NASA Technical Reports Server (NTRS)
Panda, P. C.; Ruoff, A. L.
1979-01-01
A sensitive microprofilometer was used to determine the onset of yielding in the anvils of a supported opposed anvil device for the case of 3% cobalt-cemented tungsten carbide as the anvil material. In addition, it is shown how the commencement of yielding in boron carbide pistons, the yield strength being known, can be used to obtain the transition pressure to a conducting phase in gallium phosphide. The transition pressures of bismuth and gallium phosphide are obtained and it is found that these transitions are extremely close to the maximum attainable pressure in, respectively, a maraging steel and a 3% cobalt-cemented tungsten carbide.
Bulanov, S. S.; Esarey, E.; Schroeder, C. B.; ...
2015-03-13
Radiation Pressure Acceleration is a highly efficient mechanism of laser driven ion acceleration, with the laser energy almost totally transferrable to the ions in the relativistic regime. There is a fundamental limit on the maximum attainable ion energy, which is determined by the group velocity of the laser. In the case of a tightly focused laser pulses, which are utilized to get the highest intensity, another factor limiting the maximum ion energy comes into play, the transverse expansion of the target. Transverse expansion makes the target transparent for radiation, thus reducing the effectiveness of acceleration. Utilization of an external guidingmore » structure for the accelerating laser pulse may provide a way of compensating for the group velocity and transverse expansion effects.« less
Goozée, Justine V; Murdoch, Bruce E; Theodoros, Deborah G
2002-01-01
A miniature pressure transducer was used to assess the interlabial contact pressures produced by a group of 19 adults (mean age 30.6 years) with dysarthria following severe traumatic brain injury (TBI) during a set of speech and nonspeech tasks. Ten parameters relating to lip strength, endurance, rate of movement and lip pressure accuracy and stability were measured from the nonspeech tasks. The results attained by the TBI group were compared against a group of 19 age- and sex-matched control subjects. Significant differences between the groups were found for maximum interlabial contact pressure, maximum rate of repetition of maximum pressure, and lip pressure accuracy at 50 and 10% levels of maximum pressure. In regards to speech, the interlabial contact pressures generated by the TBI group and control group did not differ significantly. When expressed as percentages of maximum pressure, however, the TBI group's interlabial pressures appeared to have been generated with greater physiological effort. Copyright 2002 S. Karger AG, Basel
The Gaseous Explosive Reaction at Constant Pressure : Further Data on the Effect of Inert Gases
NASA Technical Reports Server (NTRS)
Stevens, F W
1932-01-01
An investigation of gaseous explosive reactions is discussed in this report. Measurements were taken to calculate the maximum flame temperature attained and making correlations with existing thermal data on this reaction.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Laurinat, J.; Kesterson, M.; Hensel, S.
The documented safety analysis for the Savannah River Site evaluates the consequences of a postulated 1000 °C fire in a glovebox. The radiological dose consequences for a pressurized release of plutonium oxide powder during such a fire depend on the maximum pressure that is attained inside the oxide storage vial. To enable evaluation of the dose consequences, pressure transients and venting flow rates have been calculated for exposure of the storage vial to the fire. A standard B vial with a capacity of approximately 8 cc was selected for analysis. The analysis compares the pressurization rate from heating and evaporationmore » of moisture adsorbed onto the plutonium oxide contents of the vial with the pressure loss due to venting of gas through the threaded connection between the vial cap and body. Tabulated results from the analysis include maximum pressures, maximum venting velocities, and cumulative vial volumes vented during the first 10 minutes of the fire transient. Results are obtained for various amounts of oxide in the vial, various amounts of adsorbed moisture, different vial orientations, and different surface fire exposures.« less
Light-scattering study of the glass transition in lubricants
NASA Technical Reports Server (NTRS)
Alsaad, M. A.; Winer, W. O.; Medina, F. D.; Oshea, D. C.
1977-01-01
The sound velocity of four lubricants has been measured as a function of temperature and pressure using Brillouin scattering. A change in slope of the velocity as a function of temperature or pressure allowed the determination of the glass transition temperature and pressure. The glass transition data were used to construct a phase diagram for each lubricant. The data indicate that the glass transition temperature increased with pressure at a rate which ranged from 120 to 200 C/GPa. The maximum pressure attained was 0.69 GPa and the temperature range was from 25 to 100 C.
Radiation pressure acceleration: The factors limiting maximum attainable ion energy
Bulanov, S. S.; Esarey, E.; Schroeder, C. B.; ...
2016-04-15
Radiation pressure acceleration (RPA) is a highly efficient mechanism of laser-driven ion acceleration, with near complete transfer of the laser energy to the ions in the relativistic regime. However, there is a fundamental limit on the maximum attainable ion energy, which is determined by the group velocity of the laser. The tightly focused laser pulses have group velocities smaller than the vacuum light speed, and, since they offer the high intensity needed for the RPA regime, it is plausible that group velocity effects would manifest themselves in the experiments involving tightly focused pulses and thin foils. However, in this case,more » finite spot size effects are important, and another limiting factor, the transverse expansion of the target, may dominate over the group velocity effect. As the laser pulse diffracts after passing the focus, the target expands accordingly due to the transverse intensity profile of the laser. Due to this expansion, the areal density of the target decreases, making it transparent for radiation and effectively terminating the acceleration. The off-normal incidence of the laser on the target, due either to the experimental setup, or to the deformation of the target, will also lead to establishing a limit on maximum ion energy.« less
Advanced cooling techniques for high-pressure hydrocarbon-fueled engines
NASA Technical Reports Server (NTRS)
Cook, R. T.
1979-01-01
The regenerative cooling limits (maximum chamber pressure) for 02/hydrocarbon gas generator and staged combustion cycle rocket engines over a thrust range of 89,000 N (20,000lbf) to 2,669,000 N (600,000 lbf) for a reusable life of 250 missions were defined. Maximum chamber pressure limits were first determined for the three propellant combinations (O2/CH4, O2/C3H8, and O2/RP-1 without a carbon layer (unenhanced designs). Chamber pressure cooling enhancement limits were then established for seven thermal barriers. The thermal barriers evaluated for these designs were: carbon layer, ceramic coating, graphite liner, film cooling, transpiration cooling, zoned combustion, and a combination of two of the above. All fluid barriers were assessed a 3 percent performance loss. Sensitivity studies were then conducted to determine the influence of cycle life and RP-1 decomposition temperature on chamber pressure limits. Chamber and nozzle design parameters are presented for the unenahanced and enhanced designs. The maximum regenerative cooled chamber pressure limits were attained with the O2/CH4 propellant combination. The O2/RP-1 designs relied on a carbon layer and liquid gas injection chamber contours, short chamber, to be competitive with the other two propellant combinations. This was attributed to the low decomposition temperature of RP-1.
Two-dimensional unsteady lift problems in supersonic flight
NASA Technical Reports Server (NTRS)
Heaslet, Max A; Lomax, Harvard
1949-01-01
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either experiencing a sudden angle-of-attack change or entering a sharp-edge gust. From these pressure distributions the indicial lift functions applicable to unsteady lift problems are determined for two cases. Results are presented which permit the determination of maximum increment in lift coefficient attained by an unrestrained airfoil during its flight through a gust. As an application of these results, the minimum altitude for safe flight through a specific gust is calculated for a particular supersonic wing of given strength and wing loading.
Anderson, Robert C.
1976-06-22
1. A method for joining beryllium to beryllium by diffusion bonding, comprising the steps of coating at least one surface portion of at least two beryllium pieces with nickel, positioning a coated surface portion in a contiguous relationship with an other surface portion, subjecting the contiguously disposed surface portions to an environment having an atmosphere at a pressure lower than ambient pressure, applying a force upon the beryllium pieces for causing the contiguous surface portions to abut against each other, heating the contiguous surface portions to a maximum temperature less than the melting temperature of the beryllium, substantially uniformly decreasing the applied force while increasing the temperature after attaining a temperature substantially above room temperature, and maintaining a portion of the applied force at a temperature corresponding to about maximum temperature for a duration sufficient to effect the diffusion bond between the contiguous surface portions.
Jet plume injection and combustion system for internal combustion engines
Oppenheim, A.K.; Maxson, J.A.; Hensinger, D.M.
1993-12-21
An improved combustion system for an internal combustion engine is disclosed wherein a rich air/fuel mixture is furnished at high pressure to one or more jet plume generator cavities adjacent to a cylinder and then injected through one or more orifices from the cavities into the head space of the cylinder to form one or more turbulent jet plumes in the head space of the cylinder prior to ignition of the rich air/fuel mixture in the cavity of the jet plume generator. The portion of the rich air/fuel mixture remaining in the cavity of the generator is then ignited to provide a secondary jet, comprising incomplete combustion products which are injected into the cylinder to initiate combustion in the already formed turbulent jet plume. Formation of the turbulent jet plume in the head space of the cylinder prior to ignition has been found to yield a higher maximum combustion pressure in the cylinder, as well as shortening the time period to attain such a maximum pressure. 24 figures.
Jet plume injection and combustion system for internal combustion engines
Oppenheim, Antoni K.; Maxson, James A.; Hensinger, David M.
1993-01-01
An improved combustion system for an internal combustion engine is disclosed wherein a rich air/fuel mixture is furnished at high pressure to one or more jet plume generator cavities adjacent to a cylinder and then injected through one or more orifices from the cavities into the head space of the cylinder to form one or more turbulent jet plumes in the head space of the cylinder prior to ignition of the rich air/fuel mixture in the cavity of the jet plume generator. The portion of the rich air/fuel mixture remaining in the cavity of the generator is then ignited to provide a secondary jet, comprising incomplete combustion products which are injected into the cylinder to initiate combustion in the already formed turbulent jet plume. Formation of the turbulent jet plume in the head space of the cylinder prior to ignition has been found to yield a higher maximum combustion pressure in the cylinder, as well as shortening the time period to attain such a maximum pressure.
Preliminary tests of an advanced high-temperature combustion system
NASA Technical Reports Server (NTRS)
Wear, J. D.; Trout, A. M.; Smith, J. M.; Jacobs, R. E.
1983-01-01
A combustion system has been developed to operate efficiently and with good durability at inlet pressures to 4.05 MPa (40 atm), inlet air temperatures to 900 K, and exhaust gas temperatures to 2480 K. A preliminary investigation of this system was conducted at inlet pressures to 0.94 MPa (9 atm), a nominal inlet air temperature of 560 K, and exhaust gas temperatures to 2135 K. A maximum combustion efficiency of 98.5 percent was attained at a fuel-air ratio of 0.033; the combustion efficiency decreased to about 90 percent as the fuel-air ratio was increased to 0.058. An average liner metal temperature of 915 K, 355 kelvins greater than the nominal inlet air temperature, was reached with an average exhaust gas temperature of 2090 K. The maximum local metal temperature at this condition was about 565 kelvins above the nominal inlet air temperature and decreased to 505 kelvins above with increasing combustor pressure. Tests to determine the isothermal total pressure loss of the combustor showed a liner loss of 1.1 percent and a system loss of 6.5 percent.
