493086-piezoelectric-transformers-low-voltage-generation-gas-discharges-ionic-winds-atmospheric-air','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22493086-piezoelectric-transformers-low-voltage-generation-gas-discharges-ionic-winds-atmospheric-air"><span>Piezoelectric transformers for low-voltage generation of gas discharges and ionic <span class="hlt">winds</span> in atmospheric <span class="hlt">air</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>Johnson, Michael J.; Go, David B., E-mail: dgo@nd.edu; Department of Chemical and Biomolecular Engineering, University of Notre Dame, Notre Dame, Indianapolis 46556</p> <p></p> <p>To generate a gas discharge (plasma) in atmospheric <span class="hlt">air</span> requires an electric field that exceeds the breakdown threshold of ∼30 kV/cm. Because of safety, size, or cost constraints, the large applied voltages required to generate such fields are often prohibitive for portable applications. In this work, piezoelectric transformers are used to amplify a low input applied voltage (<30 V) to generate breakdown in <span class="hlt">air</span> without the need for conventional high-voltage electrical equipment. Piezoelectric transformers (PTs) use their inherent electromechanical resonance to produce a voltage amplification, such that the surface of the piezoelectric exhibits a large surface voltage that can generate corona-like dischargesmore » on its corners or on adjacent electrodes. In the proper configuration, these discharges can be used to generate a bulk <span class="hlt">air</span> flow called an ionic <span class="hlt">wind</span>. In this work, PT-driven discharges are characterized by measuring the discharge current and the velocity of the induced ionic <span class="hlt">wind</span> with ionic <span class="hlt">winds</span> generated using input voltages as low as 7 V. The characteristics of the discharge change as the input voltage increases; this modifies the resonance of the system and subsequent required operating parameters.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4120006','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4120006"><span>Prosthetics socket that incorporates an <span class="hlt">air</span> splint system focusing on dynamic interface <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2014-01-01</p> <p>Background The interface <span class="hlt">pressure</span> between the residual limb and prosthetic socket has a significant effect on an amputee’s satisfaction and comfort. This paper presents the design and performance of a new prosthetic socket that uses an <span class="hlt">air</span> splint system. Methods The <span class="hlt">air</span> splint prosthetic socket system was implemented by combining the <span class="hlt">air</span> splint with a <span class="hlt">pressure</span> sensor that the transhumeral user controls through the use of a microcontroller. The modular construction of the system developed allows the FSR <span class="hlt">pressure</span> sensors that are placed inside the <span class="hlt">air</span> splint socket to determine the required size and fitting for the socket used. Fifteen transhumeral amputees participated in the study. Results The subject’s dynamic <span class="hlt">pressure</span> on the socket that’s applied while wearing the <span class="hlt">air</span> splint systems was recorded using F-socket transducers and microcontroller analysis. The values collected by the F-socket sensor for the <span class="hlt">air</span> splint prosthetic socket system were determined accordingly by comparing the dynamic <span class="hlt">pressure</span> applied using statically socket. The <span class="hlt">pressure</span> volume of the <span class="hlt">air</span> splint fluctuated and was recorded at an average of 38 kPa (2.5) to 41 kPa (1.3) over three hours. Conclusion The <span class="hlt">air</span> splint socket might reduce the <span class="hlt">pressure</span> within the interface of residual limb. This is particularly important during the daily life activities and may reduce the pain and discomfort at the residual limb in comparison to the static socket. The potential development of an auto-adjusted socket that uses an <span class="hlt">air</span> splint system as the prosthetic socket will be of interest to researchers involved in rehabilitation engineering, prosthetics and orthotics. PMID:25085005</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170000762','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170000762"><span>Identifying Stratospheric <span class="hlt">Air</span> Intrusions and Associated Hurricane-Force <span class="hlt">Wind</span> Events over the North Pacific Ocean</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Malloy, Kelsey; Folmer, Michael J.; Phillips, Joseph; Sienkiewicz, Joseph M.; Berndt, Emily</p> <p>2017-01-01</p> <p>Motivation: Ocean data is sparse: reliance on satellite imagery for marine forecasting; Ocean Prediction Center (OPC) –“mariner’s weather lifeline”. Responsible for: Pacific, Atlantic, Pacific Alaska surface analyses –24, 48, 96 hrs.; <span class="hlt">Wind</span> & wave analyses –24, 48, 96 hrs.; Issue warnings, make decisions, Geostationary Operational Environmental Satellite –R Series (now GOES-16), Compared to the old GOES: 3 times spectral resolution, 4 times spatial resolution, 5 times faster coverage; Comparable to Japanese Meteorological Agency’s Himawari-8, used a lot throughout this research. Research Question: How can integrating satellite data imagery and derived products help forecasters improve prognosis of rapid cyclogenesis and hurricane-force <span class="hlt">wind</span> events? Phase I –Identifying stratospheric <span class="hlt">air</span> intrusions: Water Vapor –6.2, 6.9, 7.3 micron channels; Airmass RGB Product; <span class="hlt">AIRS</span>, IASI, NUCAPS total column ozone and ozone anomaly; ASCAT (A/B) and AMSR-2 <span class="hlt">wind</span> data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title49-vol5/pdf/CFR-2011-title49-vol5-sec393-51.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title49-vol5/pdf/CFR-2011-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-10-01</p> <p>... 49 Transportation 5 2011-10-01 2011-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraphs (b), (c), (d) or (e) of this section. (b) Hydraulic brakes. Vehicles manufactured on or after...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol5/pdf/CFR-2014-title49-vol5-sec393-51.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol5/pdf/CFR-2014-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... 49 Transportation 5 2014-10-01 2014-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraphs (b), (c), (d) or (e) of this section. (b) Hydraulic brakes. Vehicles manufactured on or after...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1916834T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1916834T"><span>Planar time-resolved PIV for velocity and <span class="hlt">pressure</span> retrieval in atmospheric boundary layer over surface waves.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Troitskaya, Yuliya; Kandaurov, Alexander; Sergeev, Daniil; Bopp, Maximilian; Caulliez, Guillemette</p> <p>2017-04-01</p> <p><span class="hlt">Air</span>-sea coupling in general is important for weather, climate, fluxes. <span class="hlt">Wind</span> wave source is crucially important for surface waves' modeling. But the <span class="hlt">wind</span>-wave growth rate is strongly uncertain. Using direct measurements of <span class="hlt">pressure</span> by wave-following Elliott probe [1] showed, weak and indefinite dependence of <span class="hlt">wind</span>-wave growth rate on the wave steepness, while Grare et.al. [2] discuss the limitations of direct measurements of <span class="hlt">pressure</span> associated with the inability to measure the <span class="hlt">pressure</span> close to the surface by contact methods. Recently non-invasive methods for determining the <span class="hlt">pressure</span> on the basis of technology of time-resolved PIV are actively developed [3]. Retrieving <span class="hlt">air</span> flow velocities by 2D PIV techniques was started from Reul et al [4]. The first attempt for retrieving <span class="hlt">wind</span> <span class="hlt">pressure</span> field of waves in the laboratory tank from the time-resolved PIV measurements was done in [5]. The experiments were performed at the Large <span class="hlt">Air</span>-Sea Interaction Facility (LASIF) - MIO/Luminy (length 40 m, cross section of <span class="hlt">air</span> channel 3.2 x 1.6 m). For 18 regimes with <span class="hlt">wind</span> speed up to 14 m/s including presence of puddle waves, a combination of time resolved PIV technique and optical measurements of water surface form was applied to detailed investigation of the characteristics of the <span class="hlt">wind</span> flow over the water surface. Ammonium chloride smoke was used for flow visualization illuminated by two 6 Wt blue diode lasers combined into a vertical laser plane. Particle movement was captured with high-speed camera using Scheimpflug technique (up to 20 kHz frame rate with 4-frame bursts, spatial resolution about 190 μm, field of view 314x12 mm). Velocity <span class="hlt">air</span> flow field was retrieved by PIV images processing with adaptive cross-correlation method on the curvilinear grid following surface wave form. The resulting time resolved instantaneous velocity fields on regular grid allowed us to obtain momentum fluxes directly from measured <span class="hlt">air</span> velocity fluctuations. The average <span class="hlt">wind</span> velocity patterns were</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('http://adsabs.harvard.edu/abs/2015ClDy...45.1699K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015ClDy...45.1699K"><span>Recent recovery of surface <span class="hlt">wind</span> speed after decadal decrease: a focus on South Korea</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, JongChun; Paik, Kyungrock</p> <p>2015-09-01</p> <p>We investigate the multi-decadal variability of observed surface <span class="hlt">wind</span> speed around South Korea. It is found that surface <span class="hlt">wind</span> speed exhibits decreasing trend from mid-1950s until 2003, which is similar with the trends reported for other parts of the world. However, the decreasing trend ceases and becomes unclear since then. It is revealed that decreasing <span class="hlt">wind</span> speed until 2003 is strongly associated with the decreasing trend of the spatial variance in both atmospheric <span class="hlt">pressure</span> and <span class="hlt">air</span> temperature across the East Asia for the same period. On the contrary, break of decreasing trend in surface <span class="hlt">wind</span> speed since 2003 is associated with increasing spatial variance in surface temperature over the East Asia. Ground observation shows that surface <span class="hlt">wind</span> speed and <span class="hlt">air</span> temperature exhibit highly negative correlations for both summer and winter prior to 2003. However, since 2003, the correlations differ between seasons. We suggest that mechanisms behind the recent <span class="hlt">wind</span> speed trend are different between summer and winter. This is on the basis of an interesting finding that <span class="hlt">air</span> temperature has decreased while surface temperature has increased during winter months since 2003. We hypothesize that such contrasting temperature trends indicate more frequent movement of external cold <span class="hlt">air</span> mass into the region since 2003. We also hypothesize that increasing summer <span class="hlt">wind</span> speed is driven by intrusion of warm <span class="hlt">air</span> mass into the region which is witnessed via increasing spatial variance in surface temperature across East Asia and the fact that both <span class="hlt">air</span> and surface temperature rise together.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20060026024','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20060026024"><span>Anomalous Shocks on the Measured Near-Field <span class="hlt">Pressure</span> Signatures of Low-Boom <span class="hlt">Wind</span>-Tunnel Models</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mack, Robert J.</p> <p>2006-01-01</p> <p>Unexpected shocks on <span class="hlt">wind</span>-tunnel-measured <span class="hlt">pressure</span> signatures prompted questions about design methods, <span class="hlt">pressure</span> signature measurement techniques, and the quality of measurements in the flow fields near lifting models. Some of these unexpected shocks were the result of component integration methods. Others were attributed to the three-dimension nature of the flow around a lifting model, to inaccuracies in the prediction of the area-ruled lift, or to wing-tip stall effects. This report discusses the low-boom model <span class="hlt">wind</span>-tunnel data where these unexpected shocks were initially observed, the physics of the lifting wing/body model's flow field, the <span class="hlt">wind</span>-tunnel data used to evaluate the applicability of methods for calculating equivalent areas due to lift, the performance of lift prediction codes, and tip stall effects so that the cause of these shocks could be determined.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=69843&keyword=kernel&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50','EPA-EIMS'); return false;" href="https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=69843&keyword=kernel&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50"><span>LOCATING NEARBY SOURCES OF <span class="hlt">AIR</span> POLLUTION BY NONPARAMETRIC REGRESSION OF ATMOSPHERIC CONCENTRATIONS ON <span class="hlt">WIND</span> DIRECTION. (R826238)</span></a></p> <p><a target="_blank" href="http://oaspub.epa.gov/eims/query.page">EPA Science Inventory</a></p> <p></p> <p></p> <p><p>The relationship of the concentration of <span class="hlt">air</span> pollutants to <span class="hlt">wind</span> direction has been determined by nonparametric regression using a Gaussian kernel. The results are smooth curves with error bars that allow for the accurate determination of the <span class="hlt">wind</span> direction where the concentrat...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016EGUGA..18.2585S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016EGUGA..18.2585S"><span>The lunar semidiurnal <span class="hlt">air</span> <span class="hlt">pressure</span> tide in in-situ data and ECMWF reanalyses</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schindelegger, Michael; Dobslaw, Henryk</p> <p>2016-04-01</p> <p>A gridded empirical model of the lunar semidiurnal <span class="hlt">air</span> <span class="hlt">pressure</span> tide L2 is deduced through multiquadric interpolation of more than 2000 globally distributed tidal estimates from land barometers and moored buoys. The resulting climatology serves as an independent standard to validate the barometric L2 oscillations that are present in ECMWF's (European Centre for Medium-Range Weather Forecasts) global atmospheric reanalyses despite the omission of gravitational forcing mechanisms in the involved forecast routines. Inconsistencies between numerical and empirical L2 solutions are found to be small even though the reanalysis models typically underestimate equatorial peak <span class="hlt">pressures</span> by 10-20% and produce slightly deficient tidal phases in latitudes south of 30°N. Through using a time-invariant reference surface over both land and water and assimilating marine <span class="hlt">pressure</span> data without accounting for vertical sensor movements due to the M2 ocean tide, ECMWF-based tidal solutions are also prone to strong local artifacts. Additionally, the dependency of the lunar tidal oscillation in atmospheric analysis systems on the meteorological input data is demonstrated based on a recent ECMWF twentieth-century reanalysis (ERA-20C) which draws its all of its observational constraints from in-situ registrations of <span class="hlt">pressure</span> and surface <span class="hlt">winds</span>. The L2 signature prior to 1950 is particularly indicative of distinct observing system changes, such as the paucity of marine data during both World Wars or the opening of the Panama Canal in 1914 and the associated adjustment of commercial shipping routes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSM11B2309V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSM11B2309V"><span>Tracking a Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Pulses' Impact Through the Magnetosphere Using the Heliophysics System Observatory</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vidal-Luengo, S.; Moldwin, M.</p> <p>2017-12-01</p> <p>During northward Interplanetary Magnetic Field (IMF) Bz conditions, the magnetosphere acts as a closed "cavity" and reacts to solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> pulses more simply than during southward IMF conditions. Effects of solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> have been observed as geomagnetic lobe compressions depending on the characteristics of the <span class="hlt">pressure</span> pulse and the spacecraft location. One of the most important aspects of this study is the incorporation of simultaneous observations by different missions, such as <span class="hlt">WIND</span>, CLUSTER, THEMIS, MMS, Van Allen Probes and GOES as well as magnetometer ground stations that allow us to map the magnetosphere response at different locations during the propagation of a <span class="hlt">pressure</span> pulse. In this study we used the SYM-H as an indicator of dynamic <span class="hlt">pressure</span> pulses occurrence from 2007 to 2016. The selection criteria for events are: (1) the increase in the index must be bigger than 10 [nT] and (2) the rise time must be in less than 5 minutes. Additionally, the events must occur under northward IMF and at the same time at least one spacecraft has to be located in the magnetosphere nightside. Using this methodology we found 66 <span class="hlt">pressure</span> pulse events for analysis. Most of them can be classified as step function <span class="hlt">pressure</span> pulses or as sudden impulses (increase followed immediately by a decrease of the dynamic <span class="hlt">pressure</span>). Under these two categories the results show some systematic signatures depending of the location of the spacecraft. For both kind of <span class="hlt">pressure</span> pulse signatures, compressions are observed on the dayside. However, on the nightside compressions and/or South-then-North magnetic signatures can be observed for step function like <span class="hlt">pressure</span> pulses, meanwhile for the sudden impulse kind of <span class="hlt">pressure</span> pulses the magnetospheric response seems to be less global and more dependent on the local conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083221','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083221"><span>Simple Experiments for Teaching <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Shamsipour, Gholamreza</p> <p>2006-01-01</p> <p>Everyone who teaches physics knows very well that sometimes a simple device or experiment can help to make a concept clear. In this paper, inspired by "The Jumping Pencil" by Martin Gardner, I will discuss a simple demonstration device that can be used to start the study of <span class="hlt">air</span> <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol5/pdf/CFR-2013-title49-vol5-sec393-51.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol5/pdf/CFR-2013-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... 49 Transportation 5 2013-10-01 2013-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraph (f), must be equipped with a signal that provides a warning to the driver when a failure occurs in...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol5/pdf/CFR-2012-title49-vol5-sec393-51.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol5/pdf/CFR-2012-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... 49 Transportation 5 2012-10-01 2012-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraph (f), must be equipped with a signal that provides a warning to the driver when a failure occurs in...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..274a2046S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..274a2046S"><span>Simulation and Experiment Research on Fatigue Life of High <span class="hlt">Pressure</span> <span class="hlt">Air</span> Pipeline Joint</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shang, Jin; Xie, Jianghui; Yu, Jian; Zhang, Deman</p> <p>2017-12-01</p> <p>High <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint is important part of high <span class="hlt">pressure</span> <span class="hlt">air</span> system, whose reliability is related to the safety and stability of the system. This thesis developed a new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint, carried out dynamics research on CB316-1995 and new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint with finite element method, deeply analysed the join forms of different design schemes and effect of materials on stress, tightening torque and fatigue life of joint. Research team set up vibration/pulse test bench, carried out joint fatigue life contrast test. The result shows: the maximum stress of the joint is inverted in the inner side of the outer sleeve nut, which is consistent with the failure mode of the crack on the outer sleeve nut in practice. Simulation and experiment of fatigue life and tightening torque of new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint are better than CB316-1995 joint.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930081405','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930081405"><span>Compression-ignition Engine Performance at Altitudes and at Various <span class="hlt">Air</span> <span class="hlt">Pressures</span> and Temperatures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moore, Charles S; Collins, John H</p> <p>1937-01-01</p> <p>Engine test results are presented for simulated altitude conditions. A displaced-piston combustion chamber on a 5- by 7-inch single cylinder compression-ignition engine operating at 2,000 r.p.m. was used. Inlet <span class="hlt">air</span> temperature equivalent to standard altitudes up to 14,000 feet were obtained. Comparison between performance at altitude of the unsupercharged compression-ignition engine compared favorably with the carburetor engine. Analysis of the results for which the inlet <span class="hlt">air</span> temperature, inlet <span class="hlt">air</span> <span class="hlt">pressure</span>, and inlet and exhaust <span class="hlt">pressure</span> were varied indicates that engine performance cannot be reliably corrected on the basis of inlet <span class="hlt">air</span> density or weight of <span class="hlt">air</span> charge. Engine power increases with inlet <span class="hlt">air</span> <span class="hlt">pressure</span> and decreases with inlet <span class="hlt">air</span> temperatures very nearly as straight line relations over a wide range of <span class="hlt">air</span>-fuel ratios. Correction factors are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/15009599','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/15009599"><span>Preliminary Assessment of Potential Avian Interactions at Four Proposed <span class="hlt">Wind</span> Energy Facilities on Vandenberg <span class="hlt">Air</span> Force Base, California</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>Not Available</p> <p></p> <p>The United States <span class="hlt">Air</span> Force (USAF) is investigating whether to install <span class="hlt">wind</span> turbines to provide a supplemental source of electricity at Vandenberg <span class="hlt">Air</span> Force Base (VAFB) near Lompoc, California. As part of that investigation, VAFB sought assistance from the U.S. Department of Energy's National Renewable Energy Laboratory (NREL) to provide a preliminary characterization of the potential risk to wildlife resources (mainly birds and bats) from <span class="hlt">wind</span> turbine installations. With <span class="hlt">wind</span> power development expanding throughout North America and Europe, concerns have surfaced over the number of bird fatalities associated with <span class="hlt">wind</span> turbines. Guidelines developed for the <span class="hlt">wind</span> industry by the Nationalmore » <span class="hlt">Wind</span> Coordinating Committee (NWCC) recommend assessing potential impacts to birds, bats, and other potentially sensitive resources before construction. The primary purpose of an assessment is to identify potential conflicts with sensitive resources, to assist developers with identifying their permitting needs, and to develop strategies to avoid impacts or to mitigate their effects. This report provides a preliminary (Phase I) biological assessment of potential impacts to birds and bats that might result from construction and operation of the proposed <span class="hlt">wind</span> energy facilities on VAFB.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010050636','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010050636"><span>Application of <span class="hlt">Pressure</span>-Based Wall Correction Methods to Two NASA Langley <span class="hlt">Wind</span> Tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Iyer, V.; Everhart, J. L.</p> <p>2001-01-01</p> <p>This paper is a description and status report on the implementation and application of the WICS wall interference method to the National Transonic Facility (NTF) and the 14 x 22-ft subsonic <span class="hlt">wind</span> tunnel at the NASA Langley Research Center. The method calculates free-<span class="hlt">air</span> corrections to the measured parameters and aerodynamic coefficients for full span and semispan models when the tunnels are in the solid-wall configuration. From a data quality point of view, these corrections remove predictable bias errors in the measurement due to the presence of the tunnel walls. At the NTF, the method is operational in the off-line and on-line modes, with three tests already computed for wall corrections. At the 14 x 22-ft tunnel, initial implementation has been done based on a test on a full span wing. This facility is currently scheduled for an upgrade to its wall <span class="hlt">pressure</span> measurement system. With the addition of new wall orifices and other instrumentation upgrades, a significant improvement in the wall correction accuracy is expected.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19860000282&hterms=Gun&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DGun','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19860000282&hterms=Gun&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DGun"><span>Controlled-Temperature Hot-<span class="hlt">Air</span> Gun</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Munoz, M. C.</p> <p>1986-01-01</p> <p>Materials that find applications in <span class="hlt">wind</span> tunnels first tested in laboratory. Hot-<span class="hlt">Air</span> Gun differs from commercial units in that flow rate and temperature monitored and controlled. With typical compressed-airsupply <span class="hlt">pressure</span> of 25 to 38 psi (170 to 260 kPa), flow rate and maximum temperature are 34 stdft3/min (0.96 stdm3/min) and 1,090 degrees F (590 degrees C), respectively. Resembling elaborate but carefully regulated hot-<span class="hlt">air</span> gun, setup used to apply blasts of <span class="hlt">air</span> temperatures above 1,500 degrees F (815 degrees C) to test specimens.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820015361','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820015361"><span>Determination of <span class="hlt">wind</span> tunnel constraint effects by a unified <span class="hlt">pressure</span> signature method. Part 2: Application to jet-in-crossflow</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hackett, J. E.; Sampath, S.; Phillips, C. G.</p> <p>1981-01-01</p> <p>The development of an improved jet-in-crossflow model for estimating <span class="hlt">wind</span> tunnel blockage and angle-of-attack interference is described. Experiments showed that the simpler existing models fall seriously short of representing far-field flows properly. A new, vortex-source-doublet (VSD) model was therefore developed which employs curved trajectories and experimentally-based singularity strengths. The new model is consistent with existing and new experimental data and it predicts tunnel wall (i.e. far-field) <span class="hlt">pressures</span> properly. It is implemented as a preprocessor to the wall-<span class="hlt">pressure</span>-signature-based tunnel interference predictor. The supporting experiments and theoretical studies revealed some new results. Comparative flow field measurements with 1-inch "free-<span class="hlt">air</span>" and 3-inch impinging jets showed that vortex penetration into the flow, in diameters, was almost unaltered until 'hard' impingement occurred. In modeling impinging cases, a 'plume redirection' term was introduced which is apparently absent in previous models. The effects of this term were found to be very significant.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20737925','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20737925"><span>Compressed-<span class="hlt">air</span> work is entering the field of high <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Le Péchon, J Cl; Gourdon, G</p> <p>2010-01-01</p> <p>Since 1850, compressed-<span class="hlt">air</span> work has been used to prevent shafts or tunnels under construction from flooding. Until the 1980s, workers were digging in compressed-<span class="hlt">air</span> environments. Since the introduction of tunnel boring machines (TBMs), very little digging under <span class="hlt">pressure</span> is needed. However, the wearing out of cutter-head tools requires inspection and repair. Compressed-<span class="hlt">air</span> workers enter the <span class="hlt">pressurized</span> working chamber only occasionally to perform such repairs. <span class="hlt">Pressures</span> between 3.5 and 4.5 bar, that stand outside a reasonable range for <span class="hlt">air</span> breathing, were reached by 2002. Offshore deep diving technology had to be adapted to TBM work. Several sites have used mixed gases: in Japan for deep shaft sinking (4.8 bar), in The Netherlands at Western Scheldt Tunnels (6.9 bar), in Russia for St. Petersburg Metro (5.8 bar) and in the United States at Seattle (5.8 bar). Several tunnel projects are in progress that may involve higher <span class="hlt">pressures</span>: Hallandsås (Sweden) interventions in heliox saturation up to 13 bar, and Lake Mead (U.S.) interventions to about 12 bar (2010). Research on TBMs and grouting technologies tries to reduce the requirements for hyperbaric works. Adapted international rules, expertise and services for saturation work, shuttles and trained personnel matching industrial requirements are the challenges.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930017953','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930017953"><span>Analysis of Fluctuating Static <span class="hlt">Pressure</span> Measurements in a Large High Reynolds Number Transonic Cryogenic <span class="hlt">Wind</span> Tunnel. Ph.D. Thesis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Igoe, William B.</p> <p>1991-01-01</p> <p>Dynamic measurements of fluctuating static <span class="hlt">pressure</span> levels were made using flush mounted high frequency response <span class="hlt">pressure</span> transducers at eleven locations in the circuit of the National Transonic Facility (NTF) over the complete operating range of this <span class="hlt">wind</span> tunnel. Measurements were made at test section Mach numbers from 0.2 to 1.2, at <span class="hlt">pressure</span> from 1 to 8.6 atmospheres and at temperatures from ambient to -250 F, resulting in dynamic flow disturbance measurements at the highest Reynolds numbers available in a transonic ground test facility. Tests were also made independently at variable Mach number, variable Reynolds number, and variable drivepower, each time keeping the other two variables constant thus allowing for the first time, a distinct separation of these three important variables. A description of the NTF emphasizing its flow quality features, details on the calibration of the instrumentation, results of measurements with the test section slots covered, downstream choke, effects of liquid nitrogen injection and gaseous nitrogen venting, comparisons between <span class="hlt">air</span> and nitrogen, isolation of the effects of Mach number, Reynolds number, and fan drive power, and identification of the sources of significant flow disturbances is included. The results indicate that primary sources of flow disturbance in the NTF may be edge-tones generated by test section sidewall re-entry flaps and the venting of nitrogen gas from the return leg of the tunnel circuit between turns 3 and 4 in the cryogenic mode of operation. The tests to isolate the effects of Mach number, Reynolds number, and drive power indicate that Mach number effects predominate. A comparison with other transonic <span class="hlt">wind</span> tunnels shows that the NTF has low levels of test section fluctuating static <span class="hlt">pressure</span> especially in the high subsonic Mach number range from 0.7 to 0.9.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5228218','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5228218"><span>Impacts of Changes of Indoor <span class="hlt">Air</span> <span class="hlt">Pressure</span> and <span class="hlt">Air</span> Exchange Rate in Vapor Intrusion Scenarios</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Shen, Rui; Suuberg, Eric M.</p> <p>2016-01-01</p> <p>There has, in recent years, been increasing interest in understanding the transport processes of relevance in vapor intrusion of volatile organic compounds (VOCs) into buildings on contaminated sites. These studies have included fate and transport modeling. Most such models have simplified the prediction of indoor <span class="hlt">air</span> contaminant vapor concentrations by employing a steady state assumption, which often results in difficulties in reconciling these results with field measurements. This paper focuses on two major factors that may be subject to significant transients in vapor intrusion situations, including the indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and the <span class="hlt">air</span> exchange rate in the subject building. A three-dimensional finite element model was employed with consideration of daily and seasonal variations in these factors. From the results, the variations of indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and <span class="hlt">air</span> exchange rate are seen to contribute to significant variations in indoor <span class="hlt">air</span> contaminant vapor concentrations. Depending upon the assumptions regarding the variations in these parameters, the results are only sometimes consistent with the reports of several orders of magnitude in indoor <span class="hlt">air</span> concentration variations from field studies. The results point to the need to examine more carefully the interplay of these factors in order to quantitatively understand the variations in potential indoor <span class="hlt">air</span> exposures. PMID:28090133</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28090133','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28090133"><span>Impacts of Changes of Indoor <span class="hlt">Air</span> <span class="hlt">Pressure</span> and <span class="hlt">Air</span> Exchange Rate in Vapor Intrusion Scenarios.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shen, Rui; Suuberg, Eric M</p> <p>2016-02-01</p> <p>There has, in recent years, been increasing interest in understanding the transport processes of relevance in vapor intrusion of volatile organic compounds (VOCs) into buildings on contaminated sites. These studies have included fate and transport modeling. Most such models have simplified the prediction of indoor <span class="hlt">air</span> contaminant vapor concentrations by employing a steady state assumption, which often results in difficulties in reconciling these results with field measurements. This paper focuses on two major factors that may be subject to significant transients in vapor intrusion situations, including the indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and the <span class="hlt">air</span> exchange rate in the subject building. A three-dimensional finite element model was employed with consideration of daily and seasonal variations in these factors. From the results, the variations of indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and <span class="hlt">air</span> exchange rate are seen to contribute to significant variations in indoor <span class="hlt">air</span> contaminant vapor concentrations. Depending upon the assumptions regarding the variations in these parameters, the results are only sometimes consistent with the reports of several orders of magnitude in indoor <span class="hlt">air</span> concentration variations from field studies. The results point to the need to examine more carefully the interplay of these factors in order to quantitatively understand the variations in potential indoor <span class="hlt">air</span> exposures.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec57-13015.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>... 30 Mineral Resources 1 2010-07-01 2010-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and...-UNDERGROUND METAL AND NONMETAL MINES Compressed <span class="hlt">Air</span> and Boilers § 57.13015 Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec56-13015.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>... 30 Mineral Resources 1 2010-07-01 2010-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and... METAL AND NONMETAL MINES Compressed <span class="hlt">Air</span> and Boilers § 56.13015 Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels...</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('http://adsabs.harvard.edu/abs/2016AGUFM.A54F..01N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFM.A54F..01N"><span>Further Studies of Observational Undersampling of the Surface <span class="hlt">Wind</span> and <span class="hlt">Pressure</span> Fields in the Hurricane Inner-Core</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nolan, D. S.; Klotz, B.</p> <p>2016-12-01</p> <p>Obtaining the best estimate of tropical cyclone (TC) intensity is vital for operational forecasting centers to produce accurate forecasts and to issue appropriate warnings. Aircraft data traditionally provide the most reliable information about the TC inner core and surrounding environment, but sampling strategies and observing platforms associated with reconnaissance aircraft have inherent deficiencies that contribute to the uncertainty of the intensity estimate. One such instrument, the stepped frequency microwave radiometer (SFMR) on the NOAA WP-3D aircraft, provides surface <span class="hlt">wind</span> speeds along the aircraft flight track. However, the standard "figure-4" flight pattern substantially limits the azimuthal coverage of the eyewall, such that the chance of observing the true peak <span class="hlt">wind</span> speeds is actually quite small. By simulating flights through a high-resolution simulation of Hurricane Isabel (2003), a previous study found that the 1-minute mean (maximum) SFMR <span class="hlt">winds</span> underestimate a 6-hour running mean maximum <span class="hlt">wind</span> (i.e. best track) by 7.5-10%. This project applies the same methodology to a suite of hurricane simulations with even higher resolution and more sophisticated physical parameterizations. These include the hurricane nature run of Nolan et al. (2013), the second hurricane nature run, a simulation of Hurricane Bill (2009), and additional idealized simulations. For the nature run cases, we find that the mean underestimate of the best-track estimate is 12-15%, considerably higher than determined from the Isabel simulation, while the other cases are similar to the previous result. Comparisons of the various cases indicates that the primary factors that lead to greater undersampling rates are storm size and storm asymmetry. Minimum surface <span class="hlt">pressure</span> is also frequently estimated from <span class="hlt">pressures</span> reported by dropsondes released into the eye, with a standard correction of 1 hPa per 10 knots of <span class="hlt">wind</span> at the time of "splash." Statistics from thousands of simulated splash</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091386','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091386"><span>Tables for <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zahm, A F; Louden, F A</p> <p>1930-01-01</p> <p>In Technical Report no. 247 of the National Advisory Committee for Aeronautics theoretical formulas are given from which was computed a table for the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds, such as those of aircraft and propeller blades. In that report, the table gave incompressible and adiabatic stop <span class="hlt">pressures</span> of <span class="hlt">air</span> for even-speed intervals in miles per hour and for some even-speed intervals in knots per hour. Table II of the present report extends the above-mentioned table by including the stop <span class="hlt">pressures</span> of <span class="hlt">air</span> for even-speed intervals in miles per hour, feet per-second, knots per hour, kilometers per hour, and meters per second. The <span class="hlt">pressure</span> values in table II are also more exact than values given in the previous table. To furnish the aeronautical engineer with ready numerical formulas for finding the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest, table I has been derived for the standard values specified below it. This table first presents the theoretical <span class="hlt">pressure</span>-speed formulas and their working forms in C. G. S. Units as given in NACA Technical Report No. 247, then furnishes additional working formulas for several special units of speed. (author)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010cosp...38.3367R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010cosp...38.3367R"><span><span class="hlt">Air</span> Circulation and Heat Exchange under Reduced <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rygalov, Vadim; Wheeler, Raymond; Dixon, Mike; Hillhouse, Len; Fowler, Philip</p> <p></p> <p>Low <span class="hlt">pressure</span> atmospheres were suggested for Space Greenhouses (SG) design to minimize sys-tem construction and re-supply materials, as well as system manufacturing and deployment costs. But rarified atmospheres modify heat exchange mechanisms what finally leads to alter-ations in thermal control for low <span class="hlt">pressure</span> closed environments. Under low atmospheric <span class="hlt">pressures</span> (e.g., lower than 25 kPa compare to 101.3 kPa for normal Earth atmosphere), convection is becoming replaced by diffusion and rate of heat exchange reduces significantly. During a period from 2001 to 2009, a series of hypobaric experiments were conducted at Space Life Sciences Lab (SLSLab) NASA's Kennedy Space Center and the Department of Space Studies, University of North Dakota. Findings from these experiments showed: -<span class="hlt">air</span> circulation rate decreases non-linearly with lowering of total atmospheric <span class="hlt">pressure</span>; -heat exchange slows down with <span class="hlt">pressure</span> decrease creating risk of thermal stress (elevated leaf tem-peratures) for plants in closed environments; -low <span class="hlt">pressure</span>-induced thermal stress could be reduced by either lowering system temperature set point or increasing forced convection rates (circulation fan power) within certain limits; <span class="hlt">Air</span> circulation is an important constituent of controlled environments and plays crucial role in material and heat exchange. Theoretical schematics and mathematical models are developed from a series of observations. These models can be used to establish optimal control algorithms for low <span class="hlt">pressure</span> environments, such as a space greenhouse, as well as assist in fundamental design concept developments for these or similar habitable structures.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880020437','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880020437"><span>An experimental study of an adaptive-wall <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Celik, Zeki; Roberts, Leonard</p> <p>1988-01-01</p> <p>A series of adaptive wall ventilated <span class="hlt">wind</span> tunnel experiments was carried out to demonstrate the feasibility of using the side wall <span class="hlt">pressure</span> distribution as the flow variable for the assessment of compatibility with free <span class="hlt">air</span> conditions. Iterative and one step convergence methods were applied using the streamwise velocity component, the side wall <span class="hlt">pressure</span> distribution and the normal velocity component in order to investigate their relative merits. The advantage of using the side wall <span class="hlt">pressure</span> as the flow variable is to reduce the data taking time which is one the major contributors to the total testing time. In ventilated adaptive wall <span class="hlt">wind</span> tunnel testing, side wall <span class="hlt">pressure</span> measurements require simple instrumentation as opposed to the Laser Doppler Velocimetry used to measure the velocity components. In ventilated adaptive wall tunnel testing, influence coefficients are required to determine the <span class="hlt">pressure</span> corrections in the plenum compartment. Experiments were carried out to evaluate the influence coefficients from side wall <span class="hlt">pressure</span> distributions, and from streamwise and normal velocity distributions at two control levels. Velocity measurements were made using a two component Laser Doppler Velocimeter system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110011475','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110011475"><span>Statistical Short-Range Guidance for Peak <span class="hlt">Wind</span> Speed Forecasts at Edwards <span class="hlt">Air</span> Force Base, CA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dreher, Joseph G.; Crawford, Winifred; Lafosse, Richard; Hoeth, Brian; Burns, Kerry</p> <p>2009-01-01</p> <p>The peak <span class="hlt">winds</span> near the surface are an important forecast element for space shuttle landings. As defined in the Flight Rules (FR), there are peak <span class="hlt">wind</span> thresholds that cannot be exceeded in order to ensure the safety of the shuttle during landing operations. The National Weather Service Spaceflight Meteorology Group (SMG) is responsible for weather forecasts for all shuttle landings, and is required to issue surface average and 10-minute peak <span class="hlt">wind</span> speed forecasts. They indicate peak <span class="hlt">winds</span> are a challenging parameter to forecast. To alleviate the difficulty in making such <span class="hlt">wind</span> forecasts, the Applied Meteorology Unit (AMU) developed a PC-based graphical user interface (GUI) for displaying peak <span class="hlt">wind</span> climatology and probabilities of exceeding peak <span class="hlt">wind</span> thresholds for the Shuttle Landing Facility (SLF) at Kennedy Space Center (KSC; Lambert 2003). However, the shuttle occasionally may land at Edwards <span class="hlt">Air</span> Force Base (EAFB) in southern California when weather conditions at KSC in Florida are not acceptable, so SMG forecasters requested a similar tool be developed for EAFB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28501653','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28501653"><span>Incorporating <span class="hlt">wind</span> availability into land use regression modelling of <span class="hlt">air</span> quality in mountainous high-density urban environment.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shi, Yuan; Lau, Kevin Ka-Lun; Ng, Edward</p> <p>2017-08-01</p> <p>Urban <span class="hlt">air</span> quality serves as an important function of the quality of urban life. Land use regression (LUR) modelling of <span class="hlt">air</span> quality is essential for conducting health impacts assessment but more challenging in mountainous high-density urban scenario due to the complexities of the urban environment. In this study, a total of 21 LUR models are developed for seven kinds of <span class="hlt">air</span> pollutants (gaseous <span class="hlt">air</span> pollutants CO, NO 2 , NO x , O 3 , SO 2 and particulate <span class="hlt">air</span> pollutants PM 2.5 , PM 10 ) with reference to three different time periods (summertime, wintertime and annual average of 5-year long-term hourly monitoring data from local <span class="hlt">air</span> quality monitoring network) in Hong Kong. Under the mountainous high-density urban scenario, we improved the traditional LUR modelling method by incorporating <span class="hlt">wind</span> availability information into LUR modelling based on surface geomorphometrical analysis. As a result, 269 independent variables were examined to develop the LUR models by using the "ADDRESS" independent variable selection method and stepwise multiple linear regression (MLR). Cross validation has been performed for each resultant model. The results show that <span class="hlt">wind</span>-related variables are included in most of the resultant models as statistically significant independent variables. Compared with the traditional method, a maximum increase of 20% was achieved in the prediction performance of annual averaged NO 2 concentration level by incorporating <span class="hlt">wind</span>-related variables into LUR model development. Copyright © 2017 Elsevier Inc. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA020223','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA020223"><span>Aircraft Carrier Turbulence Study for Predicting <span class="hlt">Air</span> Flow Dynamics with Increasing <span class="hlt">Wind</span>-Over-Deck Velocities</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1968-03-28</p> <p>AD-A020 223 AIRCRAFT CARRIER TURBULENCE STUDY FOR PREDICTING <span class="hlt">AIR</span> FLOW DYNAMICS WITH INCREASING <span class="hlt">WIND</span>-OVER-DECK VELOCITIES S. Frost Naval <span class="hlt">Air</span>...Copy NAVAL <span class="hlt">AIR</span> ENGINEERING CENTERElPILAOUPHBA, PENNSYLVANIA 19112 Q Had-NG7~ CODE IDEN NO. *OOM 28 MARCH 4fe AIRCRAFT CARRIER TUJRBULENCE STUDY FOR...carrier dynamics. Ike- comirendations for future experimental and theoretical studies are give,. DD 1473 EDITIOIN 0F I NOV SS IS O@SOLETE S - ’i02</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010059240','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010059240"><span>Development of Dynamic Flow Field <span class="hlt">Pressure</span> Probes Suitable for Use in Large Scale Supersonic <span class="hlt">Wind</span> Tunnels</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</p> <p>2000-01-01</p> <p>A series of dynamic flow field <span class="hlt">pressure</span> probes were developed for use in large-scale supersonic <span class="hlt">wind</span> tunnels at NASA Glenn Research Center. These flow field probes include pitot, static, and five-hole conical <span class="hlt">pressure</span> probes that are capable of capturing fast acting flow field <span class="hlt">pressure</span> transients that occur on a millisecond time scale. The pitot and static probes can be used to determine local Mach number time histories during a transient event. The five-hole conical <span class="hlt">pressure</span> probes are used primarily to determine local flow angularity, but can also determine local Mach number. These probes were designed, developed, and tested at the NASA Glenn Research Center. They were also used in a NASA Glenn 10-by 10-Foot Supersonic <span class="hlt">Wind</span> Tunnel (SWT) test program where they successfully acquired flow field <span class="hlt">pressure</span> data in the vicinity of a propulsion system during an engine compressor staff and inlet unstart transient event. Details of the design, development, and subsequent use of these probes are discussed in this report.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19750021905','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19750021905"><span>Development of solar <span class="hlt">wind</span> shock models with tensor plasma <span class="hlt">pressure</span> for data analysis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Abraham-Shrauner, B.</p> <p>1975-01-01</p> <p>The development of solar <span class="hlt">wind</span> shock models with tensor plasma <span class="hlt">pressure</span> and the comparison of some of the shock models with the satellite data from Pioneer 6 through Pioneer 9 are reported. Theoretically, difficulties were found in non-turbulent fluid shock models for tensor <span class="hlt">pressure</span> plasmas. For microscopic shock theories nonlinear growth caused by plasma instabilities was frequently not clearly demonstrated to lead to the formation of a shock. As a result no clear choice for a shock model for the bow shock or interplanetary tensor <span class="hlt">pressure</span> shocks emerged.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1353479-value-compressed-air-energy-storage-wind-transmission-constrained-electric-power-systems','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1353479-value-compressed-air-energy-storage-wind-transmission-constrained-electric-power-systems"><span>The value of compressed <span class="hlt">air</span> energy storage with <span class="hlt">wind</span> in transmission-constrained electric power systems</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Denholm, Paul; Sioshansi, Ramteen</p> <p>2009-05-05</p> <p>In this paper, we examine the potential advantages of co-locating <span class="hlt">wind</span> and energy storage to increase transmission utilization and decrease transmission costs. Co-location of <span class="hlt">wind</span> and storage decreases transmission requirements, but also decreases the economic value of energy storage compared to locating energy storage at the load. This represents a tradeoff which we examine to estimate the transmission costs required to justify moving storage from load-sited to <span class="hlt">wind</span>-sited in three different locations in the United States. We examined compressed <span class="hlt">air</span> energy storage (CAES) in three “<span class="hlt">wind</span> by wire” scenarios with a variety of transmission and CAES sizes relative to amore » given amount of <span class="hlt">wind</span>. In the sites and years evaluated, the optimal amount of transmission ranges from 60% to 100% of the <span class="hlt">wind</span> farm rating, with the optimal amount of CAES equal to 0–35% of the <span class="hlt">wind</span> farm rating, depending heavily on <span class="hlt">wind</span> resource, value of electricity in the local market, and the cost of natural gas.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=heat+AND+exchange&pg=3&id=EJ582662','ERIC'); return false;" href="https://eric.ed.gov/?q=heat+AND+exchange&pg=3&id=EJ582662"><span>Balloons and Bottles: Activities on <span class="hlt">Air</span>-Sea Heat Exchange.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Murphree, Tom</p> <p>1998-01-01</p> <p>Presents an activity designed to demonstrate how heating and cooling an <span class="hlt">air</span> mass affects its temperature, volume, density, and <span class="hlt">pressure</span>. Illustrates how thermal energy can cause atmospheric motion such as expansion, contraction, and <span class="hlt">winds</span>. (Author/WRM)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDM17009G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDM17009G"><span>Harnessing <span class="hlt">Wind</span> Power in Moving Reference Frames with Application to Vehicles</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Goushcha, Oleg; Felicissimo, Robert; Danesh-Yazdi, Amir; Andreopoulos, Yiannis</p> <p>2017-11-01</p> <p>The extraction of <span class="hlt">wind</span> power from unique configurations embedded in moving vehicles by using micro-turbine devices has been investigated. In such moving environments, the specific power of the <span class="hlt">air</span> motion is much greater and less intermittent than in stationary <span class="hlt">wind</span> turbines anchored to the ground in open atmospheric conditions. In a translational frame of reference, the rate of work done by the drag force acting on the <span class="hlt">wind</span> harnessing device due the relative motion of <span class="hlt">air</span> should be taken into account in the overall performance evaluation through an energy balance. A device with a venting tube has been tested that connects a high-<span class="hlt">pressure</span> stagnating flow region in the front of the vehicle with a low-<span class="hlt">pressure</span> region at its rear. Our analysis identified two key areas to focus on for potentially significant rewards: (1) Vehicles with high energy conversion efficiency which require a high mass flow rate through the venting duct, and (2) low efficiency vehicles with wakes, which will be globally affected by the introduction of the venting duct device in a manner that reduces their drag so that there is a net gain in power generation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840014842','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840014842"><span>Aerodynamic effect of combustor inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> on fuel jet atomization</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ingebo, R. D.</p> <p>1984-01-01</p> <p>Mean drop diameters were measured with a recently developed scanning radiometer in a study of the atomization of liquid jets injected cross stream in high velocity and high <span class="hlt">pressure</span> airflows. At constant inlet <span class="hlt">air</span> <span class="hlt">pressure</span>, reciprocal mean drop diameter, was correlated with airflow mass velocity. Over a combustor inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> range of 1 to 21 atmospheres, the ratio of orifice to mean drop diameter, D(O)/D(M), was correlated with the product of Weber and Reynolds number, WeRe, and with the molecular scale momentum transfer ratio of gravitational to inertial forces.