Design and test of three active flutter suppression controllers
NASA Technical Reports Server (NTRS)
Christhilf, David M.; Waszak, Martin R.; Adams, William M.; Srinathkumar, S.; Mukhopadhyay, Vivek
1991-01-01
Three flutter suppression control law design techniques are presented. Each uses multiple control surfaces and/or sensors. The first uses linear combinations of several accelerometer signals together with dynamic compensation to synthesize the modal rate of the critical mode for feedback to distributed control surfaces. The second uses traditional tools (pole/zero loci and Nyquist diagrams) to develop a good understanding of the flutter mechanism and produce a controller with minimal complexity and good robustness to plant uncertainty. The third starts with a minimum energy Linear Quadratic Gaussian controller, applies controller order reduction, and then modifies weight and noise covariance matrices to improve multi-variable robustness. The resulting designs were implemented digitally and tested subsonically on the Active Flexible Wing (AFW) wind tunnel model. Test results presented here include plant characteristics, maximum attained closed-loop dynamic pressure, and Root Mean Square control surface activity. A key result is that simultaneous symmetric and antisymmetric flutter suppression was achieved by the second control law, with a 24 percent increase in attainable dynamic pressure.
Gafoor, V Abdul; Smita, B; Jose, James
2017-01-01
Idiopathic intracranial hypertension (IIH) is increased intracranial pressure (ICP) with normal cerebrospinal fluid (CSF) contents, in the absence of an intracranial mass, hydrocephalus, or other identifiable causes. The current knowledge of the treatment outcome of IIH is limited, and the data on the natural history of this entity are scant. The objective of the study is to study the treatment response of IIH by serially measuring the CSF opening pressure and to delineate the factors influencing the same. A prospective observational study in a cohort of fifty patients with IIH in whom CSF opening pressure was serially measured at pre-specified intervals. The mean CSF opening pressure at baseline was 302.4 ± 51.69 mm of H 2 O (range: 220-410). Even though a higher body mass index (BMI) showed a trend toward a higher CSF opening pressure, the association was not significant ( P = 0.168). However, the age of the patient had a significant negative correlation with the CSF pressure ( P = 0.006). The maximum reduction in CSF pressure occurred in the first 3 months of treatment, and thereafter it plateaued. Remission was attained in 12 (24%) patients. BMI had the strongest association with remission ( P = 0.001). In patients with IIH, treatment response is strongly related to BMI. However, patients with normal BMI are also shown to relapse and hence should have continuous, long-term follow-up. The reduction in CSF pressure attained in the first 3 months could reflect the long-term response to treatment.
Schmid, A; Kollmer, A; Mathys, R G; Witholt, B
1998-08-01
Many pseudomonads and other bacteria can grow on aliphatic and aromatic hydrocarbons that occur in the environment. We are examining the potential of such organisms as biocatalysts for the oxidation of a variety of substituted aliphatic and aromatic compounds. To attain a high production rate of oxidation products via such biotransformations, we have focused on two-liquid phase culture systems. In these systems, cells are grown in liquid media consisting of an aqueous phase containing water-soluble growth substrates and droplets of a water-immicible organic solvent containing bioconversion substrates and products. For industrial applications of such two-liquid phase processes, several questions remain. What are the maximum rates at which apolar compounds can be transferred from the apolar phase to cells growing in the aqueous phase, i.e., what are the maximum space-time yields attainable in two-liquid phase fermentations under practical conditions? What does an efficient downstream processing of two-liquid phase medium involve? What safety regimes should be considered in working with flammable organic solvents? Can elevated pressure be used to increase oxygen transfer? Based on answers to these questions, we have recently developed a high-pressure, explosion-proof bioreactor system with Bioengineering AG (Wald, Switzerland), which will be installed in our pilot plant and used to explore two-liquid phase bioconversions at a pilot scale.
Abandoned coal mine stores gas for Colorado peak-day demands
DOE Office of Scientific and Technical Information (OSTI.GOV)
Brown, L.W.
1978-09-01
Since 1961, the Leyden Mine, from which 6 million tons of coal had been removed to leave a 150 million cu ft void, has been used for gas storage at 250 psig max pressure, after the hoisting and ventilation shafts had been sealed with concrete, rock, sand, and mud. Following several withdrawal expansions, a design for maximum delivery of 230 million cu ft/day for five days with a pressure drop in the cavern down to 100 psig was developed to satisfy customer requirements for peak shaving. This required redesigning the gathering system by looping large existing lines, eliminating inefficient ones,more » and drilling additional wells; installing three lightweight 3500-hp Centaur turbine/compressor units from Solar Turbines International to provide the minimum 200 psig compressor discharge pressure needed for gas distribution on peak usage days; and installing Donaldson Co. engine air-inlet silencers on the turbine inlets to reduce noise levels below the public code requirement. In the 1977-78 heating season, the Leyden facility produced 196 million cu ft/day of gas; with continued load growth and well drilling to reduce pressure loss, the maximum design flow rate will be attained.« less
Velisavljevic, N.; Sinogeikin, S.; Saavedra, R.; ...
2014-05-07
Here, we have designed a portable pressure controller module to tune compression rates and maximum pressures attainable in a standard gas-membrane diamond anvil cell (DAC). During preliminary experiments, performed on zirconium (Zr) metal sample, pressure jumps of up to 80 GPa were systematically obtained in less than 0.2s (resulting in compression rate of few GPa/s up to more than 400 GPa/s). In-situ x-ray diffraction and electrical resistance measurements were performed simultaneously during this rapid pressure increase to provide the first time resolved data on α → ω → β structural evolution in Zr at high pressures. Direct control of compressionmore » rates and peak pressures, which can be held for prolonged time, allows for investigation of structural evolution and kinetics of structural phase transitions of materials under previously unexplored compression rate-pressure conditions that bridge traditional static and shock/dynamic experimental platforms.« less
NASA Technical Reports Server (NTRS)
Hasan, Mohammad M.; Balasubramaniam, R.
2012-01-01
Experiments performed with Freon 113 in the space shuttle have shown that in a pro- cess of very slow heating, high liquid superheats can be sustained for a long period in microgravity. In a closed system explosive vaporization of superheated liquid resulted in pressure spikes of varying magnitudes. In this paper, we analyze the pressure rise in a partially lled closed tank in which a large vapor bubble (i.e., ullage) is initially present, and the liquid is subjected to a low wall heat ux. The liquid layer adjacent to the wall becomes superheated until the temperature for nucleation of the bubbles (or the incipience of boiling) is achieved. In the absence of the gravity-induced convection large quantities of superheated liquid can accumulate over time near the heated surface. Once the incipience temperature is attained, explosive boiling occurs and the vapor bubbles that are produced on the heater surface tend to quickly raise the tank pressure. The liquid-vapor saturation temperature increases as well. These two e ects tend to induce condensation of the large ullage bubble that is initially present, and tends to mitigate the tank pressure rise. As a result, the tank pressure is predicted to rise sharply, attain a maximum, and subsequently decay slowly. The predicted pressure rise is compared with experimental results obtained in the microgravity environments of the space shuttle for Freon 113. The analysis is appli- cable, in general to heating of liquid in closed containers in microgravity and to cryogenic fuel tanks, in particular where small heat leaks into the tank are unavoidable.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Trifonov, Y.I.; Legin, E.K.; Suglobov, D.N.
1986-03-01
The authors find that the solubility of di-2-ethylhexyl phosphates rises considerably under the influence of gaseous ammonia on the solvent-LnA/sub 3/ system when a mixture of octane and octanol is used as solvent. The dissolving power of ammonia rises with alcohol concentration and attains the maximum at an alcohol content of ca 20 vol. %. An equation is presented that describes the dependence of the LnA/sub 3/ solubility on the partial amonia pressure.
Prediction of blood pressure and blood flow in stenosed renal arteries using CFD
NASA Astrophysics Data System (ADS)
Jhunjhunwala, Pooja; Padole, P. M.; Thombre, S. B.; Sane, Atul
2018-04-01
In the present work an attempt is made to develop a diagnostive tool for renal artery stenosis (RAS) which is inexpensive and in-vitro. To analyse the effects of increase in the degree of severity of stenosis on hypertension and blood flow, haemodynamic parameters are studied by performing numerical simulations. A total of 16 stenosed models with varying degree of stenosis severity from 0-97.11% are assessed numerically. Blood is modelled as a shear-thinning, non-Newtonian fluid using the Carreau model. Computational Fluid Dynamics (CFD) analysis is carried out to compute the values of flow parameters like maximum velocity and maximum pressure attained by blood due to stenosis under pulsatile flow. These values are further used to compute the increase in blood pressure and decrease in available blood flow to kidney. The computed available blood flow and secondary hypertension for varying extent of stenosis are mapped by curve fitting technique using MATLAB and a mathematical model is developed. Based on these mathematical models, a quantification tool is developed for tentative prediction of probable availability of blood flow to the kidney and severity of stenosis if secondary hypertension is known.
NASA Astrophysics Data System (ADS)
Pathak, Vishwa Bandhu; Tripathi, V. K.
2007-02-01
Nonlinear electromagnetic eigenmodes of collisional and collisionless plasmas, when the temporal extent of the modes is longer than the ambipolar diffusion time, have been investigated. The nonlinearity in a collisionless plasma arises through ponderomotive force, whereas in collisional plasmas Ohmic nonlinearity prevails. The mode structure in both cases, representing a balance between the nonlinearity-induced self-convergence and diffraction-induced divergence, closely resembles Gaussian form. The spot size of the mode decreases with the increasing axial amplitude of the laser, attains a minimum, and then rises very gradually. The modes are susceptible to stimulated Brillouin backscattering. The growth rate of the Brillouin process initially increases with mode amplitude, attains a maximum, and then decreases. The reduction in the growth rate is caused by strong electron evacuation from the axial region by the ponderomotive force and thermal pressure gradient force created by nonuniform Ohmic heating.
Subsystem Analysis/Optimization for the X-34 Main Propulsion System
NASA Technical Reports Server (NTRS)
McDonald, J. P.; Hedayat, A.; Brown, T. M.; Knight, K. C.; Champion, R. H., Jr.
1998-01-01
The Orbital Sciences Corporation X-34 vehicle demonstrates technologies and operations key to future reusable launch vehicles. The general flight performance goal of this unmanned rocket plane is Mach 8 flight at an altitude of 250,000 feet. The Main Propulsion System (MPS) supplies liquid propellants to the main engine, which provides the primary thrust for attaining mission goals. Major MPS design and operational goals are aircraft-like ground operations, quick turnaround between missions, and low initial/operational costs. Analyses related to optimal MPS subsystem design are reviewed in this paper. A pressurization system trade weighs maintenance/reliability concerns against those for safety in a comparison of designs using pressure regulators versus orifices to control pressurant flow. A propellant dump/feed system analysis weighs the issues of maximum allowable vehicle landing weight, trajectory, and MPS complexity to arrive at a final configuration for propellant dump/feed systems.
Interaction of air shock waves and porous compressible materials
NASA Astrophysics Data System (ADS)
Gvozdeva, L. G.; Faresov, Yu. M.; Fokeyev, V. P.
1986-05-01
Interaction of air shock waves and porous compressible materials was studied in an experiment with two foam-plastic materials: PPU-3M-1 polyurethane (density 33 kg/cu m) and much more rigid PKhV-1 polyvinyl chloride (density 50 kg/cu m). Tests were performed in a shock tube with 0.1x0.1 m square cross-section, a single diaphragm separating its 8 m long low-pressure segment with inspection zone and 1.5 m long high-pressure segment. The instrumentation included an array of piezoelectric pressure transducers and a digital frequency meter for velocity measurements, a Tectronix 451A oscillograph, and IAB-451 shadowgraph, and a ZhFR camera with slit scanning. Air was used as compressing gas, its initial pressure being varied from 10(3) Pa to 10(5) Pa, helium and nitrogen were used as propelling gas. The impact velocity of shock waves was varied over the N(M) = 2-5 range of the Mach number. The maximum amplitude of the pressure pulse increased as the thickness of the foam layer was increased up to 80 mm and then remained constant with further increases of that thickness, at a level depending on the material and on the intitial conditions. A maximum pressure rise by a factor of approximately 10 was attained, with 1.3 x 10(3) Pa initial pressure and an impact velocity N(M) = 5. Reducing the initial pressure to below (0.1-0.3) x 10(3) Pa, with the impact velocity maintained at N(M) = 5, reduced the pressure rise to a factor below 3. The results are interpreted taking into account elasticity forces in the solid skeleton phase and gas filtration through the pores.
NASA Astrophysics Data System (ADS)
Rizvi, S. Tauqeer ul Islam; Linshu, He; ur Rehman, Tawfiq; Rafique, Amer Farhan
2012-11-01
A numerical optimization study of lifting body re-entry vehicles is presented for nominal as well as shallow entry conditions for Medium and Intermediate Range applications. Due to the stringent requirement of a high degree of accuracy for conventional vehicles, lifting re-entry can be used to attain the impact at the desired terminal flight path angle and speed and thus can potentially improve accuracy of the re-entry vehicle. The re-entry of a medium range and intermediate range vehicles is characterized by very high negative flight path angle and low re-entry speed as compared to a maneuverable re-entry vehicle or a common aero vehicle intended for an intercontinental range. Highly negative flight path angles at the re-entry impose high dynamic pressure as well as heat loads on the vehicle. The trajectory studies are carried out to maximize the cross range of the re-entry vehicle while imposing a maximum dynamic pressure constraint of 350 KPa with a 3 MW/m2 heat rate limit. The maximum normal acceleration and the total heat load experienced by the vehicle at the stagnation point during the maneuver have been computed for the vehicle for possible future conceptual design studies. It has been found that cross range capability of up to 35 km can be achieved with a lifting-body design within the heat rate and the dynamic pressure boundary at normal entry conditions. For shallow entry angle of -20 degree and intermediate ranges a cross range capability of up to 250 km can be attained for a lifting body design with less than 10 percent loss in overall range. The normal acceleration also remains within limits. The lifting-body results have also been compared with wing-body results at shallow entry condition. An hp-adaptive pseudo-spectral method has been used for constrained trajectory optimization.
Flow-Field Survey in the Test Region of the SR-71 Aircraft Test Bed Configuration
NASA Technical Reports Server (NTRS)
Mizukami, Masashi; Jones, Daniel; Weinstock, Vladimir D.
2000-01-01
A flat plate and faired pod have been mounted on a NASA SR-71A aircraft for use as a supersonic flight experiment test bed. A test article can be placed on the flat plate; the pod can contain supporting systems. A series of test flights has been conducted to validate this test bed configuration. Flight speeds to a maximum of Mach 3.0 have been attained. Steady-state sideslip maneuvers to a maximum of 2 deg have been conducted, and the flow field in the test region has been surveyed. Two total-pressure rakes, each with two flow-angle probes, have been placed in the expected vicinity of an experiment. Static-pressure measurements have been made on the flat plate. At subsonic and low supersonic speeds with no sideslip, the flow in the surveyed region is quite uniform. During sideslip maneuvers, localized flow distortions impinge on the test region. Aircraft sideslip does not produce a uniform sidewash over the test region. At speeds faster than Mach 1.5, variable-pressure distortions were observed in the test region. Boundary-layer thickness on the flat plate at the rake was less than 2.1 in. For future experiments, a more focused and detailed flow-field survey than this one would be desirable.
Analysis of Surface Roughness at Overlapping Laser Shock Peening
NASA Astrophysics Data System (ADS)
Dai, F. Z.; Zhang, Z. D.; Zhou, J. Z.; Lu, J. Z.; Zhang, Y. K.
2016-02-01
The overlapping effects on surface roughness are studied when samples are treated by laser shock peening (LSP). Surface roughness of overlapped circular laser spot is calculated by ISO 25178 height parameters. The usually used overlapping styles namely isosceles-right-triangle-style (AAP) and equilateral-triangle-style (AAA) are carefully investigated when the overlapping degree in x-axis (ηx) is below 50%. Surface roughness of isosceles-right-triangle-style attains its minimum value at ηx of 29.3%, and attains its maximum value at ηx of 43.6%. Surface roughness of equilateral-triangle-style attains its minimum value at ηx of 42.3%, and attains its maximum value at ηx of 32%. Experimental results are well consistent with theoretical analysis.
A Realization of Theoretical Maximum Performance in IPSec on Gigabit Ethernet
NASA Astrophysics Data System (ADS)
Onuki, Atsushi; Takeuchi, Kiyofumi; Inada, Toru; Tokiniwa, Yasuhisa; Ushirozawa, Shinobu
This paper describes “IPSec(IP Security) VPN system" and how it attains a theoretical maximum performance on Gigabit Ethernet. The Conventional System is implemented by software. However, the system has several bottlenecks which must be overcome to realize a theoretical maximum performance on Gigabit Ethernet. Thus, we newly propose IPSec VPN System with the FPGA(Field Programmable Gate Array) based hardware architecture, which transmits a packet by the pipe-lined flow processing and has 6 parallel structure of encryption and authentication engines. We show that our system attains the theoretical maximum performance in the short packet which is difficult to realize until now.
Bravo, Diamond Y.; Umaña-Taylor, Adriana J.; Toomey, Russell B.; Updegraff, Kimberly A.; Jahromi, Laudan B.
2017-01-01
The current longitudinal study examined how Mexican-origin adolescent mothers’ (N = 204) reports of acculturative stress during late adolescence were associated with their educational attainment and engagement in risky behaviors in young adulthood, 4 years post-partum; we also examined whether this association was mediated by discrepancies between adolescents’ educational aspirations and expectations. Findings revealed that mothers’ greater reports of stress regarding English competency pressures and pressures to assimilate were associated with a larger gap between their aspirations and expectations. Mothers’ reports of greater stress from pressures against assimilation, however, were associated with a smaller gap between aspirations and expectations. As expected, a larger gap between aspirations and expectations was associated with lower educational attainment and increased engagement in risky behaviors. Finally, significant mediation emerged, suggesting that the influence of stress from English competency pressures and pressures to assimilate on young mothers’ educational attainment and engagement in risky behaviors was mediated through the aspiration–expectation gap. Findings are discussed with respect to understanding discrepancies between young mothers’ aspirations and expectations in the context of acculturative stress. PMID:29263563
Aerojet advanced engine concept
NASA Technical Reports Server (NTRS)
Schoenman, L.
1984-01-01
The future orbit transfer vehicle (OTV) requirements which dictate the need for a highly versatile, highly reliable, reusable propulsion module are discussed. To attain maximum operational economy, space-basing is essential. This requires a reusable, maintenance free engine. The design features of this space based engine are defined. A new engine cycle and its advantages allow all the maintenance goals to be attained. Rubbing contact and interpropellant seals and purges are eliminated when GO2 is used to drive the LO2 pump. The TPA design has only one moving part. The use of both GH2 and GO2 to drive the turbines lowers the turbine temperatures in addition lower GH2 temperatures and pressures improve chamber cooling and longer life. The use of GO2 as a turbine drive fluid is addressed. Space based engines require an integrated control and health monitoring system to improve system reliability and eliminate all scheduled maintenance. It is concluded that all OTV propulsion requirements can be fulfilled with a single engine. The technological developments required to demonstrate that engine are outlined.
High pressure generation using scaled-up Kawai-cell
NASA Astrophysics Data System (ADS)
Shatskiy, A.; Katsura, T.; Litasov, K. D.; Shcherbakova, A. V.; Borzdov, Y. M.; Yamazaki, D.; Yoneda, A.; Ohtani, E.; Ito, E.
2011-11-01
A scaled-up version of a 6-8 Kawai-type multianvil apparatus equipped with 47-mm WC anvils has been developed at the Institute for the Study of the Earth's Interior for operation over pressure ranging up to 19 and 24 GPa using the conventional system with larger compressional volumes between 1.2 and 0.4 cm 3, respectively. This system is used under uniaxial compression along cube diagonal of the Kawai-cell up to the press load of 19 MN. Experiments are performed using octahedral pressure media (PM) made of MgO- and ZrO 2-based semi-sintered ceramics and unfired pyrophyllite gaskets. In this study we used "Toshiba-F" grade WC anvils allowing pressure generation up to 24 GPa. We perform pressure calibrations at room and high temperatures, with octahedron/anvil truncation edge-length ratios ( a0/ b, mm) of 12.2/6, 14/6, 14/7, 16/7, 18/7, 18/9, and 18/10. Different configurations show that an increase in edge-length ratio of a0/b permits the achievement of higher pressure, which agrees with the results of Frost at al. (Frost, D.J., Poe, B.T., Tronnes, R.G., Liebske, C., Duba, A., Rubie, D.C., 2004. A new large-volume multianvil system. Phys. Earth Planet. Inter. 143, 507). However, it also shifts the pressure maximum to higher press loads, in some cases exceeding the capacity of a press. Our and Frost et al. (2004) data reveal that the 14/6, 18/8, and 18/10 assemblies are the most suitable in generating pressures of up to 19-24 GPa at 19 MN press load limits. The assemblies with a low a0/ b ratio have a lower upper pressure limit; however, they exhibit a systematically higher efficiency in pressure generation at low press loads. Consequently, assemblages with high and low a0/ b ratios should be used in high and low pressure experiments, respectively. For example, the 18/12 assembly is suitable for 5-11 GPa pressure range (Stoyanov, E., Haussermann, U., Leinenweber, K., 2010. Large-volume multianvil cells designed for chemical synthesis at high pressures. High Pressure Res., 30, 175), whereas the 14/6, 18/8 ( Frost et al., 2004), and 18/10 assemblies are suitable for 22-24, 19-23, and 11-19 GPa pressure ranges, respectively. The maximum pressure generation achieved in the present study is 24 GPa, using the 14/6 assembly. This appears to be the maximum pressure level attainable by using WC anvils.
Thanapan, Puthamaluk; Prasertsukdee, Saipin; Vachalathiti, Roongtiwa
2013-03-01
The study investigated how the subjects, 18 children with spastic diplegia aged 7-14 years, attained sit-to-stand (STS). The children were divided into two groups and three STS conditions: 1) those who could attain STS independently (I-STS), 2) those who could not attain STS independently (D-STS), and 3) subjects from the D-STS condition who could successfully attain STS with the walker (W-STS). The results showed that I-STS had more mean maximum horizontal location of the upper body and knee than the hip. All body segments of D-STS followed the same model as the I-STS condition, but they moved with less magnitude than I-STS. W-STS presented both pattern and magnitudes relatively similar to I-STS. Furthermore, I-STS showed the highest mean maximum horizontal and vertical velocities of body segments, when compared with the other STS conditions. W-STS performed the mean maximum horizontal and vertical linear velocities of all selected segments close to D-STS did.
Modeling human orthostatic responses on the Moon and on Mars.