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ExFl...57...64G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ExFl...57...64G"><span>Free-stream static <span class="hlt">pressure</span> measurements in the Longshot hypersonic <span class="hlt">wind</span> tunnel and sensitivity analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Grossir, Guillaume; Van Hove, Bart; Paris, Sébastien; Rambaud, Patrick; Chazot, Olivier</p> <p>2016-05-01</p> <p>The performance of fast-response slender static <span class="hlt">pressure</span> probes is evaluated in the short-duration, cold-gas, VKI Longshot hypersonic <span class="hlt">wind</span> tunnel. Free-stream Mach numbers range between 9.5 and 12, and unit Reynolds numbers are within 3-10 × 106/m. Absolute <span class="hlt">pressure</span> sensors are fitted within the probes, and an inexpensive calibration method, suited to low static <span class="hlt">pressure</span> environments (200-1000 Pa), is described. Transfer functions relating the probe measurements p w to the free-stream static <span class="hlt">pressure</span> p ∞ are established for the Longshot flow conditions based on numerical simulations. The <span class="hlt">pressure</span> ratios p w / p ∞ are found to be close to unity for both laminar and turbulent boundary layers. Weak viscous effects characterized by small viscous interaction parameters {bar{χ }}<1.5 are confirmed experimentally for probe aspect ratios of L/ D > 16.5 by installing multiple <span class="hlt">pressure</span> sensors in a single probe. The effect of <span class="hlt">pressure</span> orifice geometry is also evaluated experimentally and found to be negligible for either straight or chamfered holes, 0.6-1 mm in diameter. No sensitivity to probe angle of attack could be evidenced for α < 0.33°. <span class="hlt">Pressure</span> measurements are compared to theoretical predictions assuming an isentropic nozzle flow expansion. Significant deviations from this ideal case and the Mach 14 contoured nozzle design are uncovered. Validation of the static <span class="hlt">pressure</span> measurements is obtained by comparing shock wave locations on Schlieren photographs to numerical predictions using free-stream properties derived from the static <span class="hlt">pressure</span> probes. While these results apply to the Longshot <span class="hlt">wind</span> tunnel, the present methodology and sensitivity analysis can guide similar investigations for other hypersonic test facilities.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150002878','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150002878"><span>Development of a Climatology of Vertically Complete <span class="hlt">Wind</span> Profiles from Doppler Radar <span class="hlt">Wind</span> Profiler Systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Barbre, Robert, Jr.</p> <p>2015-01-01</p> <p>Assessment of space vehicle loads and trajectories during design requires a large sample of <span class="hlt">wind</span> profiles at the altitudes where <span class="hlt">winds</span> affect the vehicle. Traditionally, this altitude region extends from near 8-14 km to address maximum dynamic <span class="hlt">pressure</span> upon ascent into space, but some applications require knowledge of measured <span class="hlt">wind</span> profiles at lower altitudes. Such applications include crew capsule pad abort and plume damage analyses. Two Doppler Radar <span class="hlt">Wind</span> Profiler (DRWP) systems exist at the United States <span class="hlt">Air</span> Force (USAF) Eastern Range and at the National Aeronautics and Space Administration's Kennedy Space Center. The 50-MHz DRWP provides <span class="hlt">wind</span> profiles every 3-5 minutes from roughly 2.5-18.5 km, and five 915-MHz DRWPs provide <span class="hlt">wind</span> profiles every 15 minutes from approximately 0.2-3.0 km. Archived <span class="hlt">wind</span> profiles from all systems underwent rigorous quality control (QC) processes, and concurrent measurements from the QC'ed 50- and 915-MHz DRWP archives were spliced into individual profiles that extend from about 0.2-18.5 km. The archive contains combined profiles from April 2000 to December 2009, and thousands of profiles during each month are available for use by the launch vehicle community. This paper presents the details of the QC and splice methodology, as well as some attributes of the archive.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ZNatA..71.1167F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ZNatA..71.1167F"><span>Bernoulli-Langevin <span class="hlt">Wind</span> Speed Model for Simulation of Storm Events</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fürstenau, Norbert; Mittendorf, Monika</p> <p>2016-12-01</p> <p>We present a simple nonlinear dynamics Langevin model for predicting the instationary <span class="hlt">wind</span> speed profile during storm events typically accompanying extreme low-<span class="hlt">pressure</span> situations. It is based on a second-degree Bernoulli equation with δ-correlated Gaussian noise and may complement stationary stochastic <span class="hlt">wind</span> models. Transition between increasing and decreasing <span class="hlt">wind</span> speed and (quasi) stationary normal <span class="hlt">wind</span> and storm states are induced by the sign change of the controlling time-dependent rate parameter k(t). This approach corresponds to the simplified nonlinear laser dynamics for the incoherent to coherent transition of light emission that can be understood by a phase transition analogy within equilibrium thermodynamics [H. Haken, Synergetics, 3rd ed., Springer, Berlin, Heidelberg, New York 1983/2004.]. Evidence for the nonlinear dynamics two-state approach is generated by fitting of two historical <span class="hlt">wind</span> speed profiles (low-<span class="hlt">pressure</span> situations "Xaver" and "Christian", 2013) taken from Meteorological Terminal <span class="hlt">Air</span> Report weather data, with a logistic approximation (i.e. constant rate coefficients k) to the solution of our dynamical model using a sum of sigmoid functions. The analytical solution of our dynamical two-state Bernoulli equation as obtained with a sinusoidal rate ansatz k(t) of period T (=storm duration) exhibits reasonable agreement with the logistic fit to the empirical data. Noise parameter estimates of speed fluctuations are derived from empirical fit residuals and by means of a stationary solution of the corresponding Fokker-Planck equation. Numerical simulations with the Bernoulli-Langevin equation demonstrate the potential for stochastic <span class="hlt">wind</span> speed profile modeling and predictive filtering under extreme storm events that is suggested for applications in anticipative <span class="hlt">air</span> traffic management.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21514044','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21514044"><span>Temperature and <span class="hlt">pressure</span> influence on maximum rates of <span class="hlt">pressure</span> rise during explosions of propane-<span class="hlt">air</span> mixtures in a spherical vessel.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razus, D; Brinzea, V; Mitu, M; Movileanu, C; Oancea, D</p> <p>2011-06-15</p> <p>The maximum rates of <span class="hlt">pressure</span> rise during closed vessel explosions of propane-<span class="hlt">air</span> mixtures are reported, for systems with various initial concentrations, <span class="hlt">pressures</span> and temperatures ([C(3)H(8)]=2.50-6.20 vol.%, p(0)=0.3-1.3 bar; T(0)=298-423 K). Experiments were performed in a spherical vessel (Φ=10 cm) with central ignition. The deflagration (severity) index K(G), calculated from experimental values of maximum rates of <span class="hlt">pressure</span> rise is examined against the adiabatic deflagration index, K(G, ad), computed from normal burning velocities and peak explosion <span class="hlt">pressures</span>. At constant temperature and fuel/oxygen ratio, both the maximum rates of <span class="hlt">pressure</span> rise and the deflagration indices are linear functions of total initial <span class="hlt">pressure</span>, as reported for other fuel-<span class="hlt">air</span> mixtures. At constant initial <span class="hlt">pressure</span> and composition, the maximum rates of <span class="hlt">pressure</span> rise and deflagration indices are slightly influenced by the initial temperature; some influence of the initial temperature on maximum rates of <span class="hlt">pressure</span> rise is observed only for propane-<span class="hlt">air</span> mixtures far from stoichiometric composition. The differentiated temperature influence on the normal burning velocities and the peak explosion <span class="hlt">pressures</span> might explain this behaviour. Copyright © 2011 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930015891','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930015891"><span>NASA Lewis 8- by 6-foot supersonic <span class="hlt">wind</span> tunnel user manual</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Soeder, Ronald H.</p> <p>1993-01-01</p> <p>The 8- by 6-Foot Supersonic <span class="hlt">Wind</span> Tunnel (SWT) at Lewis Research Center is available for use by qualified researchers. This manual contains tunnel performance maps which show the range of total temperature, total <span class="hlt">pressure</span>, static <span class="hlt">pressure</span>, dynamic <span class="hlt">pressure</span>, altitude, Reynolds number, and mass flow as a function of test section Mach number. These maps are applicable for both the aerodynamic and propulsion cycle. The 8- by 6-Foot Supersonic <span class="hlt">Wind</span> Tunnel is an atmospheric facility with a test section Mach number range from 0.36 to 2.0. General support systems (<span class="hlt">air</span> systems, hydraulic system, hydrogen system, infrared system, laser system, laser sheet system, and schlieren system are also described as are instrumentation and data processing and acquisition systems. Pretest meeting formats are outlined. Tunnel user responsibility and personal safety requirements are also stated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120015454','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120015454"><span>Vandenberg <span class="hlt">Air</span> Force Base Upper Level <span class="hlt">Wind</span> Launch Weather Constraints</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Shafer, Jaclyn A.; Wheeler, Mark M.</p> <p>2012-01-01</p> <p>The 30th Operational Support Squadron Weather Flight (30 OSSWF) provides comprehensive weather services to the space program at Vandenberg <span class="hlt">Air</span> Force Base (VAFB) in California. One of their responsibilities is to monitor upper-level <span class="hlt">winds</span> to ensure safe launch operations of the Minuteman III ballistic missile. The 30 OSSWF tasked the Applied Meteorology Unit (AMU) to analyze VAFB sounding data with the goal of determining the probability of violating (PoV) their upper-level thresholds for <span class="hlt">wind</span> speed and shear constraints specific to this launch vehicle, and to develop a tool that will calculate the PoV of each constraint on the day of launch. In order to calculate the probability of exceeding each constraint, the AMU collected and analyzed historical data from VAFB. The historical sounding data were retrieved from the National Oceanic and Atmospheric Administration Earth System Research Laboratory archive for the years 1994-2011 and then stratified into four sub-seasons: January-March, April-June, July-September, and October-December. The maximum <span class="hlt">wind</span> speed and 1000-ft shear values for each sounding in each subseason were determined. To accurately calculate the PoV, the AMU determined the theoretical distributions that best fit the maximum <span class="hlt">wind</span> speed and maximum shear datasets. Ultimately it was discovered that the maximum <span class="hlt">wind</span> speeds follow a Gaussian distribution while the maximum shear values follow a lognormal distribution. These results were applied when calculating the averages and standard deviations needed for the historical and real-time PoV calculations. In addition to the requirements outlined in the original task plan, the AMU also included forecast sounding data from the Rapid Refresh model. This information provides further insight for the launch weather officers (LWOs) when determining if a <span class="hlt">wind</span> constraint violation will occur over the next few hours on day of launch. The interactive graphical user interface (GUI) for this project was developed in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20050009951&hterms=time+management+skills&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dtime%2Bmanagement%2Bskills','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20050009951&hterms=time+management+skills&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dtime%2Bmanagement%2Bskills"><span><span class="hlt">Wind</span> Prediction Accuracy for <span class="hlt">Air</span> Traffic Management Decision Support Tools</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cole, Rod; Green, Steve; Jardin, Matt; Schwartz, Barry; Benjamin, Stan</p> <p>2000-01-01</p> <p>The performance of <span class="hlt">Air</span> Traffic Management and flight deck decision support tools depends in large part on the accuracy of the supporting 4D trajectory predictions. This is particularly relevant to conflict prediction and active advisories for the resolution of conflicts and the conformance with of traffic-flow management flow-rate constraints (e.g., arrival metering / required time of arrival). Flight test results have indicated that <span class="hlt">wind</span> prediction errors may represent the largest source of trajectory prediction error. The tests also discovered relatively large errors (e.g., greater than 20 knots), existing in pockets of space and time critical to ATM DST performance (one or more sectors, greater than 20 minutes), are inadequately represented by the classic RMS aggregate prediction-accuracy studies of the past. To facilitate the identification and reduction of DST-critical <span class="hlt">wind</span>-prediction errors, NASA has lead a collaborative research and development activity with MIT Lincoln Laboratories and the Forecast Systems Lab of the National Oceanographic and Atmospheric Administration (NOAA). This activity, begun in 1996, has focussed on the development of key metrics for ATM DST performance, assessment of <span class="hlt">wind</span>-prediction skill for state of the art systems, and development/validation of system enhancements to improve skill. A 13 month study was conducted for the Denver Center airspace in 1997. Two complementary <span class="hlt">wind</span>-prediction systems were analyzed and compared to the forecast performance of the then standard 60 km Rapid Update Cycle - version 1 (RUC-1). One system, developed by NOAA, was the prototype 40-km RUC-2 that became operational at NCEP in 1999. RUC-2 introduced a faster cycle (1 hr vs. 3 hr) and improved mesoscale physics. The second system, Augmented <span class="hlt">Winds</span> (AW), is a prototype en route <span class="hlt">wind</span> application developed by MITLL based on the Integrated Terminal <span class="hlt">Wind</span> System (ITWS). AW is run at a local facility (Center) level, and updates RUC predictions based on an</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/2014AIPC.1616..233R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AIPC.1616..233R"><span>Indoor modeling of the <span class="hlt">wind</span> <span class="hlt">pressure</span> in solar installations with flat and step-like frames for HCPV modules</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rumyantsev, Valery D.; Ashcheulov, Yury V.; Chekalin, Alexander V.; Chumakov, Yury S.; Shvarts, Maxim Z.; Timofeev, Vladimir V.</p> <p>2014-09-01</p> <p>As a rule, the HCPV modules are mounted on solar trackers in a form of a flat panel. <span class="hlt">Wind</span> <span class="hlt">pressure</span> is one of the key factors limiting the operation capabilities of such type solar installations. At the PV Lab of the Ioffe Institute, the sun-trackers with step-like frame for modules have been proposed and developed, which have a potential for significant reduction of <span class="hlt">wind</span> <span class="hlt">pressure</span>. Such a reduction is realized in a wide range of the frame tilt angles the most typical for day-light operation of solar installations. In the present work, theoretical consideration and indoor experiments with mechanical models of installation frames have been carried out. A <span class="hlt">wind</span> tunnel has been used as an experimental instrument for quantitative comparison in conventional units of expected <span class="hlt">wind</span> loads on module frames of different designs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMEP43G..02S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMEP43G..02S"><span>A Broad Continuum of Aeolian Impact Ripple Sizes on Mars is Allowed by Low Dynamic <span class="hlt">Wind</span> <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sullivan, R. J., Jr.; Kok, J. F.; Yizhaq, H.</p> <p>2017-12-01</p> <p>Aeolian impact ripples are generated by impacts of <span class="hlt">wind</span>-blown sand grains, and are common in environments with loose sand on Earth and Mars. Previous work has shown that, within a fully developed saltation cloud, impact ripple height grows upward into the boundary layer until limited by the effects of increasing <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> at the crest (e.g., lengthening of splash trajectories, or direct entrainment of grains by the <span class="hlt">wind</span>). On Earth, this process limits ripples of well-sorted 250 µm dune sands to heights of millimeters, and strong <span class="hlt">winds</span> can impose sufficient lateral dynamic <span class="hlt">pressure</span> to flatten and erase these ripples. Rover observations show much larger ripple-like bedforms on Mars, raising questions about their formative mechanism. Here, we hypothesize that two factors allow impact ripples to grow much higher on Mars than on Earth: (1) previous work predicts a much larger difference between impact threshold and fluid threshold <span class="hlt">wind</span> speeds on Mars than on Earth; and (2) recent analysis has revealed how low saltation flux can be initiated and sustained well below fluid threshold on Mars, allowing impact ripples to migrate entirely under prevailing conditions of relatively low <span class="hlt">wind</span> speeds in the thin martian atmosphere. Under these circumstances, martian ripples would need to grow much larger than on Earth before reaching their maximum height limited by <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> effects. Because the initial size of impact ripples is similar on Mars and Earth, this should generate a much broader continuum of impact ripple sizes on Mars. Compared with Earth, far more time should be needed on Mars for impact ripples to achieve their maximum possible size. Consequently, in cases where <span class="hlt">wind</span> azimuths are mixed but one azimuth is more dominant than others, martian impact ripples of all sizes can exist together in the same setting, with the largest examples reflecting the most common/formative <span class="hlt">wind</span> azimuths. In cases where <span class="hlt">wind</span> azimuth is not dominated by a single</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013MeScT..24i5302P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013MeScT..24i5302P"><span>Measurement of temperature and <span class="hlt">pressure</span> on the surface of a blunt cone using FBG sensor in hypersonic <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Prasad, A. S. Guru; Sharath, U.; Nagarjun, V.; Hegde, G. M.; Asokan, S.</p> <p>2013-09-01</p> <p>Measurement of temperature and <span class="hlt">pressure</span> exerted on the leeward surface of a blunt cone specimen has been demonstrated in the present work in a hypersonic <span class="hlt">wind</span> tunnel using fiber Bragg grating (FBG) sensors. The experiments were conducted on a 30° apex-angle blunt cone with 51 mm base diameter at <span class="hlt">wind</span> flow speeds of Mach 6.5 and 8.35 in a 300 mm hypersonic <span class="hlt">wind</span> tunnel of Indian Institute of Science, Bangalore. A special <span class="hlt">pressure</span> insensitive temperature sensor probe along with the conventional bare FBG sensors was used for explicit temperature and aerodynamic <span class="hlt">pressure</span> measurement respectively on the leeward surface of the specimen. computational fluid dynamics (CFD) simulation of the flow field around the blunt cone specimen has also been carried out to obtain the temperature and <span class="hlt">pressure</span> at conditions analogous to experiments. The results obtained from FBG sensors and the CFD simulations are found to be in good agreement with each other.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19720017686','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19720017686"><span>Atmospheric <span class="hlt">pressure</span>, density, temperature and <span class="hlt">wind</span> variations between 50 and 200 km</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Justus, C. G.; Woodrum, A.</p> <p>1972-01-01</p> <p>Data on atmospheric <span class="hlt">pressure</span>, density, temperature and <span class="hlt">winds</span> between 50 and 200 km were collected from sources including Meteorological Rocket Network data, ROBIN falling sphere data, grenade release and pitot tube data, meteor <span class="hlt">winds</span>, chemical release <span class="hlt">winds</span>, satellite data, and others. These data were analyzed by a daily difference method and results on the distribution statistics, magnitude, and spatial structure of the irregular atmospheric variations are presented. Time structures of the irregular variations were determined by the analysis of residuals from harmonic analysis of time series data. The observed height variations of irregular <span class="hlt">winds</span> and densities are found to be in accord with a theoretical relation between these two quantities. The latitude variations (at 50 - 60 km height) show an increasing trend with latitude. A possible explanation of the unusually large irregular <span class="hlt">wind</span> magnitudes of the White Sands MRN data is given in terms of mountain wave generation by the Sierra Nevada range about 1000 km west of White Sands. An analytical method is developed which, based on an analogy of the irregular motion field with axisymmetric turbulence, allows measured or model correlation or structure functions to be used to evaluate the effective frequency spectra of scalar and vector quantities of a spacecraft moving at any speed and at any trajectory elevation angle.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160006469','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160006469"><span>Time-Accurate Unsteady <span class="hlt">Pressure</span> Loads Simulated for the Space Launch System at <span class="hlt">Wind</span> Tunnel Conditions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Alter, Stephen J.; Brauckmann, Gregory J.; Kleb, William L.; Glass, Christopher E.; Streett, Craig L.; Schuster, David M.</p> <p>2015-01-01</p> <p>A transonic flow field about a Space Launch System (SLS) configuration was simulated with the Fully Unstructured Three-Dimensional (FUN3D) computational fluid dynamics (CFD) code at <span class="hlt">wind</span> tunnel conditions. Unsteady, time-accurate computations were performed using second-order Delayed Detached Eddy Simulation (DDES) for up to 1.5 physical seconds. The surface <span class="hlt">pressure</span> time history was collected at 619 locations, 169 of which matched locations on a 2.5 percent <span class="hlt">wind</span> tunnel model that was tested in the 11 ft. x 11 ft. test section of the NASA Ames Research Center's Unitary Plan <span class="hlt">Wind</span> Tunnel. Comparisons between computation and experiment showed that the peak surface <span class="hlt">pressure</span> RMS level occurs behind the forward attach hardware, and good agreement for frequency and power was obtained in this region. Computational domain, grid resolution, and time step sensitivity studies were performed. These included an investigation of pseudo-time sub-iteration convergence. Using these sensitivity studies and experimental data comparisons, a set of best practices to date have been established for FUN3D simulations for SLS launch vehicle analysis. To the author's knowledge, this is the first time DDES has been used in a systematic approach and establish simulation time needed, to analyze unsteady <span class="hlt">pressure</span> loads on a space launch vehicle such as the NASA SLS.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=aerodynamics&pg=5&id=EJ823335','ERIC'); return false;" href="https://eric.ed.gov/?q=aerodynamics&pg=5&id=EJ823335"><span>Respiratory and Laryngeal Responses to an Oral <span class="hlt">Air</span> <span class="hlt">Pressure</span> Bleed during Speech</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Huber, Jessica E.; Stathopoulos, Elaine T.</p> <p>2003-01-01</p> <p>Researchers have hypothesized that the respiratory and laryngeal speech subsystems would respond to an <span class="hlt">air</span> <span class="hlt">pressure</span> bleed, but these responses have not been empirically studied. The present study examined the nature of the responses of the respiratory and laryngeal subsystems to an <span class="hlt">air</span> <span class="hlt">pressure</span> bleed in order to provide information relevant to the…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130010089','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130010089"><span>A Peak <span class="hlt">Wind</span> Probability Forecast Tool for Kennedy Space Center and Cape Canaveral <span class="hlt">Air</span> Force Station</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crawford, Winifred; Roeder, William</p> <p>2008-01-01</p> <p>This conference abstract describes the development of a peak <span class="hlt">wind</span> forecast tool to assist forecasters in determining the probability of violating launch commit criteria (LCC) at Kennedy Space Center (KSC) and Cape Canaveral <span class="hlt">Air</span> Force Station (CCAFS) in east-central Florida. The peak <span class="hlt">winds</span> are an important forecast element for both the Space Shuttle and Expendable Launch Vehicle (ELV) programs. The LCC define specific peak <span class="hlt">wind</span> thresholds for each launch operation that cannot be exceeded in order to ensure the safety of the vehicle. The 45th Weather Squadron (45 WS) has found that peak <span class="hlt">winds</span> are a challenging parameter to forecast, particularly in the cool season months of October through April. Based on the importance of forecasting peak <span class="hlt">winds</span>, the 45 WS tasked the Applied Meteorology Unit (AMU) to develop a short-range peak-<span class="hlt">wind</span> forecast tool to assist in forecasting LCC violatioas.The tool will include climatologies of the 5-minute mean end peak <span class="hlt">winds</span> by month, hour, and direction, and probability distributions of the peak <span class="hlt">winds</span> as a function of the 5-minute mean <span class="hlt">wind</span> speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014BoLMe.150..381W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014BoLMe.150..381W"><span>Numerical Simulations of Laminar <span class="hlt">Air</span>-Water Flow of a Non-linear Progressive Wave at Low <span class="hlt">Wind</span> Speed</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wen, X.; Mobbs, S.</p> <p>2014-03-01</p> <p>A numerical simulation for two-dimensional laminar <span class="hlt">air</span>-water flow of a non-linear progressive water wave with large steepness is performed when the background <span class="hlt">wind</span> speed varies from zero to the wave phase speed. It is revealed that in the water the difference between the analytical solution of potential flow and numerical solution of viscous flow is very small, indicating that both solutions of the potential flow and viscous flow describe the water wave very accurately. In the <span class="hlt">air</span> the solutions of potential and viscous flows are very different due to the effects of viscosity. The velocity distribution in the airflow is strongly influenced by the background <span class="hlt">wind</span> speed and it is found that three <span class="hlt">wind</span> speeds, , (the maximum orbital velocity of a water wave), and (the wave phase speed), are important in distinguishing different features of the flow patterns.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AdAtS..31.1127L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AdAtS..31.1127L"><span>Mapping near-surface <span class="hlt">air</span> temperature, <span class="hlt">pressure</span>, relative humidity and <span class="hlt">wind</span> speed over Mainland China with high spatiotemporal resolution</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Tao; Zheng, Xiaogu; Dai, Yongjiu; Yang, Chi; Chen, Zhuoqi; Zhang, Shupeng; Wu, Guocan; Wang, Zhonglei; Huang, Chengcheng; Shen, Yan; Liao, Rongwei</p> <p>2014-09-01</p> <p>As part of a joint effort to construct an atmospheric forcing dataset for mainland China with high spatiotemporal resolution, a new approach is proposed to construct gridded near-surface temperature, relative humidity, <span class="hlt">wind</span> speed and surface <span class="hlt">pressure</span> with a resolution of 1 km×1 km. The approach comprises two steps: (1) fit a partial thin-plate smoothing spline with orography and reanalysis data as explanatory variables to ground-based observations for estimating a trend surface; (2) apply a simple kriging procedure to the residual for trend surface correction. The proposed approach is applied to observations collected at approximately 700 stations over mainland China. The generated forcing fields are compared with the corresponding components of the National Centers for Environmental Prediction (NCEP) Climate Forecast System Reanalysis dataset and the Princeton meteorological forcing dataset. The comparison shows that, both within the station network and within the resolutions of the two gridded datasets, the interpolation errors of the proposed approach are markedly smaller than the two gridded datasets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800017094','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800017094"><span><span class="hlt">Pressure</span> and temperature fields associated with aero-optics tests. [transonic <span class="hlt">wind</span> tunnel tests</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Raman, K. R.</p> <p>1980-01-01</p> <p>The experimental investigation carried out in a 6 x 6 ft <span class="hlt">wind</span> tunnel on four model configurations in the aero-optics series of tests are described. The data obtained on the random <span class="hlt">pressures</span> (static and total <span class="hlt">pressures</span>) and total temperatures are presented. In addition, the data for static <span class="hlt">pressure</span> fluctuations on the Coelostat turret model are presented. The measurements indicate that the random <span class="hlt">pressures</span> and temperature are negligible compared to their own mean (or steady state) values for the four models considered, thus allowing considerable simplification in the calculations to obtain the statistical properties of the density field. In the case of the Coelostat model tests these simplifications cannot be assumed a priori and require further investigation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec56-13015.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2011-07-01 2011-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec56-13015.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2012-07-01 2012-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec57-13015.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2014-07-01 2014-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec56-13015.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2014-07-01 2014-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec56-13015.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2013-07-01 2013-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec57-13015.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2012-07-01 2012-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec57-13015.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2013-07-01 2013-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec57-13015.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2011-07-01 2011-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19780043820&hterms=Magnetic+energy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DMagnetic%2Benergy','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19780043820&hterms=Magnetic+energy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DMagnetic%2Benergy"><span>Design of single-<span class="hlt">winding</span> energy-storage reactors for dc-to-dc converters using <span class="hlt">air</span>-gapped magnetic-core structures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ohri, A. K.; Wilson, T. G.; Owen, H. A., Jr.</p> <p>1977-01-01</p> <p>A procedure is presented for designing <span class="hlt">air</span>-gapped energy-storage reactors for nine different dc-to-dc converters resulting from combinations of three single-<span class="hlt">winding</span> power stages for voltage stepup, current stepup and voltage stepup/current stepup and three controllers with control laws that impose constant-frequency, constant transistor on-time and constant transistor off-time operation. The analysis, based on the energy-transfer requirement of the reactor, leads to a simple relationship for the required minimum volume of the <span class="hlt">air</span> gap. Determination of this minimum <span class="hlt">air</span> gap volume then permits the selection of either an <span class="hlt">air</span> gap or a cross-sectional core area. Having picked one parameter, the minimum value of the other immediately leads to selection of the physical magnetic structure. Other analytically derived equations are used to obtain values for the required turns, the inductance, and the maximum rms <span class="hlt">winding</span> current. The design procedure is applicable to a wide range of magnetic material characteristics and physical configurations for the <span class="hlt">air</span>-gapped magnetic structure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040087338','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040087338"><span>Data Fusion in <span class="hlt">Wind</span> Tunnel Testing; Combined <span class="hlt">Pressure</span> Paint and Model Deformation Measurements (Invited)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bell, James H.; Burner, Alpheus W.</p> <p>2004-01-01</p> <p>As the benefit-to-cost ratio of advanced optical techniques for <span class="hlt">wind</span> tunnel measurements such as Video Model Deformation (VMD), <span class="hlt">Pressure</span>-Sensitive Paint (PSP), and others increases, these techniques are being used more and more often in large-scale production type facilities. Further benefits might be achieved if multiple optical techniques could be deployed in a <span class="hlt">wind</span> tunnel test simultaneously. The present study discusses the problems and benefits of combining VMD and PSP systems. The desirable attributes of useful optical techniques for <span class="hlt">wind</span> tunnels, including the ability to accommodate the myriad optical techniques available today, are discussed. The VMD and PSP techniques are briefly reviewed. Commonalties and differences between the two techniques are discussed. Recent <span class="hlt">wind</span> tunnel experiences and problems when combining PSP and VMD are presented, as are suggestions for future developments in combined PSP and deformation measurements.</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://ntrs.nasa.gov/search.jsp?R=19840054186&hterms=Fuel+Jet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DFuel%2BJet','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19840054186&hterms=Fuel+Jet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3DFuel%2BJet"><span>Aerodynamic effect of combustor inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> on fuel jet atomization</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ingebo, R. D.</p> <p>1984-01-01</p> <p>Mean drop diameters were measured with a recently developed scanning radiometer in a study of the atomization of liquid jets injected cross stream in high velocity and high <span class="hlt">pressure</span> airflows. At constant inlet <span class="hlt">air</span> <span class="hlt">pressure</span>, reciprocal mean drop diameter was correlated with airflow mass velocity. Over a combustor inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> range of 1 to 21 atmospheres, the ratio of orifice to mean drop diameter, D(O)/D(M), was correlated with the product of Weber and Reynolds number, WeRe, and with the molecular scale momentum transfer ratio of gravitational to inertial forces. Previously announced in STAR as N84-22910</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120016396','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120016396"><span>Design of Rail Instrumentation for <span class="hlt">Wind</span> Tunnel Sonic Boom Measurements and Computational-Experimental Comparisons</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cliff, Susan E.; Elmiligui, A.; Aftosmis, M.; Morgenstern, J.; Durston, D.; Thomas, S.</p> <p>2012-01-01</p> <p>An innovative <span class="hlt">pressure</span> rail concept for <span class="hlt">wind</span> tunnel sonic boom testing of modern aircraft configurations with very low overpressures was designed with an adjoint-based solution-adapted Cartesian grid method. The computational method requires accurate free-<span class="hlt">air</span> calculations of a test article as well as solutions modeling the influence of rail and tunnel walls. Specialized grids for accurate Euler and Navier-Stokes sonic boom computations were used on several test articles including complete aircraft models with flow-through nacelles. The computed <span class="hlt">pressure</span> signatures are compared with recent results from the NASA 9- x 7-foot Supersonic <span class="hlt">Wind</span> Tunnel using the advanced rail design.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMPP31A2258S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMPP31A2258S"><span>Measuring Ancient <span class="hlt">Air</span> <span class="hlt">Pressure</span> Using Fossilized Cyanobacteria</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Silverman, S. N.; Som, S. M.; Gordon, R.; Bebout, B.</p> <p>2016-12-01</p> <p>The evolution of Earth's atmosphere has been governed by biological evolution. The dominant <span class="hlt">air</span> component, nitrogen, has undergone substantial variation over geological time. Today, the partial <span class="hlt">pressure</span> of nitrogen is 0.79 bar, but this value could have been much higher during early Earth1. The nitrogen partial <span class="hlt">pressure</span> is postulated to have dropped to a maximum of 0.5 bar before the Great Oxidation Event 2.4 billion years ago, and subsequently recovered to the 0.8 bar value of our modern atmosphere over the next 330 million years2. We are placing constraints on the trajectory of this recovery by investigating how nitrogen partial <span class="hlt">pressure</span> influences the morphology of a certain species of filamentous cyanobacteria that has been found fossilized in 2 billion year old rocks. These filamentous cyanobacteria convert nitrogen from its dissolved gaseous state (N2) to a biologically useful state (i.e. NH3) when the latter is present at growth-limiting concentrations in their aquatic environment. Such cyanobacteria develop heterocysts (specialized, visually distinct cells), which fix the nitrogen and laterally distribute it to neighboring cells along the one-dimensional filament. We suggest that the distance between heterocysts reflects the nitrogen partial <span class="hlt">pressure</span> dissolved in water, which is related to atmospheric pN2 by Henry's law. In the laboratory, we are quantifying the relationship between heterocyst distance, variance and covariance to atmospheric pN2 by subjecting cyanobacteria (in media devoid of nitrate) to different partial <span class="hlt">pressures</span> of N2 at a constant temperature and lighting for the representative species Anabaena variabilis. As far as we know, such experiments have not been previously conducted. This new geobarometer will complement existing methods of quantifying ancient nitrogen partial <span class="hlt">pressure</span>. 1Goldblatt, Colin, et al. "Nitrogen-enhanced greenhouse warming on early Earth." Nature Geoscience 2 (2009): 891-896. 2Som, S., et al. "Earth's <span class="hlt">air</span> <span class="hlt">pressure</span> 2</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/11071051','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/11071051"><span><span class="hlt">Air</span>-braked cycle ergometers: validity of the correction factor for barometric <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Finn, J P; Maxwell, B F; Withers, R T</p> <p>2000-10-01</p> <p>Barometric <span class="hlt">pressure</span> exerts by far the greatest influence of the three environmental factors (barometric <span class="hlt">pressure</span>, temperature and humidity) on power outputs from <span class="hlt">air</span>-braked ergometers. The barometric <span class="hlt">pressure</span> correction factor for power outputs from <span class="hlt">air</span>-braked ergometers is in widespread use but apparently has never been empirically validated. Our experiment validated this correction factor by calibrating two <span class="hlt">air</span>-braked cycle ergometers in a hypobaric chamber using a dynamic calibration rig. The results showed that if the power output correction for changes in <span class="hlt">air</span> resistance at barometric <span class="hlt">pressures</span> corresponding to altitudes of 38, 600, 1,200 and 1,800 m above mean sea level were applied, then the coefficients of variation were 0.8-1.9% over the range of 160-1,597 W. The overall mean error was 3.0 % but this included up to 0.73 % for the propagated error that was associated with errors in the measurement of: a) temperature b) relative humidity c) barometric <span class="hlt">pressure</span> d) force, distance and angular velocity by the dynamic calibration rig. The overall mean error therefore approximated the +/- 2.0% of true load that was specified by the Laboratory Standards Assistance Scheme of the Australian Sports Commission. The validity of the correction factor for barometric <span class="hlt">pressure</span> on power output was therefore demonstrated over the altitude range of 38-1,800 m.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22056165','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22056165"><span>Multi-stage versus single-stage inflation and deflation cycle for alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattresses to prevent <span class="hlt">pressure</span> ulcers in hospitalised patients: a randomised-controlled clinical trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Demarré, L; Beeckman, D; Vanderwee, K; Defloor, T; Grypdonck, M; Verhaeghe, S</p> <p>2012-04-01</p> <p>The duration and the amount of <span class="hlt">pressure</span> and shear must be reduced in order to minimize the risk of <span class="hlt">pressure</span> ulcer development. Alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattresses with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells have been developed to relieve <span class="hlt">pressure</span> by sequentially inflating and deflating the <span class="hlt">air</span> cells. Evidence about the effectiveness of this type of mattress in clinical practice is lacking. This study aimed to compare the effectiveness of an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress that has a standard single-stage inflation and deflation cycle of the <span class="hlt">air</span> cells with an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. A randomised controlled trial was performed in a convenience sample of 25 wards in five hospitals in Belgium. In total, 610 patients were included and randomly assigned to the experimental group (n=298) or the control group (n=312). In the experimental group, patients were allocated to an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. In the control group, patients were allocated to an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with a standard single-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. The outcome was defined as cumulative <span class="hlt">pressure</span> ulcer incidence (Grade II-IV). An intention-to-treat analysis was performed. There was no significant difference in cumulative <span class="hlt">pressure</span> ulcer incidence (Grade II-IV) between both groups (Exp.=5.7%, Contr.=5.8%, p=0.97). When patients developed a <span class="hlt">pressure</span> ulcer, the median time was 5.0 days in the experimental group (IQR=3.0-8.5) and 8.0 days in the control group (IQR=3.0-8.5) (Mann-Whitney U-test=113, p=0.182). The probability to remain <span class="hlt">pressure</span> ulcer free during the observation period in this trial did not differ significantly between the experimental group and the control group (log-rank χ(2)=0.013, df=1, p=0.911). An alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840014950','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840014950"><span><span class="hlt">Wind</span> and solar powered turbine</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wells, I. D.; Koh, J. L.; Holmes, M. (Inventor)</p> <p>1984-01-01</p> <p>A power generating station having a generator driven by solar heat assisted ambient <span class="hlt">wind</span> is described. A first plurality of radially extendng <span class="hlt">air</span> passages direct ambient <span class="hlt">wind</span> to a radial flow <span class="hlt">wind</span> turbine disposed in a centrally located opening in a substantially disc-shaped structure. A solar radiation collecting surface having black bodies is disposed above the fist plurality of <span class="hlt">air</span> passages and in communication with a second plurality of radial <span class="hlt">air</span> passages. A cover plate enclosing the second plurality of radial <span class="hlt">air</span> passages is transparent so as to permit solar radiation to effectively reach the black bodies. The second plurality of <span class="hlt">air</span> passages direct ambient <span class="hlt">wind</span> and thermal updrafts generated by the black bodies to an axial flow turbine. The rotating shaft of the turbines drive the generator. The solar and <span class="hlt">wind</span> drien power generating system operates in electrical cogeneration mode with a fuel powered prime mover.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PlST...20c5401W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PlST...20c5401W"><span>Exploration to generate atmospheric <span class="hlt">pressure</span> glow discharge plasma in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wenzheng, LIU; Chuanlong, MA; Shuai, ZHAO; Xiaozhong, CHEN; Tahan, WANG; Luxiang, ZHAO; Zhiyi, LI; Jiangqi, NIU; Liying, ZHU; Maolin, CHAI</p> <p>2018-03-01</p> <p>Atmospheric <span class="hlt">pressure</span> glow discharge (APGD) plasma in <span class="hlt">air</span> has high application value. In this paper, the methods of generating APGD plasma in <span class="hlt">air</span> are discussed, and the characteristics of dielectric barrier discharge (DBD) in non-uniform electric field are studied. It makes sure that APGD in <span class="hlt">air</span> is formed by DBD in alternating current electric field with using the absorbing electron capacity of electret materials to provide initial electrons and to end the discharge progress. Through designing electric field to form two-dimensional space varying electric field and three-dimensional space varying electric field, the development of electron avalanches in <span class="hlt">air</span>-gap is suppressed effectively and a large space of APGD plasma in <span class="hlt">air</span> is generated. Further, through combining electrode structures, a large area of APGD plasma in <span class="hlt">air</span> is generated. On the other hand, by using the method of increasing the density of initial electrons, millimeter-gap glow discharge in atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> is formed, and a maximum gap distance between electrodes is 8 mm. By using the APGD plasma surface treatment device composed of contact electrodes, the surface modification of high polymer materials such as aramid fiber and polyester are studied and good effect of modifications is obtained. The present paper provides references for the researchers of industrial applications of plasma.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25030238','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25030238"><span>Can we trust intraocular <span class="hlt">pressure</span> measurements in eyes with intracameral <span class="hlt">air</span>?</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Jóhannesson, Gauti; Lindén, Christina; Eklund, Anders; Behndig, Anders; Hallberg, Per</p> <p>2014-10-01</p> <p>To evaluate the effect of intracameral <span class="hlt">air</span> on intraocular <span class="hlt">pressure</span> (IOP) measurements using Goldmann applanation tonometry (GAT) and applanation resonance tonometry (ART) in an in-vitro porcine eye model. IOP was measured on thirteen freshly enucleated eyes at three reference <span class="hlt">pressures</span>: 20, 30, and 40 mmHg. Six measurements/method were performed in a standardized order with GAT and ART respectively. <span class="hlt">Air</span> was injected intracamerally in the same manner as during Descemet's stripping endothelial keratoplasty (DSEK) and Descemet's membrane endothelial keratoplasty (DMEK), and the measurements were repeated. Measured IOP increased significantly for both tonometry methods after <span class="hlt">air</span> injection: 0.7 ± 2.1 mmHg for GAT and 10.6 ± 4.9 mmHg for ART. This difference was significant at each reference <span class="hlt">pressure</span> for ART but not for GAT. Although slightly affected, this study suggests that we can trust GAT IOP-measurements in eyes with intracameral <span class="hlt">air</span>, such as after DSEK/DMEK operations. Ultrasound-based methods such as ART should not be used.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19840019620&hterms=winglet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dwinglet','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19840019620&hterms=winglet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dwinglet"><span>KC-135 wing and winglet flight <span class="hlt">pressure</span> distributions, loads, and wing deflection results with some <span class="hlt">wind</span> tunnel comparisons</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Montoya, L. C.; Jacobs, P.; Flechner, S.; Sims, R.</p> <p>1982-01-01</p> <p>A full-scale winglet flight test on a KC-135 airplane with an upper winglet was conducted. Data were taken at Mach numbers from 0.70 to 0.82 at altitudes from 34,000 feet to 39,000 feet at stabilized flight conditions for wing/winglet configurations of basic wing tip, 15/-4 deg, 15/-2 deg, and 0/-4 deg winglet cant/incidence. An analysis of selected <span class="hlt">pressure</span> distribution and data showed that with the basic wing tip, the flight and <span class="hlt">wind</span> tunnel wing <span class="hlt">pressure</span> distribution data showed good agreement. With winglets installed, the effects on the wing <span class="hlt">pressure</span> distribution were mainly near the tip. Also, the flight and <span class="hlt">wind</span> tunnel winglet <span class="hlt">pressure</span> distributions had some significant differences primarily due to the oilcanning in flight. However, in general, the agreement was good. For the winglet cant and incidence configuration presented, the incidence had the largest effect on the winglet <span class="hlt">pressure</span> distributions. The incremental flight wing deflection data showed that the semispan <span class="hlt">wind</span> tunnel model did a reasonable job of simulating the aeroelastic effects at the wing tip. The flight loads data showed good agreement with predictions at the design point and also substantiated the predicted structural penalty (load increase) of the 15 deg cant/-2 deg incidence winglet configuration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980227993','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980227993"><span><span class="hlt">Wind</span>-Tunnel Tests of Seven Static-<span class="hlt">Pressure</span> Probes at Transonic Speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Capone, Francis J.</p> <p>1961-01-01</p> <p><span class="hlt">Wind</span>-tunnel tests have been conducted to determine the errors of 3 seven static-<span class="hlt">pressure</span> probes mounted very close to the nose of a body of revolution simulating a missile forebody. The tests were conducted at Mach numbers from 0.80 to 1.08 and at angles of attack from -1.7 deg to 8.4 deg. The test Reynolds number per foot varied from 3.35 x 10(exp 6) to 4.05 x 10(exp 6). For three 4-vane, gimbaled probes, the static-<span class="hlt">pressure</span> errors remained constant throughout the test angle-of-attack range for all Mach numbers except 1.02. For two single-vane, self-rotating probes having two orifices at +/-37.5 deg. from the plane of symmetry on the lower surface of the probe body, the static-<span class="hlt">pressure</span> error varied as much as 1.5 percent of free-stream static <span class="hlt">pressure</span> through the test angle-of- attack range for all Mach numbers. For two fixed, cone-cylinder probes of short length and large diameter, the static-<span class="hlt">pressure</span> error varied over the test angle-of-attack range at constant Mach numbers as much as 8 to 10 percent of free-stream static <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820013163','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820013163"><span>Fluctuating <span class="hlt">pressures</span> on fan blades of a turbofan engine: Static and <span class="hlt">wind</span>-tunnel investigations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Schoenster, J. A.</p> <p>1982-01-01</p> <p>To investigate the fan noise generated from turbofan engines, miniature <span class="hlt">pressure</span> transducers were used to measure the fluctuating <span class="hlt">pressure</span> on the fan blades of a JT15D engine. Tests were conducted with the engine operating on an outdoor test stand and in a <span class="hlt">wind</span> tunnel. It was found that a potential flow interaction between the fan blades and six, large support struts in the bypass duct is a dominant noise source in the JT15D engine. Effects of varying fan speed and the forward speed on the blade <span class="hlt">pressure</span> are also presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19850003724&hterms=foot+model&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dfoot%2Bmodel','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19850003724&hterms=foot+model&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dfoot%2Bmodel"><span>Experiences with a high-blockage model tested in the NASA Ames 12-foot <span class="hlt">pressure</span> <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Coder, D. W.</p> <p>1984-01-01</p> <p>Representation of the flow around full-scale ships was sought in the subsonic <span class="hlt">wind</span> tunnels in order to a Hain Reynolds numbers as high as possible. As part of the quest to attain the largest possible Reynolds number, large models with high blockage are used which result in significant wall interference effects. Some experiences with such a high blockage model tested in the NASA Ames 12-foot <span class="hlt">pressure</span> <span class="hlt">wind</span> tunnel are summarized. The main results of the experiment relating to <span class="hlt">wind</span> tunnel wall interference effects are also presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091863','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091863"><span>Intercooler cooling-<span class="hlt">air</span> weight flow and <span class="hlt">pressure</span> drop for minimum drag loss</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Reuter, J George; Valerino, Michael F</p> <p>1944-01-01</p> <p>An analysis has been made of the drag losses in airplane flight of cross-flow plate and tubular intercoolers to determine the cooling-<span class="hlt">air</span> weight flow and <span class="hlt">pressure</span> drop that give a minimum drag loss for any given cooling effectiveness and, thus, a maximum power-plant net gain due to charge-<span class="hlt">air</span> cooling. The drag losses considered in this analysis are those due to (1) the extra drag imposed on the airplane by the weight of the intercooler, its duct, and its supports and (2) the drag sustained by the cooling <span class="hlt">air</span> in flowing through the intercooler and its duct. The investigation covers a range of conditions of altitude, airspeed, lift-drag ratio, supercharger-<span class="hlt">pressure</span> ratio, and supercharger adiabatic efficiency. The optimum values of cooling <span class="hlt">air</span> <span class="hlt">pressure</span> drop and weight flow ratio are tabulated. Curves are presented to illustrate the results of the analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1002841','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1002841"><span>Detection of <span class="hlt">Wind</span> Turbine Power Performance Abnormalities Using Eigenvalue Analysis</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2014-12-23</p> <p>area, Cp is the power coefficient, β is the blade-pitch angle, λ is the tip-speed ra- tio and u is the <span class="hlt">wind</span> speed (Lydia, Selvakumar , Kumar, & Kumar...2013). Furthermore, the <span class="hlt">air</span> density ρ is equal to: ρ = p RT (2) where p is the absolute <span class="hlt">air</span> <span class="hlt">pressure</span> and R is the specific gas constant; these two...CONFERENCE OF THE PROGNOSTICS AND HEALTH MANAGEMENT SOCIETY 2014 2013 conference on. Cios, K. J., Pedrycz, W., Swiniarski, R . W., & Kurgan, L. A</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1002842','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1002842"><span>Detection of <span class="hlt">Wind</span> Turbine Power Performance Abnormalities Using Eigenvalue Analysis</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2014-10-02</p> <p>area, Cp is the power coefficient, β is the blade-pitch angle, λ is the tip-speed ra- tio and u is the <span class="hlt">wind</span> speed (Lydia, Selvakumar , Kumar, & Kumar...2013). Furthermore, the <span class="hlt">air</span> density ρ is equal to: ρ = p RT (2) where p is the absolute <span class="hlt">air</span> <span class="hlt">pressure</span> and R is the specific gas constant; these two...CONFERENCE OF THE PROGNOSTICS AND HEALTH MANAGEMENT SOCIETY 2014 2013 conference on. Cios, K. J., Pedrycz, W., Swiniarski, R . W., & Kurgan, L. A</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PApGe.tmp.1266S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PApGe.tmp.1266S"><span><span class="hlt">Wind</span>-Induced <span class="hlt">Air</span>-Flow Patterns in an Urban Setting: Observations and Numerical Modeling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sattar, Ahmed M. A.; Elhakeem, Mohamed; Gerges, Bishoy N.; Gharabaghi, Bahram; Gultepe, Ismail</p> <p>2018-04-01</p> <p>City planning can have a significant effect on <span class="hlt">wind</span> flow velocity patterns and thus natural ventilation. Buildings with different heights are roughness elements that can affect the near- and far-field <span class="hlt">wind</span> flow velocity. This paper aims at investigating the impact of an increase in building height on the nearby velocity fields. A prototype urban setting of buildings with two different heights (25 and 62.5 cm) is built up and placed in a <span class="hlt">wind</span> tunnel. <span class="hlt">Wind</span> flow velocity around the buildings is mapped at different heights. <span class="hlt">Wind</span> tunnel measurements are used to validate a 3D-numerical Reynolds averaged Naviers-Stokes model. The validated model is further used to calculate the <span class="hlt">wind</span> flow velocity patterns for cases with different building heights. It was found that increasing the height of some buildings in an urban setting can lead to the formation of large horseshoe vortices and eddies around building corners. A separation area is formed at the leeward side of the building, and the recirculation of <span class="hlt">air</span> behind the building leads to the formation of slow rotation vortices. The opposite effect is observed in the wake (cavity) region of the buildings, where both the cavity length and width are significantly reduced, and this resulted in a pronounced increase in the <span class="hlt">wind</span> flow velocity. A significant increase in the <span class="hlt">wind</span> flow velocity in the wake region of tall buildings with a value of up to 30% is observed. The spatially averaged velocities around short buildings also increased by 25% compared to those around buildings with different heights. The increase in the height of some buildings is found to have a positive effect on the <span class="hlt">wind</span> ventilation at the pedestrian level.