Beck, Paula; Tank, Jens; Gauger, Peter; Beck, Luis E J; Zirngibl, Hubert; Jordan, Jens; Limper, Ulrich
2018-06-01
Since manned missions to the Moon and Mars are planned, we conducted active standing tests with lunar, Martian, terrestrial, and 1.8 loads of inertial resistance (+G z ) modeled through defined parabolic flight maneuvers. We hypothesized that the cardiovascular response to active standing is proportional to the +G z load. During partial-+G z parabolic flights, 14 healthy test subjects performed active stand-up maneuvers under 1 +G z , lunar (0.16 +G z ), Martian (0.38 +G z ), and hyper inertial resistance (1.8 +G z ) while heart rate and finger blood pressure were continuously monitored. We quantified amplitudes and timing of orthostatic response immediately following standing up. The maximum early heart rate increase was 21 (SD ± 10) bpm with lunar, 23 (± 11) bpm with Martian, 34 (± 17) bpm with terrestrial +G z , and 40 (± 11) bpm hyper +G z . The time to maximum heart rate increased gradually with increasing loads of inertial resistance. The transient blood pressure reduction was most pronounced with hyper +G z but did not differ significantly between lunar and Martian +G z . The mean arterial pressure nadir was reached significantly later with Martian and lunar compared to 1 +G z . Paradoxically, the time for blood pressure to recover was shortest with terrestrial +G z . While load of inertial resistance directly affects the magnitude of the transient blood pressure reduction and heart rate response to active standing, blood pressure stabilization is most rapidly attained during terrestrial +G z . The observation might suggest that the human cardiovascular system is tuned to cope with orthostatic stress on earth.
Effect of alignment perturbations in a trans-tibial prosthesis user: A pilot study.
Courtney, Anna; Orendurff, Michael S; Buis, Arjan
2016-04-01
A recurring complication in trans-tibial prosthetic limb users is "poor socket fit" with painful residuum-socket interfaces, a consequence of excess pressure. This is due to both poor socket fit and poor socket alignment; however, the interaction of these factors has not been quantified. Through evaluation of kinetic data this study aimed to articulate an interaction uniting socket design, alignment and interface pressures. The results will help to refine future studies and will hopefully help determine whether sockets can be designed, fitted and aligned to maximize mobility whilst minimizing injurious forces. Interface pressures were recorded throughout ambulation in one user with "optimal (reference) alignment" followed by 5 malalignments in a patellar tendon-bearing and a hydrocast socket. Marked differences in pressure distribution were discovered when equating the patellar tendon-bearing against the hydrocast socket and when comparing interface pressures from reference with offset alignment. Patellar tendon-bearing sockets were found to be more sensitive to alignment perturbations than hydrocast sockets. A complex interaction was found, with the most prominent finding demonstrating the requisite for attainment of optimal alignment: a translational alignment error of 10 mm can increase maximum peak pressures by 227% (mean 17.5%). Refinements for future trials are described and the necessity for future research into socket design, alignment and interface pressures has been estabilished.
Atmospheric-pressure plasma jet system for silicon etching without fluorocarbon gas feed
NASA Astrophysics Data System (ADS)
Ohtsu, Yasunori; Nagamatsu, Kenta
2018-01-01
We developed an atmospheric-pressure plasma jet (APPJ) system with a tungsten rod electrode coated with C2F4 particles of approximately 0.3 µm diameter for the surface treatment of a silicon wafer. The APPJ was generated by dielectric barrier discharge with a driving frequency of 22 kHz using a He gas flow. The characteristics of the APPJ were examined under various experimental conditions. The plasma jet length increased proportionally to the electric field. It was found that the treatment area of the silicon wafer was approximately 1 mm in diameter. By atomic force microscopy analysis, minute irregularities with a maximum length of about 600 nm and part of a ring-shaped trench were observed. A Si etching rate of approximately 400 nm/min was attained at a low power of 6 W and a He flow rate of 1 L/min without introducing molecular gas including F atoms.
Drag Reduction Through Distributed Electric Propulsion
NASA Technical Reports Server (NTRS)
Stoll, Alex M.; Bevirt, JoeBen; Moore, Mark D.; Fredericks, William J.; Borer, Nicholas K.
2014-01-01
One promising application of recent advances in electric aircraft propulsion technologies is a blown wing realized through the placement of a number of electric motors driving individual tractor propellers spaced along each wing. This configuration increases the maximum lift coefficient by providing substantially increased dynamic pressure across the wing at low speeds. This allows for a wing sized near the ideal area for maximum range at cruise conditions, imparting the cruise drag and ride quality benefits of this smaller wing size without decreasing takeoff and landing performance. A reference four-seat general aviation aircraft was chosen as an exemplary application case. Idealized momentum theory relations were derived to investigate tradeoffs in various design variables. Navier-Stokes aeropropulsive simulations were performed with various wing and propeller configurations at takeoff and landing conditions to provide insight into the effect of different wing and propeller designs on the realizable effective maximum lift coefficient. Similar analyses were performed at the cruise condition to ensure that drag targets are attainable. Results indicate that this configuration shows great promise to drastically improve the efficiency of small aircraft.
Loturco, Irineu; Artioli, Guilherme Giannini; Kobal, Ronaldo; Gil, Saulo; Franchini, Emerson
2014-07-01
This study investigated the relationship between punching acceleration and selected strength and power variables in 19 professional karate athletes from the Brazilian National Team (9 men and 10 women; age, 23 ± 3 years; height, 1.71 ± 0.09 m; and body mass [BM], 67.34 ± 13.44 kg). Punching acceleration was assessed under 4 different conditions in a randomized order: (a) fixed distance aiming to attain maximum speed (FS), (b) fixed distance aiming to attain maximum impact (FI), (c) self-selected distance aiming to attain maximum speed, and (d) self-selected distance aiming to attain maximum impact. The selected strength and power variables were as follows: maximal dynamic strength in bench press and squat-machine, squat and countermovement jump height, mean propulsive power in bench throw and jump squat, and mean propulsive velocity in jump squat with 40% of BM. Upper- and lower-body power and maximal dynamic strength variables were positively correlated to punch acceleration in all conditions. Multiple regression analysis also revealed predictive variables: relative mean propulsive power in squat jump (W·kg-1), and maximal dynamic strength 1 repetition maximum in both bench press and squat-machine exercises. An impact-oriented instruction and a self-selected distance to start the movement seem to be crucial to reach the highest acceleration during punching execution. This investigation, while demonstrating strong correlations between punching acceleration and strength-power variables, also provides important information for coaches, especially for designing better training strategies to improve punching speed.
Code of Federal Regulations, 2010 CFR
2010-07-01
... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver... Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of silver... Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of...
NASA Technical Reports Server (NTRS)
Boltz, Frederick W.; Kenyon, George C.; Allen, Clyde Q.
1960-01-01
An investigation was conducted in the Ames 12-Foot Low-Turbulence Pressure Tunnel to determine the effects of sweep on the boundary-layer stability characteristics of an untapered variable-sweep wing having an NACA 64(2)A015 section normal to the leading edge. Pressure distribution and transition were measured on the wing at low speeds at sweep angles of 0, 10, 20, 30, 40, and 50 deg. and at angles of attack from -3 to 3 deg. The investigation also included flow-visualization studies on the surface at sweep angles from 0 to 50 deg. and total pressure surveys in the boundary layer at a sweep angle of 30 deg. for angles of attack from -12 to 0 deg. It was found that sweep caused premature transition on the wing under certain conditions. This effect resulted from the formation of vortices in the boundary layer when a critical combination of sweep angle, pressure gradient, and stream Reynolds number was attained. A useful parameter in indicating the combined effect of these flow variables on vortex formation and on beginning transition is the crossflow Reynolds number. The critical values of crossflow Reynolds number for vortex formation found in this investigation range from about 135 to 190 and are in good agreement with those reported in previous investigations. The values of crossflow Reynolds number for beginning transitions were found to be between 190 and 260. For each condition (i.e., development of vortices and initiation of transition at a given location) the lower values in the specified ranges were obtained with a light coating of flow-visualization material on the surface. A method is presented for the rapid computation of crossflow Reynolds number on any swept surface for which the pressure distribution is known. From calculations based on this method, it was found that the maximum values of crossflow Reynolds number are attained under conditions of a strong pressure gradient and at a sweep angle of about 50 deg. Due to the primary dependence on pressure gradient, effects of sweep in causing premature transition are generally first encountered on the lower surfaces of wings operating at positive angles of attack.
Comparing Numerical Spall Simulations with a Nonlinear Spall Formation Model
NASA Astrophysics Data System (ADS)
Ong, L.; Melosh, H. J.
2012-12-01
Spallation accelerates lightly shocked ejecta fragments to speeds that can exceed the escape velocity of the parent body. We present high-resolution simulations of nonlinear shock interactions in the near surface. Initial results show the acceleration of near-surface material to velocities up to 1.8 times greater than the peak particle velocity in the detached shock, while experiencing little to no shock pressure. These simulations suggest a possible nonlinear spallation mechanism to produce the high-velocity, low show pressure meteorites from other planets. Here we pre-sent the numerical simulations that test the production of spall through nonlinear shock interactions in the near sur-face, and compare the results with a model proposed by Kamegai (1986 Lawrence Livermore National Laboratory Report). We simulate near-surface shock interactions using the SALES_2 hydrocode and the Murnaghan equation of state. We model the shock interactions in two geometries: rectangular and spherical. In the rectangular case, we model a planar shock approaching the surface at a constant angle phi. In the spherical case, the shock originates at a point below the surface of the domain and radiates spherically from that point. The angle of the shock front with the surface is dependent on the radial distance of the surface point from the shock origin. We model the target as a solid with a nonlinear Murnaghan equation of state. This idealized equation of state supports nonlinear shocks but is tem-perature independent. We track the maximum pressure and maximum velocity attained in every cell in our simula-tions and compare them to the Hugoniot equations that describe the material conditions in front of and behind the shock. Our simulations demonstrate that nonlinear shock interactions in the near surface produce lightly shocked high-velocity material for both planar and cylindrical shocks. The spall is the result of the free surface boundary condi-tion, which forces a pressure gradient from the peak shock pressure to the zero pressure boundary. The nonlinear shock interactions occur where the pressure contours curve to accommodate the free surface. The material within this spall zone is ejected at speeds up to 1.8 km s-1 for an imposed pulse of 1 km s-1. Where the ejection velocities are highest, the maximum pressure attained in each cell is effectively zero. We compare our simulation results with a model for nonlinear shock interactions proposed by Kamegai (1986). This model recognizes that the material behind the shock is compressed and has a higher soundspeed than the mate-rial in front of the shock. As the rarefaction wave moves behind the shock, its increased velocity through the com-pressed material combines with the residual particle velocity behind the shock to "catch up" with the shock. This occurs in the near surface where the sum of the compressed sound speed and the residual particle velocity is greater than or equal to the shock velocity. Initial results for the spherical shocks qualitatively match the volume described by this model, but differ significantly in the quantitative slope of the curve defining the region of interaction. We continue to test the Kamegai model with high-resolution numerical simulations of shock interactions to determine its potential application to planetary spallation.
Using second-sound shock waves to probe the intrinsic critical velocity of liquid helium II
NASA Technical Reports Server (NTRS)
Turner, T. N.
1983-01-01
A critical velocity truly intrinsic to liquid helium II is experimentally sought in the bulk fluid far from the apparatus walls. Termed the 'fundamental critical velocity,' it necessarily is caused by mutual interactions which operate between the two fluid components and which are activated at large relative velocities. It is argued that flow induced by second-sound shock waves provides the ideal means by which to activate and isolate the fundamental critical velocity from other extraneous fluid-wall interactions. Experimentally it is found that large-amplitude second-sound shock waves initiate a breakdown in the superfluidity of helium II, which is dramatically manifested as a limit to the maximum attainable shock strength. This breakdown is shown to be caused by a fundamental critical velocity. Secondary effects include boiling for ambient pressures near the saturated vapor pressure or the formation of helium I boundary layers at higher ambient pressures. When compared to the intrinsic critical velocity discovered in highly restricted geometries, the shock-induced critical velocity displays a similar temperature dependence and is the same order of magnitude.