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19910035061&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19910035061&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure"><span><span class="hlt">Pressure</span> Distribution and <span class="hlt">Air</span> Data System for the Aeroassist Flight Experiment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gibson, Lorelei S.; Siemers, Paul M., III; Kern, Frederick A.</p> <p>1989-01-01</p> <p>The Aeroassist Flight Experiment (AFE) is designed to provide critical flight data necessary for the design of future Aeroassist Space Transfer Vehicles (ASTV). This flight experiment will provide aerodynamic, aerothermodynamic, and environmental data for verification of experimental and computational flow field techniques. The <span class="hlt">Pressure</span> Distribution and <span class="hlt">Air</span> Data System (PD/ADS), one of the measurement systems incorporated into the AFE spacecraft, is designed to provide accurate <span class="hlt">pressure</span> measurements on the windward surface of the vehicle. These measurements will be used to determine the <span class="hlt">pressure</span> distribution and <span class="hlt">air</span> data parameters (angle of attack, angle of sideslip, and free-stream dynamic <span class="hlt">pressure</span>) encountered by the blunt-bodied vehicle over an altitude range of 76.2 km to 94.5 km. Design and development data are presented and include: measurement requirements, measurement heritage, theoretical studies to define the vehicle environment, flush-mounted orifice configuration, <span class="hlt">pressure</span> transducer selection and performance evaluation data, and <span class="hlt">pressure</span> tubing response analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4288121','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4288121"><span>Acute <span class="hlt">Air</span> Pollution Exposure and Blood <span class="hlt">Pressure</span> at Delivery Among Women With and Without Hypertension</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Männistö, Tuija; Liu, Danping; Leishear, Kira; Sherman, Seth; Laughon, S. Katherine</p> <p>2015-01-01</p> <p>BACKGROUND Chronic <span class="hlt">air</span> pollution exposure increases risk for hypertensive disorders of pregnancy, but the effect of acute <span class="hlt">air</span> pollution exposure on blood <span class="hlt">pressure</span> during pregnancy is less well known. METHODS We studied 151,276 singleton term deliveries from the Consortium on Safe Labor (2002–2008) with clinical blood <span class="hlt">pressure</span> measured at admission to labor/delivery and diagnoses of hypertensive disorders collected from electronic medical records and hospital discharge summaries. <span class="hlt">Air</span> pollution exposures were estimated for the admission hour and the 4 hours preceding admission using a modified version of the Community Multiscale <span class="hlt">Air</span> Quality models and observed <span class="hlt">air</span> monitoring data. Blood <span class="hlt">pressure</span> was categorized as normal; high normal; and mild, moderate, or severe hypertension based on pregnancy cut points. Adjusted ordinal logistic regression estimated the odds of women having a higher admission blood <span class="hlt">pressure</span> category as a function of <span class="hlt">air</span> pollutant, hypertensive disorders, and their interaction effect. RESULTS Odds of high blood <span class="hlt">pressure</span> at admission to labor/delivery were increased in normotensive women after exposure to nitrogen oxides (by 0.2%/5 units), sulfur dioxide (by 0.3%/1 unit), carbon monoxide and several <span class="hlt">air</span> toxics (by 3%–4%/high exposure). The effects were often similar or stronger among women with gestational hypertension and preeclampsia. Exposure to particulate matter <10 μm increased odds of high blood <span class="hlt">pressure</span> in women with preeclampsia by 3%/5 units. CONCLUSIONS <span class="hlt">Air</span> pollution can influence admission blood <span class="hlt">pressure</span> in term deliveries and may increase likelihood of preeclampsia screening at delivery admission. PMID:24795401</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23455767','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23455767"><span>Torricelli and the ocean of <span class="hlt">air</span>: the first measurement of barometric <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>West, John B</p> <p>2013-03-01</p> <p>The recognition of barometric <span class="hlt">pressure</span> was a critical step in the development of environmental physiology. In 1644, Evangelista Torricelli described the first mercury barometer in a remarkable letter that contained the phrase, "We live submerged at the bottom of an ocean of the element <span class="hlt">air</span>, which by unquestioned experiments is known to have weight." This extraordinary insight seems to have come right out of the blue. Less than 10 years before, the great Galileo had given an erroneous explanation for the related problem of pumping water from a deep well. Previously, Gasparo Berti had filled a very long lead vertical tube with water and showed that a vacuum formed at the top. However, Torricelli was the first to make a mercury barometer and understand that the mercury was supported by the <span class="hlt">pressure</span> of the <span class="hlt">air</span>. Aristotle stated that the <span class="hlt">air</span> has weight, although this was controversial for some time. Galileo described a method of measuring the weight of the <span class="hlt">air</span> in detail, but for reasons that are not clear his result was in error by a factor of about two. Torricelli surmised that the <span class="hlt">pressure</span> of the <span class="hlt">air</span> might be less on mountains, but the first demonstration of this was by Blaise Pascal. The first <span class="hlt">air</span> pump was built by Otto von Guericke, and this influenced Robert Boyle to carry out his classical experiments of the physiological effects of reduced barometric <span class="hlt">pressure</span>. These were turning points in the early history of high-altitude physiology.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21305591','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21305591"><span>Comparison of <span class="hlt">air</span>-charged and water-filled urodynamic <span class="hlt">pressure</span> measurement catheters.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cooper, M A; Fletter, P C; Zaszczurynski, P J; Damaser, M S</p> <p>2011-03-01</p> <p>Catheter systems are utilized to measure <span class="hlt">pressure</span> for diagnosis of voiding dysfunction. In a clinical setting, patient movement and urodynamic pumps introduce hydrostatic and motion artifacts into measurements. Therefore, complete characterization of a catheter system includes its response to artifacts as well its frequency response. The objective of this study was to compare the response of two disposable clinical catheter systems: water-filled and <span class="hlt">air</span>-charged, to controlled <span class="hlt">pressure</span> signals to assess their similarities and differences in <span class="hlt">pressure</span> transduction. We characterized frequency response using a transient step test, which exposed the catheters to a sudden change in <span class="hlt">pressure</span>; and a sinusoidal frequency sweep test, which exposed the catheters to a sinusoidal <span class="hlt">pressure</span> wave from 1 to 30 Hz. The response of the catheters to motion artifacts was tested using a vortex and the response to hydrostatic <span class="hlt">pressure</span> changes was tested by moving the catheter tips to calibrated heights. Water-filled catheters acted as an underdamped system, resonating at 10.13 ± 1.03 Hz and attenuating signals at frequencies higher than 19 Hz. They demonstrated significant motion and hydrostatic artifacts. <span class="hlt">Air</span>-charged catheters acted as an overdamped system and attenuated signals at frequencies higher than 3.02 ± 0.13 Hz. They demonstrated significantly less motion and hydrostatic artifacts than water-filled catheters. The transient step and frequency sweep tests gave comparable results. <span class="hlt">Air</span>-charged and water-filled catheters respond to <span class="hlt">pressure</span> changes in dramatically different ways. Knowledge of the characteristics of the <span class="hlt">pressure</span>-measuring system is essential to finding the best match for a specific application. Copyright © 2011 Wiley-Liss, Inc.</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/2018MAP...130..259L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MAP...130..259L"><span>A note on the correlation between circular and linear variables with an application to <span class="hlt">wind</span> direction and <span class="hlt">air</span> temperature data in a Mediterranean climate</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lototzis, M.; Papadopoulos, G. K.; Droulia, F.; Tseliou, A.; Tsiros, I. X.</p> <p>2018-04-01</p> <p>There are several cases where a circular variable is associated with a linear one. A typical example is <span class="hlt">wind</span> direction that is often associated with linear quantities such as <span class="hlt">air</span> temperature and <span class="hlt">air</span> humidity. The analysis of a statistical relationship of this kind can be tested by the use of parametric and non-parametric methods, each of which has its own advantages and drawbacks. This work deals with correlation analysis using both the parametric and the non-parametric procedure on a small set of meteorological data of <span class="hlt">air</span> temperature and <span class="hlt">wind</span> direction during a summer period in a Mediterranean climate. Correlations were examined between hourly, daily and maximum-prevailing values, under typical and non-typical meteorological conditions. Both tests indicated a strong correlation between mean hourly <span class="hlt">wind</span> directions and mean hourly <span class="hlt">air</span> temperature, whereas mean daily <span class="hlt">wind</span> direction and mean daily <span class="hlt">air</span> temperature do not seem to be correlated. In some cases, however, the two procedures were found to give quite dissimilar levels of significance on the rejection or not of the null hypothesis of no correlation. The simple statistical analysis presented in this study, appropriately extended in large sets of meteorological data, may be a useful tool for estimating effects of <span class="hlt">wind</span> on local climate studies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMNH51D1931E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMNH51D1931E"><span>An experimental study of geyser-like flows induced by a <span class="hlt">pressurized</span> <span class="hlt">air</span> pocket</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Elayeb, I. S.; Leon, A.; Choi, Y.; Alnahit, A. O.</p> <p>2015-12-01</p> <p>Previous studies argues that the entrapment of <span class="hlt">pressurized</span> <span class="hlt">air</span> pockets within combined sewer systems can produce geyser flows, which is an oscillating jetting of a mixture of gas-liquid flows. To verify that <span class="hlt">pressurized</span> <span class="hlt">air</span> pockets can effectively produce geysers, laboratory experiments were conducted. However, past experiments were conducted in relatively small-scale apparatus (i.e. maximum φ2" vertical shaft). This study conducted a set of experiments in a larger apparatus. The experimental setup consists of an upstream head tank, a downstream head tank, a horizontal pipe (46.5ft long, φ6") and a vertical pipe (10ft long, φ6"). The initial condition for the experiments is constant flow discharge through the horizontal pipe. The experiments are initiated by injecting an <span class="hlt">air</span> pocket with pre-determined volume and <span class="hlt">pressure</span> at the upstream end of the horizontal pipe. The <span class="hlt">air</span> pocket propagates through the horizontal pipe until it arrives to the vertical shaft, where it is released producing a geyser-like flow. Three flow rates in the horizontal pipe and three injected <span class="hlt">air</span> <span class="hlt">pressures</span> were tested. The variables measured were <span class="hlt">pressure</span> at two locations in the horizontal pipe and two locations in the vertical pipe. High resolution videos at two regions in the vertical shaft were also recorded. To gain further insights in the physics of <span class="hlt">air</span>-water interaction, the laboratory experiments were complemented with numerical simulations conducted using a commercial 3D CFD model, previously validated with experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19760026180','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19760026180"><span>Results of tests CS4 and CS5 to investigate dynamic loads and <span class="hlt">pressures</span> on 0.03-scale models (Ax1319-3/4 and 45-0) of mated 747 cam and space shuttle orbiter in the Boeing transonic <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>1976-01-01</p> <p>A 0.03-scale model of the 747 CAM/Orbiter was tested in an 8 x 12 foot transonic <span class="hlt">wind</span> tunnel. Dynamic loads, <span class="hlt">pressure</span>, and empennage flow field data were obtained using <span class="hlt">pressure</span> transducers, strain gages, and a split film anemometer. The test variables included Mach number, angle of attack, sideslip angle, orbiter tailcone on and off, orbiter partial tailcone, orbiter nozzle <span class="hlt">air</span> scoops, orbiter body flap angle, and orbiter elevon angle.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008IJTPE.128.1439Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008IJTPE.128.1439Y"><span>Insulation Technology in Dry <span class="hlt">Air</span> and Vacuum for a 72kV Low <span class="hlt">Pressured</span> Dry <span class="hlt">Air</span> Insulated Switchgear</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yoshida, Tadahiro; Koga, Hiromi; Harada, Takakazu; Miki, Shinichi; Arioka, Masahiro; Sato, Shinji; Yoshida, Satoru; Inoue, Naoaki; Maruyama, Akihiko; Takeuchi, Toshie</p> <p></p> <p>A new 72kV rated low <span class="hlt">pressured</span> dry <span class="hlt">air</span> insulated switchgear applying electromagnetic actuation and function that supports CBM has been developed. First, dielectric characteristics in dry <span class="hlt">air</span> under lightning impulse application has been investigated at bare and insulator covered electrodes. Dependence of the breakdown electric field strength on the effective area has been clarified to apply the configuration design of the insulation mold for the vacuum interrupter. In addition, moisture volume dependence on surface resistance has been clarified to decide moisture volume in gas <span class="hlt">pressure</span> tank. Next, a new vacuum circuit breaker (VCB) has been designed. To keep dimensions from former 72kV SF6 gas insulated switchgear, distance between contacts in vacuum interrupter is needed to be shorter than that of former switchgear. Voltage withstand capability between electrodes practically designed for vacuum interrupter has been investigated under dc voltage application simulated the small capacitive current breaking test. Gap configuration including contacts and slits has been optimized and distance has been shortened 11% from former switchgear. As a result, the new low <span class="hlt">pressured</span> dry <span class="hlt">air</span> insulated switchgear has been designed comparably in outer size to former SF6 gas insulated switchgear. Using dry <span class="hlt">air</span> as an insulation medium with low <span class="hlt">pressure</span> has been able to reduce the environmental burden.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJCEM..19...69A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJCEM..19...69A"><span>Modeling <span class="hlt">pressure</span> relationships of inspired <span class="hlt">air</span> into the human lung bifurcations through simulations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aghasafari, Parya; Ibrahim, Israr B. M.; Pidaparti, Ramana</p> <p>2018-03-01</p> <p>Applied <span class="hlt">pressure</span> on human lung wall has great importance on setting up protective ventilatory strategies, therefore, estimating <span class="hlt">pressure</span> relationships in terms of specific parameters would provide invaluable information specifically during mechanical ventilation (MV). A three-dimensional model from a healthy human lung MRI is analyzed by computational fluid dynamic (CFD), and results for <span class="hlt">pressure</span> are curve fitted to estimate relationships that associate <span class="hlt">pressure</span> to breathing time, cross section and generation numbers of intended locations. Among all possible functions, it is observed that exponential and polynomial <span class="hlt">pressure</span> functions present most accurate results for normal breathing (NB) and MV, respectively. For validation, <span class="hlt">pressure</span>-location curves from CFD and results from this study are compared and good correlations are found. Also, estimated <span class="hlt">pressure</span> values are used to calculate <span class="hlt">pressure</span> drop and airway resistance to the induced <span class="hlt">air</span> into the lung bifurcations. It is concluded that maximum <span class="hlt">pressure</span> drop appeared in generation number 2 and medium sized airways show higher resistance to <span class="hlt">air</span> flow and that resistance decreased as cross sectional area increased through the model. Results from this study are in good agreement with previous studies and provide potentials for further studies on influence of <span class="hlt">air</span> <span class="hlt">pressure</span> on human lung tissue and reducing lung injuries during MV.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1341735-applying-large-datasets-developing-better-understanding-air-leakage-measurement-homes','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1341735-applying-large-datasets-developing-better-understanding-air-leakage-measurement-homes"><span>Applying large datasets to developing a better understanding of <span class="hlt">air</span> leakage measurement in homes</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Walker, I. S.; Sherman, M. H.; Joh, J.; ...</p> <p>2013-03-01</p> <p><span class="hlt">Air</span> tightness is an important property of building envelopes. It is a key factor in determining infiltration and related wall-performance properties such as indoor <span class="hlt">air</span> quality, maintainability and moisture balance. <span class="hlt">Air</span> leakage in U.S. houses consumes roughly 1/3 of the HVAC energy but provides most of the ventilation used to control IAQ. There are several methods for measuring <span class="hlt">air</span> tightness that may result in different values and sometimes quite different uncertainties. The two main approaches trade off bias and precision errors and thus result indifferent outcomes for accuracy and repeatability. To interpret results from the two approaches, various questions needmore » to be addressed, such as the need to measure the flow exponent, the need to make both <span class="hlt">pressurization</span> and depressurization measurements and the role of <span class="hlt">wind</span> in determining the accuracy and precision of the results. This article uses two large datasets of blower door measurements to reach the following conclusions. For most tests the <span class="hlt">pressure</span> exponent should be measured but for <span class="hlt">wind</span> speeds greater than 6 m/s a fixed <span class="hlt">pressure</span> exponent reduces experimental error. The variability in reported <span class="hlt">pressure</span> exponents is mostly due to changes in envelope leakage characteristics. Finally, it is preferable to test in both <span class="hlt">pressurization</span> and depressurization modes due to significant differences between the results in these two modes.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091314','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091314"><span><span class="hlt">Pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zahm, A F</p> <p>1927-01-01</p> <p>The text gives theoretical formulas from which is computed a table for the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds, such as those of aircraft and propeller blades. <span class="hlt">Pressure</span> graphs are given for speeds from 1 cm. Sec. up to those of swift projectiles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018EPJWC.18002103S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018EPJWC.18002103S"><span>CFD study on the effects of boundary conditions on <span class="hlt">air</span> flow through an <span class="hlt">air</span>-cooled condenser</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sumara, Zdeněk; Šochman, Michal</p> <p>2018-06-01</p> <p>This study focuses on the effects of boundary conditions on effectiveness of an <span class="hlt">air</span>-cooled condenser (ACC). Heat duty of ACC is very often calculated for ideal uniform velocity field which does not correspond to reality. Therefore, this study studies the effect of <span class="hlt">wind</span> and different landscapes on <span class="hlt">air</span> flow through ACC. For this study software OpenFOAM was used and the flow was simulated with the use of RANS equations. For verification of numerical setup a model of one ACC cell with dimensions of platform 1.5×1.5 [m] was used. In this experiment static <span class="hlt">pressures</span> behind fan and <span class="hlt">air</span> flows through a model of surface of condenser for different rpm of fan were measured. In OpenFOAM software a virtual clone of this experiment was built and different meshes, turbulent models and numerical schemes were tested. After tuning up numerical setup virtual model of real ACC system was built. Influence of <span class="hlt">wind</span>, landscape and height of ACC on <span class="hlt">air</span> flow through ACC has been investigated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19770020261','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19770020261"><span>High <span class="hlt">pressure</span> flame system for pollution studies with results for methane-<span class="hlt">air</span> diffusion flames</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, I. M.; Maahs, H. G.</p> <p>1977-01-01</p> <p>A high <span class="hlt">pressure</span> flame system was designed and constructed for studying nitrogen oxide formation in fuel <span class="hlt">air</span> combustion. Its advantages and limitations were demonstrated by tests with a confined laminar methane <span class="hlt">air</span> diffusion flame over the <span class="hlt">pressure</span> range from 1 to 50 atm. The methane issued from a 3.06 mm diameter port concentrically into a stream of <span class="hlt">air</span> contained within a 20.5 mm diameter chimney. As the combustion <span class="hlt">pressure</span> is increased, the flame changes in shape from wide and convex to slender and concave, and there is a marked increase in the amount of luminous carbon. The height of the flame changes only moderately with <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010ems..confE.213M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010ems..confE.213M"><span>Dynamical downscaling of <span class="hlt">wind</span> fields for <span class="hlt">wind</span> power applications</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mengelkamp, H.-T.; Huneke, S.; Geyer, J.</p> <p>2010-09-01</p> <p>Dynamical downscaling of <span class="hlt">wind</span> fields for <span class="hlt">wind</span> power applications H.-T. Mengelkamp*,**, S. Huneke**, J, Geyer** *GKSS Research Center Geesthacht GmbH **anemos Gesellschaft für Umweltmeteorologie mbH Investments in <span class="hlt">wind</span> power require information on the long-term mean <span class="hlt">wind</span> potential and its temporal variations on daily to annual and decadal time scales. This information is rarely available at specific <span class="hlt">wind</span> farm sites. Short-term on-site measurements usually are only performed over a 12 months period. These data have to be set into the long-term perspective through correlation to long-term consistent <span class="hlt">wind</span> data sets. Preliminary <span class="hlt">wind</span> information is often asked for to select favourable <span class="hlt">wind</span> sites over regional and country wide scales. Lack of high-quality <span class="hlt">wind</span> measurements at weather stations was the motivation to start high resolution <span class="hlt">wind</span> field simulations The simulations are basically a refinement of global scale reanalysis data by means of high resolution simulations with an atmospheric mesoscale model using high-resolution terrain and land-use data. The 3-dimensional representation of the atmospheric state available every six hours at 2.5 degree resolution over the globe, known as NCAR/NCEP reanalysis data, forms the boundary conditions for continuous simulations with the non-hydrostatic atmospheric mesoscale model MM5. MM5 is nested in itself down to a horizontal resolution of 5 x 5 km². The simulation is performed for different European countries and covers the period 2000 to present and is continuously updated. Model variables are stored every 10 minutes for various heights. We have analysed the <span class="hlt">wind</span> field primarily. The <span class="hlt">wind</span> data set is consistent in space and time and provides information on the regional distribution of the long-term mean <span class="hlt">wind</span> potential, the temporal variability of the <span class="hlt">wind</span> potential, the vertical variation of the <span class="hlt">wind</span> potential, and the temperature, and <span class="hlt">pressure</span> distribution (<span class="hlt">air</span> density). In the context of <span class="hlt">wind</span> power these data are used </p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1046108','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1046108"><span><span class="hlt">Wind</span> flow through shrouded <span class="hlt">wind</span> turbines</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2017-03-01</p> <p>were so patient with me during this process, sometimes spending hours in the <span class="hlt">wind</span> tunnel room with me while I performed what seemed like endless runs ...disorderly <span class="hlt">wind</span> velocities that result from the rotating turbine blades . In 2011, a study conducted by the White House Office of Science and...targets, and scattering target returns” [4]. Furthermore, the shadowing effects from spinning <span class="hlt">wind</span> turbine blades can adversely impact <span class="hlt">air</span>-traffic</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17390794','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17390794"><span>Classification of spray nozzles based on droplet size distributions and <span class="hlt">wind</span> tunnel tests.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>De Schamphelerie, M; Spanoghe, P; Nuyttens, D; Baetens, K; Cornelis, W; Gabriels, D; Van der Meeren, P</p> <p>2006-01-01</p> <p>Droplet size distribution of a pesticide spray is recognised as a main factor affecting spray drift. As a first approximation, nozzles can be classified based on their droplet size spectrum. However, the risk of drift for a given droplet size distribution is also a function of spray structure, droplet velocities and entrained <span class="hlt">air</span> conditions. <span class="hlt">Wind</span> tunnel tests to determine actual drift potentials of the different nozzles have been proposed as a method of adding an indication of the risk of spray drift to the existing classification based on droplet size distributions (Miller et al, 1995). In this research <span class="hlt">wind</span> tunnel tests were performed in the <span class="hlt">wind</span> tunnel of the International Centre for Eremology (I.C.E.), Ghent University, to determine the drift potential of different types and sizes of nozzles at various spray <span class="hlt">pressures</span>. Flat Fan (F) nozzles Hardi ISO 110 02, 110 03, 110 04, 110 06; Low-Drift (LD) nozzles Hardi ISO 110 02, 110 03, 110 04 and Injet <span class="hlt">Air</span> Inclusion (AI) nozzles Hardi ISO 110 02, 110 03, 110 04 were tested at a spray <span class="hlt">pressures</span> of 2, 3 and 4 bar. The droplet size spectra of the F and the LD nozzles were measured with a Malvern Mastersizer at spray <span class="hlt">pressures</span> 2 bar, 3 bar and 4 bar. The Malvern spectra were used to calculate the Volume Median Diameters (VMD) of the sprays.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24502287','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24502287"><span>Breaking <span class="hlt">wind</span> to survive: fishes that breathe <span class="hlt">air</span> with their gut.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nelson, J A</p> <p>2014-03-01</p> <p>Several taxonomically disparate groups of fishes have evolved the ability to extract oxygen from the <span class="hlt">air</span> with elements of their gut. Despite perceived difficulties with balancing digestive and respiratory function, gut <span class="hlt">air</span> breathing (GAB) has evolved multiple times in fishes and several GAB families are among the most successful fish families in terms of species numbers. When gut segments evolve into an <span class="hlt">air</span>-breathing organ (ABO), there is generally a specialized region for exchange of gases where the gut wall has diminished, vascularization has increased, capillaries have penetrated into the luminal epithelium and surfactant is produced. This specialized region is generally separated from digestive portions of the gut by sphincters. GAB fishes tend to be facultative <span class="hlt">air</span> breathers that use <span class="hlt">air</span> breathing to supplement aquatic respiration in hypoxic waters. Some hindgut breathers may be continuous, but not obligate <span class="hlt">air</span> breathers (obligate <span class="hlt">air</span> breathers drown if denied access to <span class="hlt">air</span>). Gut ABOs are generally used only for oxygen uptake; CO₂ elimination seems to occur via the gills and skin in all GAB fishes studied. Aerial ventilation in GAB fishes is driven primarily by oxygen partial <span class="hlt">pressure</span> of the water (PO₂) and possibly also by metabolic demand. The effect of aerial ventilation on branchial ventilation and the cardiovascular system is complex and generalizations across taxa or ABO type are not currently possible. Blood from GAB fishes generally has a low blood oxygen partial <span class="hlt">pressure</span> that half saturates haemoglobin (p50) with a very low erythrocytic nucleoside triphosphate concentration [NTP]. GAB behaviour in nature depends on the social and ecological context of the animal as well as on physiological factors. © 2014 The Fisheries Society of the British Isles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130012628','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130012628"><span>Developing a Peak <span class="hlt">Wind</span> Probability Forecast Tool for Kennedy Space Center and Cape Canaveral <span class="hlt">Air</span> Force Station</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lambert, WInifred; Roeder, William</p> <p>2007-01-01</p> <p>This conference presentation describes the development of a peak <span class="hlt">wind</span> forecast tool to assist forecasters in determining the probability of violating launch commit criteria (LCC) at Kennedy Space Center (KSC) and Cape Canaveral <span class="hlt">Air</span> Force Station (CCAFS) in east-central Florida. The peak <span class="hlt">winds</span> are an important forecast element for both the Space Shuttle and Expendable Launch Vehicle (ELV) programs. The LCC define specific peak <span class="hlt">wind</span> thresholds for each launch operation that cannot be exceeded in order to ensure the safety of the vehicle. The 45th Weather Squadron (45 WS) has found that peak <span class="hlt">winds</span> are a challenging parameter to forecast, particularly in the cool season months of October through April. Based on the importance of forecasting peak <span class="hlt">winds</span>, the 45 WS tasked the Applied Meteorology Unit (AMU) to develop a short-range peak-<span class="hlt">wind</span> forecast tool to assist in forecasting LCC violations. The tool will include climatologies of the 5-minute mean and peak <span class="hlt">winds</span> by month, hour, and direction, and probability distributions of the peak <span class="hlt">winds</span> as a function of the 5-minute mean <span class="hlt">wind</span> speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880013119','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880013119"><span>Monthly mean global climatology of temperature, <span class="hlt">wind</span>, geopotential height, and <span class="hlt">pressure</span> for 0 - 120 km</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fleming, Eric L.; Chandra, Sushil; Schoeberl, Mark R.; Barnett, John J.</p> <p>1988-01-01</p> <p>A monthly mean climatology is presented of temperature, <span class="hlt">wind</span>, and geopotential height with nearly pole-to-pole coverage (80 S to 80 N) for 0 to 210 km, which can be used as a function of altitude and <span class="hlt">pressure</span>. The purpose is to provide a reference for various atmospheric research and analysis activities. Data sources and methods of computation are described; in general, hydrostatic and thermal <span class="hlt">wind</span> balance are maintained at all levels and latitudes. As observed in a series of cross-sectional plots, this climatology accurately reproduces most of the characteristic features of the atmosphere such as equatorial <span class="hlt">wind</span> and the general structure of the tropopause, stratopause, and mesopause. A series of zonal <span class="hlt">wind</span> profiles is also represented comparing this climatological <span class="hlt">wind</span> with monthly mean climatological direct <span class="hlt">wind</span> measurements in the upper mesosphere and lower thermosphere. The temperature and zonal <span class="hlt">wind</span> climatology at stratospheric levels is compared with corresponding data from the National Meteorological Center, and general agreement is observed between the two data sets. Tables of the climatological values as a function of latitude and height for each month are contained in Appendix B, and are also available in floppy disk.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29255277','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29255277"><span>Satellite Observations of Imprint of Oceanic Current on <span class="hlt">Wind</span> Stress by <span class="hlt">Air</span>-Sea Coupling.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Renault, Lionel; McWilliams, James C; Masson, Sebastien</p> <p>2017-12-18</p> <p>Mesoscale eddies are present everywhere in the ocean and partly determine the mean state of the circulation and ecosystem. The current feedback on the surface <span class="hlt">wind</span> stress modulates the <span class="hlt">air</span>-sea transfer of momentum by providing a sink of mesoscale eddy energy as an atmospheric source. Using nine years of satellite measurements of surface stress and geostrophic currents over the global ocean, we confirm that the current-induced surface stress curl is linearly related to the current vorticity. The resulting coupling coefficient between current and surface stress (s τ [N s m -3 ]) is heterogeneous and can be roughly expressed as a linear function of the mean surface <span class="hlt">wind</span>. s τ expresses the sink of eddy energy induced by the current feedback. This has important implications for <span class="hlt">air</span>-sea interaction and implies that oceanic mean and mesoscale circulations and their effects on surface-layer ventilation and carbon uptake are better represented in oceanic models that include this feedback.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120003387','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120003387"><span>Forecasting Cool Season Daily Peak <span class="hlt">Winds</span> at Kennedy Space Center and Cape Canaveral <span class="hlt">Air</span> Force Station</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Barrett, Joe, III; Short, David; Roeder, William</p> <p>2008-01-01</p> <p>The expected peak <span class="hlt">wind</span> speed for the day is an important element in the daily 24-Hour and Weekly Planning Forecasts issued by the 45th Weather Squadron (45 WS) for planning operations at Kennedy Space Center (KSC) and Cape Canaveral <span class="hlt">Air</span> Force Station (CCAFS). The morning outlook for peak speeds also begins the warning decision process for gusts ^ 35 kt, ^ 50 kt, and ^ 60 kt from the surface to 300 ft. The 45 WS forecasters have indicated that peak <span class="hlt">wind</span> speeds are a challenging parameter to forecast during the cool season (October-April). The 45 WS requested that the Applied Meteorology Unit (AMU) develop a tool to help them forecast the speed and timing of the daily peak and average <span class="hlt">wind</span>, from the surface to 300 ft on KSC/CCAFS during the cool season. The tool must only use data available by 1200 UTC to support the issue time of the Planning Forecasts. Based on observations from the KSC/CCAFS <span class="hlt">wind</span> tower network, surface observations from the Shuttle Landing Facility (SLF), and CCAFS upper-<span class="hlt">air</span> soundings from the cool season months of October 2002 to February 2007, the AMU created multiple linear regression equations to predict the timing and speed of the daily peak <span class="hlt">wind</span> speed, as well as the background average <span class="hlt">wind</span> speed. Several possible predictors were evaluated, including persistence, the temperature inversion depth, strength, and <span class="hlt">wind</span> speed at the top of the inversion, <span class="hlt">wind</span> gust factor (ratio of peak <span class="hlt">wind</span> speed to average <span class="hlt">wind</span> speed), synoptic weather pattern, occurrence of precipitation at the SLF, and strongest <span class="hlt">wind</span> in the lowest 3000 ft, 4000 ft, or 5000 ft. Six synoptic patterns were identified: 1) surface high near or over FL, 2) surface high north or east of FL, 3) surface high south or west of FL, 4) surface front approaching FL, 5) surface front across central FL, and 6) surface front across south FL. The following six predictors were selected: 1) inversion depth, 2) inversion strength, 3) <span class="hlt">wind</span> gust factor, 4) synoptic weather pattern, 5) occurrence of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24795401','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24795401"><span>Acute <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> at delivery among women with and without hypertension.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Männistö, Tuija; Mendola, Pauline; Liu, Danping; Leishear, Kira; Sherman, Seth; Laughon, S Katherine</p> <p>2015-01-01</p> <p>Chronic <span class="hlt">air</span> pollution exposure increases risk for hypertensive disorders of pregnancy, but the effect of acute <span class="hlt">air</span> pollution exposure on blood <span class="hlt">pressure</span> during pregnancy is less well known. We studied 151,276 singleton term deliveries from the Consortium on Safe Labor (2002-2008) with clinical blood <span class="hlt">pressure</span> measured at admission to labor/delivery and diagnoses of hypertensive disorders collected from electronic medical records and hospital discharge summaries. <span class="hlt">Air</span> pollution exposures were estimated for the admission hour and the 4 hours preceding admission using a modified version of the Community Multiscale <span class="hlt">Air</span> Quality models and observed <span class="hlt">air</span> monitoring data. Blood <span class="hlt">pressure</span> was categorized as normal; high normal; and mild, moderate, or severe hypertension based on pregnancy cut points. Adjusted ordinal logistic regression estimated the odds of women having a higher admission blood <span class="hlt">pressure</span> category as a function of <span class="hlt">air</span> pollutant, hypertensive disorders, and their interaction effect. Odds of high blood <span class="hlt">pressure</span> at admission to labor/delivery were increased in normotensive women after exposure to nitrogen oxides (by 0.2%/5 units), sulfur dioxide (by 0.3%/1 unit), carbon monoxide and several <span class="hlt">air</span> toxics (by 3%-4%/high exposure). The effects were often similar or stronger among women with gestational hypertension and preeclampsia. Exposure to particulate matter <10 μm increased odds of high blood <span class="hlt">pressure</span> in women with preeclampsia by 3%/5 units. <span class="hlt">Air</span> pollution can influence admission blood <span class="hlt">pressure</span> in term deliveries and may increase likelihood of preeclampsia screening at delivery admission. © Published by Oxford University Press on behalf of American Journal of Hypertension Ltd 2014. This work is written by (a) US Government employees(s) and is in the public domain in the US.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFM.A22A..03L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFM.A22A..03L"><span>Active Sensing <span class="hlt">Air</span> <span class="hlt">Pressure</span> Using Differential Absorption Barometric Radar</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lin, B.</p> <p>2016-12-01</p> <p>Tropical storms and other severe weathers cause huge life losses and property damages and have major impacts on public safety and national security. Their observations and predictions need to be significantly improved. This effort tries to develop a feasible active microwave approach that measures surface <span class="hlt">air</span> <span class="hlt">pressure</span>, especially over open seas, from space using a Differential-absorption BArometric Radar (DiBAR) operating at 50-55 GHz O2 absorption band in order to constrain assimilated dynamic fields of numerical weather Prediction (NWP) models close to actual conditions. <span class="hlt">Air</span> <span class="hlt">pressure</span> is the most important variable that drives atmospheric dynamics, and currently can only be measured by limited in-situ observations over oceans. Even over land there is no uniform coverage of surface <span class="hlt">air</span> <span class="hlt">pressure</span> measurements. Analyses show that with the proposed space radar the errors in instantaneous (averaged) <span class="hlt">pressure</span> estimates can be as low as 4mb ( 1mb) under all weather conditions. NASA Langley research team has made substantial progresses in advancing the DiBAR concept. The feasibility assessment clearly shows the potential of surface barometry using existing radar technologies. The team has also developed a DiBAR system design, fabricated a Prototype-DiBAR (P-DiBAR) for proof-of-concept, conducted laboratory, ground and airborne P-DiBAR tests. The flight test results are consistent with the instrumentation goals. The precision and accuracy of radar surface <span class="hlt">pressure</span> measurements are within the range of the theoretical analysis of the DiBAR concept. Observational system simulation experiments for space DiBAR performance based on the existing DiBAR technology and capability show substantial improvements in tropical storm predictions, not only for the hurricane track and position but also for the hurricane intensity. DiBAR measurements will provide us an unprecedented level of the prediction and knowledge on global extreme weather and climate conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20020044134','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20020044134"><span>Sensitivity of Global Sea-<span class="hlt">Air</span> CO2 Flux to Gas Transfer Algorithms, Climatological <span class="hlt">Wind</span> Speeds, and Variability of Sea Surface Temperature and Salinity</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>McClain, Charles R.; Signorini, Sergio</p> <p>2002-01-01</p> <p>Sensitivity analyses of sea-<span class="hlt">air</span> CO2 flux to gas transfer algorithms, climatological <span class="hlt">wind</span> speeds, sea surface temperatures (SST) and salinity (SSS) were conducted for the global oceans and selected regional domains. Large uncertainties in the global sea-<span class="hlt">air</span> flux estimates are identified due to different gas transfer algorithms, global climatological <span class="hlt">wind</span> speeds, and seasonal SST and SSS data. The global sea-<span class="hlt">air</span> flux ranges from -0.57 to -2.27 Gt/yr, depending on the combination of gas transfer algorithms and global climatological <span class="hlt">wind</span> speeds used. Different combinations of SST and SSS global fields resulted in changes as large as 35% on the oceans global sea-<span class="hlt">air</span> flux. An error as small as plus or minus 0.2 in SSS translates into a plus or minus 43% deviation on the mean global CO2 flux. This result emphasizes the need for highly accurate satellite SSS observations for the development of remote sensing sea-<span class="hlt">air</span> flux algorithms.</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://www.dtic.mil/docs/citations/ADA094828','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA094828"><span>Evaluation of the Environmental Instruments, Incorporated Series 200 Dual Component <span class="hlt">Wind</span> Set.</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1980-09-01</p> <p>elements is sensed to derive the sign (+ or -), which indicates the <span class="hlt">wind</span> direction across the element pair. The reference arm of the Wheatstone bridge...Csine a for the crosswind axis, r and PF=a Vw Sine a for the headwind axis, r where Pa is the ambient <span class="hlt">air</span> density, Pr is reference density at standard...<span class="hlt">pressure</span> transducer is a hybrid linear silicon device which consists of a diaphragm and <span class="hlt">pressure</span> reference , piezoresistive sensor, signal discriminator</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810024953','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810024953"><span><span class="hlt">Wind</span> loads on flat plate photovoltaic array fields (nonsteady <span class="hlt">winds</span>)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, R. D.; Zimmerman, D. K.</p> <p>1981-01-01</p> <p>Techniques to predict the dynamic response and the structural dynamic loads of flat plate photovoltaic arrays due to <span class="hlt">wind</span> turbulence were analyzed. Guidelines for use in predicting the turbulent portion of the <span class="hlt">wind</span> loading on future similar arrays are presented. The dynamic response and the loads dynamic magnification factor of the two array configurations are similar. The magnification factors at a mid chord and outer chord location on the array illustrated and at four points on the chord are shown. The <span class="hlt">wind</span> tunnel test experimental rms <span class="hlt">pressure</span> coefficient on which magnification factors are based is shown. It is found that the largest response and dynamic magnification factor occur at a mid chord location on an array and near the trailing edge. A technique employing these magnification factors and the <span class="hlt">wind</span> tunnel test rms fluctuating <span class="hlt">pressure</span> coefficients to calculate design <span class="hlt">pressure</span> loads due to <span class="hlt">wind</span> turbulence is presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100036761','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100036761"><span>Weather Research and Forecasting Model <span class="hlt">Wind</span> Sensitivity Study at Edwards <span class="hlt">Air</span> Force Base, CA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Watson, Leela R.; Bauman, William H., III</p> <p>2008-01-01</p> <p>NASA prefers to land the space shuttle at Kennedy Space Center (KSC). When weather conditions violate Flight Rules at KSC, NASA will usually divert the shuttle landing to Edwards <span class="hlt">Air</span> Force Base (EAFB) in Southern California. But forecasting surface <span class="hlt">winds</span> at EAFB is a challenge for the Spaceflight Meteorology Group (SMG) forecasters due to the complex terrain that surrounds EAFB, One particular phenomena identified by SMG is that makes it difficult to forecast the EAFB surface <span class="hlt">winds</span> is called "<span class="hlt">wind</span> cycling". This occurs when <span class="hlt">wind</span> speeds and directions oscillate among towers near the EAFB runway leading to a challenging deorbit bum forecast for shuttle landings. The large-scale numerical weather prediction models cannot properly resolve the <span class="hlt">wind</span> field due to their coarse horizontal resolutions, so a properly tuned high-resolution mesoscale model is needed. The Weather Research and Forecasting (WRF) model meets this requirement. The AMU assessed the different WRF model options to determine which configuration best predicted surface <span class="hlt">wind</span> speed and direction at EAFB, To do so, the AMU compared the WRF model performance using two hot start initializations with the Advanced Research WRF and Non-hydrostatic Mesoscale Model dynamical cores and compared model performance while varying the physics options.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740022383','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740022383"><span>Improved fireman's compressed <span class="hlt">air</span> breathing system <span class="hlt">pressure</span> vessel development program</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>King, H. A.; Morris, E. E.</p> <p>1973-01-01</p> <p>Prototype high <span class="hlt">pressure</span> glass filament-wound, aluminum-lined <span class="hlt">pressurant</span> vessels suitable for use in a fireman's compressed <span class="hlt">air</span> breathing system were designed, fabricated, and acceptance tested in order to demonstrate the feasibility of producing such high performance, lightweight units. The 4000 psi tanks have a 60 standard cubic foot (SCF) <span class="hlt">air</span> capacity, and have a 6.5 inch diamter, 19 inch length, 415 inch volume, weigh 13 pounds when empty, and contain 33 percent more <span class="hlt">air</span> than the current 45 SCF (2250 psi) steel units. The current steel 60 SCF (3000 psi) tanks weigh approximately twice as much as the prototype when empty, and are 2 inches, or 10 percent shorter. The prototype units also have non-rusting aluminum interiors, which removes the hazard of corrosion, the need for internal coatings, and the possibility of rust particles clogging the breathing system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768090','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768090"><span>Torricelli and the Ocean of <span class="hlt">Air</span>: The First Measurement of Barometric <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2013-01-01</p> <p>The recognition of barometric <span class="hlt">pressure</span> was a critical step in the development of environmental physiology. In 1644, Evangelista Torricelli described the first mercury barometer in a remarkable letter that contained the phrase, “We live submerged at the bottom of an ocean of the element <span class="hlt">air</span>, which by unquestioned experiments is known to have weight.” This extraordinary insight seems to have come right out of the blue. Less than 10 years before, the great Galileo had given an erroneous explanation for the related problem of pumping water from a deep well. Previously, Gasparo Berti had filled a very long lead vertical tube with water and showed that a vacuum formed at the top. However, Torricelli was the first to make a mercury barometer and understand that the mercury was supported by the <span class="hlt">pressure</span> of the <span class="hlt">air</span>. Aristotle stated that the <span class="hlt">air</span> has weight, although this was controversial for some time. Galileo described a method of measuring the weight of the <span class="hlt">air</span> in detail, but for reasons that are not clear his result was in error by a factor of about two. Torricelli surmised that the <span class="hlt">pressure</span> of the <span class="hlt">air</span> might be less on mountains, but the first demonstration of this was by Blaise Pascal. The first <span class="hlt">air</span> pump was built by Otto von Guericke, and this influenced Robert Boyle to carry out his classical experiments of the physiological effects of reduced barometric <span class="hlt">pressure</span>. These were turning points in the early history of high-altitude physiology. PMID:23455767</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011AGUFM.A53D..04M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011AGUFM.A53D..04M"><span>Nocturnal <span class="hlt">Air</span> Seiches in the Arizona Meteor Crater</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Muschinski, A.; Fritts, D. C.; Zhong, S.; Oncley, S. P.</p> <p>2011-12-01</p> <p>The Arizona Meteor Crater near Winslow, AZ is 170 m deep, has a diameter of 1.2 km, and it has a nearly circular shape. The motivation of the Meteor Crater Experiment (METCRAX), conducted in October 2006, was to use the Meteor Crater as a natural laboratory to study atmospheric phenomena that are typical for small basins. Among other observations, high-resolution <span class="hlt">wind</span>, temperature and <span class="hlt">pressure</span> measurements were collected with sonics and microbarometers, respectively, during the entire month. The sensors were mounted between 0.5 m and 8.5 m AGL on seven portable towers, five of which were located within the crater and two on the crater rim. Here we report observations of nocturnal <span class="hlt">air</span> seiches, that is, standing gravity waves associated with the time-harmonic sloshing of the cold-<span class="hlt">air</span> pool that forms at the bottom of the crater due to radiative cooling at night. We present time series, spectra, and spectrograms of temperature, <span class="hlt">wind</span> and <span class="hlt">pressure</span> fluctuations that characterize those <span class="hlt">air</span> seiches. Typical seiche periods were 15 min. We compare the observations with the time-harmonic solutions of the shallow-water equation and with numerical simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040090510','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040090510"><span>The Use of Heavy Gas for Increased Reynolds Numbers in Transonic <span class="hlt">Wind</span> Tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anders, J. B.; Anderson, W. K.; Murthy, A. V.</p> <p>1998-01-01</p> <p>The use of a high molecular weight test gas to increase the Reynolds number range of transonic <span class="hlt">wind</span> tunnels is explored. Modifications to a small transonic <span class="hlt">wind</span> tunnel are described and the real gas properties of the example heavy gas (sulfur hexafluoride) are discussed. Sulfur hexafluoride is shown to increase the test Reynolds number by a factor of more than 2 over <span class="hlt">air</span> at the same Mach number. Experimental and computational <span class="hlt">pressure</span> distributions on an advanced supercritical airfoil configuration at Mach 0.7 in both sulfur hexafluoride and nitrogen are presented. Transonic similarity theory is shown to be partially successful in transforming the heavy gas results to equivalent nitrogen (<span class="hlt">air</span>) results, provided the correct definition of gamma is used.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23977309','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23977309"><span>Using <span class="hlt">wind</span> setdown and storm surge on Lake Erie to calibrate the <span class="hlt">air</span>-sea drag coefficient.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Drews, Carl</p> <p>2013-01-01</p> <p>The <span class="hlt">air</span>-sea drag coefficient controls the transfer of momentum from <span class="hlt">wind</span> to water. In modeling storm surge, this coefficient is a crucial parameter for estimating the surge height. This study uses two strong <span class="hlt">wind</span> events on Lake Erie to calibrate the drag coefficient using the Coupled Ocean Atmosphere Wave Sediment Transport (COAWST) modeling system and the the Regional Ocean Modeling System (ROMS). Simulated waves are generated on the lake with Simulating WAves Nearshore (SWAN). <span class="hlt">Wind</span> setdown provides the opportunity to eliminate wave setup as a contributing factor, since waves are minimal at the upwind shore. The study finds that model results significantly underestimate <span class="hlt">wind</span> setdown and storm surge when a typical open-ocean formulation without waves is used for the drag coefficient. The contribution of waves to <span class="hlt">wind</span> setdown and storm surge is 34.7%. Scattered lake ice also increases the effective drag coefficient by a factor of 1.1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20040008261&hterms=environmental+wind+tunnel&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Denvironmental%2Bwind%2Btunnel','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20040008261&hterms=environmental+wind+tunnel&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Denvironmental%2Bwind%2Btunnel"><span>Development and Characterization of a Low-<span class="hlt">Pressure</span> Calibration System for Hypersonic <span class="hlt">Wind</span> Tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Green, Del L.; Everhart, Joel L.; Rhode, Matthew N.</p> <p>2004-01-01</p> <p>Minimization of uncertainty is essential for accurate ESP measurements at very low free-stream static <span class="hlt">pressures</span> found in hypersonic <span class="hlt">wind</span> tunnels. Statistical characterization of environmental error sources requires a well defined and controlled calibration method. A calibration system has been constructed and environmental control software developed to control experimentation to eliminate human induced error sources. The initial stability study of the calibration system shows a high degree of measurement accuracy and precision in temperature and <span class="hlt">pressure</span> control. Control manometer drift and reference <span class="hlt">pressure</span> instabilities induce uncertainty into the repeatability of voltage responses measured from the PSI System 8400 between calibrations. Methods of improving repeatability are possible through software programming and further experimentation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-GSFC_20171208_Archive_e000709.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-GSFC_20171208_Archive_e000709.html"><span>Low <span class="hlt">pressure</span> system off Ireland</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2015-06-16</p> <p>In early June, 2015 a strong low <span class="hlt">pressure</span> system over the North Atlantic Ocean brought rain and gusty <span class="hlt">winds</span> to Ireland and the United Kingdom. The Moderate Resolution Imaging Spectroradiometer (MODIS) aboard NASA’s Aqua satellite captured this true-color image of the spiraling system on June 5. A very deep low <span class="hlt">pressure</span> area lies in the center of the spiral, just off the northwestern shore of emerald-green Ireland. Bands of cloud, containing rain and thunderstorms, swirl into the center of the low, and extend over the British Isles. A low <span class="hlt">pressure</span> system will pull in <span class="hlt">air</span> from the surrounding area, creating spiraling <span class="hlt">winds</span>. <span class="hlt">Winds</span> around the center of a low <span class="hlt">pressure</span> spiral counterclockwise in the Northern Hemisphere, as we see here (clockwise in the Southern Hemisphere) and towards the center of the system. Although the system was impressive on June 5, it intensified over the next several days. According to MarkVoganWeather.com, by June 7 the <span class="hlt">pressure</span> in the unusually deep Atlantic low, which had been hanging around 980mb, was expected to drop lower to about 978mb off of Anglesey, brining northwest gales along the Atlantic west and south coasts of Ireland, England and Wales. <span class="hlt">Winds</span> gust of up to 80 mph were possible, along with heavy rains. Credit: Jeff Schmaltz, MODIS Land Rapid Response Team, NASA GSFC NASA image use policy. NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission. Follow us on Twitter Like us on Facebook Find us on Instagram</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/863380','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/863380"><span>Isokinetic <span class="hlt">air</span> sampler</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Sehmel, George A.</p> <p>1979-01-01</p> <p>An isokinetic <span class="hlt">air</span> sampler includes a filter, a holder for the filter, an <span class="hlt">air</span> pump for drawing <span class="hlt">air</span> through the filter at a fixed, predetermined rate, an inlet assembly for the sampler having an inlet opening therein of a size such that isokinetic <span class="hlt">air</span> sampling is obtained at a particular <span class="hlt">wind</span> speed, a closure for the inlet opening and means for simultaneously opening the closure and turning on the <span class="hlt">air</span> pump when the <span class="hlt">wind</span> speed is such that isokinetic <span class="hlt">air</span> sampling is obtained. A system incorporating a plurality of such samplers provided with <span class="hlt">air</span> pumps set to draw <span class="hlt">air</span> through the filter at the same fixed, predetermined rate and having different inlet opening sizes for use at different <span class="hlt">wind</span> speeds is included within the ambit of the present invention as is a method of sampling <span class="hlt">air</span> to measure airborne concentrations of particulate pollutants as a function of <span class="hlt">wind</span> speed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26712286','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26712286"><span>Adding a custom made <span class="hlt">pressure</span> release valve during <span class="hlt">air</span> enema for intussusception: A new technique.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ahmed, Hosni Morsi; Ahmed, Osama; Ahmed, Refaat Khodary</p> <p>2015-01-01</p> <p>Non-surgical reduction remains the first line treatment of choice for intussusception. The major complication of <span class="hlt">air</span> enema reduction is bowel perforation. The authors developed a custom made <span class="hlt">pressure</span> release valve to be added to portable insufflation devices, delivering <span class="hlt">air</span> at <span class="hlt">pressures</span> accepted as safe for effective reduction of intussusception in children under fluoroscopic guidance. The aim of this study was to develop a custom made <span class="hlt">pressure</span> release valve that is suitable for the insufflation devices used for <span class="hlt">air</span> enema reduction of intussusception and to put this valve into regular clinical practice. An adjustable, custom made <span class="hlt">pressure</span> release valve was assembled by the authors using readily available components. The valve was coupled to a simple <span class="hlt">air</span> enema insufflation device. The device was used for the trial of reduction of intussusception in a prospective study that included 132 patients. The success rate for <span class="hlt">air</span> enema reduction with the new device was 88.2%. The mean <span class="hlt">pressure</span> required to achieve complete reduction was 100 mmHg. The insufflation <span class="hlt">pressure</span> never exceeded the preset value (120 mmHg). Of the successful cases, 58.3% were reduced from the first attempt while 36.1% required a second insufflation. Only 5.55% required a third insufflation to complete the reduction. In cases with unsuccessful pneumatic reduction attempt (18.1%), surgical treatment was required. Surgery ranged from simple reduction to resection with a primary end to end anastomosis. No complications from <span class="hlt">air</span> enema were recorded. The authors recommend adding <span class="hlt">pressure</span> release valves to ensure safety by avoiding <span class="hlt">pressure</span> overshoot during the procedure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28872122','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28872122"><span>Ammonia Synthesis at Low <span class="hlt">Pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cussler, Edward; McCormick, Alon; Reese, Michael; Malmali, Mahdi</p> <p>2017-08-23</p> <p>Ammonia can be synthesized at low <span class="hlt">pressure</span> by the use of an ammonia selective absorbent. The process can be driven with <span class="hlt">wind</span> energy, available locally in areas requiring ammonia for synthetic fertilizer. Such <span class="hlt">wind</span> energy is often called "stranded," because it is only available far from population centers where it can be directly used. In the proposed low <span class="hlt">pressure</span> process, nitrogen is made from <span class="hlt">air</span> using <span class="hlt">pressure</span> swing absorption, and hydrogen is produced by electrolysis of water. While these gases can react at approximately 400 °C in the presence of a promoted conventional catalyst, the conversion is often limited by the reverse reaction, which makes this reaction only feasible at high <span class="hlt">pressures</span>. This limitation can be removed by absorption on an ammine-like calcium or magnesium chloride. Such alkaline metal halides can effectively remove ammonia, thus suppressing the equilibrium constraints of the reaction. In the proposed absorption-enhanced ammonia synthesis process, the rate of reaction may then be controlled not by the chemical kinetics nor the absorption rates, but by the rate of the recycle of unreacted gases. The results compare favorably with ammonia made from a conventional small scale Haber-Bosch process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1322012','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1322012"><span>Final Report for Project: Impacts of stratification and non-equilibrium <span class="hlt">winds</span> and waves on hub-height <span class="hlt">winds</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>Patton, Edward G.</p> <p></p> <p> the <span class="hlt">wind</span> plant scale. Overall project conclusions include; In the presence of fast-moving swell (significant wave height Hs = 6.4 m, and phase speed cp = 18 ms -1), the atmospheric boundary layer grows more rapidly when waves propagate opposite to the <span class="hlt">winds</span> compared to when <span class="hlt">winds</span> and waves are aligned. <span class="hlt">Pressure</span> drag increases by nearly a factor of 2 relative to the turbulent stress for the extreme case where waves propagate at 180° compared to the <span class="hlt">pressure</span> gradient forcing. Net <span class="hlt">wind</span> speed reduces by nearly 15% at hub-height for the 180°-case compared to the 0°-case, and turbulence intensities increase by nearly a factor of 2. These impacts diminish with decreasing wave age; Stratification increases hub height <span class="hlt">wind</span> speeds and increases the vertical shear of the mean <span class="hlt">wind</span> across the rotor plane. Fortuitously, this stability-induced enhanced shear does not influence turbulence intensity at hub height, but does increase (decrease) turbulence intensity below (above) hub height. Increased stability also increases the wave-induced <span class="hlt">pressure</span> stress by ~ 10%; Off the East Coast of the United States during Coupled Boundary Layers <span class="hlt">Air</span>-Sea Transfer - Low <span class="hlt">Wind</span> (CBLAST-Low), cases with short fetch include thin stable boundary layers with depths of only a few tens of meters. In the coastal zone, the relationship between the mean <span class="hlt">wind</span> and the surface fiction velocity (u*(V )) is significantly related to <span class="hlt">wind</span> direction for weak <span class="hlt">winds</span> but is not systematically related to the <span class="hlt">air</span> sea difference of virtual potential temperature, δθv; since waves generally propagate from the south at the <span class="hlt">Air</span>-Sea Interaction Tower (ASIT) tower, these results suggest that under weak <span class="hlt">wind</span> conditions waves likely influence surface stress more than stratification does; and <span class="hlt">Winds</span> and waves are frequently misaligned in the coastal zone. Stability conditions persist for long duration. Over a four year period, the Forschungsplattformen in Nord- und Ostsee Nr. 1 (FINO1) tower (a site with long fetch) primarily</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24925548','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24925548"><span>Layers of <span class="hlt">air</span> in the water beneath the floating fern Salvinia are exposed to fluctuations in <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mayser, Matthias J; Barthlott, Wilhelm</p> <p>2014-12-01</p> <p>Superhydrophobic, hierarchically structured, technical surfaces (Lotus-effect) are of high scientific and economic interest because of their remarkable properties. Recently, the immense potential of <span class="hlt">air</span>-retaining superhydrophobic surfaces, for example, for low-friction transport of fluids and drag-reducing coatings of ships has begun to be explored. A major problem of superhydrophobic surfaces mimicking the Lotus-effect is the limited persistence of the <span class="hlt">air</span> retained, especially under rough conditions of flow. However, there are a variety of floating or diving plant and animal species that possess <span class="hlt">air</span>-retaining surfaces optimized for durable water-repellency (Salvinia-effect). Especially floating ferns of the genus Salvinia have evolved superhydrophobic surfaces capable of maintaining layers of <span class="hlt">air</span> for months. Apart from maintaining stability under water, the layer of <span class="hlt">air</span> has to withstand the stresses of water <span class="hlt">pressure</span> (up to 2.5 bars). Both of these aspects have an application to create permanent <span class="hlt">air</span> layers on ships' hulls. We investigated the effect of <span class="hlt">pressure</span> on <span class="hlt">air</span> layers in a <span class="hlt">pressure</span> cell and exposed the <span class="hlt">air</span> layer to <span class="hlt">pressures</span> of up to 6 bars. We investigated the suppression of the <span class="hlt">air</span> layer at increasing <span class="hlt">pressures</span> as well as its restoration during decreases in <span class="hlt">pressure</span>. Three of the four examined Salvinia species are capable of maintaining <span class="hlt">air</span> layers at <span class="hlt">pressures</span> relevant to the conditions applying to ships' hulls. High volumes of <span class="hlt">air</span> per surface area are advantageous for retaining at least a partial Cassie-Baxter-state under <span class="hlt">pressure</span>, which also helps in restoring the <span class="hlt">air</span> layer after depressurization. Closed-loop structures such as the baskets at the top of the "egg-beater hairs" (see main text) also help return the <span class="hlt">air</span> layer to its original level at the tip of the hairs by trapping <span class="hlt">air</span> bubbles. © The Author 2014. Published by Oxford University Press on behalf of the Society for Integrative and Comparative Biology. All rights reserved. For permissions</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080041530','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080041530"><span><span class="hlt">Air</span> Flow and <span class="hlt">Pressure</span> Drop Measurements Across Porous Oxides</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fox, Dennis S.; Cuy, Michael D.; Werner, Roger A.</p> <p>2008-01-01</p> <p>This report summarizes the results of <span class="hlt">air</span> flow tests across eight porous, open cell ceramic oxide samples. During ceramic specimen processing, the porosity was formed using the sacrificial template technique, with two different sizes of polystyrene beads used for the template. The samples were initially supplied with thicknesses ranging from 0.14 to 0.20 in. (0.35 to 0.50 cm) and nonuniform backside morphology (some areas dense, some porous). Samples were therefore ground to a thickness of 0.12 to 0.14 in. (0.30 to 0.35 cm) using dry 120 grit SiC paper. <span class="hlt">Pressure</span> drop versus <span class="hlt">air</span> flow is reported. Comparisons of samples with thickness variations are made, as are <span class="hlt">pressure</span> drop estimates. As the density of the ceramic material increases the maximum corrected flow decreases rapidly. Future sample sets should be supplied with samples of similar thickness and having uniform surface morphology. This would allow a more consistent determination of <span class="hlt">air</span> flow versus processing parameters and the resulting porosity size and distribution.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/522724','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/522724"><span>Conceptual design for an electron-beam heated hypersonic <span class="hlt">wind</span> tunnel</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>Lipinski, R.J.; Kensek, R.P.</p> <p>1997-07-01</p> <p>There is a need for hypersonic <span class="hlt">wind</span>-tunnel testing at about mach 10 and above using natural <span class="hlt">air</span> and simulating temperatures and <span class="hlt">pressures</span> which are prototypic of flight at 50 km altitude or below. With traditional <span class="hlt">wind</span>-tunnel techniques, gas cooling during expansion results in exit temperatures which are too low. Miles, et al., have proposed overcoming this difficulty by heating the <span class="hlt">air</span> with a laser beam as it expands in the <span class="hlt">wind</span>-tunnel nozzle. This report discusses an alternative option of using a high-power electron beam to heat the <span class="hlt">air</span> as it expands. In the e-beam heating concept, the electron beam ismore » injected into the <span class="hlt">wind</span>-tunnel nozzle near the exit and then is guided upstream toward the nozzle throat by a strong axial magnetic field. The beam deposits most of its power in the dense <span class="hlt">air</span> near the throat where the expansion rate is greatest. A conceptual design is presented for a large-scale system which achieves Mach 14 for 0.1 seconds with an exit diameter of 2.8 meters. It requires 450 MW of electron beam power (5 MeV at 90 A). The guiding field is 500 G for most of the transport length and increases to 100 kG near the throat to converge the beam to a 1.0-cm diameter. The beam generator is a DC accelerator using a Marx bank (of capacitors) and a diode stack with a hot cathode. 14 refs. 38 figs., 9 tabs.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1236371','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1236371"><span>Prototype Systems for Measuring Outdoor <span class="hlt">Air</span> Intake Rates in Rooftop <span class="hlt">Air</span> Handlers</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>Fisk, William J.; Chan, Wanyu R.; Hotchi, Toshifumi</p> <p>2015-01-01</p> <p>The widespread absence of systems for real-time measurement and feedback control, of minimum outdoor <span class="hlt">air</span> intake rates in HVAC systems contributes to the poor control of ventilation rates in commercial buildings. Ventilation rates affect building energy consumption and influence occupant health. The project designed fabricated and tested four prototypes of systems for measuring rates of outdoor <span class="hlt">air</span> intake into roof top <span class="hlt">air</span> handlers. All prototypes met the ±20% accuracy target at low <span class="hlt">wind</span> speeds, with all prototypes accurate within approximately ±10% after application of calibration equations. One prototype met the accuracy target without a calibration. With two of four prototypemore » measurement systems, there was no evidence that <span class="hlt">wind</span> speed or direction affected accuracy; however, <span class="hlt">winds</span> speeds were generally below usually 3.5 m s -1 (12.6 km h -1) and further testing is desirable. The airflow resistance of the prototypes was generally less than 35 Pa at maximum RTU <span class="hlt">air</span> flow rates. A <span class="hlt">pressure</span> drop of this magnitude will increase fan energy consumption by approximately 4%. The project did not have resources necessary to estimate costs of mass produced systems. The retail cost of components and materials used to construct prototypes ranged from approximately $1,200 to $1,700. The test data indicate that the basic designs developed in this project, particularly the designs of two of the prototypes, have considerable merit. Further design refinement, testing, and cost analysis would be necessary to fully assess commercial potential. The designs and test results will be communicated to the HVAC manufacturing community.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21890395','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21890395"><span>An analysis of contact stiffness between a finger and an object when wearing an <span class="hlt">air</span>-cushioned glove: the effects of the <span class="hlt">air</span> <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wu, John Z; Wimer, Bryan M; Welcome, Daniel E; Dong, Ren G</p> <p>2012-04-01</p> <p><span class="hlt">Air</span>-cushioned gloves have the advantages of lighter weight, lower cost, and unique mechanical performance, compared to gloves made of conventional engineering materials. The goal of this study is to analyze the contact interaction between fingers and object when wearing an <span class="hlt">air</span>-cushioned glove. The contact interactions between the the fingertip and <span class="hlt">air</span> bubbles, which is considered as a cell of a typical <span class="hlt">air</span>-cushioned glove, has been analyzed theoretically. Two-dimensional finite element models were developed for the analysis. The fingertip model was assumed to be composed of skin layers, subcutaneous tissue, bone, and nail. The <span class="hlt">air</span> bubbles were modeled as <span class="hlt">air</span> sealed in the container of nonelastic membrane. We simulated two common scenarios: a fingertip in contact with one single <span class="hlt">air</span> bubble and with two <span class="hlt">air</span> cushion bubbles simultaneously. Our simulation results indicated that the internal <span class="hlt">air</span> <span class="hlt">pressure</span> can modulate the fingertip-object contact characteristics. The contact stiffness reaches a minimum when the initial <span class="hlt">air</span> <span class="hlt">pressure</span> is equal to 1.3 and 1.05 times of the atmosphere <span class="hlt">pressure</span> for the single <span class="hlt">air</span> bubble and the double <span class="hlt">air</span> bubble contact, respectively. Furthermore, the simulation results indicate that the double <span class="hlt">air</span> bubble contact will result in smaller volumetric tissue strain than the single <span class="hlt">air</span> bubble contact for the same force. Published by Elsevier Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007JPhCS..90a2026P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007JPhCS..90a2026P"><span>Microcontrolled <span class="hlt">air</span>-mattress for ulcer by <span class="hlt">pressure</span> prevention</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pasluosta, Cristian F.; Fontana, Juan M.; Beltramone, Diego A.; Taborda, Ricardo A. M.</p> <p>2007-11-01</p> <p>An ulcer by <span class="hlt">pressure</span> is produced when a constant <span class="hlt">pressure</span> is exerted over the skin. This generates the collapse of the blood vessels and, therefore, a lack in the contribution of the necessary nutrients for the affected zone. As a consequence, the skin deteriorates, eventually causing an ulcer. In order to prevent it, a protocol must be applied to the patient, which is reflected on time and cost of treatment. There are some <span class="hlt">air</span> mattresses available for this purpose, but whose performance does not fulfill all requirements. The prototype designed in our laboratory is based on the principle of the <span class="hlt">air</span> mattress. Its objective is to improve on existing technologies and, due to an increased automation, reduce time dedication for personnel in charge of the patient. A clinical experience was made in the local Emergencies Hospital and also in an institution dedicated to aged patients care. In both cases, the results obtained and the comments from the personnel involved were favorable.</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('http://www.dtic.mil/docs/citations/ADA243535','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA243535"><span>Evaluation of BAUER High <span class="hlt">Pressure</span> Breathing <span class="hlt">Air</span> P-2 Purification System</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1991-08-01</p> <p>and is a coalescing type separator that removes oil and water vapors suspended in the compressed <span class="hlt">air</span> . The molecular sieve is made to adsorb oil and...filtering, moisture separation, and prevents compressed <span class="hlt">air</span> return from the charged <span class="hlt">air</span> storage flasks to the compressor during unit shutdown. A manual...1111111111111 1111 IE IH fil91i C NAVY EXPERIMENTAL DIVING UNIT REPORT NO. 10-91 EVALUATION OF BAUER HIGH <span class="hlt">PRESSURE</span> BREATHING <span class="hlt">AIR</span> P-2 PURIFICATION SYSTEM GEORGE D</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhD...51p4003T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhD...51p4003T"><span>Indoor <span class="hlt">air</span> purification by dielectric barrier discharge combined with ionic <span class="hlt">wind</span>: physical and microbiological investigations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Timmermann, E.; Prehn, F.; Schmidt, M.; Höft, H.; Brandenburg, R.; Kettlitz, M.</p> <p>2018-04-01</p> <p>A non-thermal plasma source based on a surface dielectric barrier discharge (DBD) is developed for purification of recirculating <span class="hlt">air</span> in operating theatres in hospitals. This is a challenging application due to high flow rates, short treatment times and the low threshold for ozone in the ventilated <span class="hlt">air</span>. Therefore, the surface DBD was enhanced in order to generate an ionic <span class="hlt">wind</span>, which can deflect and thus, filter out airborne microorganisms. Electrical and gas diagnostics as well as microbiological experiments were performed in a downscaled plasma source under variation of various electrical parameters, but application-oriented airflow velocity and humidity. The dependence of electrical power and ozone concentration as well as charged particles in the plasma treated <span class="hlt">air</span> on frequency, voltage and relative humidity is presented and discussed. The presence of humidity causes a more conductive dielectric surface and thus a weaker plasma formation, especially at low frequency. The airborne test bacteria, Escherichia coli, showed significant effect to plasma treatment (up to 20% reduction) and to plasma with ionic <span class="hlt">wind</span> (up to 90% removal); especially a configuration with 70% removal and an accompanying ozone concentration of only 360 ppb is promising for future application.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19870017442','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19870017442"><span>Aerodynamic characteristics of the modified 40- by 80-foot <span class="hlt">wind</span> tunnel as measured in a 1/50th-scale model</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Smith, Brian E.; Naumowicz, Tim</p> <p>1987-01-01</p> <p>The aerodynamic characteristics of the 40- by 80-Foot <span class="hlt">Wind</span> Tunnel at Ames Research Center were measured by using a 1/50th-scale facility. The model was configured to closely simulate the features of the full-scale facility when it became operational in 1986. The items measured include the aerodynamic effects due to changes in the total-<span class="hlt">pressure</span>-loss characteristics of the intake and exhaust openings of the <span class="hlt">air</span>-exchange system, total-<span class="hlt">pressure</span> distributions in the flow field at locations around the <span class="hlt">wind</span> tunnel circuit, the locations of the maximum total-<span class="hlt">pressure</span> contours, and the aerodynamic changes caused by the installation of the acoustic barrier in the southwest corner of the <span class="hlt">wind</span> tunnel. The model tests reveal the changes in the aerodynamic performance of the 1986 version of the 40- by 80-Foot <span class="hlt">Wind</span> Tunnel compared with the performance of the 1982 configuration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3747107','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3747107"><span>Using <span class="hlt">Wind</span> Setdown and Storm Surge on Lake Erie to Calibrate the <span class="hlt">Air</span>-Sea Drag Coefficient</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Drews, Carl</p> <p>2013-01-01</p> <p>The <span class="hlt">air</span>-sea drag coefficient controls the transfer of momentum from <span class="hlt">wind</span> to water. In modeling storm surge, this coefficient is a crucial parameter for estimating the surge height. This study uses two strong <span class="hlt">wind</span> events on Lake Erie to calibrate the drag coefficient using the Coupled Ocean Atmosphere Wave Sediment Transport (COAWST) modeling system and the the Regional Ocean Modeling System (ROMS). Simulated waves are generated on the lake with Simulating WAves Nearshore (SWAN). <span class="hlt">Wind</span> setdown provides the opportunity to eliminate wave setup as a contributing factor, since waves are minimal at the upwind shore. The study finds that model results significantly underestimate <span class="hlt">wind</span> setdown and storm surge when a typical open-ocean formulation without waves is used for the drag coefficient. The contribution of waves to <span class="hlt">wind</span> setdown and storm surge is 34.7%. Scattered lake ice also increases the effective drag coefficient by a factor of 1.1. PMID:23977309</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://rosap.ntl.bts.gov/view/dot/25304','DOTNTL'); return false;" href="https://rosap.ntl.bts.gov/view/dot/25304"><span>Modifications of highway <span class="hlt">air</span> pollution models for complex geometries, volume II : <span class="hlt">wind</span> tunnel test program.</span></a></p> <p><a target="_blank" href="http://ntlsearch.bts.gov/tris/index.do">DOT National Transportation Integrated Search</a></p> <p></p> <p>2002-09-01</p> <p>This is volume I1 of a two-volume report of a study to increase the scope and clarity of <span class="hlt">air</span> pollution models for : depressed highway and street canyon sites. It presents the atmospheric <span class="hlt">wind</span> tunnel program conducted to increase the : data base and i...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-GRC-1944-C-06715.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-GRC-1944-C-06715.html"><span>Refrigeration Compressors for the Altitude <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>1944-09-21</p> <p>These compressors inside the Refrigeration Building at the National Advisory Committee for Aeronautics (NACA) Aircraft Engine Research Laboratory were used to generate cold temperatures in the Altitude <span class="hlt">Wind</span> Tunnel (AWT) and Icing Research Tunnel. The AWT was a large facility that simulated actual flight conditions at high altitudes. The two primary aspects of altitude simulation are the reduction of the <span class="hlt">air</span> <span class="hlt">pressure</span> and the decrease of temperature. The Icing Research Tunnel was a smaller facility in which water droplets were added to the refrigerated <span class="hlt">air</span> stream to simulate weather conditions that produced ice buildup on aircraft. The military <span class="hlt">pressured</span> the NACA to complete the tunnels quickly so they could be of use during World War II. The NACA engineers struggled with the design of this refrigeration system, so Willis Carrier, whose Carrier Corporation had pioneered modern refrigeration, took on the project. The Carrier engineers devised the largest cooling system of its kind in the world. The system could lower the tunnels’ <span class="hlt">air</span> temperature to –47⁰ F. The cooling system was powered by 14 Carrier and York compressors, seen in this photograph, which were housed in the Refrigeration Building between the two <span class="hlt">wind</span> tunnels. The compressors converted the Freon 12 refrigerant into a liquid. The refrigerant was then pumped into zig-zag banks of cooling coils inside the tunnels’ return leg. The Freon absorbed heat from the airflow as it passed through the coils. The heat was transferred to the cooling water and sent to the cooling tower where it was dissipated into the atmosphere.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730013091','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730013091"><span>Martian tidal <span class="hlt">pressure</span> and <span class="hlt">wind</span> fields obtained from the Mariner 9 infrared spectroscopy experiment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pirraglia, J. A.; Conrath, B. J.</p> <p>1973-01-01</p> <p>Using temperature fields derived from the Mariner 9 infrared spectroscopy experiment, the Martian atmospheric tidal <span class="hlt">pressure</span> and <span class="hlt">wind</span> fields are calculated. Temperature as a function of local time, latitude, and atmospheric <span class="hlt">pressure</span> level is obtained by secular and longitudinal averaging of the data. The resulting temperature field is approximated by a spherical harmonic expansion, retaining one symmetric and one asymmetric term for wavenumber zero and wavenumber one. Vertical averaging of the linearized momentum and continuity equations results in an inhomogeneous tidal equation for surface <span class="hlt">pressure</span> fluctuations with the driving function related to the temperature field through the geopotential function and the hydrostatic equation. Solutions of the tidal equation show a diurnal fractional <span class="hlt">pressure</span> amplitude approximately equal to one half of the vertically averaged diurnal fractional temperature amplitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19740043627&hterms=field+infrared&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DNear%2Bfield%2Binfrared','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19740043627&hterms=field+infrared&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DNear%2Bfield%2Binfrared"><span>Martian tidal <span class="hlt">pressure</span> and <span class="hlt">wind</span> fields obtained from the Mariner 9 infrared spectroscopy experiment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pirraglia, J. A.; Conrath, B. J.</p> <p>1974-01-01</p> <p>Using temperature fields derived from the Mariner 9 infrared spectroscopy experiment, the Martian atmospheric tidal <span class="hlt">pressure</span> and <span class="hlt">wind</span> fields are calculated. Temperature as a function of local time, latitude, and atmospheric <span class="hlt">pressure</span> level is obtained by secular and longitudinal averaging of the data. The resulting temperature field is approximated by a spherical harmonic expansion, retaining one symmetric and one asymmetric term each for wavenumber zero and wavenumber one. Vertical averaging of the linearized momentum and continuity equations results in an inhomogeneous tidal equation for surface <span class="hlt">pressure</span> fluctuations with the driving function related to the temperature field through the geopotential function and the hydrostatic equation. Solutions of the tidal equation show a diurnal fractional <span class="hlt">pressure</span> amplitude approximately equal to one-half the vertically averaged diurnal fractional temperature amplitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhSen...7..365L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhSen...7..365L"><span>Research on a new fiber-optic axial <span class="hlt">pressure</span> sensor of transformer <span class="hlt">winding</span> based on fiber Bragg grating</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Yuan; Li, Lianqing; Zhao, Lin; Wang, Jiqiang; Liu, Tongyu</p> <p>2017-12-01</p> <p>Based on the principle of the fiber Bragg grating, a new type of fiber-optic <span class="hlt">pressure</span> sensor for axial force measurement of transformer <span class="hlt">winding</span> is designed, which is designed with the structure of bending plate beam, the optimization of the packaging process, and material of the sensor. Through the calibration experiment to calibrate the sensor, the field test results of the Taikai transformer factory show that the sensitivity of the sensor is 0.133 pm/kPa and the repeatability error is 2.7% FS. The data of the fiber-optic <span class="hlt">pressure</span> sensor in different positions maintain consistent and repeatable, which can meet the requirement of the real-time monitoring of the axial force of transformer <span class="hlt">winding</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSM41A2685O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSM41A2685O"><span>Response of the coupled M-I-T system to the March 17, 2015 solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement event</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ozturk, D. S.; Zou, S.; Slavin, J. A.; Ridley, A. J.</p> <p>2017-12-01</p> <p>When the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> is enhanced, it could perturb the global magnetosphere-ionosphere-thermosphere (M-I-T) system. The most notable indicators of such disruptions are changes in Field-Aligned Currents (FACs), ionospheric convection patterns and magnetic perturbations observed by ground magnetometers. The link between dynamic <span class="hlt">pressure</span> enhancements and FACs has been well established, but studies on how these FACs affect the ionosphere-thermosphere system are very limited. In order to understand the large-scale dynamic processes in the M-I-T system due to the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement, we study the 17 March 2015 event in detail. This is one of the most geoeffective events of the solar cycle 24 with Dst minimum of -222 nT. The <span class="hlt">Wind</span> spacecraft recorded a two-step increment in the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, from 2 nPa to 12 nPa within 3 minutes, while the IMF Bz stayed northward. We used the University of Michigan Block Adaptive Tree Solarwind Roe Upwind Scheme (BATS'R'US), global MHD code to study the generation and propagation of perturbations associated with the compression of the magnetosphere. To effectively represent the coupled magnetosphere-ionosphere system, we included the Global Magnetosphere (GM), Inner Magnetosphere (IM) and Ionospheric electrodynamic (IE) modules. 600 uniformly distributed virtual magnetometers are included in the simulation to identify the magnetic perturbations associated with the FAC pairs as well as their temporal and spatial variations. In addition, we used the IE module output to drive the University of Michigan Global Ionosphere Thermosphere Model (GITM) to study how the I-T system responds to dynamic <span class="hlt">pressure</span> enhancement. We show that as a result of the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancement, two pair of perturbation FACs develop in addition to the NBZ current system. These FACs significantly alter the ionospheric convection profile and create elongated vortices that propagate from dayside to</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110014577','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110014577"><span>30 WS North Base <span class="hlt">Wind</span> Study</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wheeler, Mark</p> <p>2011-01-01</p> <p>The 30 Weather Squadron (30 WS) is concerned about strong <span class="hlt">winds</span> observed at their northern towers without advance warning. They state that terrain influences along the extreme northern fringes of Vandenberg <span class="hlt">Air</span> Force Base (VAFB) make it difficult for forecasters to issue timely and accurate high <span class="hlt">wind</span> warnings for northeasterly <span class="hlt">wind</span> events. These events tend to occur during the winter or early spring when they are under the influence of the Great Basin high <span class="hlt">pressure</span> weather regime. The Launch Weather Officers (LWOs) have seen these rapid <span class="hlt">wind</span> increases in the current northern Towers 60, 70 and 71 in excess of their 35 kt operational warning threshold. For this task, the 30 WS requested the Applied Meteorology Unit (AMU) analyze data from days when these towers reported <span class="hlt">winds</span> in excess of 35 kt and determine if there were any precursors in the observations that would allow the LWOs to better forecast and warn their operational customers for these <span class="hlt">wind</span> events. The 30 WS provided <span class="hlt">wind</span> tower data for the cool season (October - March) from the period January 2004-March 20 IO. The AMU decoded and evaluated the <span class="hlt">wind</span> tower data for 66 days identified by the 30 WS as having high-<span class="hlt">wind</span> events. Out of the 66 event days, only 30 had <span class="hlt">wind</span> speed observations of > or =35 kt from at least one of the three northern towers. The AMU analyzed surface and upper <span class="hlt">air</span> charts to determine the synoptic conditions for each event day along with tower peak <span class="hlt">wind</span> speed and direction time series and <span class="hlt">wind</span> rose charts for all 30 event days. The analysis revealed a trend on all event days in which the tower <span class="hlt">winds</span> shifted to the northeast for a period of time before the first recorded > or =35 kt <span class="hlt">wind</span> speed. The time periods for the 30 event days ranged from 20 minutes to several hours, with a median value of 110 minutes. This trend, if monitored, could give the 30 WS forecasters a precursor to assist in issuing an operational warning before a high <span class="hlt">wind</span> event occurs. The AMU recommends developing a</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24787565','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24787565"><span>Analysis of the intraocular jet flows and <span class="hlt">pressure</span> gradients induced by <span class="hlt">air</span> and fluid infusion: mechanism of focal chorioretinal damage.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kim, Yong Joon; Jo, Sungkil; Moon, Daruchi; Joo, Youngcheol; Choi, Kyung Seek</p> <p>2014-05-01</p> <p>To comprehend the mechanism of focal chorioretinal damage by analysis of the <span class="hlt">pressure</span> distribution and dynamic <span class="hlt">pressure</span> induced by infused <span class="hlt">air</span> during fluid-<span class="hlt">air</span> exchange. A precise simulation featuring a model eye and a fluid circuit was designed to analyze fluid-<span class="hlt">air</span> exchange. The <span class="hlt">pressure</span> distribution, flow velocity, and dynamic <span class="hlt">pressure</span> induced by infusion of <span class="hlt">air</span> into an <span class="hlt">air</span>-filled eye were analyzed using an approach based on fluid dynamics. The size of the port and the infusion <span class="hlt">pressure</span> were varied during simulated iterations. We simulated infusion of an <span class="hlt">air</span>-filled eye with balanced salt solution (BSS) to better understand the mechanism of chorioretinal damage induced by infused <span class="hlt">air</span>. Infused <span class="hlt">air</span> was projected straight toward a point on the retina contralateral to the infusion port (the "vulnerable point"). The highest <span class="hlt">pressure</span> was evident at the vulnerable point, and the lowest <span class="hlt">pressure</span> was recorded on most retinal areas. Simulations using greater infusion <span class="hlt">pressure</span> and a port of larger size were associated with elevations in dynamic <span class="hlt">pressure</span> and the <span class="hlt">pressure</span> gradient. The <span class="hlt">pressure</span> gradients were 2.8 and 5.1 mm Hg, respectively, when infusion <span class="hlt">pressures</span> of 30 and 50 mm Hg were delivered through a 20-gauge port. The <span class="hlt">pressure</span> gradient associated with BSS infusion was greater than that created by <span class="hlt">air</span>, but lasted for only a moment. Our simulation explains the mechanism of focal chorioretinal damage in numerical terms. Infused <span class="hlt">air</span> induces a prolonged increase in focal <span class="hlt">pressure</span> on the vulnerable point, and this may be responsible for visual field defects arising after fluid-<span class="hlt">air</span> exchange. Copyright 2014 The Association for Research in Vision and Ophthalmology, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1918753M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1918753M"><span>Does the recent warming hiatus exist over northern Asia for winter <span class="hlt">wind</span> chill temperature?</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ma, Ying</p> <p>2017-04-01</p> <p><span class="hlt">Wind</span> chill temperature (WCT) describes the joint effect of <span class="hlt">wind</span> velocity and <span class="hlt">air</span> temperature on exposed body skin and could support policy makers in designing plans to reduce the risks of notably cold and windy weather. This study examined winter WCT over northern Asia during 1973-2013 by analyzing in situ station data. The winter WCT warming rate over the Tibetan Plateau slowed during 1999-2013 (-0.04 °C/decade) compared with that during 1973-1998 (0.67 °C/decade). The winter WCT warming hiatus has also been observed in the remainder of Northern Asia with trends of 1.11 °C/decade during 1973-1998 but -1.02 °C/decade during 1999-2013, except for the Far East of Russia (FE), where the winter WCT has continued to heat up during both the earlier period of 1973-1998 (0.54 °C/decade) and the recent period of 1999-2013 (0.75 °C/decade). The results indicate that the influence of temperature on winter WCT is greater than that of <span class="hlt">wind</span> speed over northern Asia. Atmospheric circulation changes associated with <span class="hlt">air</span> temperature and <span class="hlt">wind</span> speed were analyzed to identify the causes for the warming hiatus of winter WCT over northern Asia. The distributions of sea level <span class="hlt">pressure</span> and 500 hPa height anomalies during 1999-2013 transported cold <span class="hlt">air</span> from the high latitudes to middle latitudes, resulting in low <span class="hlt">air</span> temperature over Northern Asia except for the Far East of Russia. Over the Tibetan Plateau, the increase in <span class="hlt">wind</span> speed offset the increase in <span class="hlt">air</span> temperature during 1999-2013. For the Far East, the southerly <span class="hlt">wind</span> from the Western Pacific drove the temperature up during the 1999-2013 period via warm advection.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4590742','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4590742"><span>Long-Term <span class="hlt">Air</span> Pollution Exposure and Blood <span class="hlt">Pressure</span> in the Sister Study</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chan, Stephanie H.; Van Hee, Victor C.; Bergen, Silas; Szpiro, Adam A.; DeRoo, Lisa A.; London, Stephanie J.; Marshall, Julian D.; Sandler, Dale P.</p> <p>2015-01-01</p> <p>Background Exposure to <span class="hlt">air</span> pollution has been consistently associated with cardiovascular morbidity and mortality, but mechanisms remain uncertain. Associations with blood <span class="hlt">pressure</span> (BP) may help to explain the cardiovascular effects of <span class="hlt">air</span> pollution. Objective We examined the cross-sectional relationship between long-term (annual average) residential <span class="hlt">air</span> pollution exposure and BP in the National Institute of Environmental Health Sciences’ Sister Study, a large U.S. cohort study investigating risk factors for breast cancer and other outcomes. Methods This analysis included 43,629 women 35–76 years of age, enrolled 2003–2009, who had a sister with breast cancer. Geographic information systems contributed to satellite-based nitrogen dioxide (NO2) and fine particulate matter (≤ 2.5 μm; PM2.5) predictions at participant residences at study entry. Generalized additive models were used to examine the relationship between pollutants and measured BP at study entry, adjusting for cardiovascular disease risk factors and including thin plate splines for potential spatial confounding. Results A 10-μg/m3 increase in PM2.5 was associated with 1.4-mmHg higher systolic BP (95% CI: 0.6, 2.3; p < 0.001), 1.0-mmHg higher pulse <span class="hlt">pressure</span> (95% CI: 0.4, 1.7; p = 0.001), 0.8-mmHg higher mean arterial <span class="hlt">pressure</span> (95% CI: 0.2, 1.4; p = 0.01), and no significant association with diastolic BP. A 10-ppb increase in NO2 was associated with a 0.4-mmHg (95% CI: 0.2, 0.6; p < 0.001) higher pulse <span class="hlt">pressure</span>. Conclusions Long-term PM2.5 and NO2 exposures were associated with higher blood <span class="hlt">pressure</span>. On a population scale, such <span class="hlt">air</span> pollution–related increases in blood <span class="hlt">pressure</span> could, in part, account for the increases in cardiovascular disease morbidity and mortality seen in prior studies. Citation Chan SH, Van Hee VC, Bergen S, Szpiro AA, DeRoo LA, London SJ, Marshall JD, Kaufman JD, Sandler DP. 2015. Long-term <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> in the Sister Study. Environ Health</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-GRC-1944-C-05818.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-GRC-1944-C-05818.html"><span>Altitude <span class="hlt">Wind</span> Tunnel Control Room at the Aircraft Engine Research Laboratory</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>1944-07-21</p> <p>Operators in the control room for the Altitude <span class="hlt">Wind</span> Tunnel at the National Advisory Committee for Aeronautics (NACA) Aircraft Engine Research Laboratory remotely operate a Wright R–3350 engine in the tunnel’s test section. Four of the engines were used to power the B–29 Superfortress, a critical weapon in the Pacific theater during World War II. The <span class="hlt">wind</span> tunnel, which had been in operation for approximately six months, was the nation’s only <span class="hlt">wind</span> tunnel capable of testing full-scale engines in simulated altitude conditions. The soundproof control room was used to operate the <span class="hlt">wind</span> tunnel and control the engine being run in the test section. The operators worked with assistants in the adjacent Exhauster Building and Refrigeration Building to manage the large altitude simulation systems. The operator at the center console controlled the tunnel’s drive fan and operated the engine in the test section. Two sets of pneumatic levers near his right forearm controlled engine fuel flow, speed, and cooling. Panels on the opposite wall, out of view to the left, were used to manage the combustion <span class="hlt">air</span>, refrigeration, and exhauster systems. The control panel also displayed the master <span class="hlt">air</span> speed, altitude, and temperature gauges, as well as a plethora of <span class="hlt">pressure</span>, temperature, and airflow readings from different locations on the engine. The operator to the right monitored the manometer tubes to determine the <span class="hlt">pressure</span> levels. Despite just being a few feet away from the roaring engine, the control room remained quiet during the tests.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1788c0016W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1788c0016W"><span>Computational study: The influence of omni-directional guide vane on the flow pattern characteristic around Savonius <span class="hlt">wind</span> turbine</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wicaksono, Yoga Arob; Tjahjana, D. D. D. P.</p> <p>2017-01-01</p> <p>Standart Savonius <span class="hlt">wind</span> turbine have a low performance such as low coefficient of power and low coefficient of torque compared with another type of <span class="hlt">wind</span> turbine. This phenomenon occurs because the <span class="hlt">wind</span> stream can cause the negative <span class="hlt">pressure</span> at the returning rotor. To solve this problem, standard Savonius combined with Omni Directional Guide Vane (ODGV) proposed. The aim of this research is to study the influence of ODGV on the flow pattern characteristic around of Savonius <span class="hlt">wind</span> turbine. The numerical model is based on the Navier-Stokes equations with the standard k-ɛ turbulent model. This equation solved by a finite volume discretization method. This case was analyzed by commercial computational fluid dynamics solver such as SolidWorks Flow Simulations. Simulations were performed at the different <span class="hlt">wind</span> directions; there are 0°, 30°,60° at 4 m/s <span class="hlt">wind</span> speed. The numerical method validated with the past experimental data. The result indicated that the ODGV able to augment <span class="hlt">air</span> flow to advancing rotor and decrease the negative <span class="hlt">pressure</span> in the upstream of returning rotor compared to the bare Savonius <span class="hlt">wind</span> turbine.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ACP....1714887E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ACP....1714887E"><span>Effects of vernal equinox solar eclipse on temperature and <span class="hlt">wind</span> direction in Switzerland</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Eugster, Werner; Emmel, Carmen; Wolf, Sebastian; Buchmann, Nina; McFadden, Joseph P.; Whiteman, Charles David</p> <p>2017-12-01</p> <p>The vernal equinox total solar eclipse of 20 March 2015 produced a maximum occultation of 65.8-70.1 % over Switzerland during the morning hours (09:22 to 11:48 CET). Skies were generally clear over the Swiss Alps due to a persistent high-<span class="hlt">pressure</span> band between the UK and Russia associated with a rather weak <span class="hlt">pressure</span> gradient over the continent. To assess the effects of penumbral shading on near-surface meteorology across Switzerland, <span class="hlt">air</span> temperature data measured at 10 min intervals at 184 MeteoSwiss weather stations were used. <span class="hlt">Wind</span> speed and direction data were available from 165 of these stations. Additionally, six Swiss FluxNet eddy covariance flux (ECF) sites provided turbulent measurements at 20 Hz resolution. During maximum occultation, the temperature drop was up to 5.8 K at a mountain site where cold <span class="hlt">air</span> can pool in a topographic depression. The bootstrapped average of the maximum temperature drops of all 184 MeteoSwiss sites during the solar eclipse was 1.51 ± 0.02 K (mean ± SE). A detailed comparison with literature values since 1834 showed a temperature decrease of 2.6 ± 1.7 K (average of all reports), with extreme values up to 11 K. On fair weather days under weak larger-scale <span class="hlt">pressure</span> gradients, local thermo-topographic <span class="hlt">wind</span> systems develop that are driven by small-scale <span class="hlt">pressure</span> and temperature gradients. At one ECF site, the penumbral shading delayed the morning transition from down-valley to up-valley <span class="hlt">wind</span> conditions. At another site, it prevented this transition from occurring at all. Data from the 165 MeteoSwiss sites measuring <span class="hlt">wind</span> direction did not show a consistent pattern of <span class="hlt">wind</span> direction response to the passing of the penumbral shadow. These results suggest that the local topographic setting had an important influence on the temperature drop and the <span class="hlt">wind</span> flow patterns during the eclipse. A significant cyclonic effect of the passing penumbral shadow was found in the elevation range ≈ 1700-2700 m a. s. l., but</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24047569','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24047569"><span>Traffic-related <span class="hlt">air</span> pollution and noise and children's blood <span class="hlt">pressure</span>: results from the PIAMA birth cohort study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bilenko, Natalya; van Rossem, Lenie; Brunekreef, Bert; Beelen, Rob; Eeftens, Marloes; Hoek, Gerard; Houthuijs, Danny; de Jongste, Johan C; van Kempen, Elise; Koppelman, Gerard H; Meliefste, Kees; Oldenwening, Marieke; Smit, Henriette A; Wijga, Alet H; Gehring, Ulrike</p> <p>2015-01-01</p> <p>Elevation of a child's blood <span class="hlt">pressure</span> may cause possible health risks in later life. There is evidence for adverse effects of exposure to <span class="hlt">air</span> pollution and noise on blood <span class="hlt">pressure</span> in adults. Little is known about these associations in children. We investigated the associations of <span class="hlt">air</span> pollution and noise exposure with blood <span class="hlt">pressure</span> in 12-year-olds. Blood <span class="hlt">pressure</span> was measured at age 12 years in 1432 participants of the PIAMA birth cohort study. Annual average exposure to traffic-related <span class="hlt">air</span> pollution [NO2, mass concentrations of particulate matter with diameters of less than 2.5 µm (PM2.5) and less than 10 µm (PM10), and PM2.5 absorbance] at the participants' home and school addresses at the time of blood <span class="hlt">pressure</span> measurements was estimated by land-use regression models. <span class="hlt">Air</span> pollution exposure on the days preceding blood <span class="hlt">pressure</span> measurements was estimated from routine <span class="hlt">air</span> monitoring data. Long-term noise exposure was assessed by linking addresses to modelled equivalent road traffic noise levels. Associations of exposures with blood <span class="hlt">pressure</span> were analysed by linear regression. Effects are presented for an interquartile range increase in exposure. Long-term exposure to NO2 and PM2.5 absorbance were associated with increased diastolic blood <span class="hlt">pressure</span>, in children who lived at the same address since birth [adjusted mean difference (95% confidence interval) [mmHg] 0.83 (0.06 to 1.61) and 0.75 (-0.08 to 1.58), respectively], but not with systolic blood <span class="hlt">pressure</span>. We found no association of blood <span class="hlt">pressure</span> with short-term <span class="hlt">air</span> pollution or noise exposure. Long-term exposure to traffic-related <span class="hlt">air</span> pollution may increase diastolic blood <span class="hlt">pressure</span> in children. © The European Society of Cardiology 2013 Reprints and permissions: sagepub.co.uk/journalsPermissions.nav.