Factorial analysis of diesel engine performance using different types of biofuels.
Tashtoush, Ghassan M; Al-Widyan, Mohamad I; Albatayneh, Aiman M
2007-09-01
In this study, several bio-source-fuels like fresh and waste vegetable oil and waste animal fat were tested at different injector pressures (120, 140, 190, 210 bar) in a direct-injection, naturally aspirated, single-cylinder diesel engine with a design injection pressure of 190 bar. Using 2k factorial analysis, the effect of injection pressure (Pi) and fuel type on three engine parameters, namely, combustion efficiency (etac), mass fuel consumption (mf), and engine speed (N) was examined. It was found that Pi and fuel type significantly affected both etac and mf while they had a slight effect on engine speed. Moreover, with diesel and biodiesels, the etac increased to a maximum at 190 bar but declined at the higher Pi value. In contrast, higher Pi had a favorable effect on etac over the whole Pi range with all the other more viscous fuels tested. In addition, the mass fuel consumption consistently decreased with an increase in Pi for all the fuels including the baseline diesel fuel, with which the engine consistently attained higher etac and higher rpm compared to all the other fuels tested.
NASA Technical Reports Server (NTRS)
Erickson, Gary E.
1991-01-01
The vortex dominated aerodynamic characteristics of a generic 65 degree cropped delta wing model were studied in a wind tunnel at subsonic through supersonic speeds. The lee-side flow fields over the wing-alone configuration and the wing with leading edge extension (LEX) added were observed at M (infinity) equals 0.40 to 1.60 using a laser vapor screen technique. These results were correlated with surface streamline patterns, upper surface static pressure distributions, and six-component forces and moments. The wing-alone exhibited vortex breakdown and asymmetry of the breakdown location at the subsonic and transonic speeds. An earlier onset of vortex breakdown over the wing occurred at transonic speeds due to the interaction of the leading edge vortex with the normal shock wave. The development of a shock wave between the vortex and wing surface caused an early separation of the secondary boundary layer. With the LEX installed, wing vortex breakdown asymmetry did not occur up to the maximum angle of attack in the present test of 24 degrees. The favorable interaction of the LEX vortex with the wing flow field reduced the effects of shock waves on the wing primary and secondary vortical flows. The direct interaction of the wing and LEX vortex cores diminished with increasing Mach number. The maximum attainable vortex-induced pressure signatures were constrained by the vacuum pressure limit at the transonic and supersonic speeds.
Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
NASA Technical Reports Server (NTRS)
Bear, R M
1928-01-01
Measurements of the differential pressures on two navy air-speed nozzles, consisting of a Zahm type Pitot-Venturi tube and a SQ-16 two-pronged Pitot-static tube, in a tunnel air stream of fixed speed at various angles of pitch and yaw between 0 degrees and plus or minus 180 degrees. This shows for a range over -20 degrees to +20 degrees pitch and yaw, indicated air speeds varying very slightly over 2 per cent for the Zahm type and a maximum of about 5 per cent for the SQ-16 type from the calibrated speed at 0 degree. For both types of air-speed nozzle the indicated air speed increases slightly as the tubes are pitched or yawed several degrees from their normal 0 degrees altitude, attains a maximum around plus or minus 15 degrees to 25 degrees, declines rapidly therefrom as plus or minus 40 degrees is passed, to zero in the vicinity of plus or minus 70 degrees to 100 degrees, and thence fluctuates irregular from thereabouts to plus or minus 180 degrees. The complete variation in indicated air speed for the two tubes over 360 degree pitch and yaw is graphically portrayed in figures 9 and 10. For the same air speed and 0 degree pitch and yaw the differential pressure of the Zahm type Pitot-Venturi nozzle is about seven times that of the SQ-16 type two-prolonged Pitot-static nozzle.
NASA Astrophysics Data System (ADS)
Sogukpinar, Haci; Bozkurt, Ismail
2018-02-01
Aerodynamic performance of the airfoil plays the most important role to obtain economically maximum efficiency from a wind turbine. Therefore airfoil should have an ideal aerodynamic shape. In this study, aerodynamic simulation of S809 airfoil is conducted and obtained result compared with previously made NASA experimental result and NREL theoretical data. At first, Lift coefficient, lift to drag ratio and pressure coefficient around S809 airfoil are calculated with SST turbulence model, and are compared with experimental and other theoretical data to correlate simulation correctness of the computational approaches. And result indicates good correlation with both experimental and theoretical data. This calculation point out that as the increasing relative velocity, lift to drag ratio increases. Lift to drag ratio attain maximum at the angle around 6 degree and after that starts to decrease again. Comparison shows that CFD code used in this calculation can predict aerodynamic properties of airfoil.
High heat flux burnout in subcooled flow boiling
NASA Astrophysics Data System (ADS)
Celata, G. P.; Cumo, M.; Mariani, A.
1995-09-01
The paper reports the results of an experimental research carried out at the Heat Transfer Division of the Energy Department, C.R. Casaccia, on the thermal hydraulic characterization of subcooled flow boiling CHF under typical conditions of thermonuclear fusion reactors, i.e. high liquid velocity and subcooling. The experiment was carried out exploring the following parameters: channel diameter (from 2.5 to 8.0 mm), heated length (10 and 15 cm), liquid velocity (from 2 to 40 m/s), exit pressure (from atmospheric to 5.0 MPa), inlet temperature (from 30 to 80 °C), channel orientation (vertical and horizontal). A maximum CHF value of 60.6 MW/m2 has been obtained under the following conditions: T in=30°, p=2.5 MPa, u=40 m/s, D=2.5 mm (smooth channel) Turbulence promoters (helically coiled wires) have been employed to further enhance the CHF attainable with subcooled flow boiling. Helically coiled wires allow an increase of 50% of the maximum CHF obtained with smooth channels.
Theoretical Evaluation of the Maximum Work of Free-Piston Engine Generators
NASA Astrophysics Data System (ADS)
Kojima, Shinji
2017-01-01
Utilizing the adjoint equations that originate from the calculus of variations, we have calculated the maximum thermal efficiency that is theoretically attainable by free-piston engine generators considering the work loss due to friction and Joule heat. Based on the adjoint equations with seven dimensionless parameters, the trajectory of the piston, the histories of the electric current, the work done, and the two kinds of losses have been derived in analytic forms. Using these we have conducted parametric studies for the optimized Otto and Brayton cycles. The smallness of the pressure ratio of the Brayton cycle makes the net work done negative even when the duration of heat addition is optimized to give the maximum amount of heat addition. For the Otto cycle, the net work done is positive, and both types of losses relative to the gross work done become smaller with the larger compression ratio. Another remarkable feature of the optimized Brayton cycle is that the piston trajectory of the heat addition/disposal process is expressed by the same equation as that of an adiabatic process. The maximum thermal efficiency of any combination of isochoric and isobaric heat addition/disposal processes, such as the Sabathe cycle, may be deduced by applying the methods described here.
26 CFR 1.410(a)-4 - Maximum age conditions and time of participation.
Code of Federal Regulations, 2012 CFR
2012-04-01
... 26 Internal Revenue 5 2012-04-01 2011-04-01 true Maximum age conditions and time of participation.... § 1.410(a)-4 Maximum age conditions and time of participation. (a) Maximum age conditions—(1) General...) if the plan excludes from participation (on the basis of age) an employee who has attained an age...
26 CFR 1.410(a)-4 - Maximum age conditions and time of participation.
Code of Federal Regulations, 2011 CFR
2011-04-01
... 26 Internal Revenue 5 2011-04-01 2011-04-01 false Maximum age conditions and time of participation.... § 1.410(a)-4 Maximum age conditions and time of participation. (a) Maximum age conditions—(1) General...) if the plan excludes from participation (on the basis of age) an employee who has attained an age...
26 CFR 1.410(a)-4 - Maximum age conditions and time of participation.
Code of Federal Regulations, 2010 CFR
2010-04-01
... 26 Internal Revenue 5 2010-04-01 2010-04-01 false Maximum age conditions and time of participation... Maximum age conditions and time of participation. (a) Maximum age conditions—(1) General rule. A plan is... excludes from participation (on the basis of age) an employee who has attained an age specified by the plan...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Chattopadhyay, S., E-mail: suman.mech09@gmail.com; Mondal, P., E-mail: mondal.pradip87@gmail.com; Ghosh, S., E-mail: sudipghosh.becollege@gmail.com
Thermal performance analysis and sizing of a biomass gasification based combined power and refrigeration plant (CPR) is reported in this study. The plant is capable of producing 100 kWe of electrical output while simultaneously producing a refrigeration effect, varying from 28-68 ton of refrigeration (TR). The topping gas turbine cycle is an indirectly heated all-air cycle. A combustor heat exchanger duplex (CHX) unit burns producer gas and transfer heat to air. This arrangement avoids complex gas cleaning requirements for the biomass-derived producer gas. The exhaust air of the topping GT is utilized to run a bottoming ammonia absorption refrigeration (AAR)more » cycle via a heat recovery steam generator (HRSG), steam produced in the HRSG supplying heat to the generator of the refrigeration cycle. Effects of major operating parameters like topping cycle pressure ratio (r{sub p}) and turbine inlet temperature (TIT) on the energetic performance of the plant are studied. Energetic performance of the plant is evaluated via energy efficiency, required biomass consumption and fuel energy savings ratio (FESR). The FESR calculation method is significant for indicating the savings in fuel of a combined power and process heat plant instead of separate plants for power and process heat. The study reveals that, topping cycle attains maximum power efficiency of 30%in pressure ratio range of 8-10. Up to a certain value of pressure ratio the required air flow rate through the GT unit decreases with increase in pressure ratio and then increases with further increase in pressure ratio. The capacity of refrigeration of the AAR unit initially decreases up to a certain value of topping GT cycle pressure ratio and then increases with further increase in pressure ratio. The FESR is found to be maximized at a pressure ratio of 9 (when TIT=1100°C), the maximum value being 53%. The FESR is higher for higher TIT. The heat exchanger sizing is also influenced by the topping cycle pressure ratio and GT-TIT.« less
Mihiretu, Gezahegn T; Brodin, Malin; Chimphango, Annie F; Øyaas, Karin; Hoff, Bård H; Görgens, Johann F
2017-10-01
The viability of single-step microwave-induced pressurized hot water conditions for co-production of xylan-based biopolymers and bioethanol from aspenwood sawdust and sugarcane trash was investigated. Extraction of hemicelluloses was conducted using microwave-assisted pressurized hot water system. The effects of temperature and time on extraction yield and enzymatic digestibility of resulting solids were determined. Temperatures between 170-200°C for aspenwood and 165-195°C for sugarcane trash; retention times between 8-22min for both feedstocks, were selected for optimization purpose. Maximum xylan extraction yields of 66 and 50%, and highest cellulose digestibilities of 78 and 74%, were attained for aspenwood and sugarcane trash respectively. Monomeric xylose yields for both feedstocks were below 7%, showing that the xylan extracts were predominantly in non-monomeric form. Thus, single-step microwave-assisted hot water method is viable biorefinery approach to extract xylan from lignocelluloses while rendering the solid residues sufficiently digestible for ethanol production. Copyright © 2017 Elsevier Ltd. All rights reserved.
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.94 Section 430.94 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... reduction attainable by the application of the best available technology economically achievable (BAT... economically achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.94 Section 430.94 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... reduction attainable by the application of the best available technology economically achievable (BAT... economically achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass...