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29524199','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29524199"><span>Self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q® intubating laryngeal airway versus the LMA® Classic™: a randomized clinical trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ha, Sang Hee; Kim, Min-Soo; Suh, Jiwoo; Lee, Jong Seok</p> <p>2018-05-01</p> <p>The self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q® (<span class="hlt">air</span>-Q SP) intubating laryngeal airway is a relatively new supraglottic airway (SGA) device. The intracuff <span class="hlt">pressure</span> of <span class="hlt">air</span>-Q dynamically equilibrates with the airway <span class="hlt">pressure</span> and adjusts to the patient's pharyngeal and periglottic anatomy, potentially providing improved airway fit and seal. The aim of this prospective randomized study was to compare the clinical performance of <span class="hlt">air</span>-Q to the LMA® Classic™ SGA. Adult patients requiring general anesthesia for elective surgery were prospectively enrolled and randomly assigned to either <span class="hlt">air</span>-Q SP or the LMA Classic SGA. Oropharyngeal leak <span class="hlt">pressure</span> (primary endpoint), success rate, insertion features (insertion time, ease of insertion, requirement for device manipulation), sealing function, gastric insufflation, bronchoscopic view, and oropharyngeal complications at device insertion and following its removal (sore throat, dysphagia, dysphonia) were compared. The mean (standard deviation [SD]) oropharyngeal leak <span class="hlt">pressure</span> just after insertion was similar in the <span class="hlt">air</span>-Q SP and LMA [16.8 (4.9) vs 18.6 (5.5) cm H 2 O, respectively; mean difference, 1.8 cm H 2 O; 95% CI, -0.5 to 4.2; P = 0.13] and did not differ at ten minutes following device insertion. Median [interquartile range (IQR)] peak inspiratory <span class="hlt">pressure</span> just after insertion was lower in the <span class="hlt">air</span>-Q SP (11.0 [10.0-13.0] vs 13.0 [11.0-14.0] cmH 2 O, median difference, 1.0 cm H 2 O; 95% CI, 0.0 to 2.0; P = 0.03) but no difference was observed at ten minutes. The median [IQR] insertion time was faster with the <span class="hlt">air</span>-Q SP (15.9 [13.6-20.3] sec vs 24 [21.2-27.1] sec; median difference, 8.1 sec; 95% CI, 5.6 to 9.9; P < 0.001) and improved bronchoscopic viewing grade were seen with the <span class="hlt">air</span>-Q SP immediately after insertion (P < 0.001). No differences between the groups were observed with respect to the rate of successful insertion at first attempt, overall insertion success rate, ease of insertion, and complications. The <span class="hlt">air</span>-Q SP had similar leak</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150006031','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150006031"><span>Coupled Inertial Navigation and Flush <span class="hlt">Air</span> Data Sensing Algorithm for Atmosphere Estimation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Karlgaard, Christopher D.; Kutty, Prasad; Schoenenberger, Mark</p> <p>2015-01-01</p> <p>This paper describes an algorithm for atmospheric state estimation that is based on a coupling between inertial navigation and flush <span class="hlt">air</span> data sensing <span class="hlt">pressure</span> measurements. In this approach, the full navigation state is used in the atmospheric estimation algorithm along with the <span class="hlt">pressure</span> measurements and a model of the surface <span class="hlt">pressure</span> distribution to directly estimate atmospheric <span class="hlt">winds</span> and density using a nonlinear weighted least-squares algorithm. The approach uses a high fidelity model of atmosphere stored in table-look-up form, along with simplified models of that are propagated along the trajectory within the algorithm to provide prior estimates and covariances to aid the <span class="hlt">air</span> data state solution. Thus, the method is essentially a reduced-order Kalman filter in which the inertial states are taken from the navigation solution and atmospheric states are estimated in the filter. The algorithm is applied to data from the Mars Science Laboratory entry, descent, and landing from August 2012. Reasonable estimates of the atmosphere and <span class="hlt">winds</span> are produced by the algorithm. The observability of <span class="hlt">winds</span> along the trajectory are examined using an index based on the discrete-time observability Gramian and the <span class="hlt">pressure</span> measurement sensitivity matrix. The results indicate that bank reversals are responsible for adding information content to the system. The algorithm is then applied to the design of the <span class="hlt">pressure</span> measurement system for the Mars 2020 mission. The <span class="hlt">pressure</span> port layout is optimized to maximize the observability of atmospheric states along the trajectory. Linear covariance analysis is performed to assess estimator performance for a given <span class="hlt">pressure</span> measurement uncertainty. The results indicate that the new tightly-coupled estimator can produce enhanced estimates of atmospheric states when compared with existing algorithms.</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://hdl.handle.net/2060/19900005681','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900005681"><span>Saltation thresholds and entrainment of fine particles at Earth and Martian <span class="hlt">pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Leach, Rodman; Greeley, Ronald; Pollack, James</p> <p>1989-01-01</p> <p>An open circuit <span class="hlt">wind</span> tunnel designed to operate in a large vacuum chamber was built at NASA-Ames to investigate saltation threshold, flux, deflation rates, and other aeolian phenomena on the planet Mars. The vacuum chamber will operate at <span class="hlt">pressures</span> as low as 4 mbar, and the tunnel operates at windspeeds as high as 150 m/sec. Either <span class="hlt">air</span> or CO2 can be used as a working fluid. It was found that, to a first order approximation, the same dynamic <span class="hlt">pressure</span> was required at Martian <span class="hlt">pressure</span> to entrain or saltate particles as was required on Earth, although <span class="hlt">wind</span> and particle speed are considerably higher at Martian <span class="hlt">pressure</span>. A 2nd <span class="hlt">wind</span> tunnel, designed to operate aboard the NASA KC-135 0-g aircraft to obtain information on the effect of gravity on saltation threshold and the interparticle force at 0-g, is also described and test data presented. Some of the experiments are summarized and various aspects of low <span class="hlt">pressure</span> aeolian entrainment for particles 12 to 100 micron in diameter are discussed, some of them unique to low <span class="hlt">pressure</span> testing and some common in Earth <span class="hlt">pressure</span> particle transport testing. The facility, the modes of operation, and the materials used are described.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ApJ...774...59Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ApJ...774...59Y"><span>Small-scale <span class="hlt">Pressure</span>-balanced Structures Driven by Oblique Slow Mode Waves Measured in the Solar <span class="hlt">Wind</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yao, Shuo; He, J.-S.; Tu, C.-Y.; Wang, L.-H.; Marsch, E.</p> <p>2013-09-01</p> <p>Recently, small-scale <span class="hlt">pressure</span>-balanced structures (PBSs) were identified in the solar <span class="hlt">wind</span>, but their formation mechanism remains unclear. This work aims to reveal the dependence of the properties of small-scale PBSs on the background magnetic field (B 0) direction and thus to corroborate the in situ mechanism that forms them. We analyze the plasma and magnetic field data obtained by <span class="hlt">WIND</span> in the quiet solar <span class="hlt">wind</span> at 1 AU. First, we use a developed moving-average method to obtain B 0(s, t) for every temporal scale (s) at each time moment (t). By wavelet cross-coherence analysis, we obtain the correlation coefficients between the thermal <span class="hlt">pressure</span> P th and the magnetic <span class="hlt">pressure</span> P B, distributing against the temporal scale and the angle θxB between B 0(s, t) and Geocentric Solar Ecliptic coordinates (GSE)-x. We note that the angle coverage of a PBS decreases with shorter temporal scale, but the occurrence of the PBSs is independent of θxB. Suspecting that the isolated small PBSs are formed by compressive waves in situ, we continue this study by testing the wave modes forming a small-scale PBS with B 0(s, t) quasi-parallel to GSE-x. As a result, we identify that the cross-helicity and the compressibility attain values for a slow mode from theoretical calculations. The wave vector is derived from minimum variance analysis. Besides, the proton temperatures obey T < T ∥ derived from the velocity distribution functions, excluding a mirror mode, which is the other candidate for the formation of PBSs in situ. Thus, a small-scale PBS is shown to be driven by oblique, slow-mode waves in the solar <span class="hlt">wind</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AGUFMOS11C1660Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AGUFMOS11C1660Z"><span>On the relationships of gas transfer velocity with turbulent kinetic energy dissipation rate and <span class="hlt">wind</span> waves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhao, D.</p> <p>2012-12-01</p> <p>The exchange of carbon dioxide across the <span class="hlt">air</span>-sea interface is an important component of the atmospheric CO2 budget. Understanding how future changes in climate will affect oceanic uptake and releaser CO2 requires accurate estimation of <span class="hlt">air</span>-sea CO2 flux. This flux is typically expressed as the product of gas transfer velocity, CO2 partial <span class="hlt">pressure</span> difference in seawater and <span class="hlt">air</span>, and the CO2 solubility. As the key parameter, gas transfer velocity has long been known to be controlled by the near-surface turbulence in water, which is affected by many factors, such as <span class="hlt">wind</span> forcing, ocean waves, water-side convection and rainfall. Although the <span class="hlt">wind</span> forcing is believed as the major factor dominating the near-surface turbulence, many studies have shown that the <span class="hlt">wind</span> waves and their breaking would greatly enhance turbulence compared with the classical solid wall theory. Gas transfer velocity has been parameterized in terms of <span class="hlt">wind</span> speed, turbulent kinetic energy dissipation rate, and wave parameters on the basis of observational data or theoretical analysis. However, great discrepancies, as large as one order, exist among these formulas. In this study, we will systematically analyze the differences of gas transfer velocity proposed so far, and try to find the reason that leads to their uncertainties. Finally, a new formula for gas transfer velocity will be given in terms of <span class="hlt">wind</span> speed and <span class="hlt">wind</span> wave parameter.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.epa.gov/caa-permitting/comments-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound-offshore-renewable','PESTICIDES'); return false;" href="https://www.epa.gov/caa-permitting/comments-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound-offshore-renewable"><span>Comments for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit)</span></a></p> <p><a target="_blank" href="http://www.epa.gov/pesticides/search.htm">EPA Pesticide Factsheets</a></p> <p></p> <p></p> <p>List of comments for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit: Massachusetts Plan Approval including nonattainment NSR Appendix A requirements).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title29-vol7/pdf/CFR-2010-title29-vol7-sec1915-172.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title29-vol7/pdf/CFR-2010-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>..., 1963. They shall be subjected to a hydrostatic <span class="hlt">pressure</span> test of one and one-half times the working... quarterly by a competent person. They shall be subjected yearly to a hydrostatic <span class="hlt">pressure</span> test of one and... 29 Labor 7 2010-07-01 2010-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26121822','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26121822"><span>[Nitrous Oxide Exposure-mediated Increases in Cuff <span class="hlt">Pressure</span>: A Comparison of Disposable Type and Re-use Type <span class="hlt">air</span>-Q Devices].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Miyazaki, Yu; Komasawa, Nobuyasu; Fujiawara, Shunsuke; Majima, Nozomi; Tatsumi, Shinichi; Minami, Toshiaki</p> <p>2015-02-01</p> <p>BaCKGROUND: The present study aimed to compare nitrous oxide-mediated increases in cuff <span class="hlt">pressure</span> between the disposable type <span class="hlt">air</span>-Q (<span class="hlt">air</span>-Q-DT) and re-use type <span class="hlt">air</span>-Q (<span class="hlt">air</span>-Q-RU) in a simulated adult airway model. Automated cuff <span class="hlt">pressure</span> was adjusted to 10, 20, and 30 cmH2O. The <span class="hlt">air</span>-Q-DT and <span class="hlt">air</span>-Q-RU were exposed to 80% nitrous oxide and cuff <span class="hlt">pressure</span> was measured 15 and 30 minutes later. Cuff <span class="hlt">pressure</span> of the <span class="hlt">air</span>-Q-DT was significantly lower than that of the <span class="hlt">air</span>-Q-RU after 15 and 30 minutes, regardless of the initial <span class="hlt">pressure</span>. The polyvinyl chloride-based <span class="hlt">air</span>-Q-DT may be more effective than the silicon-based <span class="hlt">air</span>-Q-RU in preventing hyperinflation of the tracheal tube cuff in response to nitrous oxide exposure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17384764','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17384764"><span><span class="hlt">Wind</span> direction and its linkage with Vibrio cholerae dissemination.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Paz, Shlomit; Broza, Meir</p> <p>2007-02-01</p> <p>The relevance of climatic events as causative factors for cholera epidemics is well known. However, examinations of the involvement of climatic factors in intracontinental disease distribution are still absent. The spreading of cholera epidemics may be related to the dominant <span class="hlt">wind</span> direction over land. We examined the geographic diffusion of three cholera outbreaks through their linkage with the <span class="hlt">wind</span> direction: a) the progress of Vibrio cholerae O1 biotype El Tor in Africa during 1970-1971 and b) again in 2005-2006; and c) the rapid spread of Vibrio cholerae O139 over India during 1992-1993. We also discuss the possible influence of the <span class="hlt">wind</span> direction on windborn dissemination by flying insects, which may serve as vectors. Analysis of <span class="hlt">air</span> <span class="hlt">pressure</span> data at sea level and at several altitudes over Africa, India, and Bangladesh show a correspondence between the dominant <span class="hlt">wind</span> direction and the intracontinental spread of cholera. We explored the hypothesis that <span class="hlt">winds</span> have assisted the progress of cholera Vibrios throughout continents. The current analysis supports the hypothesis that aeroplankton (the tiny life forms that float in the <span class="hlt">air</span> and that may be caught and carried upward by the <span class="hlt">wind</span>, landing far from their origin) carry the cholera bacteria from one body of water to an adjacent one. This finding may improve our understanding of how climatic factors are involved in the rapid distribution of new strains throughout a vast continental area. Awareness of the aerial transfer of Vibrio cholerae may assist health authorities by improving the prediction of the disease's geographic dissemination.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19780059631&hterms=comparison+model+attitude+systems&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcomparison%2Bmodel%2Battitude%2Bsystems','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19780059631&hterms=comparison+model+attitude+systems&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcomparison%2Bmodel%2Battitude%2Bsystems"><span>Comparison of nozzle and afterbody surface <span class="hlt">pressures</span> from <span class="hlt">wind</span> tunnel and flight test of the YF-17 aircraft</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lucas, E. J.; Fanning, A. E.; Steers, L. I.</p> <p>1978-01-01</p> <p>Results are reported from the initial phase of an effort to provide an adequate technical capability to accurately predict the full scale, flight vehicle, nozzle-afterbody performance of future aircraft based on partial scale, <span class="hlt">wind</span> tunnel testing. The primary emphasis of this initial effort is to assess the current capability and identify the cause of limitations on this capability. A direct comparison of surface <span class="hlt">pressure</span> data is made between the results from an 0.1-scale model <span class="hlt">wind</span> tunnel investigation and a full-scale flight test program to evaluate the current subscale testing techniques. These data were acquired at Mach numbers 0.6, 0.8, 0.9, 1.2, and 1.5 on four nozzle configurations at various vehicle pitch attitudes. Support system interference increments were also documented during the <span class="hlt">wind</span> tunnel investigation. In general, the results presented indicate a good agreement in trend and level of the surface <span class="hlt">pressures</span> when corrective increments are applied for known effects and surface differences between the two articles under investigation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFM.A23J..01M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFM.A23J..01M"><span>Challenges in Understanding and Forecasting <span class="hlt">Winds</span> in Complex Terrain.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mann, J.; Fernando, J.; Wilczak, J. M.</p> <p>2017-12-01</p> <p>An overview will be given of some of the challenges in understanding and forecasting <span class="hlt">winds</span> in complex terrain. These challenges can occur for several different reasons including 1) gaps in our understanding of fundamental physical boundary layer processes occurring in complex terrain; 2) a lack of adequate parameterizations and/or numerical schemes in NWP models; and 3) inadequate observations for initialization of NWP model forecasts. Specific phenomena that will be covered include topographic wakes/vortices, cold pools, gap flows, and mountain-valley <span class="hlt">winds</span>, with examples taken from several <span class="hlt">air</span> quality and <span class="hlt">wind</span> energy related field programs in California as well as from the recent Second <span class="hlt">Wind</span> Forecast Improvement Program (WFIP2) field campaign in the Columbia River Gorge/Basin area of Washington and Oregon States. Recent parameterization improvements discussed will include those for boundary layer turbulence, including 3D turbulence schemes, and gravity wave drag. Observational requirements for improving <span class="hlt">wind</span> forecasting in complex terrain will be discussed, especially in the context of forecasting <span class="hlt">pressure</span> gradient driven gap flow events.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28495593','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28495593"><span>Enhanced <span class="hlt">air</span> dispersion modelling at a typical Chinese nuclear power plant site: Coupling RIMPUFF with two advanced diagnostic <span class="hlt">wind</span> models.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Liu, Yun; Li, Hong; Sun, Sida; Fang, Sheng</p> <p>2017-09-01</p> <p>An enhanced <span class="hlt">air</span> dispersion modelling scheme is proposed to cope with the building layout and complex terrain of a typical Chinese nuclear power plant (NPP) site. In this modelling, the California Meteorological Model (CALMET) and the Stationary <span class="hlt">Wind</span> Fit and Turbulence (SWIFT) are coupled with the Risø Mesoscale PUFF model (RIMPUFF) for refined <span class="hlt">wind</span> field calculation. The near-field diffusion coefficient correction scheme of the Atmospheric Relative Concentrations in the Building Wakes Computer Code (ARCON96) is adopted to characterize dispersion in building arrays. The proposed method is evaluated by a <span class="hlt">wind</span> tunnel experiment that replicates the typical Chinese NPP site. For both <span class="hlt">wind</span> speed/direction and <span class="hlt">air</span> concentration, the enhanced modelling predictions agree well with the observations. The fraction of the predictions within a factor of 2 and 5 of observations exceeds 55% and 82% respectively in the building area and the complex terrain area. This demonstrates the feasibility of the new enhanced modelling for typical Chinese NPP sites. Copyright © 2017 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130010684','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130010684"><span>Statistical Short-Range Guidance for Peak <span class="hlt">Wind</span> Speed Forecasts at Edwards <span class="hlt">Air</span> Force Base, CA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dreher, Joseph; Crawford, Winifred; Lafosse, Richard; Hoeth, Brian; Burns, Kerry</p> <p>2008-01-01</p> <p>The peak <span class="hlt">winds</span> near the surface are an important forecast element for Space Shuttle landings. As defined in the Shuttle Flight Rules (FRs), there are peak <span class="hlt">wind</span> thresholds that cannot be exceeded in order to ensure the safety of the shuttle during landing operations. The National Weather Service Spaceflight Meteorology Group (SMG) is responsible for weather forecasts for all shuttle landings. They indicate peak <span class="hlt">winds</span> are a challenging parameter to forecast. To alleviate the difficulty in making such <span class="hlt">wind</span> forecasts, the Applied Meteorology Unit (AMTJ) developed a personal computer based graphical user interface (GUI) for displaying peak <span class="hlt">wind</span> climatology and probabilities of exceeding peak-<span class="hlt">wind</span> thresholds for the Shuttle Landing Facility (SLF) at Kennedy Space Center. However, the shuttle must land at Edwards <span class="hlt">Air</span> Force Base (EAFB) in southern California when weather conditions at Kennedy Space Center in Florida are not acceptable, so SMG forecasters requested that a similar tool be developed for EAFB. Marshall Space Flight Center (MSFC) personnel archived and performed quality control of 2-minute average and 10-minute peak <span class="hlt">wind</span> speeds at each tower adjacent to the main runway at EAFB from 1997- 2004. They calculated <span class="hlt">wind</span> climatologies and probabilities of average peak <span class="hlt">wind</span> occurrence based on the average speed. The climatologies were calculated for each tower and month, and were stratified by hour, direction, and direction/hour. For the probabilities of peak <span class="hlt">wind</span> occurrence, MSFC calculated empirical and modeled probabilities of meeting or exceeding specific 10-minute peak <span class="hlt">wind</span> speeds using probability density functions. The AMU obtained and reformatted the data into Microsoft Excel PivotTables, which allows users to display different values with point-click-drag techniques. The GUT was then created from the PivotTables using Visual Basic for Applications code. The GUI is run through a macro within Microsoft Excel and allows forecasters to quickly display and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA455690','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA455690"><span>Basic Studies on High <span class="hlt">Pressure</span> <span class="hlt">Air</span> Plasmas</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2006-08-30</p> <p>which must be added a 1.5 month salary to A. Bugayev for assistance in laser and optic techniques. 2 Part II Technical report Plasma-induced phase shift...two-wavelength heterodyne interferometry applied to atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> plasma 11.1 .A. Plasma-induced phase shift - Electron density...a driver, since the error on the frequency leads to an error on the phase shift. (c) Optical elements Mirrors Protected mirrors must be used to stand</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016SPIE.9701E..0SC','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016SPIE.9701E..0SC"><span>Advancing a smart <span class="hlt">air</span> cushion system for preventing <span class="hlt">pressure</span> ulcers using projection Moiré for large deformation measurements</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cheng, Sheng-Lin; Tsai, Tsung-Heng; Lee, Carina Jean-Tien; Hsu, Yu-Hsiang; Lee, Chih-Kung</p> <p>2016-03-01</p> <p>A <span class="hlt">pressure</span> ulcer is one of the most important concerns for wheelchair bound patients with spinal cord injuries. A <span class="hlt">pressure</span> ulcer is a localized injury near the buttocks that bear ischial tuberosity oppression over a long period of time. Due to elevated compression to blood vessels, the surrounding tissues suffer from a lack of oxygen and nutrition. The ulcers eventually lead to skin damage followed by tissue necrosis. The current medical strategy is to minimize the occurrence of <span class="hlt">pressure</span> ulcers by regularly helping patients change their posture. However, these methods do not always work effectively or well. As a solution to fundamentally prevent <span class="hlt">pressure</span> ulcers, a smart <span class="hlt">air</span> cushion system was developed to detect and control <span class="hlt">pressure</span> actively. The <span class="hlt">air</span> cushion works by automatically adjusting a patient's sitting posture to effectively relieve the buttock <span class="hlt">pressure</span>. To analyze the correlation between the dynamic <span class="hlt">pressure</span> profiles of an <span class="hlt">air</span> cell with a patient's weight, a projection Moiré system was adopted to measure the deformation of an <span class="hlt">air</span> cell and its associated stress distribution. Combining a full-field deformation imaging with <span class="hlt">air</span> <span class="hlt">pressure</span> measured within an <span class="hlt">air</span> cell, the patient's weight and the stress distribution can be simultaneously obtained. By integrating a full-field optical metrology with a time varying <span class="hlt">pressure</span> sensor output coupled with different active <span class="hlt">air</span> control algorithms for various designs, we can tailor the ratio of the <span class="hlt">air</span> cells. Our preliminary data suggests that this newly developed smart <span class="hlt">air</span> cushion has the potential to selectively reduce localized compression on the tissues at the buttocks. Furthermore, it can take a patient's weight which is an additional benefit so that medical personnel can reference it to prescribe the correct drug dosages.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100021378','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100021378"><span>Statistical Short-Range Guidance for Peak <span class="hlt">Wind</span> Forecasts on Kennedy Space Center/Cape Canaveral <span class="hlt">Air</span> Force Station, Phase III</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crawford, Winifred</p> <p>2010-01-01</p> <p>This final report describes the development of a peak <span class="hlt">wind</span> forecast tool to assist forecasters in determining the probability of violating launch commit criteria (LCC) at Kennedy Space Center (KSC) and Cape Canaveral <span class="hlt">Air</span> Force Station (CCAFS). The peak <span class="hlt">winds</span> are an important forecast element for both the Space Shuttle and Expendable Launch Vehicle (ELV) programs. The LCC define specific peak <span class="hlt">wind</span> thresholds for each launch operation that cannot be exceeded in order to ensure the safety of the vehicle. The 45th Weather Squadron (45 WS) has found that peak <span class="hlt">winds</span> are a challenging parameter to forecast, particularly in the cool season months of October through April. Based on the importance of forecasting peak <span class="hlt">winds</span>, the 45 WS tasked the Applied Meteorology Unit (AMU) to develop a short-range peak-<span class="hlt">wind</span> forecast tool to assist in forecasting LCC violations.The tool includes climatologies of the 5-minute mean and peak <span class="hlt">winds</span> by month, hour, and direction, and probability distributions of the peak <span class="hlt">winds</span> as a function of the 5-minute mean <span class="hlt">wind</span> speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title42-vol1/pdf/CFR-2010-title42-vol1-sec84-149.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title42-vol1/pdf/CFR-2010-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title42-vol1/pdf/CFR-2011-title42-vol1-sec84-149.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title42-vol1/pdf/CFR-2011-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-149.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-149.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-149.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JGRA..123.2974O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JGRA..123.2974O"><span>Modeling Study of the Geospace System Response to the Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Enhancement on 17 March 2015</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ozturk, D. S.; Zou, S.; Ridley, A. J.; Slavin, J. A.</p> <p>2018-04-01</p> <p>The global magnetosphere-ionosphere-thermosphere system is intrinsically coupled and susceptible to external drivers such as solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancements. In order to understand the large-scale dynamic processes in the magnetosphere-ionosphere-thermosphere system due to the compression from the solar <span class="hlt">wind</span>, the 17 March 2015 sudden commencement was studied in detail using global numerical models. This storm was one of the most geoeffective events of the solar cycle 24 with a minimum Dst of -222 nT. The <span class="hlt">Wind</span> spacecraft recorded a 10-nPa increment in the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, while the interplanetary magnetic field BZ became further northward. The University of Michigan Block-Adaptive-Tree Solar <span class="hlt">wind</span> Roe-type Upwind Scheme global magnetohydrodynamic code was utilized to study the generation and propagation of perturbations associated with the compression of the magnetosphere system. In addition, the high-resolution electric potential and auroral power output from the magnetohydrodynamic model was used to drive the global ionosphere-thermosphere model to investigate the ionosphere-thermosphere system response to <span class="hlt">pressure</span> enhancement. During the compression, the electric potentials and convection patterns in the polar ionosphere were significantly altered when the preliminary impulse and main impulse field-aligned currents moved from dayside to nightside. As a result of enhanced frictional heating, plasma and neutral temperatures increased at the locations where the flow speeds were enhanced, whereas the electron density dropped at these locations. In particular, the region between the preliminary impulse and main impulse field-aligned currents experienced the most significant heating with 1000-K ion temperature increase and 20-K neutral temperature increase within 2 min. Comparison of the simulation results with the Poker Flat Incoherent Scatter Radar observations showed reasonable agreements despite underestimated magnitudes.</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('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4384198','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4384198"><span>Prenatal <span class="hlt">Air</span> Pollution Exposure and Newborn Blood <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Rifas-Shiman, Sheryl L.; Melly, Steven J.; Kloog, Itai; Luttmann-Gibson, Heike; Zanobetti, Antonella; Coull, Brent A.; Schwartz, Joel D.; Mittleman, Murray A.; Oken, Emily; Gillman, Matthew W.; Koutrakis, Petros; Gold, Diane R.</p> <p>2015-01-01</p> <p>Background <span class="hlt">Air</span> pollution exposure has been associated with increased blood <span class="hlt">pressure</span> in adults. Objective: We examined associations of antenatal exposure to ambient <span class="hlt">air</span> pollution with newborn systolic blood <span class="hlt">pressure</span> (SBP). Methods: We studied 1,131 mother–infant pairs in a Boston, Massachusetts, area pre-birth cohort. We calculated average exposures by trimester and during the 2 to 90 days before birth for temporally resolved fine particulate matter (≤ 2.5 μm; PM2.5), black carbon (BC), nitrogen oxides, nitrogen dioxide, ozone (O3), and carbon monoxide measured at stationary monitoring sites, and for spatiotemporally resolved estimates of PM2.5 and BC at the residence level. We measured SBP at a mean age of 30 ± 18 hr with an automated device. We used mixed-effects models to examine associations between <span class="hlt">air</span> pollutant exposures and SBP, taking into account measurement circumstances; child’s birth weight; mother’s age, race/ethnicity, socioeconomic position, and third-trimester BP; and time trend. Estimates represent differences in SBP associated with an interquartile range (IQR) increase in each pollutant. Results: Higher mean PM2.5 and BC exposures during the third trimester were associated with higher SBP (e.g., 1.0 mmHg; 95% CI: 0.1, 1.8 for a 0.32-μg/m3 increase in mean 90-day residential BC). In contrast, O3 was negatively associated with SBP (e.g., –2.3 mmHg; 95% CI: –4.4, –0.2 for a 13.5-ppb increase during the 90 days before birth). Conclusions: Exposures to PM2.5 and BC in late pregnancy were positively associated with newborn SBP, whereas O3 was negatively associated with SBP. Longitudinal follow-up will enable us to assess the implications of these findings for health during later childhood and adulthood. Citation: van Rossem L, Rifas-Shiman SL, Melly SJ, Kloog I, Luttmann-Gibson H, Zanobetti A, Coull BA, Schwartz JD, Mittleman MA, Oken E, Gillman MW, Koutrakis P, Gold DR. 2015. Prenatal <span class="hlt">air</span> pollution exposure and newborn blood <span class="hlt">pressure</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EGUGA..16.2997M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EGUGA..16.2997M"><span>Anywhere the <span class="hlt">Wind</span> Blows does Really Matter</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Montaldo, Nicola; Oren, Ram</p> <p>2014-05-01</p> <p>The variation of net ecosystem carbon exchange (NEE) has been explained at coarse scales with variation of forcing variables among climate regions and associated biomes, at the intermediate, mesoscale, with differences among dominating vegetation types and conditions, and at the misoscale with heterogeneity of the eddy covariance footprint properties. <span class="hlt">Wind</span> is rarely considered in analysis of surface fluxes for its effects on periodic budgets of water and carbon. In many regions conditions change frequently between maritime and continental depending on <span class="hlt">wind</span> velocity (VW) and direction. In these regions, water and carbon fluxes may respond to mesoscale weather patterns extending maritime influences far inland. Using eddy-covariance data from Sardinia, we show that daytime net carbon exchange (NEE) of a mixed pasture-woodland (grass-wild olive) ecosystem (Detto et al., 2006; Montaldo et al., 2008) increased with VW, especially during summer-dry conditions. As VW increased, the <span class="hlt">air</span>, humidified over sea, remains relatively moist and cool to a greater distance inland, reaching only ~50 km during slow Saharan Sirocco <span class="hlt">wind</span> but >160 km during mostly Mistral <span class="hlt">wind</span> (4 m/s) from Continental Europe. A 30% lower vapor <span class="hlt">pressure</span> deficit (D) associated with high VW (average 2 kPa at 4 m/s), allowed a 50% higher canopy stomatal conductance (gc) and, thus, photosynthesis. However, because gc and D have opposite effects on evapotranspiration (Ee), Ee was unaffected by VW. Thus, higher NEE during summertime Mistral reflects increased ecosystem water-use efficiency (We) and a departure from a costly carbon-water tradeoff. Yet many regions often experience high velocity <span class="hlt">winds</span>, attention is typically focused on the capacity of strong <span class="hlt">winds</span> to fan regional fires, threatening human habitation and natural habitats, and reducing Carbon storage (C), NEE and latent heat flux. However, depending on their origin, high velocity <span class="hlt">winds</span> can bring continental <span class="hlt">air</span> to the coast (e.g., Santa Ana <span class="hlt">winds</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA281061','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA281061"><span>Evaluation of Bauer K-20 Diesel Drive High <span class="hlt">Pressure</span> Breathing <span class="hlt">Air</span> Compressor</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1993-12-01</p> <p>was to: A. Determine if the compressor and Purification System provides compressed <span class="hlt">air</span> at the required <span class="hlt">pressures</span>, flow rates, quality and cleanliness... compressed <span class="hlt">air</span> return from the <span class="hlt">air</span> storage flasks to the compressor during unit shut down. All four stages of the compressor are protected by safety...1993. 6. Naval Ships Technical Manual, S9086-SY-STM-0O0, Chapeter 551 1st Rev. I November 1987. Compressed <span class="hlt">Air</span> Plants and Systems, para 551-4.2.21. 7</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950045290&hterms=Geomagnetic+reversal&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DGeomagnetic%2Breversal','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950045290&hterms=Geomagnetic+reversal&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DGeomagnetic%2Breversal"><span>Anomalous meridional thermospheric neutral <span class="hlt">winds</span> in the AE-E NATE data: Effects of the equatorial nighttime <span class="hlt">pressure</span> bulge</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Goembel, L.; Herrero, F. A.</p> <p>1995-01-01</p> <p>The work described here makes it possible to identify anomalous <span class="hlt">wind</span> behavior such as the nighttime meridional <span class="hlt">wind</span> abatements that occur at F-region heights. A new analysis technique uses a simple empirical <span class="hlt">wind</span> model to simulate measurements of 'normal' <span class="hlt">winds</span> (as measured by the Neutral Atmosphere and Temperature Experiment (NATE) that flew on the Atmosphere Explorer-E (AE-E)) to highlight anomalous <span class="hlt">wind</span> measurements made by the satellite while in circular orbits at 270-290 km altitude. Our approach is based on the recognition that the 'in orbit' <span class="hlt">wind</span> variation must show the combined effects of the diurnal <span class="hlt">wind</span> variation as seen from the ground with the latitude variation of the satellite orbit. For the data period 77250-78035 examined thus far, the <span class="hlt">wind</span> abatement always occurred with a corresponding <span class="hlt">pressure</span> or temperature maximum, and was detected on 12 out of the 36 nights with data. This study has revealed that the <span class="hlt">wind</span> abatement occur only during or shortly after increases in solar extreme ultraviolet (EUV) flux, as indicated by daily radio flux measurements. In the past, nighttime <span class="hlt">wind</span> reversals at mid-latitudes have been associated with increased geomagnetic activity. This study indicates that intensified solar EUV heating may be responsible for anomalous thermospheric nighttime <span class="hlt">winds</span> at mid-latitudes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980214918','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980214918"><span>Cooling <span class="hlt">Air</span> Inlet and Exit Geometries on Aircraft Engine Installations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Katz, Joseph; Corsiglia, Victor R.; Barlow, Philip R.</p> <p>1982-01-01</p> <p>A semispan wing and nacelle of a typical general aviation twin-engine aircraft was tested to evaluate the cooling capability and drag or several nacelle shapes; the nacelle shapes included cooling <span class="hlt">air</span> inlet and exit variations. The tests were conducted in the Ames Research Center 40 x 80-ft <span class="hlt">Wind</span> Tunnel. It was found that the cooling <span class="hlt">air</span> inlet geometry of opposed piston engine installations has a major effect on inlet <span class="hlt">pressure</span> recovery, but only a minor effect on drag. Exit location showed large effect on drag, especially for those locations on the sides of the nacelle where the suction characteristics were based on interaction with the wing surface <span class="hlt">pressures</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29504266','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29504266"><span>Prevention of <span class="hlt">pressure</span> ulcers with a static <span class="hlt">air</span> support surface: A systematic review.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Serraes, Brecht; van Leen, Martin; Schols, Jos; Van Hecke, Ann; Verhaeghe, Sofie; Beeckman, Dimitri</p> <p>2018-06-01</p> <p>The aims of this study were to identify, assess, and summarise available evidence about the effectiveness of static <span class="hlt">air</span> mattress overlays to prevent <span class="hlt">pressure</span> ulcers. The primary outcome was the incidence of <span class="hlt">pressure</span> ulcers. Secondary outcomes included costs and patient comfort. This study was a systematic review. Six electronic databases were consulted: Cochrane Library, EMBASE, PubMed (Medline), CINAHL (EBSCOhost interface), Science direct, and Web of Science. In addition, a hand search through reviews, conference proceedings, and the reference lists of the included studies was performed to identify additional studies. Potential studies were reviewed and assessed by 2 independent authors based on the title and abstract. Decisions regarding inclusion or exclusion of the studies were based on a consensus between the authors. Studies were included if the following criteria were met: reporting an original study; the outcome was the incidence of <span class="hlt">pressure</span> ulcer categories I to IV when using a static <span class="hlt">air</span> mattress overlay and/or in comparison with other <span class="hlt">pressure</span>-redistribution device(s); and studies published in English, French, and Dutch. No limitation was set on study setting, design, and date of publication. The methodological quality assessment was evaluated using the Critical Appraisal Skills Program Tool. Results were reported in a descriptive way to reflect the exploratory nature of the review. The searches included 13 studies: randomised controlled trials (n = 11) and cohort studies (n = 2). The mean <span class="hlt">pressure</span> ulcer incidence figures found in the different settings were, respectively, 7.8% <span class="hlt">pressure</span> ulcers of categories II to IV in nursing homes, 9.06% <span class="hlt">pressure</span> ulcers of categories I to IV in intensive care settings, and 12% <span class="hlt">pressure</span> ulcers of categories I to IV in orthopaedic wards. Seven comparative studies reported a lower incidence in the groups of patients on a static <span class="hlt">air</span> mattress overlay. Three studies reported a statistical (P < .1) lower incidence compared</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-PIA22362.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-PIA22362.html"><span>Polar <span class="hlt">Winds</span></span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2018-04-05</p> <p>This VIS image shows 'streamers' of clouds created by katabatic <span class="hlt">winds</span> at the north polar cap. Katabatic <span class="hlt">winds</span> are created by cold <span class="hlt">air</span> sinking at the pole and then speeding along the ice surface towards the edge of the polar cap. When the <span class="hlt">winds</span> enter troughs the <span class="hlt">wind</span> regime changes from laminar flow to choatic and clouds of ice particles and/or dust are visible. This <span class="hlt">wind</span> activity peaks at the start of northern hemisphere summer. Orbit Number: 53942 Latitude: 86.8433 Longitude: 99.3149 Instrument: VIS Captured: 2014-02-10 10:50 https://photojournal.jpl.nasa.gov/catalog/PIA22362</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26860399','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26860399"><span>Tracheostomy Tube Type and Inner Cannula Selection Impact <span class="hlt">Pressure</span> and Resistance to <span class="hlt">Air</span> Flow.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pryor, Lee N; Baldwin, Claire E; Ward, Elizabeth C; Cornwell, Petrea L; O'Connor, Stephanie N; Chapman, Marianne J; Bersten, Andrew D</p> <p>2016-05-01</p> <p>Advancements in tracheostomy tube design now provide clinicians with a range of options to facilitate communication for individuals receiving ventilator assistance through a cuffed tube. Little is known about the impact of these modern design features on resistance to <span class="hlt">air</span> flow. We undertook a bench model test to measure <span class="hlt">pressure</span>-flow characteristics and resistance of a range of tubes of similar outer diameter, including those enabling subglottic suction and speech. A constant inspiratory ± expiratory <span class="hlt">air</span> flow was generated at increasing flows up to 150 L/min through each tube (with or without optional, mandatory, or interchangeable inner cannula). Driving <span class="hlt">pressures</span> were measured, and resistance was calculated (cm H2O/L/s). <span class="hlt">Pressures</span> changed with increasing flow (P < .001) and tube type (P < .001), with differing patterns of <span class="hlt">pressure</span> change according to the type of tube (P < .001) and direction of <span class="hlt">air</span> flow. The single-lumen reference tube encountered the lowest inspiratory and expiratory <span class="hlt">pressures</span> compared with all double-lumen tubes (P < .001); placement of an optional inner cannula increased bidirectional tube resistance by a factor of 3. For a tube with interchangeable inner cannulas, the type of cannula altered <span class="hlt">pressure</span> and resistance differently (P < .001); the speech cannula in particular amplified <span class="hlt">pressure</span>-flow changes and increased tube resistance by more than a factor of 4. Tracheostomy tube type and inner cannula selection imposed differing <span class="hlt">pressures</span> and resistance to <span class="hlt">air</span> flow during inspiration and expiration. These differences may be important when selecting airway equipment or when setting parameters for monitoring, particularly for patients receiving supported ventilation or during the weaning process. Copyright © 2016 by Daedalus Enterprises.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950007817','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950007817"><span>Flight and full-scale <span class="hlt">wind</span>-tunnel comparison of <span class="hlt">pressure</span> distributions from an F-18 aircraft at high angles of attack. [Conducted in NASA Ames Research Center's 80 by 120 ft <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fisher, David F.; Lanser, Wendy R.</p> <p>1994-01-01</p> <p><span class="hlt">Pressure</span> distributions were obtained at nearly identical fuselage stations and wing chord butt lines in flight on the F-18 HARV at NASA Dryden Flight Research Center and in the NASA Ames Research Center's 80 by 120 ft <span class="hlt">wind</span> tunnel on a full-scale F/A-18 aircraft. The static <span class="hlt">pressures</span> were measured at the identical five stations on the forebody, three stations on the left and right leading-edge extensions, and three spanwise stations on the wing. Comparisons of the flight and <span class="hlt">wind</span>-tunnel <span class="hlt">pressure</span> distributions were made at alpha = 30 deg, 45 deg, and 60 deg/59 deg. In general, very good agreement was found. Minor differences were noted at the forebody at alpha = 45 deg and 60 deg in the magnitude of the vortex footprints and a Mach number effect was noted at the leading-edge extension at alpha = 30 deg. The inboard leading edge flap data from the <span class="hlt">wind</span> tunnel at alpha = 59 deg showed a suction peak that did not appear in the flight data. This was the result of a vortex from the corner of the leading edge flap whose path was altered by the lack of an engine simulation in the <span class="hlt">wind</span> tunnel.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/az0246.photos.009708p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/az0246.photos.009708p/"><span>27. EXTENSION OF SURGE CHAMBER AND <span class="hlt">AIR</span> PIPES TO <span class="hlt">PRESSURE</span> ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>27. EXTENSION OF SURGE CHAMBER AND <span class="hlt">AIR</span> PIPES TO <span class="hlt">PRESSURE</span> LINE, HIGHLINE PUMPING PLANT. December 11, 1920 - Highline Canal & Pumping Station, South side of Salt River between Tempe, Phoenix & Mesa, Tempe, Maricopa County, AZ</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EPJWC..9202015D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EPJWC..9202015D"><span><span class="hlt">Pressure</span> Regulators as Valves for Saving Compressed <span class="hlt">Air</span> and their Influence on System Dynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dvořák, Lukáš; Fojtášek, Kamil</p> <p>2015-05-01</p> <p><span class="hlt">Pressure</span> regulators in the field of pneumatic mechanisms can be used as valves for saving compressed <span class="hlt">air</span>. For example it can be used to reduce the <span class="hlt">pressure</span> when the piston rod is retracting unloaded and thus it is possible to save some energy. However the problem is that saving valve can significantly affect the dynamics of the pneumatic system. The lower <span class="hlt">pressure</span> in the piston rod chamber causes extension of time for retraction of the piston rod. This article compare the <span class="hlt">air</span> consumption experimentally determined and calculated, measured curves of <span class="hlt">pressure</span> in cylinder chambers and piston speed when saving valve is set up differently.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16575583','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16575583"><span>An objective classification system of <span class="hlt">air</span> mass types for Szeged, Hungary, with special attention to plant pollen levels.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Makra, László; Juhász, Miklós; Mika, János; Bartzokas, Aristides; Béczi, Rita; Sümeghy, Zoltán</p> <p>2006-07-01</p> <p>This paper discusses the characteristic <span class="hlt">air</span> mass types over the Carpathian Basin in relation to plant pollen levels over annual pollination periods. Based on the European Centre for Medium-Range Weather Forecasts dataset, daily sea-level <span class="hlt">pressure</span> fields analysed at 00 UTC were prepared for each <span class="hlt">air</span> mass type (cluster) in order to relate sea-level <span class="hlt">pressure</span> patterns to pollen levels in Szeged, Hungary. The database comprises daily values of 12 meteorological parameters and daily pollen concentrations of 24 species for their pollination periods from 1997 to 2001. Characteristic <span class="hlt">air</span> mass types were objectively defined via factor analysis and cluster analysis. According to the results, nine <span class="hlt">air</span> mass types (clusters) were detected for pollination periods of the year corresponding to pollen levels that appear with higher concentration when irradiance is moderate while <span class="hlt">wind</span> speed is moderate or high. This is the case when an anticyclone prevails in the region west of the Carpathian Basin and when Hungary is under the influence of zonal currents (<span class="hlt">wind</span> speed is high). The sea level <span class="hlt">pressure</span> systems associated with low pollen concentrations are mostly similar to those connected to higher pollen concentrations, and arise when <span class="hlt">wind</span> speed is low or moderate. Low pollen levels occur when an anticyclone prevails in the region west of the Carpathian Basin, as well as when an anticyclone covers the region with Hungary at its centre. Hence, anticyclonic or anticyclonic ridge weather situations seem to be relevant in classifying pollen levels.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010EGUGA..12..259T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010EGUGA..12..259T"><span>Laboratory modeling of <span class="hlt">air</span>-sea interaction under severe <span class="hlt">wind</span> conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Troitskaya, Yuliya; Vasiliy, Kazakov; Nicolay, Bogatov; Olga, Ermakova; Mikhail, Salin; Daniil, Sergeev; Maxim, Vdovin</p> <p>2010-05-01</p> <p><span class="hlt">Wind</span>-wave interaction at extreme <span class="hlt">wind</span> speed is of special interest now in connection with the problem of explanation of the sea surface drag saturation at the <span class="hlt">wind</span> speed exceeding 30 m/s. The idea on saturation (and even reduction) of the coefficient of aerodynamic resistance of the sea surface at hurricane <span class="hlt">wind</span> speed was first suggested by Emanuel (1995) on the basis of theoretical analysis of sensitivity of maximum <span class="hlt">wind</span> speed in a hurricane to the ratio of the enthalpy and momentum exchange coefficients. Both field (Powell, Vickery, Reinhold, 2003, French et al, 2007, Black, et al, 2007) and laboratory (Donelan et al, 2004) experiments confirmed that at hurricane <span class="hlt">wind</span> speed the sea surface drag coefficient is significantly reduced in comparison with the parameterization obtained at moderate to strong <span class="hlt">wind</span> conditions. Two groups of possible theoretical mechanisms for explanation of the effect of the sea surface drag reduction can be specified. In the first group of models developed by Kudryavtsev & Makin (2007) and Kukulka,Hara Belcher (2007), the sea surface drag reduction is explained by peculiarities of the <span class="hlt">air</span> flow over breaking waves. Another approach more appropriate for the conditions of developed sea exploits the effect of sea drops and sprays on the <span class="hlt">wind</span>-wave momentum exchange (Andreas, 2004; Makin, 2005; Kudryavtsev, 2006). The main objective of this work is investigation of factors determining momentum exchange under high <span class="hlt">wind</span> speeds basing on the laboratory experiment in a well controlled environment. The experiments were carried out in the Thermo-Stratified <span class="hlt">WInd</span>-WAve Tank (TSWIWAT) of the Institute of Applied Physics. The parameters of the facility are as follows: airflow 0 - 25 m/s (equivalent 10-m neutral <span class="hlt">wind</span> speed U10 up to 60 m/s), dimensions 10m x 0.4m x 0.7 m, temperature stratification of the water layer. Simultaneous measurements of the airflow velocity profiles and <span class="hlt">wind</span> waves were carried out in the wide range of <span class="hlt">wind</span> velocities. Airflow</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25831297','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25831297"><span>Fiber in-line Mach-Zehnder interferometer based on an inner <span class="hlt">air</span>-cavity for high-<span class="hlt">pressure</span> sensing.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Talataisong, W; Wang, D N; Chitaree, R; Liao, C R; Wang, C</p> <p>2015-04-01</p> <p>We demonstrate a fiber in-line Mach-Zehnder interferometer based on an inner <span class="hlt">air</span>-cavity with open micro-channel for high-<span class="hlt">pressure</span> sensing applications. The inner <span class="hlt">air</span>-cavity is fabricated by combining femtosecond laser micromachining and the fusion splicing technique. The micro-channel is drilled on the top of the inner <span class="hlt">air</span>-cavity to allow the high-<span class="hlt">pressure</span> gas to flow in. The fiber in-line device is miniature, robust, and stable in operation and exhibits a high <span class="hlt">pressure</span> sensitivity of ∼8,239  pm/MPa.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740010545','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740010545"><span><span class="hlt">Pressure</span> distribution on a vectored-thrust V/STOL fighter in the transition-speed range. [<span class="hlt">wind</span> tunnel tests to measure <span class="hlt">pressure</span> distribution on body and wing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mineck, R. E.; Margason, R. J.</p> <p>1974-01-01</p> <p>A <span class="hlt">wind</span>-tunnel investigation has been conducted in the Langley V/STOL tunnel with a vectored-thrust V/STOL fighter configuration to obtain detailed <span class="hlt">pressure</span> measurements on the body and on the wing in the transition-speed range. The vectored-thrust jet exhaust induced a region of negative <span class="hlt">pressure</span> coefficients on the lower surface of the wing and on the bottom of the fuselage. The location of the jet exhaust relative to the wing was a major factor in determining the extent of the region of negative <span class="hlt">pressure</span> coefficients.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000116508','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000116508"><span>BOREAS AFM-2 Wyoming King <span class="hlt">Air</span> 1994 Aircraft Sounding Data</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kelly, Robert D.; Hall, Forrest G. (Editor); Knapp, David E. (Editor); Smith, David E. (Technical Monitor)</p> <p>2000-01-01</p> <p>The BOREAS AFM-2 team used the University of Wyoming King <span class="hlt">Air</span> aircraft during IFCs 1, 2, and 3 in 1994 to collected pass-by-pass fluxes (and many other statistics) for the large number of level (constant altitude), straight-line passes used in a variety of flight patterns over the SSA and NSA and areas along the transect between these study areas. The data described here form a second set, namely soundings that were incorporated into nearly every research flight by the King <span class="hlt">Air</span> in 1994. These soundings generally went from near the surface to above the inversion layer. Most were flown immediately after takeoff or immediately after finishing the last flux pattern of that particular day's flights. The parameters that were measured include <span class="hlt">wind</span> direction, <span class="hlt">wind</span> speed, west <span class="hlt">wind</span> component (u), south <span class="hlt">wind</span> component (v), static <span class="hlt">pressure</span>, <span class="hlt">air</span> dry bulb temperature, potential temperature, dewpoint, temperature, water vapor mixing ratio, and CO2 concentration. Data on the aircraft's location, attitude, and altitude during data collection are also provided. These data are stored in tabular ASCH files. The data files are available on a CD-ROM (see document number 20010000884) or from the Oak Ridge National Laboratory (ORNL) Distributed Active Archive Center (DAAC).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JGRA..123..385L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JGRA..123..385L"><span>The Effects of Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Changes on the Substorm Auroras and Energetic Electron Injections on 24 August 2005</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, L. Y.; Wang, Z. Q.</p> <p>2018-01-01</p> <p>After the passage of an interplanetary (IP) shock at 06:13 UT on 24 August 2005, the enhancement (>6 nPa) of solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> and the southward turning of interplanetary magnetic field (IMF) cause the earthward movement of dayside magnetopause and the drift loss of energetic particles near geosynchronous orbit. The persistent electron drift loss makes the geosynchronous satellites cannot observe the substorm electron injection phenomenon during the two substorm expansion phases (06:57-07:39 UT) on that day. Behind the IP shock, the fluctuations ( 0.5-3 nPa) of solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> not only alter the dayside auroral brightness but also cause the entire auroral oval to swing in the day-night direction. However, there is no Pi2 pulsation in the nightside auroral oval during the substorm growth phase from 06:13 to 06:57 UT. During the subsequent two substorm expansion phases, the substorm expansion activities cause the nightside aurora oval brightening from substorm onset site to higher latitudes, and meanwhile, the enhancement (decline) of solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> makes the nightside auroral oval move toward the magnetic equator (the magnetic pole). These observations demonstrate that solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> changes and substorm expansion activities can jointly control the luminosity and location of the nightside auroral oval when the internal and external disturbances occur simultaneously. During the impact of a strong IP shock, the earthward movement of dayside magnetopause probably causes the disappearance of the substorm electron injections near geosynchronous orbit.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JGRC..122.8034B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JGRC..122.8034B"><span><span class="hlt">Wind</span> Speed and Sea State Dependencies of <span class="hlt">Air</span>-Sea Gas Transfer: Results From the High <span class="hlt">Wind</span> Speed Gas Exchange Study (HiWinGS)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Blomquist, B. W.; Brumer, S. E.; Fairall, C. W.; Huebert, B. J.; Zappa, C. J.; Brooks, I. M.; Yang, M.; Bariteau, L.; Prytherch, J.; Hare, J. E.; Czerski, H.; Matei, A.; Pascal, R. W.</p> <p>2017-10-01</p> <p>A variety of physical mechanisms are jointly responsible for facilitating <span class="hlt">air</span>-sea gas transfer through turbulent processes at the atmosphere-ocean interface. The nature and relative importance of these mechanisms evolves with increasing <span class="hlt">wind</span> speed. Theoretical and modeling approaches are advancing, but the limited quantity of observational data at high <span class="hlt">wind</span> speeds hinders the assessment of these efforts. The HiWinGS project successfully measured gas transfer coefficients (k660) with coincident wave statistics under conditions with hourly mean <span class="hlt">wind</span> speeds up to 24 m s-1 and significant wave heights to 8 m. Measurements of k660 for carbon dioxide (CO2) and dimethylsulfide (DMS) show an increasing trend with respect to 10 m neutral <span class="hlt">wind</span> speed (U10N), following a power law relationship of the form: k660 CO2˜U10N1.68 and k660 dms˜U10N1.33. Among seven high <span class="hlt">wind</span> speed events, CO2 transfer responded to the intensity of wave breaking, which depended on both <span class="hlt">wind</span> speed and sea state in a complex manner, with k660 CO2 increasing as the <span class="hlt">wind</span> sea approaches full development. A similar response is not observed for DMS. These results confirm the importance of breaking waves and bubble injection mechanisms in facilitating CO2 transfer. A modified version of the Coupled Ocean-Atmosphere Response Experiment Gas transfer algorithm (COAREG ver. 3.5), incorporating a sea state-dependent calculation of bubble-mediated transfer, successfully reproduces the mean trend in observed k660 with <span class="hlt">wind</span> speed for both gases. Significant suppression of gas transfer by large waves was not observed during HiWinGS, in contrast to results from two prior field programs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29363824','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29363824"><span>Comparison of water and <span class="hlt">air</span> charged transducer catheter <span class="hlt">pressures</span> in the evaluation of cystometrogram and voiding <span class="hlt">pressure</span> studies.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>McKinney, Timothy B; Babin, Elizabeth A; Ciolfi, Veronica; McKinney, Cynthia R; Shah, Nima</p> <p>2018-04-01</p> <p><span class="hlt">Air</span>-charged (AC) and water-perfused (WP) catheters have been evaluated for differences in measuring <span class="hlt">pressures</span> for voiding dysfunction. Typically, a two-catheter system was used. We believe that simultaneous <span class="hlt">pressure</span> measurements with AC and WP in a single catheter will provide analogous <span class="hlt">pressures</span> for coughs, Valsalvas, and maximum <span class="hlt">pressures</span> in voiding <span class="hlt">pressure</span> studies (VPS). This IRB approved prospective study included 50 women over age 21. AC dual TDOC catheters were utilized. The water-filling channel served as the bladder filler and the water <span class="hlt">pressure</span> readings. Patients were evaluated with empty bladders and at volumes of 50-100 mL, 200 mL, and maximum capacity with cough and Valsalva maneuvers. Comparative analysis was performed on maximum stress peak <span class="hlt">pressures</span>. At maximum bladder capacity, VPS was done and maximum voiding <span class="hlt">pressure</span> was recorded. Comparing coughs and Valsalva maneuvers <span class="hlt">pressures</span>, there was significant increase in variability between AC and WP measurements with less than 50 mL volume (P < 0.001). Significant correlations were observed between AC and WP measurements for coughs and Valsalvas with bladder volume over 50 mL. Visual impression showed virtually identical tracings. Cough measurements had an average difference of 0.25 cmH 2 O (±8.81) and Valsalva measurements had an average difference of 3.15 cmH 2 O (±4.72). Thirty-eight women had usable maximum voiding <span class="hlt">pressure</span> measurements and had a strong correlation. Cystometrogram and maximum voiding <span class="hlt">pressure</span> measurements done with either water or <span class="hlt">air</span> charged catheters will yield similarly accurate results and are comparable. Results suggest more variability at low bladder volumes <50 mL. © 2018 Wiley Periodicals, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1982Entro..18..122L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1982Entro..18..122L"><span>A project for exploitation of a new form of solar energy: the <span class="hlt">wind</span> chill. I - The importance to the energy field. II - Application for building heat and electricity production</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Le Goff, P.</p> <p></p> <p>Calculations of the temperature, humidity, <span class="hlt">pressure</span>, and velocity of the <span class="hlt">wind</span> at different locations are provided to demonstrate that energy characteristics of the <span class="hlt">wind</span> other than the mechanical <span class="hlt">pressure</span> exerted by the <span class="hlt">wind</span> on obstacles are significant. A system is described, based on the heat pump principle, which takes advantage of the thermal inertia of the <span class="hlt">wind</span>, known to remain around freezing even in Siberian winters. An analysis of the energy available for heat transfer in a site in France demonstrates that the dryness, warmth, or chill of a cubic meter of <span class="hlt">air</span> contains, continuously, 100-1000 times the kinetic energy of moving <span class="hlt">air</span>. In excess of one kilowatt/sq m is available for extraction by heat pumps based on designs for ocean thermal energy conversion. An electric generating system is described which would yield 10-50 times the mechanical power of a windmill using the same collector area. Finally, a wall heat exchanger for a house is presented which would gain heat energy proportional to the severity of the winter <span class="hlt">wind</span>.</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('http://adsabs.harvard.edu/abs/2015ExFl...56...84D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015ExFl...56...84D"><span>Picosecond ballistic imaging of diesel injection in high-temperature and high-<span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Duran, Sean P.; Porter, Jason M.; Parker, Terence E.</p> <p>2015-04-01</p> <p>The first successful demonstration of picosecond ballistic imaging using a 15-ps-pulse-duration laser in diesel sprays at temperature and <span class="hlt">pressure</span> is reported. This technique uses an optical Kerr effect shutter constructed from a CS2 liquid cell and a 15-ps pulse at 532 nm. The optical shutter can be adjusted to produce effective imaging pulses between 7 and 16 ps. This technique is used to image the near-orifice region (first 3 mm) of diesel sprays from a high-<span class="hlt">pressure</span> single-hole fuel injector. Ballistic imaging of dodecane and methyl oleate sprays injected into ambient <span class="hlt">air</span> and diesel injection at preignition engine-like conditions are reported. Dodecane was injected into <span class="hlt">air</span> heated to 600 °C and <span class="hlt">pressurized</span> to 20 atm. The resulting images of the near-orifice region at these conditions reveal dramatic shedding of the liquid near the nozzle, an effect that has been predicted, but to our knowledge never before imaged. These shedding structures have an approximate spatial frequency of 10 mm-1 with lengths from 50 to 200 μm. Several parameters are explored including injection <span class="hlt">pressure</span>, liquid fuel temperature, <span class="hlt">air</span> temperature and <span class="hlt">pressure</span>, and fuel type. Resulting trends are summarized with accompanying images.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://rosap.ntl.bts.gov/view/dot/35042','DOTNTL'); return false;" href="https://rosap.ntl.bts.gov/view/dot/35042"><span>Post-Tensioning Duct <span class="hlt">Air</span> <span class="hlt">Pressure</span> Testing Effects on Web Cracking</span></a></p> <p><a target="_blank" href="http://ntlsearch.bts.gov/tris/index.do">DOT National Transportation Integrated Search</a></p> <p></p> <p>2015-01-01</p> <p>Nevada Department of Transportation (NDOT) post-tensioned concrete bridges have experienced web cracking near the post-tensioning ducts during the construction process. The ducts were <span class="hlt">air</span> <span class="hlt">pressure</span> tested to ensure the duct can successfully be grouted...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19830006994','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19830006994"><span><span class="hlt">Wind</span> tunnel evaluation of <span class="hlt">air</span>-foil performance using simulated ice shapes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bragg, M. B.; Zaguli, R. J.; Gregorek, G. M.</p> <p>1982-01-01</p> <p>A two-phase <span class="hlt">wind</span> tunnel test was conducted in the 6 by 9 foot Icing Research Tunnel (IRT) at NASA Lewis Research Center to evaluate the effect of ice on the performance of a full scale general aviation wing. In the first IRT tests, rime and glaze shapes were carefully documented as functions of angle of attack and free stream conditions. Next, simulated ice shapes were constructed for two rime and two glaze shapes and used in the second IRT tunnel entry. The ice shapes and the clean airfoil were tapped to obtain surface <span class="hlt">pressures</span> and a probe used to measure the wake characteristics. These data were recorded and processed, on-line, with a minicomputer/digital data acquisition system. The effect of both rime and glaze ice on the <span class="hlt">pressure</span> distribution, Cl, Cd, and Cm are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29606673','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29606673"><span><span class="hlt">Pressure</span> Injury Development in Patients Treated by Critical Care <span class="hlt">Air</span> Transport Teams: A Case-Control Study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dukes, Susan F; Maupin, Genny M; Thomas, Marilyn E; Mortimer, Darcy L</p> <p>2018-04-01</p> <p>The US <span class="hlt">Air</span> Force transports critically ill patients from all over the world, with transport times commonly ranging from 6 to 11 hours. Few outcome measures have been tracked for these patients. Traditional methods to prevent <span class="hlt">pressure</span> injuries in civilian hospitals are often not feasible in the military transport environment. The incidence rate and risk factors are described of en route-related <span class="hlt">pressure</span> injuries for patients overseen by the Critical Care <span class="hlt">Air</span> Transport Team. This retrospective, case-control, medical records review investigated risk factors for <span class="hlt">pressure</span> injury in patients who developed a <span class="hlt">pressure</span> injury after their transport flight compared with those with no documented <span class="hlt">pressure</span> injuries. The <span class="hlt">pressure</span> injury rate was 4.9%. Between 2008 and 2012, 141 patients in whom <span class="hlt">pressure</span> injuries developed and who had received care by the team were matched with 141 patients cared for by the team but did not have <span class="hlt">pressure</span> injury. According to regression analysis, body mass index and 2 or more Critical Care <span class="hlt">Air</span> Transport Team transports per patient were associated with <span class="hlt">pressure</span> injury development. Although the <span class="hlt">pressure</span> injury rate of 4.9% in this cohort of patients is consistent with that reported by civilian critical care units, the rate must be interpreted with caution, because civilian study data frequently represent the entire intensive care unit length of stay. Targeted interventions for patients with increased body mass index and 2 or more critical care <span class="hlt">air</span> transports per patient may help decrease the development of <span class="hlt">pressure</span> injury in these patients. ©2018 American Association of Critical-Care Nurses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/803766','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/803766"><span>A study of <span class="hlt">pressure</span> losses in residential <span class="hlt">air</span> distribution systems</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>Abushakra, Bass; Walker, Iain S.; Sherman, Max H.</p> <p>2002-07-01</p> <p>An experimental study was conducted to evaluate the <span class="hlt">pressure</span> drop characteristics of residential duct system components that are either not available or not thoroughly (sometimes incorrectly) described in existing duct design literature. The tests were designed to imitate cases normally found in typical residential and light commercial installations. The study included three different sizes of flexible ducts, under different compression configurations, splitter boxes, supply boots, and a fresh <span class="hlt">air</span> intake hood. The experimental tests conformed to ASHRAE Standard 120P--''Methods of Testing to Determine Flow Resistance of HVAC <span class="hlt">Air</span> Ducts and Fittings''. The flexible duct study covered compressibility and bending effectsmore » on the total <span class="hlt">pressure</span> drop, and the results showed that the available published references tend to underestimate the effects of compression in flexible ducts that can increase <span class="hlt">pressure</span> drops by up to a factor of nine. The supply boots were tested under different configurations including a setup where a flexible duct elbow connection was considered as an integral part of the supply boot. The supply boots results showed that diffusers can increase the <span class="hlt">pressure</span> drop by up to a factor of two in exit fittings, and the installation configuration can increase the <span class="hlt">pressure</span> drop by up to a factor of five. The results showed that it is crucial for designers and contractors to be aware of the compressibility effects of the flexible duct, and the installation of supply boots and diffusers.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980223963','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980223963"><span>The Real-Time Wall Interference Correction System of the NASA Ames 12-Foot <span class="hlt">Pressure</span> <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ulbrich, Norbert</p> <p>1998-01-01</p> <p>An improved version of the Wall Signature Method was developed to compute wall interference effects in three-dimensional subsonic <span class="hlt">wind</span> tunnel testing of aircraft models in real-time. The method may be applied to a full-span or a semispan model. A simplified singularity representation of the aircraft model is used. Fuselage, support system, propulsion simulator, and separation wake volume blockage effects are represented by point sources and sinks. Lifting effects are represented by semi-infinite line doublets. The singularity representation of the test article is combined with the measurement of <span class="hlt">wind</span> tunnel test reference conditions, wall <span class="hlt">pressure</span>, lift force, thrust force, pitching moment, rolling moment, and pre-computed solutions of the subsonic potential equation to determine first order wall interference corrections. Second order wall interference corrections for pitching and rolling moment coefficient are also determined. A new procedure is presented that estimates a rolling moment coefficient correction for wings with non-symmetric lift distribution. Experimental data obtained during the calibration of the Ames Bipod model support system and during tests of two semispan models mounted on an image plane in the NASA Ames 12 ft. <span class="hlt">Pressure</span> <span class="hlt">Wind</span> Tunnel are used to demonstrate the application of the wall interference correction method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4568288','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4568288"><span>Reminiscences on the study of <span class="hlt">wind</span> waves</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>MITSUYASU, Hisashi</p> <p>2015-01-01</p> <p>The <span class="hlt">wind</span> blowing over sea surface generates tiny <span class="hlt">wind</span> waves. They develop with time and space absorbing <span class="hlt">wind</span> energy, and become huge <span class="hlt">wind</span> waves usually referred to ocean surface waves. The <span class="hlt">wind</span> waves cause not only serious sea disasters but also take important roles in the local and global climate changes by affecting the fluxes of momentum, heat and gases (e.g. CO2) through the <span class="hlt">air</span>-sea boundary. The present paper reviews the selected studies on <span class="hlt">wind</span> waves conducted by our group in the Research Institute for Applied Mechanics (RIAM), Kyushu University. The themes discussed are interactions between water waves and <span class="hlt">winds</span>, the energy spectrum of <span class="hlt">wind</span> waves, nonlinear properties of <span class="hlt">wind</span> waves, and the effects of surfactant on some <span class="hlt">air</span>-sea interaction phenomena. PMID:25864467</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25864467','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25864467"><span>Reminiscences on the study of <span class="hlt">wind</span> waves.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mitsuyasu, Hisashi</p> <p>2015-01-01</p> <p>The <span class="hlt">wind</span> blowing over sea surface generates tiny <span class="hlt">wind</span> waves. They develop with time and space absorbing <span class="hlt">wind</span> energy, and become huge <span class="hlt">wind</span> waves usually referred to ocean surface waves. The <span class="hlt">wind</span> waves cause not only serious sea disasters but also take important roles in the local and global climate changes by affecting the fluxes of momentum, heat and gases (e.g. CO2) through the <span class="hlt">air</span>-sea boundary. The present paper reviews the selected studies on <span class="hlt">wind</span> waves conducted by our group in the Research Institute for Applied Mechanics (RIAM), Kyushu University. The themes discussed are interactions between water waves and <span class="hlt">winds</span>, the energy spectrum of <span class="hlt">wind</span> waves, nonlinear properties of <span class="hlt">wind</span> waves, and the effects of surfactant on some <span class="hlt">air</span>-sea interaction phenomena.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012EGUGA..14.3267B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012EGUGA..14.3267B"><span>Comparison of ionospheric convection and the transpolar potential before and after solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> fronts: implications for magnetospheric reconnection</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Boudouridis, A.; Zesta, E.; Lyons, L. R.; Kim, H.-J.; Lummerzheim, D.; Wiltberger, M.; Weygand, J. M.; Ruohoniemi, J. M.; Ridley, A. J.</p> <p>2012-04-01</p> <p>The solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, both through its steady state value and through its variations, plays an important role in the determination of the state of the terrestrial magnetosphere and ionosphere, its effects being only secondary to those of the Interplanetary Magnetic Field (IMF). Recent studies have demonstrated the significant effect solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> enhancements have on ionospheric convection and the transpolar potential. Further studies have shown a strong response of the polar cap boundary and thus the open flux content of the magnetosphere. These studies clearly illustrate the strong coupling of solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> fronts to the terrestrial magnetosphere-ionosphere system. We present statistical studies of the response of Super Dual Auroral Radar Network (SuperDARN) flows, and Assimilative Mapping of Ionospheric Electrodynamics (AMIE) transpolar potentials to sudden enhancements in solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>. The SuperDARN results show that the convection is enhanced within both the dayside and nightside ionosphere. The dayside response is more clear and immediate, while the response on the nightside is slower and more evident for low IMF By values. AMIE results show that the overall convection, represented by the transpolar potential, has a strong response immediately after an increase in <span class="hlt">pressure</span>, with magnitude and duration modulated by the background IMF Bz conditions. We compare the location of the SuperDARN convection enhancements with the location and motion of the polar cap boundary, as determined by POLAR Ultra-Violet Imager (UVI) images and runs of the Lyon-Fedder-Mobarry (LFM) global magnetohydrodynamic model for specific events. We find that the boundary exhibits a poleward motion after the increase in dynamic <span class="hlt">pressure</span>. The enhanced ionospheric flows and the poleward motion of the boundary on the nightside are both signatures of enhanced tail reconnection, a conclusion that is reinforced by the observation of the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.epa.gov/caa-permitting/application-documents-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound','PESTICIDES'); return false;" href="https://www.epa.gov/caa-permitting/application-documents-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound"><span>Application Documents for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit)</span></a></p> <p><a target="_blank" href="http://www.epa.gov/pesticides/search.htm">EPA Pesticide Factsheets</a></p> <p></p> <p></p> <p>List of application documents for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit: Massachusetts Plan Approval including nonattainment NSR Appendix A requirements).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title29-vol7/pdf/CFR-2011-title29-vol7-sec1915-172.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title29-vol7/pdf/CFR-2011-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... 29 Labor 7 2011-07-01 2011-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 1915.172 Section 1915.172 Labor Regulations Relating to Labor (Continued) OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR (CONTINUED) OCCUPATIONAL SAFETY AND HEALTH STANDARDS FOR SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28361867','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28361867"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-03-31</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ∼3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NatCo...814950S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NatCo...814950S"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-03-01</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ~3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381006','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381006"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-01-01</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ∼3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics. PMID:28361867</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011RScI...82i4704Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011RScI...82i4704Z"><span>Static voltage distribution between turns of secondary <span class="hlt">winding</span> of <span class="hlt">air</span>-core spiral strip transformer and its application</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Hong-bo; Liu, Jin-liang; Cheng, Xin-bing; Zhang, Yu</p> <p>2011-09-01</p> <p>The static voltage distribution between <span class="hlt">winding</span> turns has great impact on output characteristics and lifetime of the <span class="hlt">air</span>-core spiral strip pulse transformer (ACSSPT). In this paper, <span class="hlt">winding</span> inductance was calculated by electromagnetic theory, so that the static voltage distribution between turns of secondary <span class="hlt">winding</span> of ACSSPT was analyzed conveniently. According to theoretical analysis, a voltage gradient because of the turn-to-turn capacitance was clearly noticeable across the ground turns. Simulation results of Pspice and CST EM Studio codes showed that the voltage distribution between turns of secondary <span class="hlt">winding</span> had linear increments from the output turn to the ground turn. In experiment, the difference in increased voltage between the ground turns and the output turns of a 20-turns secondary <span class="hlt">winding</span> is almost 50%, which is believed to be responsible for premature breakdown of the insulation, particularly between the ground turns. The experimental results demonstrated the theoretical analysis and simulation results, which had important value for stable and long lifetime ACSSPT design. A new ACSSPT with improved structure has been used successfully in intense electron beam accelerators steadily.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ERL....11d4024A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ERL....11d4024A"><span>Ground-level climate at a peatland <span class="hlt">wind</span> farm in Scotland is affected by <span class="hlt">wind</span> turbine operation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Armstrong, Alona; Burton, Ralph R.; Lee, Susan E.; Mobbs, Stephen; Ostle, Nicholas; Smith, Victoria; Waldron, Susan; Whitaker, Jeanette</p> <p>2016-04-01</p> <p>The global drive to produce low-carbon energy has resulted in an unprecedented deployment of onshore <span class="hlt">wind</span> turbines, representing a significant land use change for <span class="hlt">wind</span> energy generation with uncertain consequences for local climatic conditions and the regulation of ecosystem processes. Here, we present high-resolution data from a <span class="hlt">wind</span> farm collected during operational and idle periods that shows the <span class="hlt">wind</span> farm affected several measures of ground-level climate. Specifically, we discovered that operational <span class="hlt">wind</span> turbines raised <span class="hlt">air</span> temperature by 0.18 °C and absolute humidity (AH) by 0.03 g m-3 during the night, and increased the variability in <span class="hlt">air</span>, surface and soil temperature throughout the diurnal cycle. Further, the microclimatic influence of turbines on <span class="hlt">air</span> temperature and AH decreased logarithmically with distance from the nearest turbine. These effects on ground-level microclimate, including soil temperature, have uncertain implications for biogeochemical processes and ecosystem carbon cycling, including soil carbon stocks. Consequently, understanding needs to be improved to determine the overall carbon balance of <span class="hlt">wind</span> energy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5089803','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5089803"><span>A preliminary investigation of the <span class="hlt">air</span>-bone gap: Changes in intracochlear sound <span class="hlt">pressure</span> with <span class="hlt">air</span>- and bone-conducted stimuli after cochlear implantation</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Banakis Hartl, Renee M.; Mattingly, Jameson K.; Greene, Nathaniel T.; Jenkins, Herman A.; Cass, Stephen P.; Tollin, Daniel J.</p> <p>2016-01-01</p> <p>Hypothesis A cochlear implant electrode within the cochlea contributes to the <span class="hlt">air</span>-bone gap (ABG) component of postoperative changes in residual hearing after electrode insertion. Background Preservation of residual hearing after cochlear implantation has gained importance as simultaneous electric-acoustic stimulation allows for improved speech outcomes. Postoperative loss of residual hearing has previously been attributed to sensorineural changes; however, presence of increased postoperative <span class="hlt">air</span>-bone gap remains unexplained and could result in part from altered cochlear mechanics. Here, we sought to investigate changes to these mechanics via intracochlear <span class="hlt">pressure</span> measurements before and after electrode implantation to quantify the contribution to postoperative <span class="hlt">air</span>-bone gap. Methods Human cadaveric heads were implanted with titanium fixtures for bone conduction transducers. Velocities of stapes capitulum and cochlear promontory between the two windows were measured using single-axis laser Doppler vibrometry and fiber-optic sensors measured intracochlear <span class="hlt">pressures</span> in scala vestibuli and tympani for <span class="hlt">air</span>- and bone-conducted stimuli before and after cochlear implant electrode insertion through the round window. Results Intracochlear <span class="hlt">pressures</span> revealed only slightly reduced responses to <span class="hlt">air</span>-conducted stimuli consistent with prior literature. No significant changes were noted to bone-conducted stimuli after implantation. Velocities of the stapes capitulum and the cochlear promontory to both stimuli were stable following electrode placement. Conclusion Presence of a cochlear implant electrode causes alterations in intracochlear sound <span class="hlt">pressure</span> levels to <span class="hlt">air</span>, but not bone, conducted stimuli and helps to explain changes in residual hearing noted clinically. These results suggest the possibility of a cochlear conductive component to postoperative changes in hearing sensitivity. PMID:27579835</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19770003810','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19770003810"><span><span class="hlt">Wind</span> measurement system</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cliff, W. C.; Huffaker, R. M.; Dahm, W. K.; Thomson, J. A. L.; Lawrence, T. R.; Krause, M. C.; Wilson, D. J. (Inventor)</p> <p>1976-01-01</p> <p>A system for remotely measuring vertical and horizontal <span class="hlt">winds</span> present in discrete volumes of <span class="hlt">air</span> at selected locations above the ground is described. A laser beam is optically focused in range by a telescope, and the output beam is conically scanned at an angle about a vertical axis. The backscatter, or reflected light, from the ambient particulates in a volume of <span class="hlt">air</span>, the focal volume, is detected for shifts in wavelength, and from these, horizontal and vertical <span class="hlt">wind</span> components are computed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-157.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2012-10-01 2012-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-157.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2013-10-01 2013-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</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('https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-157.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2014-10-01 2014-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110011477','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110011477"><span>Weather Research and Forecasting Model <span class="hlt">Wind</span> Sensitivity Study at Edwards <span class="hlt">Air</span> Force Base, CA</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Watson, Leela R.; Bauman, William H., III; Hoeth, Brian</p> <p>2009-01-01</p> <p>This abstract describes work that will be done by the Applied Meteorology Unit (AMU) in assessing the success of different model configurations in predicting "<span class="hlt">wind</span> cycling" cases at Edwards <span class="hlt">Air</span> Force Base, CA (EAFB), in which the <span class="hlt">wind</span> speeds and directions oscillate among towers near the EAFB runway. The Weather Research and Forecasting (WRF) model allows users to choose among two dynamical cores - the Advanced Research WRF (ARW) and the Non-hydrostatic Mesoscale Model (NMM). There are also data assimilation analysis packages available for the initialization of the WRF model - the Local Analysis and Prediction System (LAPS) and the Advanced Regional Prediction System (ARPS) Data Analysis System (ADAS). Having a series of initialization options and WRF cores, as well as many options within each core, creates challenges for local forecasters, such as determining which configuration options are best to address specific forecast concerns. The goal of this project is to assess the different configurations available and determine which configuration will best predict surface <span class="hlt">wind</span> speed and direction at EAFB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083715','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083715"><span>Experimental <span class="hlt">Air</span> <span class="hlt">Pressure</span> Tank Systems for Process Control Education</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Long, Christopher E.; Holland, Charles E.; Gatzke, Edward P.</p> <p>2006-01-01</p> <p>In process control education, particularly in the field of chemical engineering, there is an inherent need for industrially relevant hands-on apparatuses that enable one to bridge the gap between the theoretical content of coursework and real-world applications. At the University of South Carolina, two experimental <span class="hlt">air-pressure</span> tank systems have…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AtmEn.175...92L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AtmEn.175...92L"><span>Field evaluation of vegetation and noise barriers for mitigation of near-freeway <span class="hlt">air</span> pollution under variable <span class="hlt">wind</span> conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lee, Eon S.; Ranasinghe, Dilhara R.; Ahangar, Faraz Enayati; Amini, Seyedmorteza; Mara, Steven; Choi, Wonsik; Paulson, Suzanne; Zhu, Yifang</p> <p>2018-02-01</p> <p>Traffic-related <span class="hlt">air</span> pollutants are a significant public health concern, particularly near freeways. Previous studies have suggested either soundwall or vegetation barriers might reduce the near-freeway <span class="hlt">air</span> pollution. This study aims to investigate the effectiveness of a combination of both soundwall and vegetation barrier for reducing ultrafine particles (UFPs, diameter ≤ 100 nm) and PM2.5 (diameter ≤ 2.5 μm) concentrations. Concurrent data collection was carried out at both upwind and downwind fixed locations approximately 10-15 m away from the edge of two major freeways in California. This study observed that the reduction of UFP and PM2.5 was generally greater with the combination barrier than with either soundwall or vegetation alone. Since there were no non-barrier sites at the study locations, the reductions reported here are all in relative terms. The soundwall barrier was more effective for reducing PM2.5 (25-53%) than UFPs (0-5%), and was most effective (51-53% for PM2.5) when the <span class="hlt">wind</span> speed ranged between 1 and 2 m/s. Under the same range of <span class="hlt">wind</span> speed, the vegetation barrier had little effect (0-5%) on reducing PM2.5; but was effective at reducing UFP (up to 50%). For both types of roadside barrier, decreasing <span class="hlt">wind</span> speed resulted in greater net reduction of UFPs (i.e., total number particle concentrations; inversely proportional). This trend was observed, however, only within specific particle size ranges (i.e., diameter < 20 nm for the soundwall barrier and 12-60 nm for the vegetation barrier). Out of these size ranges, the reduction of UFP concentration was proportional to increasing <span class="hlt">wind</span> speed. Overall findings of this study support positive effects of soundwall and vegetation barriers for near-freeway <span class="hlt">air</span> pollution mitigation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150002872','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150002872"><span>Assimilation of <span class="hlt">Wind</span> Profiles from Multiple Doppler Radar <span class="hlt">Wind</span> Profilers for Space Launch Vehicle Applications</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Decker, Ryan K.; Walker, John R.; Barbre, Robert E., Jr.; Leach, Richard D.</p> <p>2015-01-01</p> <p>Atmospheric <span class="hlt">wind</span> data are required by space launch vehicles in order to assess flight vehicle loads and performance on day-of-launch. Space launch ranges at NASA's Kennedy Space Center co-located with the United States <span class="hlt">Air</span> Force's (USAF) Eastern Range (ER) at Cape Canaveral <span class="hlt">Air</span> Force Station and USAF's Western Range (WR) at Vandenberg <span class="hlt">Air</span> Force Base have extensive networks of in-situ and remote sensing instrumentation to measure atmospheric <span class="hlt">winds</span>. Each instrument's technique to measure <span class="hlt">winds</span> has advantages and disadvantages in regards to use within vehicle trajectory analyses. Balloons measure <span class="hlt">wind</span> at all altitudes necessary for vehicle assessments, but two primary disadvantages exist when applying balloon output. First, balloons require approximately one hour to reach required altitudes. Second, balloons are steered by atmospheric <span class="hlt">winds</span> down range of the launch site that could significantly differ from those <span class="hlt">winds</span> along the vehicle ascent trajectory. These issues are mitigated by use of vertically pointing Doppler Radar <span class="hlt">Wind</span> Profilers (DRWPs). However, multiple DRWP instruments are required to provide <span class="hlt">wind</span> data over altitude ranges necessary for vehicle trajectory assessments. The various DRWP systems have different operating configurations resulting in different temporal and spatial sampling intervals. Therefore, software was developed to combine data from both DRWP-generated profiles into a single profile for use in vehicle trajectory analyses. This paper will present details of the splicing software algorithms and will provide sample output.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ExFl...57...82D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ExFl...57...82D"><span>Global surface <span class="hlt">pressure</span> measurements of static and dynamic stall on a <span class="hlt">wind</span> turbine airfoil at low Reynolds number</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Disotell, Kevin J.; Nikoueeyan, Pourya; Naughton, Jonathan W.; Gregory, James W.</p> <p>2016-05-01</p> <p>Recognizing the need for global surface measurement techniques to characterize the time-varying, three-dimensional loading encountered on rotating <span class="hlt">wind</span> turbine blades, fast-responding <span class="hlt">pressure</span>-sensitive paint (PSP) has been evaluated for resolving unsteady aerodynamic effects in incompressible flow. Results of a study aimed at demonstrating the laser-based, single-shot PSP technique on a low Reynolds number <span class="hlt">wind</span> turbine airfoil in static and dynamic stall are reported. PSP was applied to the suction side of a Delft DU97-W-300 airfoil (maximum thickness-to-chord ratio of 30 %) at a chord Reynolds number of 225,000 in the University of Wyoming open-return <span class="hlt">wind</span> tunnel. Static and dynamic stall behaviors are presented using instantaneous and phase-averaged global <span class="hlt">pressure</span> maps. In particular, a three-dimensional <span class="hlt">pressure</span> topology driven by a stall cell pattern is detected near the maximum lift condition on the steady airfoil. Trends in the PSP-measured <span class="hlt">pressure</span> topology on the steady airfoil were confirmed using surface oil visualization. The dynamic stall case was characterized by a sinusoidal pitching motion with mean angle of 15.7°, amplitude of 11.2°, and reduced frequency of 0.106 based on semichord. PSP images were acquired at selected phase positions, capturing the breakdown of nominally two-dimensional flow near lift stall, development of post-stall suction near the trailing edge, and a highly three-dimensional topology as the flow reattaches. Structural patterns in the surface <span class="hlt">pressure</span> topologies are considered from the analysis of the individual PSP snapshots, enabled by a laser-based excitation system that achieves sufficient signal-to-noise ratio in the single-shot images. The PSP results are found to be in general agreement with observations about the steady and unsteady stall characteristics expected for the airfoil.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1987srti.rept.....W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1987srti.rept.....W"><span>Soviet research on the transport of intense relativistic electron beams through high-<span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wells, Nikita</p> <p>1987-05-01</p> <p>Soviet development of intense relativistic electron beams (IREB) through background <span class="hlt">air</span> at <span class="hlt">pressures</span> from 1/100 Torr to atmospheric is analyzed as reflected by Soviet open literature of the last 15 years. Important Soviet findings include: (1) the formation of a plasma channel created by an IREB propagating through background <span class="hlt">air</span> and the effect of beam parameters upon the plasma channel parameters (and vice versa); (2) determination of the background <span class="hlt">air</span> <span class="hlt">pressure</span> for the optimum transport of IREB in two ranges, an ion focused regime at 0.06 to 0.09 Torr and a low <span class="hlt">pressure</span> window at 1 Torr; (3) observation of current enhancement, whereby the IREB-induced current in plasma is higher than the initial beam current; and (4) the effect of resistive hose instability on IREB propagation. This research is characterized by absence of high energy experimentation. A conclusion of the research is that, for optimum beam transport through <span class="hlt">air</span>, it is imperative to ensure conditions that allow full neutralization of the IREB's self-fields along the entire path of the beam's transport.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=respiratory+AND+system&pg=6&id=EJ696527','ERIC'); return false;" href="https://eric.ed.gov/?q=respiratory+AND+system&pg=6&id=EJ696527"><span><span class="hlt">Air</span> <span class="hlt">Pressure</span> Responses to Sudden Vocal Tract <span class="hlt">Pressure</span> Bleeds during Production of Stop Consonants: New Evidence of Aeromechanical Regulation.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Zajac, David J.; Weissler, Mark C.</p> <p>2004-01-01</p> <p>Two studies were conducted to evaluate short-latency vocal tract <span class="hlt">air</span> <span class="hlt">pressure</span> responses to sudden <span class="hlt">pressure</span> bleeds during production of voiceless bilabial stop consonants. It was hypothesized that the occurrence of respiratory reflexes would be indicated by distinct patterns of responses as a function of bleed magnitude. In Study 1, 19 adults…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ApJ...776...94Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ApJ...776...94Y"><span>Small-scale <span class="hlt">Pressure</span>-balanced Structures Driven by Mirror-mode Waves in the Solar <span class="hlt">Wind</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yao, Shuo; He, J.-S.; Tu, C.-Y.; Wang, L.-H.; Marsch, E.</p> <p>2013-10-01</p> <p>Recently, small-scale <span class="hlt">pressure</span>-balanced structures (PBSs) have been studied with regard to their dependence on the direction of the local mean magnetic field B0 . The present work continues these studies by investigating the compressive wave mode forming small PBSs, here for B0 quasi-perpendicular to the x-axis of Geocentric Solar Ecliptic coordinates (GSE-x). All the data used were measured by <span class="hlt">WIND</span> in the quiet solar <span class="hlt">wind</span>. From the distribution of PBSs on the plane determined by the temporal scale and angle θxB between the GSE-x and B0 , we notice that at θxB = 115° the PBSs appear at temporal scales ranging from 700 s to 60 s. In the corresponding temporal segment, the correlations between the plasma thermal <span class="hlt">pressure</span> P th and the magnetic <span class="hlt">pressure</span> P B, as well as that between the proton density N p and the magnetic field strength B, are investigated. In addition, we use the proton velocity distribution functions to calculate the proton temperatures T and T ∥. Minimum Variance Analysis is applied to find the magnetic field minimum variance vector BN . We also study the time variation of the cross-helicity σc and the compressibility C p and compare these with values from numerical predictions for the mirror mode. In this way, we finally identify a short segment that has T > T ∥, proton β ~= 1, both pairs of P th-P B and N p-B showing anti-correlation, and σc ≈ 0 with C p > 0. Although the examination of σc and C p is not conclusive, it provides helpful additional information for the wave mode identification. Additionally, BN is found to be highly oblique to B0 . Thus, this work suggests that a candidate mechanism for forming small-scale PBSs in the quiet solar <span class="hlt">wind</span> is due to mirror-mode waves.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMGC43J..08M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMGC43J..08M"><span>Increased Surface <span class="hlt">Wind</span> Speeds Follow Diminishing Arctic Sea Ice</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mioduszewski, J.; Vavrus, S. J.; Wang, M.; Holland, M. M.; Landrum, L.</p> <p>2017-12-01</p> <p>Projections of Arctic sea ice through the end of the 21st century indicate the likelihood of a strong reduction in ice area and thickness in all seasons, leading to a substantial thermodynamic influence on the overlying atmosphere. This is likely to have an effect on <span class="hlt">winds</span> over the Arctic Basin, due to changes in atmospheric stability and/or baroclinicity. Prior research on future Arctic <span class="hlt">wind</span> changes is limited and has focused mainly on the practical impacts on wave heights in certain seasons. Here we attempt to identify patterns and likely mechanisms responsible for surface <span class="hlt">wind</span> changes in all seasons across the Arctic, particularly those associated with sea ice loss in the marginal ice zone. Sea level <span class="hlt">pressure</span>, near-surface (10 m) and upper-<span class="hlt">air</span> (850 hPa) <span class="hlt">wind</span> speeds, and lower-level dynamic and thermodynamic variables from the Community Earth System Model Large Ensemble Project (CESM-LE) were analyzed for the periods 1971-2000 and 2071-2100 to facilitate comparison between a present-day and future climate. Mean near-surface <span class="hlt">wind</span> speeds over the Arctic Ocean are projected to increase by late century in all seasons but especially during autumn and winter, when they strengthen by up to 50% locally. The most extreme <span class="hlt">wind</span> speeds in the 90th percentile change even more, increasing in frequency by over 100%. The strengthened <span class="hlt">winds</span> are closely linked to decreasing lower-tropospheric stability resulting from the loss of sea ice cover and consequent surface warming (locally over 20 ºC warmer in autumn and winter). A muted pattern of these future changes is simulated in CESM-LE historical runs from 1920-2005. The enhanced <span class="hlt">winds</span> near the surface are mostly collocated with weaker <span class="hlt">winds</span> above the boundary layer during autumn and winter, implying more vigorous vertical mixing and a drawdown of high-momentum <span class="hlt">air</span>.The implications of stronger future <span class="hlt">winds</span> include increased coastal hazards and the potential for a positive feedback with sea ice by generating higher <span class="hlt">winds</span> and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1052222','SCIGOV-DOEDE'); return false;" href="https://www.osti.gov/servlets/purl/1052222"><span>NREL National <span class="hlt">Wind</span> Technology Center (NWTC): M2 Tower; Boulder, Colorado (Data)</span></a></p> <p><a target="_blank" href="http://www.osti.gov/dataexplorer">DOE Data Explorer</a></p> <p>Jager, D.; Andreas, A.</p> <p>1996-09-24</p> <p>The National <span class="hlt">Wind</span> Technology Center (NWTC), located at the foot of the Rocky Mountains near Boulder, Colorado, is a world-class research facility managed by NREL for the U.S. Department of Energy. NWTC researchers work with members of the <span class="hlt">wind</span> energy industry to advance <span class="hlt">wind</span> power technologies that lower the cost of <span class="hlt">wind</span> energy through research and development of state-of-the-art <span class="hlt">wind</span> turbine designs. NREL's Measurement and Instrument Data Center provides data from NWTC's M2 tower which are derived from instruments mounted on or near an 82 meter (270 foot) meteorological tower located at the western edge of the NWTC site and about 11 km (7 miles) west of Broomfield, and approximately 8 km (5 miles) south of Boulder, Colorado. The data represent the mean value of readings taken every two seconds and averaged over one minute. The <span class="hlt">wind</span> speed and direction are measured at six heights on the tower and <span class="hlt">air</span> temperature is measured at three heights. The dew point temperature, relative humidity, barometric <span class="hlt">pressure</span>, totalized liquid precipitation, and global solar radiation are also available.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMSH41F..07Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMSH41F..07Z"><span>Strong Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Pulses during Solar Cycle 23 and Their Impacts on Geosynchronous Magnetic Fields</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zuo, P.</p> <p>2015-12-01</p> <p>Solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> pulse (DPP) structures, across which the dynamic <span class="hlt">pressure</span> abruptly changes over timescales from a few seconds to several minutes, are often observed in the near-Earth space environment. In this investigation, we first present a statistical study on the properties of strong dynamic <span class="hlt">pressure</span> pulses in the solar <span class="hlt">wind</span> during solar cycle 23. It is found that overwhelming majority of DPPs are associated with the solar <span class="hlt">wind</span> disturbances including the CME-related flows, the corotating interaction regions, as well as the complex ejecta. The annual variations of the averaged occurrence rate of DPPs are roughly in phase with the solar activities. Although the variabilities of geosynchronous magnetic fields (GMFs) due to the impact of positive DPPs have been well established, there appears no systematic investigations on the response of GMFs to negative DPPs. Here we also study the decompression/compression effects of very strong negative/positive DPPs on GMFs under northward IMFs. In response to the decompression of strong negative DPPs, GMFs on dayside, near the dawn and dusk on nightside are generally depressed. But near the midnight region, the responses of GMF are very diverse, being either positive or negative. For part of events when GOES is located at the midnight sector, GMF is found to abnormally increase as the result of magnetospheric decompression caused by negative DPPs. It is known that on certain conditions magnetic depression of nightside GMFs can be caused by the impact of positive DPPs. Here we found that, a stronger <span class="hlt">pressure</span> enhancement may have a higher probability of producing the exceptional depression of GMF at midnight region. Statistically, both the decompression effect of strong negative DPPs and the compression effect of strong positive DPPs depend on the magnetic local time, being stronger at the noon sector.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16615688','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16615688"><span>Testing of heat exchangers in membrane oxygenators using <span class="hlt">air</span> <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hamilton, Carole; Stein, Jutta; Seidler, Rainer; Kind, Robert; Beck, Karin; Tosok, Jürgen; Upterfofel, Jörg</p> <p>2006-03-01</p> <p>All heat exchangers (HE) in membrane oxygenators are tested by the manufacturer for water leaks during the production phase. However, for safety reasons, it is highly recommended that HEs be tested again before clinical use. The most common method is to attach the heater-cooler to the HE and allow the water to recirculate for at least 10 min, during which time a water leak should be evident. To improve the detection of water leaks, a test was devised using a <span class="hlt">pressure</span> manometer with an integrated bulb used to <span class="hlt">pressurize</span> the HE with <span class="hlt">air</span>. The cardiopulmonary bypass system is set up as per protocol. A <span class="hlt">pressure</span> manometer adapted to a 1/2" tubing is connected to the water inlet side of the oxygenator. The water outlet side is blocked with a short piece of 1/2" deadend tubing. The HE is <span class="hlt">pressurized</span> with 250 mmHg for at least 30 sec and observed for any drop. Over the last 2 years, only one oxygenator has been detected with a water leak in which the <span class="hlt">air</span>-method leaktest was performed. This unit was sent back to the manufacturer who confirmed the failure. Even though the incidence of water leaks is very low, it does occur and it is, therefore, important that all HEs are tested before they are used clinically. This method of using a <span class="hlt">pressure</span> manometer offers many advantages, as the HE can be tested outside of the operating room (OR), allowing earlier testing of the oxygenator, no water contact is necessary, and it is simple, easy and quick to perform.