Efficient robust doubly adaptive regularized regression with applications.
Karunamuni, Rohana J; Kong, Linglong; Tu, Wei
2018-01-01
We consider the problem of estimation and variable selection for general linear regression models. Regularized regression procedures have been widely used for variable selection, but most existing methods perform poorly in the presence of outliers. We construct a new penalized procedure that simultaneously attains full efficiency and maximum robustness. Furthermore, the proposed procedure satisfies the oracle properties. The new procedure is designed to achieve sparse and robust solutions by imposing adaptive weights on both the decision loss and the penalty function. The proposed method of estimation and variable selection attains full efficiency when the model is correct and, at the same time, achieves maximum robustness when outliers are present. We examine the robustness properties using the finite-sample breakdown point and an influence function. We show that the proposed estimator attains the maximum breakdown point. Furthermore, there is no loss in efficiency when there are no outliers or the error distribution is normal. For practical implementation of the proposed method, we present a computational algorithm. We examine the finite-sample and robustness properties using Monte Carlo studies. Two datasets are also analyzed.
NASA Technical Reports Server (NTRS)
Bushnell, D. M.; Tuttle, M. H.
1979-01-01
A survey was conducted and a bibliography compiled on attainment of laminar flow in air through the use of favorable pressure gradient and suction. This report contains the survey, summaries of data for both ground and flight experiments, and abstracts of referenced reports. Much early information is also included which may be of some immediate use as background material for LFC applications.
Performance Characteristics of Plane-Wall Two-Dimensional Diffusers
NASA Technical Reports Server (NTRS)
Reid, Elliott G
1953-01-01
Experiments have been made at Stanford University to determine the performance characteristics of plane-wall, two-dimensional diffusers which were so proportioned as to insure reasonable approximation of two-dimensional flow. All of the diffusers had identical entrance cross sections and discharged directly into a large plenum chamber; the test program included wide variations of divergence angle and length. During all tests a dynamic pressure of 60 pounds per square foOt was maintained at the diffuser entrance and the boundary layer there was thin and fully turbulent. The most interesting flow characteristics observed were the occasional appearance of steady, unseparated, asymmetric flow - which was correlated with the boundary-layer coalescence - and the rapid deterioration of flow steadiness - which occurred as soon as the divergence angle for maximum static pressure recovery was exceeded. Pressure efficiency was found to be controlled almost exclusively by divergence angle, whereas static pressure recovery was markedly influenced by area ratio (or length) as well as divergence angle. Volumetric efficiency. diminished as area ratio increased, and at a greater rate with small lengths than with large ones. Large values of the static-pressure-recovery coefficient were attained only with long diffusers of large area ratio; under these conditions pressure efficiency was high and. volumetric efficiency low. Auxiliary tests with asymmetric diffusers demonstrated that longitudinal pressure gradient, rather than wall divergence angle, controlled flow separation. Others showed that the addition of even a short exit duct of uniform section augmented pressure recovery. Finally, it was found that the installation of a thin, central, longitudinal partition suppressed flow separation in short diffusers and thereby improved pressure recovery
Code of Federal Regulations, 2010 CFR
2010-07-01
... Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and... monthly average mg/troy ounce of silver reduced in solution Lead 0.168 0.080 Mercury 0.100 0.040 Silver 0... property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold refined electrolytically...
Code of Federal Regulations, 2010 CFR
2010-07-01
.../troy ounce of silver from film stripping Copper 64.450 30.720 Zinc 51.360 21.150 Ammonia (as N) 6,712... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of silver from... Limitations Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.34 Section 430.34 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.14 Section 430.14 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.34 Section 430.34 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.44 Section 430.44 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.14 Section 430.14 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.44 Section 430.44 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... attainable by the application of the best available technology economically achievable (BAT). Except as... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2014 CFR
2014-07-01
... CATEGORY Secondary Tin Subcategory § 421.292 Effluent limitations guidelines representing the degree of... attainable by the application of the best practicable technology currently available: (a) Tin smelter SO2 scrubber. BPT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any...
Code of Federal Regulations, 2012 CFR
2012-07-01
... CATEGORY Secondary Tin Subcategory § 421.292 Effluent limitations guidelines representing the degree of... attainable by the application of the best practicable technology currently available: (a) Tin smelter SO2 scrubber. BPT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any...
Code of Federal Regulations, 2011 CFR
2011-07-01
... CATEGORY Secondary Tin Subcategory § 421.292 Effluent limitations guidelines representing the degree of... attainable by the application of the best practicable technology currently available: (a) Tin smelter SO2 scrubber. BPT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any...
Code of Federal Regulations, 2010 CFR
2010-07-01
... CATEGORY Secondary Tin Subcategory § 421.292 Effluent limitations guidelines representing the degree of... attainable by the application of the best practicable technology currently available: (a) Tin smelter SO2 scrubber. BPT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any...
Code of Federal Regulations, 2013 CFR
2013-07-01
... CATEGORY Secondary Tin Subcategory § 421.292 Effluent limitations guidelines representing the degree of... attainable by the application of the best practicable technology currently available: (a) Tin smelter SO2 scrubber. BPT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any...
Moderating diets to feed the future
NASA Astrophysics Data System (ADS)
Davis, Kyle F.; D'Odorico, Paolo; Rulli, Maria Cristina
2014-10-01
Population growth, dietary changes, and increasing biofuel use are placing unprecedented pressure on the global food system. While this demand likely cannot be met by expanding agricultural lands, much of the world's cropland can attain higher crop yields. Therefore, it is important to examine whether increasing crop productivity to the maximum attainable yield (i.e., yield gap closure) alone can substantially improve food security at global and national scales. Here we show that closing yield gaps through conventional technological development (i.e., fertilizers and irrigation) can potentially meet future global demand if diets are moderated and crop-based biofuel production is limited. In particular, we find that increases in dietary demand will be largely to blame should crop production fall short of demand. In converting projected diets to a globally adequate diet (3000 kcal/cap/d; 20% animal kcal) under current agrofuel use, we find that 1.8-2.6 billion additional people can be fed in 2030 and 2.1-3.1 billion additional people in 2050, depending on the extent to which yields can improve in those periods. Therefore, the simple combination of yield gap closure and moderating diets offers promise for feeding the world's population but only if long-term sustainability is the focus.
Mechanics and applications of pressure adaptive honeycomb
NASA Astrophysics Data System (ADS)
Vos, Roelof
A novel adaptive aerostructure is presented that relies on certified aerospace materials and can therefore be applied in conventional passenger aircraft. This structure consists of a honeycomb material which' cells extend over a significant length perpendicular to the plane of the cells. Each of the cells contains an inelastic pouch (or bladder) that forms a circular tube when the cell forms a perfect hexagon. By changing the cell differential pressure (CDP) the stiffness of the honeycomb can be altered. Using an external force or the elastic force within the honeycomb material, the honeycomb can be deformed such that the cells deviate from their perfect-hexagonal shape. It can be shown that by increasing the CDP, the structure eventually returns to a perfect hexagon. By doing so, a fully embedded pneumatic actuator is created that can perform work and substitute conventional low-bandwidth flight control actuators. It is shown that two approaches can be taken to regulate the stiffness of this embedded actuator: (1) The first approach relies on the pouches having a fixed amount of air in them and stiffness is altered by a change in ambient pressure. Coupled to the ambient pressure-altitude cycle that aircraft encounter during each flight, this approach yields a true adaptive aerostructure that operates independently of pilot input and is controlled solely by the altitude the aircraft is flying at. (2) The second approach relies on a controlled constant CDP. This CDP could be supplied from one of the compressor stages of the engine as a form of bleed air. Because of the air-tight pouches there would essentially be no mass flow, meaning engine efficiency would not be significantly affected due to this application. By means of a valve system the pilot could have direct control over the pressure and, consequently, the stiffness of the structure. This allows for much higher CDPs (on the order of 1MPa) than could physically be achieved by relying on the ambient pressure decrease with altitude. This option does require more infrastructure like tubing, valves, and supporting electronics from the cockpit. Applications of pressure adaptive honeycomb are tailored primarily towards low-bandwidth applications like secondary flight control. The most profound application is the morphing of an entire wing section, from leading to trailing edge, due to the adaptive honeycomb. On a smaller scale, other examples include a solid state pressure adaptive flap, a pressure adaptive droop nose, a pressure adaptive Gurney flap and a pressure adaptive engine inlet. Each of these applications is based on the same principle of stiffness alteration with pressure and can be used with either actuation option (constant mass or constant pressure). A model that relates the volumetric change of the honeycomb cells to the external blocked stress was shown to correlate well to experiments that were carried out on several test articles. Based on this model it was estimated that pressure adaptive honeycomb has a maximum mass-specific energy density of 12.4J/g, for the case of an externally applied CDP of 0.9MPa (can be supplied from a high-pressure compressor stage of a gas turbine). In addition, it was shown that a maximum strain of 76% can be achieved and that the maximum blocked stress amounts to 0.82MPa. In the case of a 40kPa drop in atmospheric pressure and constant mass of air in the pouches, the maximum mass specific energy amounts to 1.1J/g and a maximum blocked force of 70kPa can be attained. Pressure adaptive honeycomb was embedded into a 25%c adaptive flap on a NACA2412 wing section with a chord of 1.08m. Wind tunnel tests at Reynolds number of 1 million demonstrated a shift in the cl -- alpha curve upwards by an average of 0.3, thereby increasing the maximum lift coefficient from 1.27 to 1.52. This successfully demonstrated the application of pressure adaptive honeycomb embedded in a morphing aircraft structure.
Code of Federal Regulations, 2010 CFR
2010-07-01
... daily 1 Maximum monthly avg. 1 TSS 0.00998 0.00465 pH (2) (2) 1 Pounds per thousand pound of product. 2... Maximum daily 1 Maximum monthly avg. 1 O&G (as HEM) 0.00746 0.00446 TSS 0.0123 0.00508 pH (2) (2) 1 Pounds...
Code of Federal Regulations, 2011 CFR
2011-07-01
... daily 1 Maximum monthly avg. 1 TSS 0.00998 0.00465 pH (2) (2) 1 Pounds per thousand pound of product. 2... Maximum daily 1 Maximum monthly avg. 1 O&G (as HEM) 0.00746 0.00446 TSS 0.0123 0.00508 pH (2) (2) 1 Pounds...
Code of Federal Regulations, 2013 CFR
2013-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2014 CFR
2014-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2010 CFR
2010-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2012 CFR
2012-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2011 CFR
2011-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Novel duplex vapor-electrochemical method for silicon solar cells
NASA Technical Reports Server (NTRS)
Kapur, V. K.; Nanis, L.; Sanjurjo, A.
1977-01-01
Silicon obtained by the SiF4-Na reaction was analyzed by spark source mass spectrometry (SSMS). Silicon samples prepared from induction melted powder were evaluated for electrical properties using four point probe conductivity and thermoelectric methods. SiF4-Na reaction under P sub SiF4 greater than 1 atmosphere. The amount of silicon produced was increased from 25 g per batch (in the glass reactor) to greater than 70 g per batch in the stainless steel reactor. The study of the effects of reaction variables such as P sub SiF4 and maximum temperature attained on the particle size of silicon powder showed that the silicon particle size tends to grow larger with increasing pressure of the SiF4 gas in the reaction system.
Bohlen, S.R.; Eckert, J.O.; Hankins, W.B.