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920068530&hterms=missing+data&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Dmissing%2Bdata','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920068530&hterms=missing+data&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Dmissing%2Bdata"><span>Missing <span class="hlt">pressure</span> in the dayside ionosphere of Venus</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cloutier, P. A.; Stewart, B. K.; Taylor, H. A., Jr.</p> <p>1992-01-01</p> <p>Data obtained by various instruments on the Pioneer-Venus spacecraft were used to study the conservation of momentum flux from the solar <span class="hlt">wind</span> through the dayside ionopause into the thermal Venus ionosphere. A consistent <span class="hlt">pressure</span> deficit was found below the ionopause, with a strong dependence on solar <span class="hlt">wind</span> <span class="hlt">pressure</span>. Independent of solar <span class="hlt">wind</span> <span class="hlt">pressure</span>, the <span class="hlt">pressure</span> deficit was found to decrease with decreasing altitude below the ionopause. Measurements of this <span class="hlt">pressure</span> deficit (missing <span class="hlt">pressure</span>) are presented as a function of altitude for various solar <span class="hlt">wind</span> conditions. The identity of the missing <span class="hlt">pressure</span> component and the correlation with solar <span class="hlt">wind</span> <span class="hlt">pressure</span> are discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170000893','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170000893"><span>Using C-Band Dual-Polarization Radar Signatures to Improve Convective <span class="hlt">Wind</span> Forecasting at Cape Canaveral <span class="hlt">Air</span> Force Station and NASA Kennedy Space Center</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Amiot, Corey G.; Carey, Lawrence D.; Roeder, William P.; McNamara, Todd M.; Blakeslee, Richard J.</p> <p>2017-01-01</p> <p>The United States <span class="hlt">Air</span> Force's 45th Weather Squadron (45WS) is the organization responsible for monitoring atmospheric conditions at Cape Canaveral <span class="hlt">Air</span> Force Station and NASA Kennedy Space Center (CCAFS/KSC) and issuing warnings for hazardous weather conditions when the need arises. One such warning is issued for convective <span class="hlt">wind</span> events, for which lead times of 30 and 60 minutes are desired for events with peak <span class="hlt">wind</span> gusts of 35 knots or greater (i.e., Threshold-1) and 50 knots or greater (i.e., Threshold-2), respectively (Roeder et al. 2014).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDF17008D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDF17008D"><span>Vertical-axis <span class="hlt">wind</span> turbine experiments at full dynamic similarity</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Duvvuri, Subrahmanyam; Miller, Mark; Brownstein, Ian; Dabiri, John; Hultmark, Marcus</p> <p>2017-11-01</p> <p>This study presents results from <span class="hlt">pressurized</span> (upto 200 atm) <span class="hlt">wind</span> tunnel tests of a self-spinning 5-blade model Vertical-Axis <span class="hlt">Wind</span> Turbine (VAWT). The model is geometrically similar (scale ratio 1:22) to a commercially available VAWT, which has a rotor diameter of 2.17 meters and blade span of 3.66 meters, and is used at the Stanford university field lab. The use of <span class="hlt">pressurized</span> <span class="hlt">air</span> as working fluid allows for the unique ability to obtain full dynamic similarity with field conditions in terms of matched Reynolds numbers (Re), tip-speed ratios (λ), and Mach number (M). Tests were performed across a wide range of Re and λ, with the highest Re exceeding the maximum operational field Reynolds number (Remax) by a factor of 3. With an extended range of accessible Re conditions, the peak turbine power efficiency was seen to occur roughly at Re = 2 Remax and λ = 1 . Beyond Re > 2 Remax the turbine performance is invariant in Re for all λ. A clear demonstration of Reynolds number invariance for an actual full-scale <span class="hlt">wind</span> turbine lends novelty to this study, and overall the results show the viability of the present experimental technique in testing turbines at field conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050188550','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050188550"><span><span class="hlt">WIND</span> Flow Solver Released</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Towne, Charles E.</p> <p>1999-01-01</p> <p>The <span class="hlt">WIND</span> code is a general-purpose, structured, multizone, compressible flow solver that can be used to analyze steady or unsteady flow for a wide range of geometric configurations and over a wide range of flow conditions. <span class="hlt">WIND</span> is the latest product of the NPARC Alliance, a formal partnership between the NASA Lewis Research Center and the <span class="hlt">Air</span> Force Arnold Engineering Development Center (AEDC). <span class="hlt">WIND</span> Version 1.0 was released in February 1998, and Version 2.0 will be released in February 1999. The <span class="hlt">WIND</span> code represents a merger of the capabilities of three existing computational fluid dynamics codes--NPARC (the original NPARC Alliance flow solver), NXAIR (an <span class="hlt">Air</span> Force code used primarily for unsteady store separation problems), and NASTD (the primary flow solver at McDonnell Douglas, now part of Boeing).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1988asme.conf....2B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1988asme.conf....2B"><span>Heat transfer and <span class="hlt">pressure</span> drop measurements in an <span class="hlt">air</span>/molten salt direct-contact heat exchanger</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bohn, Mark S.</p> <p>1988-11-01</p> <p>This paper presents a comparison of experimental data with a recently published model of heat exchange in irrigated packed beds. Heat transfer and <span class="hlt">pressure</span> drop were measured in a 150 mm (ID) column with a 610 mm bed of metal Pall rings. Molten nitrate salt and preheated <span class="hlt">air</span> were the working fluids with a salt inlet temperature of approximately 440 C and <span class="hlt">air</span> inlet temperatures of approximately 230 C. A comparison between the experimental data and the heat transfer model is made on the basis of heat transfer from the salt. For the range of <span class="hlt">air</span> and salt flow rates tested, 0.3 to 1.2 kg/sq m/s <span class="hlt">air</span> flow and 6 to 18 kg/sq m/s salt flow, the data agree with the model within 22 percent standard deviation. In addition, a model for the column <span class="hlt">pressure</span> drop was validated, agreeing with the experimental data within 18 percent standard deviation over the range of column <span class="hlt">pressure</span> drop from 40 to 1250 Pa/m.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810012682','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810012682"><span>An investigation of <span class="hlt">air</span> solubility in Jet A fuel at high <span class="hlt">pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Faeth, G. M.</p> <p>1981-01-01</p> <p>Problems concerned with the supercritical injection concept are discussed. Supercritical injection involves dissolving <span class="hlt">air</span> into a fuel prior to injection. A similar effect is obtained by preheating the fuel so that a portion of the fuel flashes when its <span class="hlt">pressure</span> is reduced. Flashing improves atomization properties and the presence of <span class="hlt">air</span> in the primary zone of a spray flame reduces the formation of pollutants. The investigation is divided into three phases: (1) measure the solubility and density properties of fuel/gas mixtures, including Jet A/<span class="hlt">air</span>, at <span class="hlt">pressures</span> and correlate these results using theory; (2) investigate the atomization properties of flashing liquids, including fuel/dissolved gas systems. Determine and correlate the effect of inlet properties and injector geometry on mass flow rates, Sauter mean diameter and spray angles; (3) examine the combustion properties of flashing injection in an open burner flame, considering flame shape and soot production.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=physics+AND+glass&pg=2&id=EJ1025234','ERIC'); return false;" href="https://eric.ed.gov/?q=physics+AND+glass&pg=2&id=EJ1025234"><span>The Jar Magic--Instructional Activities for Teaching <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Ku, Bing-Hong; Chen, Chyong-Sun</p> <p>2013-01-01</p> <p>There are a variety of impressive activities designed for teaching the concept of <span class="hlt">air</span> <span class="hlt">pressure</span> to junior high school students. Water, glasses, balloons, plastic bottles, and suction cups are some of the items commonly used in these experiments. For example, if we take a glass of water, cover it with a piece of cardboard, and invert the glass,…</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('https://www.osti.gov/servlets/purl/984517','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/984517"><span><span class="hlt">Wind</span> turbine generators having <span class="hlt">wind</span> assisted cooling systems and cooling methods</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Bagepalli, Bharat [Niskayuna, NY; Barnes, Gary R [Delanson, NY; Gadre, Aniruddha D [Rexford, NY; Jansen, Patrick L [Scotia, NY; Bouchard, Jr., Charles G.; Jarczynski, Emil D [Scotia, NY; Garg, Jivtesh [Cambridge, MA</p> <p>2008-09-23</p> <p>A <span class="hlt">wind</span> generator includes: a nacelle; a hub carried by the nacelle and including at least a pair of <span class="hlt">wind</span> turbine blades; and an electricity producing generator including a stator and a rotor carried by the nacelle. The rotor is connected to the hub and rotatable in response to <span class="hlt">wind</span> acting on the blades to rotate the rotor relative to the stator to generate electricity. A cooling system is carried by the nacelle and includes at least one ambient <span class="hlt">air</span> inlet port opening through a surface of the nacelle downstream of the hub and blades, and a duct for flowing <span class="hlt">air</span> from the inlet port in a generally upstream direction toward the hub and in cooling relation to the stator.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810007124','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810007124"><span>Determination of <span class="hlt">wind</span> from NIMBUS 6 satellite sounding data</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Carle, W. E.; Scoggins, J. R.</p> <p>1981-01-01</p> <p>Objective methods of computing upper level and surface <span class="hlt">wind</span> fields from NIMBUS 6 satellite sounding data are developed. These methods are evaluated by comparing satellite derived and rawinsonde <span class="hlt">wind</span> fields on gridded constant <span class="hlt">pressure</span> charts in four geographical regions. Satellite-derived and hourly observed surface <span class="hlt">wind</span> fields are compared. Results indicate that the best satellite-derived <span class="hlt">wind</span> on constant <span class="hlt">pressure</span> charts is a geostrophic <span class="hlt">wind</span> derived from highly smoothed fields of geopotential height. Satellite-derived <span class="hlt">winds</span> computed in this manner and rawinsonde <span class="hlt">winds</span> show similar circulation patterns except in areas of small height gradients. Magnitudes of the standard deviation of the differences between satellite derived and rawinsonde <span class="hlt">wind</span> speeds range from approximately 3 to 12 m/sec on constant <span class="hlt">pressure</span> charts and peak at the jet stream level. Fields of satellite-derived surface <span class="hlt">wind</span> computed with the logarithmic <span class="hlt">wind</span> law agree well with fields of observed surface <span class="hlt">wind</span> in most regions. Magnitudes of the standard deviation of the differences in surface <span class="hlt">wind</span> speed range from approximately 2 to 4 m/sec, and satellite derived surface <span class="hlt">winds</span> are able to depict flow across a cold front and around a low <span class="hlt">pressure</span> center.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940019889','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940019889"><span>Improved <span class="hlt">pressure</span> measurement system for calibration of the NASA LeRC 10x10 supersonic <span class="hlt">wind</span> tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Blumenthal, Philip Z.; Helland, Stephen M.</p> <p>1994-01-01</p> <p>This paper discusses a method used to provide a significant improvement in the accuracy of the Electronically Scanned <span class="hlt">Pressure</span> (ESP) Measurement System by means of a fully automatic floating <span class="hlt">pressure</span> generating system for the ESP calibration and reference <span class="hlt">pressures</span>. This system was used to obtain test section Mach number and flow angularity measurements over the full envelope of test conditions for the 10 x 10 Supersonic <span class="hlt">Wind</span> Tunnel. The uncertainty analysis and actual test data demonstrated that, for most test conditions, this method could reduce errors to about one-third to one-half that obtained with the standard system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PlST...18..732W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PlST...18..732W"><span>Thermodynamic and Transport Properties of Real <span class="hlt">Air</span> Plasma in Wide Range of Temperature and <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Chunlin; Wu, Yi; Chen, Zhexin; Yang, Fei; Feng, Ying; Rong, Mingzhe; Zhang, Hantian</p> <p>2016-07-01</p> <p><span class="hlt">Air</span> plasma has been widely applied in industrial manufacture. In this paper, both dry and humid <span class="hlt">air</span> plasmas' thermodynamic and transport properties are calculated in temperature 300-100000 K and <span class="hlt">pressure</span> 0.1-100 atm. To build a more precise model of real <span class="hlt">air</span> plasma, over 70 species are considered for composition. Two different methods, the Gibbs free energy minimization method and the mass action law method, are used to determinate the composition of the <span class="hlt">air</span> plasma in a different temperature range. For the transport coefficients, the simplified Chapman-Enskog method developed by Devoto has been applied using the most recent collision integrals. It is found that the presence of CO2 has almost no effect on the properties of <span class="hlt">air</span> plasma. The influence of H2O can be ignored except in low <span class="hlt">pressure</span> <span class="hlt">air</span> plasma, in which the saturated vapor <span class="hlt">pressure</span> is relatively high. The results will serve as credible inputs for computational simulation of <span class="hlt">air</span> plasma. supported by the National Key Basic Research Program of China (973 Program)(No. 2015CB251002), National Natural Science Foundation of China (Nos. 51521065, 51577145), the Science and Technology Project Funds of the Grid State Corporation (SGTYHT/13-JS-177), the Fundamental Research Funds for the Central Universities, and State Grid Corporation Project (GY71-14-004)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.ars.usda.gov/research/publications/publication/?seqNo115=342843','TEKTRAN'); return false;" href="http://www.ars.usda.gov/research/publications/publication/?seqNo115=342843"><span><span class="hlt">Wind</span> erosion processes and control</span></a></p> <p><a target="_blank" href="https://www.ars.usda.gov/research/publications/find-a-publication/">USDA-ARS?s Scientific Manuscript database</a></p> <p></p> <p></p> <p><span class="hlt">Wind</span> erosion continues to threaten the sustainability of our nations' soil, <span class="hlt">air</span>, and water resources. To effectively apply conservation systems to prevent <span class="hlt">wind</span> driven soil loss, an understanding of the fundamental processes of <span class="hlt">wind</span> erosion is necessary so that land managers can better recognize the ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA578419','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA578419"><span>Predicting the Turbulent <span class="hlt">Air</span>-Sea Surface Fluxes, Including Spray Effects, from Weak to Strong <span class="hlt">Winds</span></span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2012-09-30</p> <p>almost complete decoupling of the <span class="hlt">wind</span> field from the sea surface . As a result of the weak surface stress, the flow becomes almost free from the...shore flow . In turn, wave growth and the associated surface roughness (z0) are limited. Consequently, the stability increases further in a...1 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Predicting the Turbulent <span class="hlt">Air</span>-Sea Surface Fluxes</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091358','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091358"><span>Forces on Elliptic Cylinders in Uniform <span class="hlt">Air</span> Stream</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zahm, A F; Smith, R H; Louden, F A</p> <p>1929-01-01</p> <p>This report presents the results of <span class="hlt">wind</span> tunnel tests on four elliptic cylinders with various fineness ratios, conducted in the Navy Aerodynamic Laboratory, Washington. The object of the tests was to investigate the characteristics of sections suitable for streamline wire which normally has an elliptic section with a fineness ratio of 4.0; also to learn whether a reduction in fineness ratio would result in improvement; also to determine the <span class="hlt">pressure</span> distribution on the model of fineness ratio of 4. Four elliptic cylinders with fineness ratios of 2.5, 3.0, 3.5, and 4.0 were made and then tested in the 8 by 8 <span class="hlt">wind</span> tunnel; first, for cross-<span class="hlt">wind</span> force, drag, and yawing moment at 30 miles an hour and various angles of yaw; next for drag 0 degree pitch and 0 degree yaw and various <span class="hlt">wind</span> speeds; then for end effect on the smallest and largest models; and lastly for <span class="hlt">pressure</span> distribution over the surface of the largest model at 0 degree pitch and 0 degree yaw and various <span class="hlt">wind</span> speeds. In all tests, the length of the model was transverse to the current. The results are given for standard <span class="hlt">air</span> density, p = .002378 slug per cubic foot. This account is a slight revised form of report no. 315. A summary of conclusions is given at the end of the text. (author)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17687455','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17687455"><span>Elevated plasma endothelin-1 and pulmonary arterial <span class="hlt">pressure</span> in children exposed to <span class="hlt">air</span> pollution.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Calderón-Garcidueñas, Lilian; Vincent, Renaud; Mora-Tiscareño, Antonieta; Franco-Lira, Maricela; Henríquez-Roldán, Carlos; Barragán-Mejía, Gerardo; Garrido-García, Luis; Camacho-Reyes, Laura; Valencia-Salazar, Gildardo; Paredes, Rogelio; Romero, Lina; Osnaya, Hector; Villarreal-Calderón, Rafael; Torres-Jardón, Ricardo; Hazucha, Milan J; Reed, William</p> <p>2007-08-01</p> <p>Controlled exposures of animals and humans to particulate matter (PM) or ozone <span class="hlt">air</span> pollution cause an increase in plasma levels of endothelin-1, a potent vasoconstrictor that regulates pulmonary arterial <span class="hlt">pressure</span>. The primary objective of this field study was to determine whether Mexico City children, who are chronically exposed to levels of PM and O(3) that exceed the United States <span class="hlt">air</span> quality standards, have elevated plasma endothelin-1 levels and pulmonary arterial <span class="hlt">pressures</span>. We conducted a study of 81 children, 7.9 +/- 1.3 years of age, lifelong residents of either northeast (n = 19) or southwest (n = 40) Mexico City or Polotitlán (n = 22), a control city with PM and O(3) levels below the U.S. <span class="hlt">air</span> quality standards. Clinical histories, physical examinations, and complete blood counts were done. Plasma endothelin-1 concentrations were determined by immunoassay, and pulmonary arterial <span class="hlt">pressures</span> were measured by Doppler echocardiography. Mexico City children had higher plasma endothelin-1 concentrations compared with controls (p < 0.001). Mean pulmonary arterial <span class="hlt">pressure</span> was elevated in children from both northeast (p < 0.001) and southwest (p < 0.05) Mexico City compared with controls. Endothelin-1 levels in Mexico City children were positively correlated with daily outdoor hours (p = 0.012), and 7-day cumulative levels of PM <span class="hlt">air</span> pollution < 2.5 mum in aerodynamic diameter (PM(2.5)) before endothelin-1 measurement (p = 0.03). Chronic exposure of children to PM(2.5) is associated with increased levels of circulating endothelin-1 and elevated mean pulmonary arterial <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/873149','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/873149"><span>Simplified configuration for the combustor of an oil burner using a low <span class="hlt">pressure</span>, high flow <span class="hlt">air</span>-atomizing nozzle</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Butcher, Thomas A.; Celebi, Yusuf; Fisher, Leonard</p> <p>2000-09-15</p> <p>The invention relates to clean burning of fuel oil with <span class="hlt">air</span>. More specifically, to a fuel burning combustion head using a low-<span class="hlt">pressure</span>, high <span class="hlt">air</span> flow atomizing nozzle so that there will be a complete combustion of oil resulting in a minimum emission of pollutants. The improved fuel burner uses a low <span class="hlt">pressure</span> <span class="hlt">air</span> atomizing nozzle that does not result in the use of additional compressors or the introduction of <span class="hlt">pressurized</span> gases downstream, nor does it require a complex design. Inventors:</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009AIPC.1148..112N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009AIPC.1148..112N"><span>Numerical Study of <span class="hlt">Pressure</span> Field in Laterally Closed Industrial Buildings with Curved Metallic Roofs due to the <span class="hlt">Wind</span> Effect by FEM and European Rule Comparison</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nieto, P. J. García; del Coz Díaz, J. J.; Vilán, J. A. Vilán; Placer, C. Casqueiro</p> <p>2009-08-01</p> <p>In this paper, an evaluation of distribution of the <span class="hlt">air</span> <span class="hlt">pressure</span> is determined throughout the laterally closed industrial buildings with curved metallic roofs due to the <span class="hlt">wind</span> effect by the finite element method (FEM). The non-linearity is due to Reynolds-averaged Navier-Stokes (RANS) equations that govern the turbulent flow. The Navier-Stokes equations are non-linear partial differential equations and this non-linearity makes most problems difficult to solve and is part of the cause of turbulence. The RANS equations are time-averaged equations of motion for fluid flow. They are primarily used while dealing with turbulent flows. Turbulence is a highly complex physical phenomenon that is pervasive in flow problems of scientific and engineering concern like this one. In order to solve the RANS equations a two-equation model is used: the standard k-ɛ model. The calculation has been carried out keeping in mind the following assumptions: turbulent flow, an exponential-like <span class="hlt">wind</span> speed profile with a maximum velocity of 40 m/s at 10 m reference height, and different heights of the building ranging from 6 to 10 meters. Finally, the forces and moments are determined on the cover, as well as the distribution of <span class="hlt">pressures</span> on the same one, comparing the numerical results obtained with the Spanish CTE DB SE-AE, Spanish NBE AE-88 and European standard rules, giving place to the conclusions that are exposed in the study.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800003315','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800003315"><span><span class="hlt">Wind</span> Loads on Flat Plate Photovoltaic Array Fields</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, R.; Zimmerman, D.</p> <p>1979-01-01</p> <p>The aerodynamic forces resulting from <span class="hlt">winds</span> acting on flat plate photovoltaic arrays were investigated. Local <span class="hlt">pressure</span> distributions and total aerodynamic forces on the arrays are shown. Design loads are presented to cover the conditions of array angles relative to the ground from 20 deg to 60 deg, variable array spacings, a ground clearance gap up to 1.2 m (4 ft) and array slant heights of 2.4 m (8 ft) and 4.8 m (16 ft). Several means of alleviating the <span class="hlt">wind</span> loads on the arrays are detailed. The expected reduction of the steady state <span class="hlt">wind</span> velocity with the use of fences as a load alleviation device are indicated to be in excess of a factor of three for some conditions. This yields steady state <span class="hlt">wind</span> load reductions as much as a factor of ten compared to the load incurred if no fence is used to protect the arrays. This steady state <span class="hlt">wind</span> load reduction is offset by the increase in turbulence due to the fence but still an overall load reduction of 2.5 can be realized. Other load alleviation devices suggested are the installation of <span class="hlt">air</span> gaps in the arrays, blocking the flow under the arrays and rounding the edges of the array. A <span class="hlt">wind</span> tunnel test plan to supplement the theoretical study and to evaluate the load alleviation devices is outlined.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015Icar..250..368B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015Icar..250..368B"><span><span class="hlt">Winds</span>, waves and shorelines from ancient martian seas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Banfield, Don; Donelan, Mark; Cavaleri, Luigi</p> <p>2015-04-01</p> <p>We consider under what environmental conditions water waves (and thus eventually shorelines) should be expected to be produced on hypothetical ancient martian seas and lakes. For <span class="hlt">winds</span> and atmospheric <span class="hlt">pressures</span> that are too small, no waves should be expected, and thus no shorelines. If the <span class="hlt">winds</span> and atmospheric <span class="hlt">pressure</span> are above some threshold, then waves can be formed, and shorelines are possible. We establish these criteria separating conditions under which waves will or will not form on an ancient martian open body of water. We consider not only atmospheric <span class="hlt">pressure</span> and <span class="hlt">wind</span>, but also temperature and salinity, but find these latter effects to be secondary. The normal criterion for the onset of water waves under terrestrial conditions is extended to recognize the greater atmospheric viscous boundary layer depth for low atmospheric <span class="hlt">pressures</span>. We used terrestrial wave models to predict the wave environment expected for reasonable ranges of atmospheric <span class="hlt">pressure</span> and <span class="hlt">wind</span> for end-member cases of ocean salinity. These models were modified only to reflect the different fluids considered at Mars, the different martian surface gravity, and the varying atmospheric <span class="hlt">pressure</span>, <span class="hlt">wind</span> and fetch. The models were favorably validated against one another, and also against experiments conducted in a wave tank in a <span class="hlt">pressure</span> controlled <span class="hlt">wind</span> tunnel (NASA Ames MARSWIT). We conclude that if wave-cut shorelines can be confirmed on Mars, this can constrain the range of possible atmospheric <span class="hlt">pressures</span> and <span class="hlt">wind</span> speeds that could have existed when the open water was present on Mars.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930080842','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930080842"><span>A New Method of Testing in <span class="hlt">Wind</span> Tunnels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Margoulis, W</p> <p>1921-01-01</p> <p>Now, in existing <span class="hlt">wind</span> tunnels, using a horsepower of 100 to 300, the models are generally made to a 1/10 scale and the speed is appreciably lower than the speeds currently attained by airplanes. The Reynolds number realized is thus 15 to 25 times smaller than that reached by airplanes in free flight, while the ratio of speed to the velocity of sound is between a third and three quarters of the true ratio. The necessary increases in either the diameter of the <span class="hlt">wind</span> tunnel or the velocity of the airstream are too costly. However, the author shows that it is possible to have <span class="hlt">wind</span> tunnels in which the Reynolds number will be greater than that now obtained by airplanes, and in which the ratio of the velocity to the velocity of sound will also be greater than that realized in practice, by employing a gas other than <span class="hlt">air</span>, at a <span class="hlt">pressure</span> and temperature different from those of the surrounding atmosphere. The gas is carbonic acid, a gas having a low coefficient of viscosity, high density, and a low ratio of specific heat. The positive results of using carbonic acid in <span class="hlt">wind</span> tunnel tests are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23192299','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23192299"><span>Numerical modeling on <span class="hlt">air</span> quality in an urban environment with changes of the aspect ratio and <span class="hlt">wind</span> direction.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Yassin, Mohamed F</p> <p>2013-06-01</p> <p>Due to heavy traffic emissions within an urban environment, <span class="hlt">air</span> quality during the last decade becomes worse year by year and hazard to public health. In the present work, numerical modeling of flow and dispersion of gaseous emissions from vehicle exhaust in a street canyon were investigated under changes of the aspect ratio and <span class="hlt">wind</span> direction. The three-dimensional flow and dispersion of gaseous pollutants were modeled using a computational fluid dynamics (CFD) model which was numerically solved using Reynolds-averaged Navier-Stokes (RANS) equations. The diffusion flow field in the atmospheric boundary layer within the street canyon was studied for different aspect ratios (W/H=1/2, 3/4, and 1) and <span class="hlt">wind</span> directions (θ=90°, 112.5°, 135°, and 157.5°). The numerical models were validated against <span class="hlt">wind</span> tunnel results to optimize the turbulence model. The numerical results agreed well with the <span class="hlt">wind</span> tunnel results. The simulation demonstrated that the minimum concentration at the human respiration height within the street canyon was on the windward side for aspect ratios W/H=1/2 and 1 and <span class="hlt">wind</span> directions θ=112.5°, 135°, and 157.5°. The pollutant concentration level decreases as the <span class="hlt">wind</span> direction and aspect ratio increase. The <span class="hlt">wind</span> velocity and turbulence intensity increase as the aspect ratio and <span class="hlt">wind</span> direction increase.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18529171','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18529171"><span>High-Reynolds-number turbulent-boundary-layer wall <span class="hlt">pressure</span> fluctuations with skin-friction reduction by <span class="hlt">air</span> injection.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Winkel, Eric S; Elbing, Brian R; Ceccio, Steven L; Perlin, Marc; Dowling, David R</p> <p>2008-05-01</p> <p>The hydrodynamic <span class="hlt">pressure</span> fluctuations that occur on the solid surface beneath a turbulent boundary layer are a common source of flow noise. This paper reports multipoint surface <span class="hlt">pressure</span> fluctuation measurements in water beneath a high-Reynolds-number turbulent boundary layer with wall injection of <span class="hlt">air</span> to reduce skin-friction drag. The experiments were conducted in the U.S. Navy's Large Cavitation Channel on a 12.9-m-long, 3.05-m-wide hydrodynamically smooth flat plate at freestream speeds up to 20 ms and downstream-distance-based Reynolds numbers exceeding 200 x 10(6). <span class="hlt">Air</span> was injected from one of two spanwise slots through flush-mounted porous stainless steel frits (approximately 40 microm mean pore diameter) at volume flow rates from 17.8 to 142.5 l/s per meter span. The two injectors were located 1.32 and 9.78 m from the model's leading edge and spanned the center 87% of the test model. Surface <span class="hlt">pressure</span> measurements were made with 16 flush-mounted transducers in an "L-shaped" array located 10.7 m from the plate's leading edge. When compared to no-injection conditions, the observed wall-<span class="hlt">pressure</span> variance was reduced by as much as 87% with <span class="hlt">air</span> injection. In addition, <span class="hlt">air</span> injection altered the inferred convection speed of <span class="hlt">pressure</span> fluctuation sources and the streamwise coherence of <span class="hlt">pressure</span> fluctuations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.epa.gov/caa-permitting/final-permit-documents-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound','PESTICIDES'); return false;" href="https://www.epa.gov/caa-permitting/final-permit-documents-cape-wind-associates-llc-horseshoe-shoal-nantucket-sound"><span>Final Permit Documents for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit)</span></a></p> <p><a target="_blank" href="http://www.epa.gov/pesticides/search.htm">EPA Pesticide Factsheets</a></p> <p></p> <p></p> <p>List of finla permit documents for the Cape <span class="hlt">Wind</span> Associates, LLC, Horseshoe Shoal, Nantucket Sound (Offshore Renewable Energy Project/OCS <span class="hlt">Air</span> Permit: Massachusetts Plan Approval including nonattainment NSR Appendix A requirements).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28163877','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28163877"><span><span class="hlt">Wind</span> and water tunnel testing of a morphing aquatic micro <span class="hlt">air</span> vehicle.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Siddall, Robert; Ortega Ancel, Alejandro; Kovač, Mirko</p> <p>2017-02-06</p> <p>Aerial robots capable of locomotion in both <span class="hlt">air</span> and water would enable novel mission profiles in complex environments, such as water sampling after floods or underwater structural inspections. The design of such a vehicle is challenging because it implies significant propulsive and structural design trade-offs for operation in both fluids. In this paper, we present a unique Aquatic Micro <span class="hlt">Air</span> Vehicle (AquaMAV), which uses a reconfigurable wing to dive into the water from flight, inspired by the plunge diving strategy of water diving birds in the family Sulidae . The vehicle's performance is investigated in <span class="hlt">wind</span> and water tunnel experiments, from which we develop a planar trajectory model. This model is used to predict the dive behaviour of the AquaMAV, and investigate the efficacy of passive dives initiated by wing folding as a means of water entry. The paper also includes first field tests of the AquaMAV prototype where the folding wings are used to initiate a plunge dive.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5206604','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5206604"><span><span class="hlt">Wind</span> and water tunnel testing of a morphing aquatic micro <span class="hlt">air</span> vehicle</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Ortega Ancel, Alejandro; Kovač, Mirko</p> <p>2017-01-01</p> <p>Aerial robots capable of locomotion in both <span class="hlt">air</span> and water would enable novel mission profiles in complex environments, such as water sampling after floods or underwater structural inspections. The design of such a vehicle is challenging because it implies significant propulsive and structural design trade-offs for operation in both fluids. In this paper, we present a unique Aquatic Micro <span class="hlt">Air</span> Vehicle (AquaMAV), which uses a reconfigurable wing to dive into the water from flight, inspired by the plunge diving strategy of water diving birds in the family Sulidae. The vehicle's performance is investigated in <span class="hlt">wind</span> and water tunnel experiments, from which we develop a planar trajectory model. This model is used to predict the dive behaviour of the AquaMAV, and investigate the efficacy of passive dives initiated by wing folding as a means of water entry. The paper also includes first field tests of the AquaMAV prototype where the folding wings are used to initiate a plunge dive. PMID:28163877</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20040070945&hterms=balance+sheet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbalance%2Bsheet','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20040070945&hterms=balance+sheet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbalance%2Bsheet"><span>Differential Velocity between Solar <span class="hlt">Wind</span> Protons and Alpha Particles in <span class="hlt">Pressure</span> Balance Structures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yamauchi, Yohei; Suess, Steven T.; Steinberg, John T.; Sakurai, Takashi</p> <p>2004-01-01</p> <p><span class="hlt">Pressure</span> balance structures (PBSs) are a common high-plasma beta feature in high-latitude, high-speed solar <span class="hlt">wind</span>. They have been proposed as remnants of coronal plumes. If true, they should reflect the observation that plumes are rooted in unipolar magnetic flux concentrations in the photosphere and are heated as oppositely directed flux is advected into and reconnects with the flux concentration. A minimum variance analysis (MVA) of magnetic discontinuities in PBSs showed there is a larger proportion of tangential discontinuities than in the surrounding high-speed <span class="hlt">wind</span>, supporting the hypothesis that plasmoids or extended current sheets are formed during reconnection at the base of plumes. To further evaluate the character of magnetic field discontinuities in PBSs, differential streaming between alpha particles and protons is analyzed here for the same sample of PBSs used in the MVA. Alpha particles in high-speed <span class="hlt">wind</span> generally have a higher radial flow speed than protons. However, if the magnetic field is folded back on itself, as in a large-amplitude Alfven wave, alpha particles will locally have a radial flow speed less than protons. This characteristic is used here to distinguish between folded back magnetic fields (which would contain rotational discontinuities) and tangential discontinuities using Ulysses high-latitude, high-speed solar <span class="hlt">wind</span> data. The analysis indicates that almost all reversals in the radial magnetic field in PBSs are folded back field lines. This is found to also be true outside PBSs, supporting existing results for typical high-speed, high-latitude <span class="hlt">wind</span>. There remains a small number of cases that appear not to be folds in the magnetic field and which may be flux tubes with both ends rooted in the Sun. The distinct difference in MVA results inside and outside PBSs remains unexplained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20040000498&hterms=balance+sheet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbalance%2Bsheet','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20040000498&hterms=balance+sheet&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbalance%2Bsheet"><span>Differential Velocity Between Solar <span class="hlt">Wind</span> Protons and Alpha Particles in <span class="hlt">Pressure</span> Balance Structures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yamauchi, Y.; Suess, S. T.; Steinberg, J. T.; Sakurai, T.</p> <p>2003-01-01</p> <p><span class="hlt">Pressure</span> balance structures (PBSs) are a common high plasma beta feature in high latitude, high speed solar <span class="hlt">wind</span>. They have been proposed as remnants of coronal plumes. If true, they should reflect the observation that plumes are rooted in unipolar magnetic flux concentrations in the photosphere and are heated as oppositely directed flux is advected into and reconnects with the flux concentration. A minimum variance analysis (MVA) of magnetic discontinuities in PBSs showed there is a larger proportion of tangential discontinuities than in the surrounding high speed <span class="hlt">wind</span>, supporting the hypothesis that plasmoids or extended current sheets are formed during reconnection at the base of plumes. To further evaluate the character of magnetic field discontinuities in PBSs, differential streaming between alpha particles and protons is analyzed here for the same sample of PBSs used in the MVA. Alpha particles in high speed <span class="hlt">wind</span> generally have a higher radial flow speed than protons. However, if the magnetic field is folded back on itself, as in a large amplitude Alfven wave, alpha particles will locally have a radial flow speed less than protons. This characteristic is used here to distinguish between folded back magnetic fields (which would contain rotational discontinuities) and tangential discontinuities using Ulysses high latitude, high speed solar <span class="hlt">wind</span> data. The analysis indicates that almost all reversals in the radial magnetic field in PBSs are folded back field lines. This is found to also be true outside PBSs, supporting existing results for typical high speed, high latitude <span class="hlt">wind</span>. There remains a small number of cases that appear not to be folds in the magnetic field and which may be flux tubes with both ends rooted in the Sun. The distinct difference in MVA results inside and outside PBSs remains unexplained.</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://ntrs.nasa.gov/search.jsp?R=19870012585&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870012585&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure"><span>Investigation of the reaction of liquid hydrogen with liquid <span class="hlt">air</span> in a <span class="hlt">pressure</span> tube</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Karb, Erich H.</p> <p>1987-01-01</p> <p>A <span class="hlt">pressure</span> tube should protect the FR-2 reactor from the consequences of a hydrogen-<span class="hlt">air</span> reaction, which is conceivable in the breakdown of several safety devices of the planned cold neutron source Project FR-2/16. The magnitudes and time pattern of the <span class="hlt">pressures</span> to be expected were investigated. In the geometry used and the ignition mechanism selected, which is comparable to the strongest ignition process conceivable in the reactor, the reaction proceeds with greater probability than combustion. The combustion is possibly smaller if local limited partial detonations are superimposed. The magnitude of the <span class="hlt">pressure</span> was determined by the masses of the reaction partners, liquid H2 and liquid <span class="hlt">air</span>, and determines their ratio to each other.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19720005584','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19720005584"><span>An inventory of aeronautical ground research facilities. Volume 2: <span class="hlt">Air</span> breathing engine test facilities</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pirrello, C. J.; Hardin, R. D.; Heckart, M. V.; Brown, K. R.</p> <p>1971-01-01</p> <p>The inventory covers free jet and direct connect altitude cells, sea level static thrust stands, sea level test cells with ram <span class="hlt">air</span>, and propulsion <span class="hlt">wind</span> tunnels. Free jet altitude cells and propulsion <span class="hlt">wind</span> tunnels are used for evaluation of complete inlet-engine-exhaust nozzle propulsion systems under simulated flight conditions. These facilities are similar in principal of operation and differ primarily in test section concept. The propulsion <span class="hlt">wind</span> tunnel provides a closed test section and restrains the flow around the test specimen while the free jet is allowed to expand freely. A chamber of large diameter about the free jet is provided in which desired operating <span class="hlt">pressure</span> levels may be maintained. Sea level test cells with ram <span class="hlt">air</span> provide controlled, conditioned <span class="hlt">air</span> directly to the engine face for performance evaluation at low altitude flight conditions. Direct connect altitude cells provide a means of performance evaluation at simulated conditions of Mach number and altitude with <span class="hlt">air</span> supplied to the flight altitude conditions. Sea level static thrust stands simply provide an instrumented engine mounting for measuring thrust at zero airspeed. While all of these facilities are used for integrated engine testing, a few provide engine component test capability.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26741497','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26741497"><span>Effect of Different Levels of <span class="hlt">Pressure</span> Relieving <span class="hlt">Air</span>-Mattress Firmness on Cough Strength.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kamikawa, Norimichi; Taito, Shunsuke; Takahashi, Makoto; Sekikawa, Kiyokazu; Hamada, Hironobu</p> <p>2016-01-01</p> <p>Cough is an important host-defense mechanism. The elderly and patients who are severely ill cannot cough effectively when lying in the supine position. Furthermore, <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattresses are recommended for preventing the development of <span class="hlt">pressure</span> ulcers. In this study, we clarified whether or not the cough peak flow (CPF), an index of cough strength, is affected by different firmness levels of a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress in healthy volunteers in the supine position. Fifty-two healthy young men participated. All the measurements were carried out on each participant in the supine position on a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress. The participants were assessed at two firmness levels, a "hard" and "soft" mode. The CPF, forced vital capacity (FVC), maximal expiratory <span class="hlt">pressure</span> (PEmax), and maximal inspiratory <span class="hlt">pressure</span> (PImax) were determined for each mode. The sinking distance of the body into the mattress was measured without any activity and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax, and PImax were determined for each mode. The sinking distance of the body into the mattress was measured and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax and PImax values of the participants coughing on the mattress were significantly lower when the mattress was in "soft" than in "hard" mode. The differences between the sinking distances of the mattress in "soft" and "hard" modes were larger for the anterior superior iliac spine. A harder mattress may lead to increased CPF in healthy young men lying in the supine position, and increased CPF may be important for host defense.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29113035','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29113035"><span>Room-Temperature <span class="hlt">Pressure</span>-Induced Optically-Actuated Fabry-Perot Nanomechanical Resonator with Multilayer Graphene Diaphragm in <span class="hlt">Air</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Li, Cheng; Lan, Tian; Yu, Xiyu; Bo, Nan; Dong, Jingyu; Fan, Shangchun</p> <p>2017-11-04</p> <p>We demonstrated a miniature and in situ ~13-layer graphene nanomechanical resonator by utilizing a simple optical fiber Fabry-Perot (F-P) interferometric excitation and detection scheme. The graphene film was transferred onto the endface of a ferrule with a 125-μm inner diameter. In contrast to the pre-tension induced in membrane that increased quality ( Q ) factor to ~18.5 from ~3.23 at room temperature and normal <span class="hlt">pressure</span>, the limited effects of <span class="hlt">air</span> damping on resonance behaviors at 10 -2 and 10⁵ Pa were demonstrated by characterizing graphene F-P resonators with open and micro-<span class="hlt">air</span>-gap cavities. Then in terms of optomechanical behaviors of the resonator with an <span class="hlt">air</span> micro-cavity configuration using a polished ferrule substrate, measured resonance frequencies were increased to the range of 509-542 kHz from several kHz with a maximum Q factor of 16.6 despite the lower Knudsen number ranging from 0.0002 to 0.0006 in damping <span class="hlt">air</span> over a relative <span class="hlt">pressure</span> range of 0-199 kPa. However, there was the little dependence of Q on resonance frequency. Note that compared with the inferior F-P cavity length response to applied <span class="hlt">pressures</span> due to interfacial <span class="hlt">air</span> leakage, the developed F-P resonator exhibited a consistent fitted <span class="hlt">pressure</span> sensitivity of 1.18 × 10⁵ kHz³/kPa with a good linearity error of 5.16% in the tested range. These measurements shed light on the pre-stress-dominated <span class="hlt">pressure</span>-sensitive mechanisms behind <span class="hlt">air</span> damping in in situ F-P resonant sensors using graphene or other 2D nanomaterials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28834825','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28834825"><span>Intraocular <span class="hlt">Pressure</span> Fluctuations and 24-Hour Continuous Monitoring for Glaucoma Risk in <span class="hlt">Wind</span> Instrument Players.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>de Crom, Ronald M P C; Webers, Carroll A B; van Kooten-Noordzij, Marina A W; Michiels, Agnes C; Schouten, Jan S A G; Berendschot, Tos T J M; Beckers, Henny J M</p> <p>2017-10-01</p> <p>The purpose of this study is to investigate the influence of playing a <span class="hlt">wind</span> instrument on intraocular <span class="hlt">pressure</span> (IOP) and to monitor 24-hour (IOP) fluctuations in <span class="hlt">wind</span> musicians of symphony and <span class="hlt">wind</span> orchestras to compare IOP levels during normal daily activities with IOP levels during playing. Professional and amateur musicians of symphony and <span class="hlt">wind</span> orchestras were invited to participate. A total of 42 participants, 9 with glaucoma, underwent a routine ophthalmologic examination. IOP measurements were taken before and immediately after 20 minutes of playing <span class="hlt">wind</span> instruments. In addition, 6 participants underwent 24-hour IOP monitoring with the Triggerfish (Sensimed AG, Switzerland) sensing contact lens, during which they kept an activity logbook. Eleven professionals and 31 amateur musicians participated in the study. A total of 7 eyes of 6 patients underwent additional 24-hour IOP monitoring. Mean IOP before playing was 13.6±2.6 mm Hg, IOP change after playing was +1.5±2.2 mm Hg with a significant difference between professionals (2.5±1.5 mm Hg) and amateurs (1.1±2.3 mm Hg). There were no significant differences in IOP change between subjects with or without glaucoma. During 24-hour IOP monitoring there were slight increases in IOP while playing an instrument, but also during other activities and overnight. These latter IOP levels were similar or even higher than the IOP rise caused by playing a <span class="hlt">wind</span> instrument. IOP often rises after playing <span class="hlt">wind</span> instruments, but similar or even higher IOP levels seem to occur during common other daily activities or at night. These peaks may be relevant for glaucomatous field progression and treatment of glaucoma patients.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010043986','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010043986"><span>A <span class="hlt">Wind</span> Tunnel Study on the Mars Pathfinder (MPF) Lander Descent <span class="hlt">Pressure</span> Sensor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Soriano, J. Francisco; Coquilla, Rachael V.; Wilson, Gregory R.; Seiff, Alvin; Rivell, Tomas</p> <p>2001-01-01</p> <p>The primary focus of this study was to determine the accuracy of the Mars Pathfinder lander local <span class="hlt">pressure</span> readings in accordance with the actual ambient atmospheric <span class="hlt">pressures</span> of Mars during parachute descent. In order to obtain good measurements, the plane of the lander <span class="hlt">pressure</span> sensor opening should ideally be situated so that it is parallel to the freestream. However, due to two unfavorable conditions, the sensor was positioned in locations where correction factors are required. One of these disadvantages is due to the fact that the parachute attachment point rotated the lander's center of gravity forcing the location of the <span class="hlt">pressure</span> sensor opening to be off tangent to the freestream. The second and most troublesome factor was that the lander descends with slight oscillations that could vary the amplitude of the sensor readings. In order to accurately map the correction factors required at each sensor position, an experiment simulating the lander descent was conducted in the Martian Surface <span class="hlt">Wind</span> Tunnel at NASA Ames Research Center. Using a 115 scale model at Earth ambient <span class="hlt">pressures</span>, the test settings provided the necessary Reynolds number conditions in which the actual lander was possibly subjected to during the descent. In the analysis and results of this experiment, the readings from the lander sensor were converted to the form of <span class="hlt">pressure</span> coefficients. With a contour map of <span class="hlt">pressure</span> coefficients at each lander oscillatory position, this report will provide a guideline to determine the correction factors required for the Mars Pathfinder lander descent <span class="hlt">pressure</span> sensor readings.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19780013483','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19780013483"><span>A method of calibrating <span class="hlt">wind</span> velocity sensors with a modified gas flow calibrator</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stump, H. P.</p> <p>1978-01-01</p> <p>A procedure was described for calibrating <span class="hlt">air</span> velocity sensors in the exhaust flow of a gas flow calibrator. The average velocity in the test section located at the calibrator exhaust was verified from the mass flow rate accurately measured by the calibrator's precision sonic nozzles. <span class="hlt">Air</span> at elevated <span class="hlt">pressures</span> flowed through a series of screens, diameter changes, and flow straighteners, resulting in a smooth flow through the open test section. The modified system generated <span class="hlt">air</span> velocities of 2 to 90 meters per second with an uncertainty of about two percent for speeds below 15 meters per second and four percent for the higher speeds. <span class="hlt">Wind</span> tunnel data correlated well with that taken in the flow calibrator.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22518756-strong-solar-wind-dynamic-pressure-pulses-interplanetary-sources-impacts-geosynchronous-magnetic-fields','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22518756-strong-solar-wind-dynamic-pressure-pulses-interplanetary-sources-impacts-geosynchronous-magnetic-fields"><span>STRONG SOLAR <span class="hlt">WIND</span> DYNAMIC <span class="hlt">PRESSURE</span> PULSES: INTERPLANETARY SOURCES AND THEIR IMPACTS ON GEOSYNCHRONOUS MAGNETIC FIELDS</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>Zuo, Pingbing; Feng, Xueshang; Wang, Yi</p> <p></p> <p>In this investigation, we first present a statistical result of the interplanetary sources of very strong solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> pulses (DPPs) detected by <span class="hlt">WIND</span> during solar cycle 23. It is found that the vast majority of strong DPPs reside within solar <span class="hlt">wind</span> disturbances. Although the variabilities of geosynchronous magnetic fields (GMFs) due to the impact of positive DPPs have been well established, there appears to be no systematic investigations on the response of GMFs to negative DPPs. Here, we study both the decompression effects of very strong negative DPPs and the compression from strong positive DPPs on GMFs atmore » different magnetic local time sectors. In response to the decompression of strong negative DPPs, GMFs on the dayside near dawn and near dusk on the nightside, are generally depressed. But near the midnight region, the responses of GMF are very diverse, being either positive or negative. For part of the events when GOES is located at the midnight sector, the GMF is found to abnormally increase as the result of magnetospheric decompression caused by negative DPPs. It is known that under certain conditions magnetic depression of nightside GMFs can be caused by the impact of positive DPPs. Here, we find that a stronger <span class="hlt">pressure</span> enhancement may have a higher probability of producing the exceptional depression of GMF at the midnight region. Statistically, both the decompression effect of strong negative DPPs and the compression effect of strong positive DPPs depend on the magnetic local time, which are stronger at the noon sector.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17572748','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17572748"><span><span class="hlt">Pressure</span> measurement in supersonic <span class="hlt">air</span> flow by differential absorptive laser-induced thermal acoustics.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hart, Roger C; Herring, G C; Balla, R Jeffrey</p> <p>2007-06-15</p> <p>Nonintrusive, off-body flow barometry in Mach 2 airflow has been demonstrated in a large-scale supersonic <span class="hlt">wind</span> tunnel using seedless laser-induced thermal acoustics (LITA). The static <span class="hlt">pressure</span> of the gas flow is determined with a novel differential absorption measurement of the ultrasonic sound produced by the LITA pump process. Simultaneously, the streamwise velocity and static gas temperature of the same spatially resolved sample volume were measured with this nonresonant time-averaged LITA technique. Mach number, temperature, and <span class="hlt">pressure</span> have 0.2%, 0.4%, and 4% rms agreement, respectively, in comparison with known free-stream conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20090011252','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20090011252"><span><span class="hlt">Pressure</span> Measurement in Supersonic <span class="hlt">Air</span> Flow by Differential Absorptive Laser-Induced Thermal Acoustics</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hart, Roger C.; Herring, Gregory C.; Balla, Robert J.</p> <p>2007-01-01</p> <p>Nonintrusive, off-body flow barometry in Mach-2 airflow has been demonstrated in a large-scale supersonic <span class="hlt">wind</span> tunnel using seedless laser-induced thermal acoustics (LITA). The static <span class="hlt">pressure</span> of the gas flow is determined with a novel differential absorption measurement of the ultrasonic sound produced by the LITA pump process. Simultaneously, stream-wise velocity and static gas temperature of the same spatially-resolved sample volume were measured with this nonresonant time-averaged LITA technique. Mach number, temperature and <span class="hlt">pressure</span> have 0.2%, 0.4%, and 4% rms agreement, respectively, in comparison with known free-stream conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25559870','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25559870"><span>A randomized comparison of the i-gel with the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q intubating laryngeal airway in children.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kim, Min-Soo; Lee, Jae Hoon; Han, Sang Won; Im, Young Jae; Kang, Hyo Jong; Lee, Jeong-Rim</p> <p>2015-04-01</p> <p>Supraglottic airway devices with noninflatable cuff have advantages in omitting the cuff <span class="hlt">pressure</span> monitoring and reducing potential pharyngolaryngeal complications. Typical devices without cuff inflation available in children are the i-gel and the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q intubating laryngeal airway (<span class="hlt">air</span>-Q SP). To date, there is no comparative study between these devices in pediatric patients. The purpose of this randomized study was to compare the i-gel(™) and the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q(™) intubating laryngeal airway (<span class="hlt">air</span>-Q SP) in children undergoing general anesthesia. Eighty children, 1-108 months of age, 7-30 kg of weight, and scheduled for elective surgery in which supraglottic airway devices would be suitable for airway management, were randomly assigned to either the i-gel or the <span class="hlt">air</span>-Q SP. Oropharyngeal leak <span class="hlt">pressure</span> and fiberoptic view were assessed three times as follows: after insertion and fixation of the device, 10 min after initial assessment, and after completion of surgery. We also assessed insertion parameters and complications. Insertion of the i-gel was regarded as significantly easier compared to the <span class="hlt">air</span>-Q SP (P = 0.04). Compared to the <span class="hlt">air</span>-Q SP group, the i-gel group had significantly higher oropharyngeal leak <span class="hlt">pressures</span> at all measurement points and significantly lower frequencies of gastric insufflation at 10 min after initial assessment and completion of surgery. The <span class="hlt">air</span>-Q SP group had better fiberoptic views than the i-gel group at all measurement points. Our results showed that the i-gel had easier insertion and better sealing function, and the <span class="hlt">air</span>-Q SP provided improved fiberoptic views in children requiring general anesthesia. © 2015 John Wiley & Sons Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/1002978','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/1002978"><span>Metabolic response to <span class="hlt">air</span> temperature and <span class="hlt">wind</span> in day-old mallards and a standard operative temperature scale</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Bakken, G.S.; Reynolds, P.S.; Kenow, K.P.; Korschgen, C.E.; Boysen, A.F.</p> <p>1999-01-01</p> <p>Most duckling mortality occurs during the week following hatching and is often associated with cold, windy, wet weather and scattering of the brood. We estimated the thermoregulatory demands imposed by cold, windy weather on isolated 1-d-old mallard (Anas platyrhynchos) ducklings resting in cover. We measured O-2 consumption and evaporative water loss at <span class="hlt">air</span> temperatures from 5 degrees to 25 degrees C and <span class="hlt">wind</span> speeds of 0.1, 0.2, 0.5, and 1.0 mis. Metabolic heat production increased as <span class="hlt">wind</span> increased or temperature decreased but was less sensitive to <span class="hlt">wind</span> than that of either adult passerines or small mammals. Evaporative heat loss ranged from 5% to 17% of heat production. Evaporative heal loss and the ratio of evaporative heat loss to metabolic heat production was significantly lower in rest phase. These data were used to define a standard operative temperature (T-es) scale for night or heavy overcast conditions. An increase of <span class="hlt">wind</span> speed from 0.1 to 1 mis decreased T-es by 3 degrees-5 degrees C.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910009738','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910009738"><span>F-18 high alpha research vehicle surface <span class="hlt">pressures</span>: Initial in-flight results and correlation with flow visualization and <span class="hlt">wind</span>-tunnel data</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fisher, David F.; Banks, Daniel W.; Richwine, David M.</p> <p>1990-01-01</p> <p><span class="hlt">Pressure</span> distributions measured on the forebody and the leading-edge extensions (LEX's) of the NASA F-18 high alpha research vehicle (HARV) were reported at 10 and 50 degree angles of attack and at Mach 0.20 to 0.60. The results were correlated with HARV flow visualization and 6-percent scale F-18 <span class="hlt">wind</span>-tunnel-model test results. The general trend in the data from the forebody was for the maximum suction <span class="hlt">pressure</span> peaks to first appear at an angle of attack (alpha) of approximately 19 degrees and increase in magnitude with angle of attack. The LEX <span class="hlt">pressure</span> distribution general trend was the inward progression and increase in magnitude of the maximum suction peaks up to vortex core breakdown and then the decrease and general flattening of the <span class="hlt">pressure</span> distribution beyond that. No significant effect of Mach number was noted for the forebody results. However, a substantial compressibility effect on the LEX's resulted in a significant reduction in vortex-induced suction <span class="hlt">pressure</span> as Mach number increased. The forebody primary and the LEX secondary vortex separation lines, from surface flow visualization, correlated well with the end of <span class="hlt">pressure</span> recovery, leeward and windward, respectively, of maximum suction <span class="hlt">pressure</span> peaks. The flight to <span class="hlt">wind</span>-tunnel correlations were generally good with some exceptions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AGUFMSM22B..02K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AGUFMSM22B..02K"><span>Radiation Belt Transport Driven by Solar <span class="hlt">Wind</span> Dynamic <span class="hlt">Pressure</span> Fluctuations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kress, B. T.; Hudson, M. K.; Ukhorskiy, A. Y.; Mueller, H.</p> <p>2012-12-01</p> <p>The creation of the Earth's outer zone radiation belts is attributed to earthward transport and adiabatic acceleration of electrons by drift-resonant interactions with electromagnetic fluctuations in the magnetosphere. Three types of radial transport driven by solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> fluctuations that have been identified are: (1) radial diffusion [Falthammer, 1965], (2) significant changes in the phase space density radial profile due to a single or few ULF drift-resonant interactions [Ukhorskiy et al., 2006; Degeling et al., 2008], and (3) shock associated injections of radiation belt electrons occurring in less than a drift period [Li et al., 1993]. A progress report will be given on work to fully characterize different forms of radial transport and their effect on the Earth's radiation belts. The work is being carried out by computing test-particle trajectories in electric and magnetic fields from a simple analytic ULF field model and from global MHD simulations of the magnetosphere. Degeling, A. W., L. G. Ozeke, R. Rankin, I. R. Mann, and K. Kabin (2008), Drift resonant generation of peaked relativistic electron distributions by Pc 5 ULF waves, textit{J. Geophys. Res., 113}, A02208, doi:10.1029/2007JA012411. Fälthammar, C.-G. (1965), Effects of Time-Dependent Electric Fields on Geomagnetically Trapped Radiation, J. Geophys. Res., 70(11), 2503-2516, doi:10.1029/JZ070i011p02503. Li, X., I. Roth, M. Temerin, J. R. Wygant, M. K. Hudson, and J. B. Blake (1993), Simulation of the prompt energization and transport of radiation belt particles during the March 24, 1991 SSC, textit{Geophys. Res. Lett., 20}(22), 2423-2426, doi:10.1029/93GL02701. Ukhorskiy, A. Y., B. J. Anderson, K. Takahashi, and N. A. Tsyganenko (2006), Impact of ULF oscillations in solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span> on the outer radiation belt electrons, textit{Geophys. Res. Lett., 33}(6), L06111, doi:10.1029/2005GL024380.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1356151-simultaneous-disappearances-plasmaspheric-hiss-exohiss-chorus-waves-triggered-sudden-decrease-solar-wind-dynamic-pressure','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1356151-simultaneous-disappearances-plasmaspheric-hiss-exohiss-chorus-waves-triggered-sudden-decrease-solar-wind-dynamic-pressure"><span>Simultaneous disappearances of plasmaspheric hiss, exohiss, and chorus waves triggered by a sudden decrease in solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Liu, Nigang; Su, Zhenpeng; Gao, Zhonglei; ...</p> <p>2016-12-29</p> <p>Magnetospheric whistler mode waves are of great importance in the radiation belt electron dynamics. In this paper, on the basis of the analysis of a rare event with the simultaneous disappearances of whistler mode plasmaspheric hiss, exohiss, and chorus triggered by a sudden decrease in the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, we provide evidences for the following physical scenarios: (1) nonlinear generation of chorus controlled by the geomagnetic field inhomogeneity, (2) origination of plasmaspheric hiss from chorus, and (3) leakage of plasmaspheric hiss into exohiss. Finally, following the reduction of the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, the dayside geomagnetic field configuration withmore » the enhanced inhomogeneity became unfavorable for the generation of chorus, and the quenching of chorus directly caused the disappearances of plasmaspheric hiss and then exohiss.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1356151','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1356151"><span>Simultaneous disappearances of plasmaspheric hiss, exohiss, and chorus waves triggered by a sudden decrease in solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</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>Liu, Nigang; Su, Zhenpeng; Gao, Zhonglei</p> <p></p> <p>Magnetospheric whistler mode waves are of great importance in the radiation belt electron dynamics. In this paper, on the basis of the analysis of a rare event with the simultaneous disappearances of whistler mode plasmaspheric hiss, exohiss, and chorus triggered by a sudden decrease in the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, we provide evidences for the following physical scenarios: (1) nonlinear generation of chorus controlled by the geomagnetic field inhomogeneity, (2) origination of plasmaspheric hiss from chorus, and (3) leakage of plasmaspheric hiss into exohiss. Finally, following the reduction of the solar <span class="hlt">wind</span> dynamic <span class="hlt">pressure</span>, the dayside geomagnetic field configuration withmore » the enhanced inhomogeneity became unfavorable for the generation of chorus, and the quenching of chorus directly caused the disappearances of plasmaspheric hiss and then exohiss.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/821423','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/821423"><span>ANOMALOUSLY <span class="hlt">PRESSURED</span> GAS DISTRIBUTION IN THE <span class="hlt">WIND</span> RIVER BASIN, WYOMING</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>Dr. Ronald C. Surdam</p> <p>2003-03-31</p> <p>Anomalously <span class="hlt">pressured</span> gas (APG) assets, typically called ''basin-center'' gas accumulations, represent either an underdeveloped or undeveloped energy resource in the Rocky Mountain Laramide Basins (RMLB). Historically, the exploitation of these gas resources has proven to be very difficult and costly. In this topical report, an improved exploration strategy is outlined in conjunction with a more detailed description of new diagnostic techniques that more efficiently detect anomalously <span class="hlt">pressured</span>, gas-charged domains. The ability to delineate gas-charged domains occurring below a regional velocity inversion surface allows operators to significantly reduce risk in the search for APG resources. The <span class="hlt">Wind</span> River Basin was chosenmore » for this demonstration because of the convergence of public data availability (i.e., thousands of mud logs and DSTs and 2400 mi of 2-D seismic lines); the evolution of new diagnostic techniques; a 175 digital sonic log suite; a regional stratigraphic framework; and corporate interest. In the exploration scheme discussed in this topical report, the basinwide gas distribution is determined in the following steps: (1) A detailed velocity model is established from sonic logs, 2-D seismic lines, and, if available, 3-D seismic data. In constructing the seismic interval velocity field, automatic picking technology using continuous, statistically-derived interval velocity selection, as well as conventional graphical interactive methodologies are utilized. (2) Next, the ideal regional velocity/depth function is removed from the observed sonic or seismic velocity/depth profile. The constructed ideal regional velocity/depth function is the velocity/depth trend resulting from the progressive burial of a rock/fluid system of constant rock/fluid composition, with all other factors remaining constant. (3) The removal of the ideal regional velocity/depth function isolates the anomalously slow velocities and allows the evaluation of (a) the regional</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740009842','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740009842"><span><span class="hlt">Wind</span> tunnel model and method</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jackson, C. M., Jr.; Summerfield, D. G. (Inventor)</p> <p>1974-01-01</p> <p>The design and development of a <span class="hlt">wind</span> tunnel model equipped with <span class="hlt">pressure</span> measuring devices are discussed. The <span class="hlt">pressure</span> measuring orifices are integrally constructed in the <span class="hlt">wind</span> tunnel model and do not contribute to distortions of the aerodynamic surface. The construction of a typical model is described and a drawing of the device is included.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150002952','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150002952"><span>Assimilation of <span class="hlt">Wind</span> Profiles from Multiple Doppler Radar <span class="hlt">Wind</span> Profilers for Space Launch Vehicle Applications</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Decker, Ryan K.; Barbre, Robert E., Jr.; Brenton, James C.; Walker, James C.; Leach, Richard D.</p> <p>2015-01-01</p> <p>Space launch vehicles utilize atmospheric <span class="hlt">winds</span> in design of the vehicle and during day-of-launch (DOL) operations to assess affects of <span class="hlt">wind</span> loading on the vehicle and to optimize vehicle performance during ascent. The launch ranges at NASA's Kennedy Space Center co-located with the United States <span class="hlt">Air</span> Force's (USAF) Eastern Range (ER) at Cape Canaveral <span class="hlt">Air</span> Force Station and USAF's Western Range (WR) at Vandenberg <span class="hlt">Air</span> Force Base have extensive networks of in-situ and remote sensing instrumentation to measure atmospheric <span class="hlt">winds</span>. Each instrument's technique to measure <span class="hlt">winds</span> has advantages and disadvantages in regards to use for vehicle engineering assessments. Balloons measure <span class="hlt">wind</span> at all altitudes necessary for vehicle assessments, but two primary disadvantages exist when applying balloon output on DOL. First, balloons need approximately one hour to reach required altitude. For vehicle assessments this occurs at 60 kft (18.3 km). Second, balloons are steered by atmospheric <span class="hlt">winds</span> down range of the launch site that could significantly differ from those <span class="hlt">winds</span> along the vehicle ascent trajectory. Figure 1 illustrates the spatial separation of balloon measurements from the surface up to approximately 55 kft (16.8 km) during the Space Shuttle launch on 10 December 2006. The balloon issues are mitigated by use of vertically pointing Doppler Radar <span class="hlt">Wind</span> Profilers (DRWPs). However, multiple DRWP instruments are required to provide <span class="hlt">wind</span> data up to 60 kft (18.3 km) for vehicle trajectory assessments. The various DRWP systems have different operating configurations resulting in different temporal and spatial sampling intervals. Therefore, software was developed to combine data from both DRWP-generated profiles into a single profile for use in vehicle trajectory analyses. Details on how data from various <span class="hlt">wind</span> measurement systems are combined and sample output will be presented in the following sections.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050182663','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050182663"><span>Progress in Validation of <span class="hlt">Wind</span>-US for Ramjet/Scramjet Combustion</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Engblom, William A.; Frate, Franco C.; Nelson, Chris C.</p> <p>2005-01-01</p> <p>Validation of the <span class="hlt">Wind</span>-US flow solver against two sets of experimental data involving high-speed combustion is attempted. First, the well-known Burrows- Kurkov supersonic hydrogen-<span class="hlt">air</span> combustion test case is simulated, and the sensitively of ignition location and combustion performance to key parameters is explored. Second, a numerical model is developed for simulation of an X-43B candidate, full-scale, JP-7-fueled, internal flowpath operating in ramjet mode. Numerical results using an ethylene-<span class="hlt">air</span> chemical kinetics model are directly compared against previously existing <span class="hlt">pressure</span>-distribution data along the entire flowpath, obtained in direct-connect testing conducted at NASA Langley Research Center. Comparison to derived quantities such as burn efficiency and thermal throat location are also made. Reasonable to excellent agreement with experimental data is demonstrated for key parameters in both simulation efforts. Additional <span class="hlt">Wind</span>-US feature needed to improve simulation efforts are described herein, including maintaining stagnation conditions at inflow boundaries for multi-species flow. An open issue regarding the sensitivity of isolator unstart to key model parameters is briefly discussed.</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('http://hdl.handle.net/2060/20160007722','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160007722"><span>Preliminary Computational Study for Future Tests in the NASA Ames 9 foot' x 7 foot <span class="hlt">Wind</span> Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pearl, Jason M.; Carter, Melissa B.; Elmiligui, Alaa A.; WInski, Courtney S.; Nayani, Sudheer N.</p> <p>2016-01-01</p> <p>The NASA Advanced <span class="hlt">Air</span> Vehicles Program, Commercial Supersonics Technology Project seeks to advance tools and techniques to make over-land supersonic flight feasible. In this study, preliminary computational results are presented for future tests in the NASA Ames 9 foot x 7 foot supersonic <span class="hlt">wind</span> tunnel to be conducted in early 2016. Shock-plume interactions and their effect on <span class="hlt">pressure</span> signature are examined for six model geometries. Near- field <span class="hlt">pressure</span> signatures are assessed using the CFD code USM3D to model the proposed test geometries in free-<span class="hlt">air</span>. Additionally, results obtained using the commercial grid generation software Pointwise Reigistered Trademark are compared to results using VGRID, the NASA Langley Research Center in-house mesh generation program.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18639301','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18639301"><span><span class="hlt">Air</span> charged and microtip catheters cannot be used interchangeably for urethral <span class="hlt">pressure</span> measurement: a prospective, single-blind, randomized trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zehnder, Pascal; Roth, Beat; Burkhard, Fiona C; Kessler, Thomas M</p> <p>2008-09-01</p> <p>We determined and compared urethral <span class="hlt">pressure</span> measurements using <span class="hlt">air</span> charged and microtip catheters in a prospective, single-blind, randomized trial. A consecutive series of 64 women referred for urodynamic investigation underwent sequential urethral <span class="hlt">pressure</span> measurements using an <span class="hlt">air</span> charged and a microtip catheter in randomized order. Patients were blinded to the type and sequence of catheter used. Agreement between the 2 catheter systems was assessed using the Bland and Altman 95% limits of agreement method. Intraclass correlation coefficients of <span class="hlt">air</span> charged and microtip catheters for maximum urethral closure <span class="hlt">pressure</span> at rest were 0.97 and 0.93, and for functional profile length they were 0.9 and 0.78, respectively. Pearson's correlation coefficients and Lin's concordance coefficients of <span class="hlt">air</span> charged and microtip catheters were r = 0.82 and rho = 0.79 for maximum urethral closure <span class="hlt">pressure</span> at rest, and r = 0.73 and rho = 0.7 for functional profile length, respectively. When applying the Bland and Altman method, <span class="hlt">air</span> charged catheters gave higher readings than microtip catheters for maximum urethral closure <span class="hlt">pressure</span> at rest (mean difference 7.5 cm H(2)O) and functional profile length (mean difference 1.8 mm). There were wide 95% limits of agreement for differences in maximum urethral closure <span class="hlt">pressure</span> at rest (-24.1 to 39 cm H(2)O) and functional profile length (-7.7 to 11.3 mm). For urethral <span class="hlt">pressure</span> measurement the <span class="hlt">air</span> charged catheter is at least as reliable as the microtip catheter and it generally gives higher readings. However, <span class="hlt">air</span> charged and microtip catheters cannot be used interchangeably for clinical purposes because of insufficient agreement. Hence, clinicians should be aware that <span class="hlt">air</span> charged and microtip catheters may yield completely different results, and these differences should be acknowledged during clinical decision making.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25625652','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25625652"><span>Prenatal <span class="hlt">air</span> pollution exposure and newborn blood <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>van Rossem, Lenie; Rifas-Shiman, Sheryl L; Melly, Steven J; Kloog, Itai; Luttmann-Gibson, Heike; Zanobetti, Antonella; Coull, Brent A; Schwartz, Joel D; Mittleman, Murray A; Oken, Emily; Gillman, Matthew W; Koutrakis, Petros; Gold, Diane R</p> <p>2015-04-01</p> <p><span class="hlt">Air</span> pollution exposure has been associated with increased blood <span class="hlt">pressure</span> in adults. We examined associations of antenatal exposure to ambient <span class="hlt">air</span> pollution with newborn systolic blood <span class="hlt">pressure</span> (SBP). We studied 1,131 mother-infant pairs in a Boston, Massachusetts, area pre-birth cohort. We calculated average exposures by trimester and during the 2 to 90 days before birth for temporally resolved fine particulate matter (≤ 2.5 μm; PM2.5), black carbon (BC), nitrogen oxides, nitrogen dioxide, ozone (O3), and carbon monoxide measured at stationary monitoring sites, and for spatiotemporally resolved estimates of PM2.5 and BC at the residence level. We measured SBP at a mean age of 30 ± 18 hr with an automated device. We used mixed-effects models to examine associations between <span class="hlt">air</span> pollutant exposures and SBP, taking into account measurement circumstances; child's birth weight; mother's age, race/ethnicity, socioeconomic position, and third-trimester BP; and time trend. Estimates represent differences in SBP associated with an interquartile range (IQR) increase in each pollutant. Higher mean PM2.5 and BC exposures during the third trimester were associated with higher SBP (e.g., 1.0 mmHg; 95% CI: 0.1, 1.8 for a 0.32-μg/m3 increase in mean 90-day residential BC). In contrast, O3 was negatively associated with SBP (e.g., -2.3 mmHg; 95% CI: -4.4, -0.2 for a 13.5-ppb increase during the 90 days before birth). Exposures to PM2.5 and BC in late pregnancy were positively associated with newborn SBP, whereas O3 was negatively associated with SBP. Longitudinal follow-up will enable us to assess the implications of these findings for health during later childhood and adulthood.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013OptFT..19...83H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013OptFT..19...83H"><span>Micro-controller based <span class="hlt">air</span> <span class="hlt">pressure</span> monitoring instrumentation system using optical fibers as sensor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hazarika, D.; Pegu, D. S.</p> <p>2013-03-01</p> <p>This paper describes a micro-controller based instrumentation system to monitor <span class="hlt">air</span> <span class="hlt">pressure</span> using optical fiber sensors. The principle of macrobending is used to develop the sensor system. The instrumentation system consists of a laser source, a beam splitter, two multi mode optical fibers, two Light Dependent Resistance (LDR) based timer circuits and a AT89S8252 micro-controller. The beam splitter is used to divide the laser beam into two parts and then these two beams are launched into two multi mode fibers. One of the multi mode fibers is used as the sensor fiber and the other one is used as the reference fiber. The use of the reference fiber is to eliminate the environmental effects while measuring the <span class="hlt">air</span> <span class="hlt">pressure</span> magnitude. The laser beams from the sensor and reference fibers are applied to two identical LDR based timer circuits. The LDR based timer circuits are interfaced to a micro-controller through its counter pins. The micro-controller samples the frequencies of the timer circuits using its counter-0 and counter-1 and the counter values are then processed to provide the measure of <span class="hlt">air</span> <span class="hlt">pressure</span> magnitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120000548','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120000548"><span>Optical <span class="hlt">air</span> data systems and methods</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Spaeth, Lisa G. (Inventor); O'Brien, Martin (Inventor); Tang, Shoou-yu (Inventor); Acott, Phillip E. (Inventor); Caldwell, Loren M. (Inventor)</p> <p>2011-01-01</p> <p>Systems and methods for sensing <span class="hlt">air</span> includes at least one, and in some embodiments three, transceivers for projecting the laser energy as laser radiation to the <span class="hlt">air</span>. The transceivers are scanned or aligned along several different axes. Each transceiver receives laser energy as it is backscattered from the <span class="hlt">air</span>. A computer processes signals from the transceivers to distinguish molecular scattered laser radiation from aerosol scattered laser radiation and determines <span class="hlt">air</span> temperatures, <span class="hlt">wind</span> speeds, and <span class="hlt">wind</span> directions based on the scattered laser radiation. Applications of the system to <span class="hlt">wind</span> power site evaluation, <span class="hlt">wind</span> turbine control, traffic safety, general meteorological monitoring and airport safety are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920007996','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920007996"><span>Results of the space shuttle vehicle ascent <span class="hlt">air</span> data system probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic <span class="hlt">wind</span> tunnel (IA-310), volume 2</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Collette, J. G. R.</p> <p>1991-01-01</p> <p>A recalibration of the Space Shuttle Vehicle Ascent <span class="hlt">Air</span> Data System probe was conducted in the Arnold Engineering and Development Center (AEDC) transonic <span class="hlt">wind</span> tunnel. The purpose was to improve on the accuracy of the previous calibration in order to reduce the existing uncertainties in the system. A probe tip attached to a 0.07-scale External Tank Forebody model was tested at angles of attack of -8 to +4 degrees and sideslip angles of -4 to +4 degrees. High precision instrumentation was used to acquire <span class="hlt">pressure</span> data at discrete Mach numbers ranging from 0.6 to 1.55. <span class="hlt">Pressure</span> coefficient uncertainties were estimated at less than 0.0020. Additional information is given in tabular form.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920007949','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920007949"><span>Results of the space shuttle vehicle ascent <span class="hlt">air</span> data system probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic <span class="hlt">wind</span> tunnel (IA-310), volume 1</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Collette, J. G. R.</p> <p>1991-01-01</p> <p>A recalibration of the Space Shuttle Vehicle Ascent <span class="hlt">Air</span> Data System probe was conducted in the Arnold Engineering Development Center (AEDC) transonic <span class="hlt">wind</span> tunnel. The purpose was to improve on the accuracy of the previous calibration in order to reduce the existing uncertainties in the system. A probe tip attached to a 0.07-scale External Tank Forebody model was tested at angles of attack of -8 to +4 degrees and sideslip angles of -4 to +4 degrees. High precision instrumentation was used to acquire <span class="hlt">pressure</span> data at discrete Mach numbers ranging from 0.6 to 1.55. <span class="hlt">Pressure</span> coefficient uncertainties were estimated at less than 0.0020. Data is given in graphical and tabular form.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130011132','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130011132"><span>Analysis of an Aircraft Honeycomb Sandwich Panel with Circular Face Sheet/Core Disbond Subjected to Ground-<span class="hlt">Air</span> <span class="hlt">Pressurization</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rinker, Martin; Krueger, Ronald; Ratcliffe, James</p> <p>2013-01-01</p> <p>The ground-<span class="hlt">air</span> <span class="hlt">pressurization</span> of lightweight honeycomb sandwich structures caused by alternating <span class="hlt">pressure</span> differences between the enclosed <span class="hlt">air</span> within the honeycomb core and the ambient environment is a well-known and controllable loading condition of aerospace structures. However, initial face sheet/core disbonds intensify the face sheet peeling effect of the internal <span class="hlt">pressure</span> load significantly and can decrease the reliability of the sandwich structure drastically. Within this paper, a numerical parameter study was carried out to investigate the criticality of initial disbonds in honeycomb sandwich structures under ground-<span class="hlt">air</span> <span class="hlt">pressurization</span>. A fracture mechanics approach was used to evaluate the loading at the disbond front. In this case, the strain energy release rate was computed via the Virtual Crack Closure Technique. Special attention was paid to the <span class="hlt">pressure</span>-deformation coupling which can decrease the <span class="hlt">pressure</span> load within the disbonded sandwich section significantly when the structure is highly deformed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160005934','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160005934"><span>Time Accurate Unsteady <span class="hlt">Pressure</span> Loads Simulated for the Space Launch System at a <span class="hlt">Wind</span> Tunnel Condition</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Alter, Stephen J.; Brauckmann, Gregory J.; Kleb, Bil; Streett, Craig L; Glass, Christopher E.; Schuster, David M.</p> <p>2015-01-01</p> <p>Using the Fully Unstructured Three-Dimensional (FUN3D) computational fluid dynamics code, an unsteady, time-accurate flow field about a Space Launch System configuration was simulated at a transonic <span class="hlt">wind</span> tunnel condition (Mach = 0.9). Delayed detached eddy simulation combined with Reynolds Averaged Naiver-Stokes and a Spallart-Almaras turbulence model were employed for the simulation. Second order accurate time evolution scheme was used to simulate the flow field, with a minimum of 0.2 seconds of simulated time to as much as 1.4 seconds. Data was collected at 480 <span class="hlt">pressure</span> taps at locations, 139 of which matched a 3% <span class="hlt">wind</span> tunnel model, tested in the Transonic Dynamic Tunnel (TDT) facility at NASA Langley Research Center. Comparisons between computation and experiment showed agreement within 5% in terms of location for peak RMS levels, and 20% for frequency and magnitude of power spectral densities. Grid resolution and time step sensitivity studies were performed to identify methods for improved accuracy comparisons to <span class="hlt">wind</span> tunnel data. With limited computational resources, accurate trends for reduced vibratory loads on the vehicle were observed. Exploratory methods such as determining minimized computed errors based on CFL number and sub-iterations, as well as evaluating frequency content of the unsteady <span class="hlt">pressures</span> and evaluation of oscillatory shock structures were used in this study to enhance computational efficiency and solution accuracy. These techniques enabled development of a set of best practices, for the evaluation of future flight vehicle designs in terms of vibratory loads.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006AtmRe..80..263C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006AtmRe..80..263C"><span><span class="hlt">Air</span> flow analysis in the upper Río Negro Valley (Argentina)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cogliati, M. G.; Mazzeo, N. A.</p> <p>2006-06-01</p> <p>The so called Upper Río Negro Valley in Argentina is one of the most important fruit and vegetable production regions of the country. It comprises the lower valleys of the Limay and Neuquén rivers and the upper Negro river valley. Out of the 41,671 cultivated hectares, 84.6% are cultivated with fruit trees, especially apple, pear and stone fruit trees. Late frosts occurring when trees are sensitive to low temperatures have a significant impact on the regional production. This study presents an analysis of <span class="hlt">air</span> flow characteristics in the Upper Río Negro Valley and its relationship with ambient <span class="hlt">air</span> flow. To such effect, observations made when synoptic-scale weather patterns were favorable for radiative frosts (light <span class="hlt">wind</span> and clear sky) or nocturnal temperature inversion in the lower layer were used. In the Negro river valley, both <span class="hlt">wind</span> channeling and downward horizontal momentum transport from ambient <span class="hlt">wind</span> were observed; in nighttime, very light <span class="hlt">wind</span> events occurred, possibly associated with drainage <span class="hlt">winds</span> from the nearby higher levels of the barda. In the Neuquén river valley, the prevailing effect appeared to be forced channeling, consistent with the results obtained in valleys where the synoptic scale <span class="hlt">wind</span> crossed the axis of the valley. In the Limay river valley, the flow was observed to blow parallel to the longitudinal valley axis, possibly influenced by <span class="hlt">pressure</span> gradient and forced channeling.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/863741','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/863741"><span><span class="hlt">Air</span> ejector augmented compressed <span class="hlt">air</span> energy storage system</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Ahrens, Frederick W.; Kartsounes, George T.</p> <p>1980-01-01</p> <p>Energy is stored in slack demand periods by charging a plurality of underground reservoirs with <span class="hlt">air</span> to the same peak storage <span class="hlt">pressure</span>, during peak demand periods throttling the <span class="hlt">air</span> from one storage reservoir into a gas turbine system at a constant inlet <span class="hlt">pressure</span> until the <span class="hlt">air</span> <span class="hlt">pressure</span> in the reservoir falls to said constant inlet <span class="hlt">pressure</span>, thereupon permitting <span class="hlt">air</span> in a second reservoir to flow into said gas turbine system while drawing <span class="hlt">air</span> from the first reservoir through a variable geometry <span class="hlt">air</span> ejector and adjusting said variable geometry <span class="hlt">air</span> ejector, said <span class="hlt">air</span> flow being essentially at the constant inlet <span class="hlt">pressure</span> of the gas turbine system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27579835','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27579835"><span>A Preliminary Investigation of the <span class="hlt">Air</span>-Bone Gap: Changes in Intracochlear Sound <span class="hlt">Pressure</span> With <span class="hlt">Air</span>- and Bone-conducted Stimuli After Cochlear Implantation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Banakis Hartl, Renee M; Mattingly, Jameson K; Greene, Nathaniel T; Jenkins, Herman A; Cass, Stephen P; Tollin, Daniel J</p> <p>2016-10-01</p> <p>A cochlear implant electrode within the cochlea contributes to the <span class="hlt">air</span>-bone gap (ABG) component of postoperative changes in residual hearing after electrode insertion. Preservation of residual hearing after cochlear implantation has gained importance as simultaneous electric-acoustic stimulation allows for improved speech outcomes. Postoperative loss of residual hearing has previously been attributed to sensorineural changes; however, presence of increased postoperative ABG remains unexplained and could result in part from altered cochlear mechanics. Here, we sought to investigate changes to these mechanics via intracochlear <span class="hlt">pressure</span> measurements before and after electrode implantation to quantify the contribution to postoperative ABG. Human cadaveric heads were implanted with titanium fixtures for bone conduction transducers. Velocities of stapes capitulum and cochlear promontory between the two windows were measured using single-axis laser Doppler vibrometry and fiber-optic sensors measured intracochlear <span class="hlt">pressures</span> in scala vestibuli and tympani for <span class="hlt">air</span>- and bone-conducted stimuli before and after cochlear implant electrode insertion through the round window. Intracochlear <span class="hlt">pressures</span> revealed only slightly reduced responses to <span class="hlt">air</span>-conducted stimuli consistent with previous literature. No significant changes were noted to bone-conducted stimuli after implantation. Velocities of the stapes capitulum and the cochlear promontory to both stimuli were stable after electrode placement. Presence of a cochlear implant electrode causes alterations in intracochlear sound <span class="hlt">pressure</span> levels to <span class="hlt">air</span>, but not bone, conducted stimuli and helps to explain changes in residual hearing noted clinically. These results suggest the possibility of a cochlear conductive component to postoperative changes in hearing sensitivity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810016895','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810016895"><span><span class="hlt">Wind</span> loads on flat plate photovoltaic array fields</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, R. D.; Zimmerman, D. K.</p> <p>1981-01-01</p> <p>The results of an experimental analysis (boundary layer <span class="hlt">wind</span> tunnel test) of the aerodynamic forces resulting from <span class="hlt">winds</span> acting on flat plate photovoltaic arrays are presented. Local <span class="hlt">pressure</span> coefficient distributions and normal force coefficients on the arrays are shown and compared to theoretical results. Parameters that were varied when determining the aerodynamic forces included tilt angle, array separation, ground clearance, protective <span class="hlt">wind</span> barriers, and the effect of the <span class="hlt">wind</span> velocity profile. Recommended design <span class="hlt">wind</span> forces and <span class="hlt">pressures</span> are presented, which envelop the test results for <span class="hlt">winds</span> perpendicular to the array's longitudinal axis. This <span class="hlt">wind</span> direction produces the maximum <span class="hlt">wind</span> loads on the arrays except at the array edge where oblique <span class="hlt">winds</span> produce larger edge <span class="hlt">pressure</span> loads. The arrays located at the outer boundary of an array field have a protective influence on the interior arrays of the field. A significant decrease of the array <span class="hlt">wind</span> loads were recorded in the <span class="hlt">wind</span> tunnel test on array panels located behind a fence and/or interior to the array field compared to the arrays on the boundary and unprotected from the <span class="hlt">wind</span>. The magnitude of this decrease was the same whether caused by a fence or upwind arrays.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790015294&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790015294&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure"><span><span class="hlt">Air</span> <span class="hlt">pressure</span> measurement</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ballard, H. N.</p> <p>1978-01-01</p> <p>The <span class="hlt">pressure</span> measurement was made by a Model 830J Rosemont sensor which utilized the principle of a changing <span class="hlt">pressure</span> to change correspondingly the capacitance of the <span class="hlt">pressure</span> sensitive element. The sensor's range was stated to be from zero to 100 Torr (14 km); however, the sensor was not activated until an altitude of 20 km (41 Torr) was reached during the balloon ascent. The resolution of the sensor was specified by the manufacturer as infinitesimal; however, associated electronic and <span class="hlt">pressure</span> readout systems limit the resolution to .044 Torr. Thus in the vicinity of an altitude of 30 km the <span class="hlt">pressure</span> resolution corresponded to an altitude resolution of approximately 33 meters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ExFl...59...25B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ExFl...59...25B"><span>Inverse measurement of wall <span class="hlt">pressure</span> field in flexible-wall <span class="hlt">wind</span> tunnels using global wall deformation data</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Brown, Kenneth; Brown, Julian; Patil, Mayuresh; Devenport, William</p> <p>2018-02-01</p> <p>The Kevlar-wall anechoic <span class="hlt">wind</span> tunnel offers great value to the aeroacoustics research community, affording the capability to make simultaneous aeroacoustic and aerodynamic measurements. While the aeroacoustic potential of the Kevlar-wall test section is already being leveraged, the aerodynamic capability of these test sections is still to be fully realized. The flexibility of the Kevlar walls suggests the possibility that the internal test section flow may be characterized by precisely measuring small deflections of the flexible walls. Treating the Kevlar fabric walls as tensioned membranes with known pre-tension and material properties, an inverse stress problem arises where the <span class="hlt">pressure</span> distribution over the wall is sought as a function of the measured wall deflection. Experimental wall deformations produced by the <span class="hlt">wind</span> loading of an airfoil model are measured using digital image correlation and subsequently projected onto polynomial basis functions which have been formulated to mitigate the impact of measurement noise based on a finite-element study. Inserting analytic derivatives of the basis functions into the equilibrium relations for a membrane, full-field <span class="hlt">pressure</span> distributions across the Kevlar walls are computed. These inversely calculated <span class="hlt">pressures</span>, after being validated against an independent measurement technique, can then be integrated along the length of the test section to give the sectional lift of the airfoil. Notably, these first-time results are achieved with a non-contact technique and in an anechoic environment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740008684','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740008684"><span><span class="hlt">Wind</span> machines. [aerodynamics of sailwing vehicles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lissaman, P. B. S.</p> <p>1973-01-01</p> <p>The basic elements of the <span class="hlt">air</span>/water momentum exchange are described by the environment, the potential, the <span class="hlt">air</span> and water subsystems, the total system, and the rule. Many of these topics have direct analogues in aerogenerator design. Aspects of optimal sail design and of waveless hulls are briefly outlined. A <span class="hlt">wind</span> driven vehicle capable of moving directly downwind faster than the <span class="hlt">wind</span>, is reported. The lecture is illustrated with slides and movie clips showing surfing catamarans, land and water versions of the Bauer vehicle, hang gliding, land sailing, and <span class="hlt">wind</span> surfing.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/5563892-horizontal-wind-powered-reaction-turbine-electrical-generator','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/5563892-horizontal-wind-powered-reaction-turbine-electrical-generator"><span>Horizontal <span class="hlt">wind</span> powered reaction turbine electrical generator</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>de Geus, A.M.</p> <p>1980-05-27</p> <p>A horizontal <span class="hlt">wind</span> powered electrical generator is disclosed in which a horizontal reaction turbine is disposed within an augmentor cowling which extends downwind of the turbine. First stage curved stator blades interconnect the augmentor with the turbine cowling, and secondary stator blades are spaced downwind from said primary stator blades to extend inwardly from the augmentor to terminate short of the turbine cowling. These secondary stator blades have a greater angle of departure than the primary stator blades to increase the rotational velocity of the <span class="hlt">air</span> at the expense of its axial velocity while permitting the axial velocity of themore » <span class="hlt">air</span> moving inwardly of the secondary stator blades to be undiminished. A venturi-structured diffusor is carried by said augmentor in a downwind position to lower the <span class="hlt">pressure</span> generally and assist the action of the secondary stator blades.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MeScT..29f4002S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MeScT..29f4002S"><span>Measurement of the refractive index of <span class="hlt">air</span> in a low-<span class="hlt">pressure</span> regime and the applicability of traditional empirical formulae</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schödel, René; Walkov, Alexander; Voigt, Michael; Bartl, Guido</p> <p>2018-06-01</p> <p>The refractive index of <span class="hlt">air</span> is a major limiting factor in length measurements by interferometry, which are mostly performed under atmospheric conditions. Therefore, especially in the last century, measurement and description of the <span class="hlt">air</span> refractive index was a key point in order to achieve accuracy in the realisation of the length by interferometry. Nevertheless, interferometric length measurements performed in vacuum are much more accurate since the wavelength of the light is not affected by the <span class="hlt">air</span> refractive index. However, compared with thermal conditions in <span class="hlt">air</span>, in high vacuum heat conduction is missing. In such a situation, dependent on the radiative thermal equilibrium, a temperature distribution can be very inhomogeneous. Using a so-called contact gas instead of high vacuum is a very effective way to enable heat conduction on nearly the same level as under atmospheric <span class="hlt">pressure</span> conditions whereby keeping the effect of the <span class="hlt">air</span> refractive index on a small level. As physics predicts, and as we have demonstrated previously, helium seems like the optimal contact gas because of its large heat conduction and its refractive index that can be calculated from precisely known parameters. On the other hand, helium gas situated in a vacuum chamber could easily be contaminated, e.g. by <span class="hlt">air</span> leakage from outside. Above the boiling point of oxygen (‑183 °C) it is therefore beneficial to use dry <span class="hlt">air</span> as a contact gas. In such an approach, the <span class="hlt">air</span> refractive index could be calculated based on measured quantities for <span class="hlt">pressure</span> and temperature. However, existing formulas for the <span class="hlt">air</span> refractive index are not valid in the low-<span class="hlt">pressure</span> regime. Although it seems reasonable that the refractivity (n  ‑  1) of dry <span class="hlt">air</span> simply downscales with the <span class="hlt">pressure</span>, to our knowledge there is no experimental evidence for the applicability of any empirical formula. This evidence is given in the present paper which reports on highly accurate measurements of the <span class="hlt">air</span> refractive index for the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4704731','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4704731"><span>Effect of Different Levels of <span class="hlt">Pressure</span> Relieving <span class="hlt">Air</span>-Mattress Firmness on Cough Strength</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Kamikawa, Norimichi; Taito, Shunsuke; Takahashi, Makoto; Sekikawa, Kiyokazu; Hamada, Hironobu</p> <p>2016-01-01</p> <p>Cough is an important host-defense mechanism. The elderly and patients who are severely ill cannot cough effectively when lying in the supine position. Furthermore, <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattresses are recommended for preventing the development of <span class="hlt">pressure</span> ulcers. In this study, we clarified whether or not the cough peak flow (CPF), an index of cough strength, is affected by different firmness levels of a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress in healthy volunteers in the supine position. Fifty-two healthy young men participated. All the measurements were carried out on each participant in the supine position on a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress. The participants were assessed at two firmness levels, a “hard” and “soft” mode. The CPF, forced vital capacity (FVC), maximal expiratory <span class="hlt">pressure</span> (PEmax), and maximal inspiratory <span class="hlt">pressure</span> (PImax) were determined for each mode. The sinking distance of the body into the mattress was measured without any activity and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax, and PImax were determined for each mode. The sinking distance of the body into the mattress was measured and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax and PImax values of the participants coughing on the mattress were significantly lower when the mattress was in “soft” than in “hard” mode. The differences between the sinking distances of the mattress in “soft” and “hard” modes were larger for the anterior superior iliac spine. A harder mattress may lead to increased CPF in healthy young men lying in the supine position, and increased CPF may be important for host defense. PMID:26741497</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910008196','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910008196"><span>Interpretation of combined <span class="hlt">wind</span> profiler and aircraft-measured tropospheric <span class="hlt">winds</span> and clear <span class="hlt">air</span> turbulence</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Thomson, D. W.; Syrett, William J.; Fairall, C. W.</p> <p>1991-01-01</p> <p>In the first experiment, it was found that <span class="hlt">wind</span> profilers are far better suited for the detailed examination of jet stream structure than are weather balloons. The combination of good vertical resolution with not previously obtained temporal resolution reveals structural details not seen before. Development of probability-derived shear values appears possible. A good correlation between pilot reports of turbulence and <span class="hlt">wind</span> shear was found. In the second experiment, hourly measurements of <span class="hlt">wind</span> speed and direction obtained using two <span class="hlt">wind</span> profiling Doppler radars during two prolonged jet stream occurrences over western Pennsylvania were analyzed. In particular, the time-variant characteristics of derived shear profiles were examined. Profiler data dropouts were studied in an attempt to determine possible reasons for the apparently reduced performance of profiling radar operating beneath a jet stream. Richardson number and <span class="hlt">wind</span> shear statistics were examined along with pilot reports of turbulence in the vicinity of the profiler.</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. Their policies may differ from this site.</div> </div><!-- container --> <footer><a id="backToTop" href="#top"> </a><nav><a id="backToTop" href="#top"> </a><ul class="links"><a id="backToTop" href="#top"> </a><li><a id="backToTop" href="#top"></a><a href="/sitemap.html">Site Map</a></li> <li><a href="/members/index.html">Members Only</a></li> <li><a href="/website-policies.html">Website Policies</a></li> <li><a href="https://doe.responsibledisclosure.com/hc/en-us" target="_blank">Vulnerability Disclosure Program</a></li> <li><a href="/contact.html">Contact Us</a></li> </ul> <div class="small">Science.gov is maintained by the U.S. Department of Energy's <a href="https://www.osti.gov/" target="_blank">Office of Scientific and Technical Information</a>, in partnership with <a href="https://www.cendi.gov/" target="_blank">CENDI</a>.</div> </nav> </footer> <script type="text/javascript"><!-- // var lastDiv = ""; function showDiv(divName) { // hide last div if (lastDiv) { document.getElementById(lastDiv).className = "hiddenDiv"; } //if value of the box is not nothing and an object with that name exists, then change the class if (divName && document.getElementById(divName)) { document.getElementById(divName).className = "visibleDiv"; lastDiv = divName; } } //--> </script> <script> /** * Function that tracks a click on an outbound link in Google Analytics. * This function takes a valid URL string as an argument, and uses that URL string * as the event label. */ var trackOutboundLink = function(url,collectionCode) { try { h = window.open(url); setTimeout(function() { ga('send', 'event', 'topic-page-click-through', collectionCode, url); }, 1000); } catch(err){} }; </script> <!-- Google Analytics --> <script> (function(i,s,o,g,r,a,m){i['GoogleAnalyticsObject']=r;i[r]=i[r]||function(){ (i[r].q=i[r].q||[]).push(arguments)},i[r].l=1*new Date();a=s.createElement(o), m=s.getElementsByTagName(o)[0];a.async=1;a.src=g;m.parentNode.insertBefore(a,m) })(window,document,'script','//www.google-analytics.com/analytics.js','ga'); ga('create', 'UA-1122789-34', 'auto'); ga('send', 'pageview'); </script> <!-- End Google Analytics --> <script> showDiv('page_1') </script> </body> </html>