1995-01-01
The phase relationships of melting of synthetic granite in the presence of an H2O-CO2 fluid were determined. These results provide constraints on the maximum temperatures of regional metamorphism attainable in vapor-saturated metapelitic and quartzofeldspathic rocks that escaped widespread melting. At pressures below 10 kbar, a fluid phase of XH2O = 0.75, 0.5, and 0.25 limits temperatures to below ~700-725, ~800-825, and ~850-875??C, respectively. As a consequence, the formation of granulite does not require CO2 concentrations in a coexisting fluid to exceed an XCO2 of 0.25-0.5. -from Authors
Code of Federal Regulations, 2013 CFR
2013-07-01
... shall not be subject to the maximum day and maximum for monthly average mass (kg/1,000 kkg or lb/million lb of metal poured; kg/1,000 kkg or lb/million lb of sand reclaimed; kg/62.3 million Sm3 or lb... pollutant property Maximum for any 1 day Maximum for monthly average kg/1,000 kkg (pounds per million pounds...
Code of Federal Regulations, 2012 CFR
2012-07-01
... shall not be subject to the maximum day and maximum for monthly average mass (kg/1,000 kkg or lb/million lb of metal poured; kg/1,000 kkg or lb/million lb of sand reclaimed; kg/62.3 million Sm3 or lb... pollutant property Maximum for any 1 day Maximum for monthly average kg/1,000 kkg (pounds per million pounds...
Code of Federal Regulations, 2014 CFR
2014-07-01
... shall not be subject to the maximum day and maximum for monthly average mass (kg/1,000 kkg or lb/million lb of metal poured; kg/1,000 kkg or lb/million lb of sand reclaimed; kg/62.3 million Sm3 or lb... pollutant property Maximum for any 1 day Maximum for monthly average kg/1,000 kkg (pounds per million pounds...
Code of Federal Regulations, 2014 CFR
2014-07-01
...) Molten salt rinse. Subpart E—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/off-kg (pounds per million off-pounds) of refractory metals treated with molten salt...
Code of Federal Regulations, 2012 CFR
2012-07-01
...) Molten salt rinse. Subpart E—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/off-kg (pounds per million off-pounds) of refractory metals treated with molten salt...
NASA Technical Reports Server (NTRS)
Dolan, Joseph F.; Fisher, Richard R. (Technical Monitor)
2001-01-01
When asked to discuss Cyg XR-1, E. E. Salpeter once concluded, 'A black hole in Cyg X(R)-1 is the most conservative hypothesis.' Recent observations now make it likely that a black hole in Cyg XR-1 is the only hypothesis tenable. Chandrasekhar first showed that compact stars - those with the inward force of gravity on their outer layers balanced by the pressure generated by the Pauli exclusion principle acting on its electrons (in white dwarfs) or nucleons (in neutron stars) - have a maximum mass. Equilibrium is achieved at a minimum of the total energy of the star, which is the sum of the positive Fermi energy and the negative gravitational energy. The maximum mass attainable in equilibrium is found by setting E = 0: M(max) = 1.5 M(Sun). If the mass of the star is larger than this, then E can be decreased without bound by decreasing the star's radius and increasing its (negative) gravitational energy. No equilibrium value of the radius exist, and general relativity predicts that gravitational collapse to a point occurs. This point singularity is a black hole.
NASA Astrophysics Data System (ADS)
Alsing, Justin; Silva, Hector O.; Berti, Emanuele
2018-04-01
We infer the mass distribution of neutron stars in binary systems using a flexible Gaussian mixture model and use Bayesian model selection to explore evidence for multi-modality and a sharp cut-off in the mass distribution. We find overwhelming evidence for a bimodal distribution, in agreement with previous literature, and report for the first time positive evidence for a sharp cut-off at a maximum neutron star mass. We measure the maximum mass to be 2.0M⊙ < mmax < 2.2M⊙ (68%), 2.0M⊙ < mmax < 2.6M⊙ (90%), and evidence for a cut-off is robust against the choice of model for the mass distribution and to removing the most extreme (highest mass) neutron stars from the dataset. If this sharp cut-off is interpreted as the maximum stable neutron star mass allowed by the equation of state of dense matter, our measurement puts constraints on the equation of state. For a set of realistic equations of state that support >2M⊙ neutron stars, our inference of mmax is able to distinguish between models at odds ratios of up to 12: 1, whilst under a flexible piecewise polytropic equation of state model our maximum mass measurement improves constraints on the pressure at 3 - 7 × the nuclear saturation density by ˜30 - 50% compared to simply requiring mmax > 2M⊙. We obtain a lower bound on the maximum sound speed attained inside the neutron star of c_s^max > 0.63c (99.8%), ruling out c_s^max < c/√{3} at high significance. Our constraints on the maximum neutron star mass strengthen the case for neutron star-neutron star mergers as the primary source of short gamma-ray bursts.
Code of Federal Regulations, 2010 CFR
2010-07-01
... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of precious metals... day Maximum for monthly average mg/troy ounce of precious metal in the granulated raw material Copper... monthly average mg/troy ounce of gold produced by cyanide stripping Copper 7.030 3.700 Cyanide (total) 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... facilities must achieve the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of...
Code of Federal Regulations, 2011 CFR
2011-07-01
... at any time. 4 No maximum monthly average limitation. 5 May be measured as hexane extractable... limitations: (1) All facilities must achieve the following effluent limitations for ammonia (as N): Effluent Limitations [BPT] Regulated parameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L...
Code of Federal Regulations, 2010 CFR
2010-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... facilities must achieve the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of...
Code of Federal Regulations, 2012 CFR
2012-07-01
... at any time. 4 No maximum monthly average limitation. 5 May be measured as hexane extractable... limitations: (1) All facilities must achieve the following effluent limitations for ammonia (as N): Effluent Limitations [BPT] Regulated parameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L...
Code of Federal Regulations, 2013 CFR
2013-07-01
... at any time. 4 No maximum monthly average limitation. 5 May be measured as hexane extractable... limitations: (1) All facilities must achieve the following effluent limitations for ammonia (as N): Effluent Limitations [BPT] Regulated parameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L...
Code of Federal Regulations, 2010 CFR
2010-07-01
... at any time. 4 No maximum monthly average limitation. 5 May be measured as hexane extractable... limitations: (1) All facilities must achieve the following effluent limitations for ammonia (as N): Effluent Limitations [BPT] Regulated parameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L...
Code of Federal Regulations, 2011 CFR
2011-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... facilities must achieve the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of...
Code of Federal Regulations, 2012 CFR
2012-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... facilities must achieve the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of...
Code of Federal Regulations, 2013 CFR
2013-07-01
... maximum monthly average limitation. 4 May be measured as hexane extractable material (HEM). (2) In... facilities must achieve the following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of...
Code of Federal Regulations, 2014 CFR
2014-07-01
... at any time. 4 No maximum monthly average limitation. 5 May be measured as hexane extractable... limitations: (1) All facilities must achieve the following effluent limitations for ammonia (as N): Effluent Limitations [BPT] Regulated parameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L...
Piloted simulation study of a balloon-assisted deployment of an aircraft at high altitude
NASA Technical Reports Server (NTRS)
Murray, James; Moes, Timothy; Norlin, Ken; Bauer, Jeffrey; Geenen, Robert; Moulton, Bryan; Hoang, Stephen
1992-01-01
A piloted simulation was used to study the feasibility of a balloon assisted deployment of a research aircraft at high altitude. In the simulation study, an unmanned, modified sailplane was carried to 110,000 ft with a high altitude balloon and released in a nose down attitude. A remote pilot controlled the aircraft through a pullout and then executed a zoom climb to a trimmed, 1 g flight condition. A small parachute was used to limit the Mach number during the pullout to avoid adverse transonic effects. The use of small rocket motor was studied for increasing the maximum attainable altitude. Aerodynamic modifications to the basic sailplane included applying supercritical airfoil gloves over the existing wing and tail surfaces. The aerodynamic model of the simulated aircraft was based on low Reynolds number wind tunnel tests and computational techniques, and included large Mach number and Reynolds number effects at high altitude. Parametric variations were performed to study the effects of launch altitude, gross weight, Mach number limit, and parachute size on the maximum attainable stabilized altitude. A test altitude of approx. 95,000 ft was attained, and altitudes in excess of 100,000 ft was attained.
Code of Federal Regulations, 2013 CFR
2013-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 48 18 TSS 115 36 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2013 CFR
2013-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2011 CFR
2011-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 48 18 TSS 115 36 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2012 CFR
2012-07-01
... concentration listed in the following table. Effluent characteristics BPT Effluent Limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2013 CFR
2013-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 163 61 TSS 216 67 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2011 CFR
2011-07-01
... concentration listed in the following table. Effluent characteristics BPT Effluent Limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2011 CFR
2011-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2014 CFR
2014-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 48 18 TSS 115 36 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2014 CFR
2014-07-01
... concentration listed in the following table. Effluent characteristics BPT Effluent Limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2013 CFR
2013-07-01
... concentration listed in the following table. Effluent characteristics BPT Effluent Limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2011 CFR
2011-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 163 61 TSS 216 67 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2012 CFR
2012-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 48 18 TSS 115 36 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2012 CFR
2012-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2014 CFR
2014-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 163 61 TSS 216 67 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2012 CFR
2012-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 163 61 TSS 216 67 pH (2) (2) 1 All units except pH are...
Code of Federal Regulations, 2014 CFR
2014-07-01
... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any one day Maximum for monthly average BOD5 64 24 TSS 130 40 pH (2) (2) 1 All units except pH are...
NASA Astrophysics Data System (ADS)
Music, Denis; Geyer, Richard W.; Hans, Marcus
2016-07-01
To increase the thermoelectric efficiency and reduce the thermal fatigue upon cyclic heat loading, alloying of amorphous NbO2 with all 3d and 5d transition metals has systematically been investigated using density functional theory. It was found that Ta fulfills the key design criteria, namely, enhancement of the Seebeck coefficient and positive Cauchy pressure (ductility gauge). These quantum mechanical predictions were validated by assessing the thermoelectric and elastic properties on combinatorial thin films, which is a high-throughput approach. The maximum power factor is 2813 μW m-1 K-2 for the Ta/Nb ratio of 0.25, which is a hundredfold increment compared to pure NbO2 and exceeds many oxide thermoelectrics. Based on the elasticity measurements, the consistency between theory and experiment for the Cauchy pressure was attained within 2%. On the basis of the electronic structure analysis, these configurations can be perceived as metallic, which is consistent with low electrical resistivity and ductile behavior. Furthermore, a pronounced quantum confinement effect occurs, which is identified as the physical origin for the Seebeck coefficient enhancement.
Orthotopic bladder substitution in men revisited: identification of continence predictors.
Koraitim, M M; Atta, M A; Foda, M K
2006-11-01
We determined the impact of the functional characteristics of the neobladder and urethral sphincter on continence results, and determined the most significant predictors of continence. A total of 88 male patients 29 to 70 years old underwent orthotopic bladder substitution with tubularized ileocecal segment (40) and detubularized sigmoid (25) or ileum (23). Uroflowmetry, cystometry and urethral pressure profilometry were performed at 13 to 36 months (mean 19) postoperatively. The correlation between urinary continence and 28 urodynamic variables was assessed. Parameters that correlated significantly with continence were entered into a multivariate analysis using a logistic regression model to determine the most significant predictors of continence. Maximum urethral closure pressure was the only parameter that showed a statistically significant correlation with diurnal continence. Nocturnal continence had not only a statistically significant positive correlation with maximum urethral closure pressure, but also statistically significant negative correlations with maximum contraction amplitude, and baseline pressure at mid and maximum capacity. Three of these 4 parameters, including maximum urethral closure pressure, maximum contraction amplitude and baseline pressure at mid capacity, proved to be significant predictors of continence on multivariate analysis. While daytime continence is determined by maximum urethral closure pressure, during the night it is the net result of 2 forces that have about equal influence but in opposite directions, that is maximum urethral closure pressure vs maximum contraction amplitude plus baseline pressure at mid capacity. Two equations were derived from the logistic regression model to predict the probability of continence after orthotopic bladder substitution, including Z1 (diurnal) = 0.605 + 0.0085 maximum urethral closure pressure and Z2 (nocturnal) = 0.841 + 0.01 [maximum urethral closure pressure - (maximum contraction amplitude + baseline pressure at mid capacity)].
Code of Federal Regulations, 2012 CFR
2012-07-01
... units (CFU) per 100 mL at any time. 3 No maximum monthly average limitation. 4 May be measured as hexane... following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2013 CFR
2013-07-01
... units (CFU) per 100 mL at any time. 3 No maximum monthly average limitation. 4 May be measured as hexane... following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2014 CFR
2014-07-01
... units (CFU) per 100 mL at any time. 3 No maximum monthly average limitation. 4 May be measured as hexane... following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2010 CFR
2010-07-01
... units (CFU) per 100 mL at any time. 3 No maximum monthly average limitation. 4 May be measured as hexane... following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
Code of Federal Regulations, 2011 CFR
2011-07-01
... units (CFU) per 100 mL at any time. 3 No maximum monthly average limitation. 4 May be measured as hexane... following effluent limitation for ammonia (as N): Effluent Limitations [BPT] Regulatedparameter Maximum daily 1 Maximum monthly avg. 1 Ammonia (as N) 8.0 4.0 1 mg/L (ppm). (2) In the case of process...
NASA Technical Reports Server (NTRS)
Oswatitsch, K.
1947-01-01
The problem of the intake of air is treated for a missile flying at supersonic speeds and of changing the kinetic energy of the air into pressure with the least possible losses. Calculations are carried out concerning the results which can be attained. After a discussion of several preliminary experiments, the practical solution of the problem at hand is indicated by model experiments. The results proved very satisfactory in view of the results which had been attained previously and the values which were anticipated theoretically.
Power requirement of rotating rods in airflow
NASA Technical Reports Server (NTRS)
Barna, P. S.; Crossman, G. R.
1974-01-01
Experiments were performed to determine the power required for rotating a rotor disc fitted with a number of radially arranged rods placed into a ducted airflow. An array of stationary rods, also radially arranged, were placed upstream close to the rotor with a small gap between the rods to cause wake interference. The results show that power increased with increasing airflow and the rate of increase varied considerably. At lower values of airflow the rate of increase was larger than at higher airflow and definite power peaks occurred at certain airflow rates, where the power attained a maximum within the test airflow range. During the test a maximum blade passage frequency of 2037 Hz was attained.
NASA Technical Reports Server (NTRS)
Kimble, Michael C.; White, Ralph E.
1991-01-01
A mathematical model of a hydrogen/oxygen alkaline fuel cell is presented that can be used to predict the polarization behavior under various power loads. The major limitations to achieving high power densities are indicated and methods to increase the maximum attainable power density are suggested. The alkaline fuel cell model describes the phenomena occurring in the solid, liquid, and gaseous phases of the anode, separator, and cathode regions based on porous electrode theory applied to three phases. Fundamental equations of chemical engineering that describe conservation of mass and charge, species transport, and kinetic phenomena are used to develop the model by treating all phases as a homogeneous continuum.
Chest wall mobility is related to respiratory muscle strength and lung volumes in healthy subjects.
Lanza, Fernanda de Cordoba; de Camargo, Anderson Alves; Archija, Lilian Rocha Ferraz; Selman, Jessyca Pachi Rodrigues; Malaguti, Carla; Dal Corso, Simone
2013-12-01
Chest wall mobility is often measured in clinical practice, but the correlations between chest wall mobility and respiratory muscle strength and lung volumes are unknown. We investigate the associations between chest wall mobility, axillary and thoracic cirtometry values, respiratory muscle strength (maximum inspiratory pressure and maximum expiratory pressure), and lung volumes (expiratory reserve volume, FEV(1), inspiratory capacity, FEV(1)/FVC), and the determinants of chest mobility in healthy subjects. In 64 healthy subjects we measured inspiratory capacity, FVC, FEV(1), expiratory reserve volume, maximum inspiratory pressure, and maximum expiratory pressure, and chest wall mobility via axillary and thoracic cirtometry. We used linear regression to evaluate the influence of the measured variables on chest wall mobility. The subjects' mean ± SD values were: age 24 ± 3 years, axillary cirtometry 6.3 ± 2.0 cm, thoracic cirtometry 7.5 ± 2.3 cm; maximum inspiratory pressure 90.4 ± 10.6% of predicted, maximum expiratory pressure 92.8 ± 13.5% of predicted, inspiratory capacity 99.7 ± 8.6% of predicted, FVC 101.9 ± 10.6% of predicted, FEV(1) 98.2 ± 10.3% of predicted, expiratory reserve volume 90.9 ± 19.9% of predicted. There were significant correlations between axillary cirtometry and FVC (r = 0.32), FEV(1) (r = 0.30), maximum inspiratory pressure (r = 0.48), maximum expiratory pressure (r = 0.25), and inspiratory capacity (r = 0.24), and between thoracic cirtometry and FVC (r = 0.50), FEV(1) (r = 0.48), maximum inspiratory pressure (r = 0.46), maximum expiratory pressure (r = 0.37), inspiratory capacity (r = 0.39), and expiratory reserve volume (r = 0.47). In multiple regression analysis the variable that best explained the axillary cirtometry variation was maximum inspiratory pressure (R(2) 0.23), and for thoracic cirtometry it was FVC and maximum inspiratory pressure (R(2) 0.32). Chest mobility in healthy subjects is related to respiratory muscle strength and lung function; the higher the axillary cirtometry and thoracic cirtometry values, the greater the maximum inspiratory pressure, maximum expiratory pressure, and lung volumes in healthy subjects.
14 CFR 29.351 - Yawing conditions.
Code of Federal Regulations, 2011 CFR
2011-01-01
... VNE— (1) Displace the cockpit directional control suddenly to the maximum deflection limited by the control stops or by the maximum pilot force specified in § 29.397(a); (2) Attain a resulting sideslip angle or 90°, whichever is less; and (3) Return the directional control suddenly to neutral. (c) To...
14 CFR 31.19 - Performance: Uncontrolled descent.
Code of Federal Regulations, 2010 CFR
2010-01-01
... single failure of the heater assembly, fuel cell system, gas value system, or maneuvering vent system, or from any single tear in the balloon envelope between tear stoppers: (1) The maximum vertical velocity attained. (2) The altitude loss from the point of failure to the point at which maximum vertical velocity...
Code of Federal Regulations, 2010 CFR
2010-07-01
... application of the best available technology economically achievable (BAT). 432.113 Section 432.113 Protection... by the application of the best available technology economically achievable (BAT). Except as provided... representing the application of BAT: Effluent Limitations [BAT] Regulatedparameter Maximum daily 1 Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... application of the best available technology economically achievable (BAT). 432.13 Section 432.13 Protection... the application of the best available technology economically achievable (BAT). Except as provided in... representing the application of BAT: Effluent Limitations [BAT] Regulatedparameter Maximum daily 1 Maximum...
Code of Federal Regulations, 2010 CFR
2010-07-01
... application of the best available technology economically achievable (BAT). 432.13 Section 432.13 Protection... the application of the best available technology economically achievable (BAT). Except as provided in... representing the application of BAT: Effluent Limitations [BAT] Regulatedparameter Maximum daily 1 Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... application of the best available technology economically achievable (BAT). 432.113 Section 432.113 Protection... by the application of the best available technology economically achievable (BAT). Except as provided... representing the application of BAT: Effluent Limitations [BAT] Regulatedparameter Maximum daily 1 Maximum...
Code of Federal Regulations, 2010 CFR
2010-07-01
... and Secondary Germanium and Gallium Subcategory § 421.183 Effluent limitations guidelines representing... liquor. BAT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant or... and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly...
Code of Federal Regulations, 2012 CFR
2012-07-01
... and Secondary Germanium and Gallium Subcategory § 421.183 Effluent limitations guidelines representing... liquor. BAT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant or... and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly...
Code of Federal Regulations, 2013 CFR
2013-07-01
... and Secondary Germanium and Gallium Subcategory § 421.183 Effluent limitations guidelines representing... liquor. BAT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant or... and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly...
Code of Federal Regulations, 2014 CFR
2014-07-01
... and Secondary Germanium and Gallium Subcategory § 421.183 Effluent limitations guidelines representing... liquor. BAT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant or... and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly...
Code of Federal Regulations, 2012 CFR
2012-07-01
... CATEGORY Primary and Secondary Germanium and Gallium Subcategory § 421.182 Effluent limitations guidelines...) Still liquor. BPT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant... Secondary Germanium and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2010 CFR
2010-07-01
... CATEGORY Primary and Secondary Germanium and Gallium Subcategory § 421.182 Effluent limitations guidelines...) Still liquor. BPT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant... Secondary Germanium and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... and Secondary Germanium and Gallium Subcategory § 421.183 Effluent limitations guidelines representing... liquor. BAT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant or... and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly...
Code of Federal Regulations, 2014 CFR
2014-07-01
... CATEGORY Primary and Secondary Germanium and Gallium Subcategory § 421.182 Effluent limitations guidelines...) Still liquor. BPT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant... Secondary Germanium and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2013 CFR
2013-07-01
... CATEGORY Primary and Secondary Germanium and Gallium Subcategory § 421.182 Effluent limitations guidelines...) Still liquor. BPT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant... Secondary Germanium and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... CATEGORY Primary and Secondary Germanium and Gallium Subcategory § 421.182 Effluent limitations guidelines...) Still liquor. BPT Limitations for the Primary and Secondary Germanium and Gallium Subcategory Pollutant... Secondary Germanium and Gallium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Bubble formation in water with addition of a hydrophobic solute.
Okamoto, Ryuichi; Onuki, Akira
2015-07-01
We show that phase separation can occur in a one-component liquid outside its coexistence curve (CX) with addition of a small amount of a solute. The solute concentration at the transition decreases with increasing the difference of the solvation chemical potential between liquid and gas. As a typical bubble-forming solute, we consider O2 in ambient liquid water, which exhibits mild hydrophobicity and its critical temperature is lower than that of water. Such a solute can be expelled from the liquid to form gaseous domains while the surrounding liquid pressure is higher than the saturated vapor pressure p cx. This solute-induced bubble formation is a first-order transition in bulk and on a partially dried wall, while a gas film grows continuously on a completely dried wall. We set up a bubble free energy ΔG for bulk and surface bubbles with a small volume fraction ϕ. It becomes a function of the bubble radius R under the Laplace pressure balance. Then, for sufficiently large solute densities above a threshold, ΔG exhibits a local maximum at a critical radius and a minimum at an equilibrium radius. We also examine solute-induced nucleation taking place outside CX, where bubbles larger than the critical radius grow until attainment of equilibrium.
Hydrogen storage and phase transformations in Mg-Pd nanoparticles
NASA Astrophysics Data System (ADS)
Callini, E.; Pasquini, L.; Rude, L. H.; Nielsen, T. K.; Jensen, T. R.; Bonetti, E.
2010-10-01
Microstructure refinement and synergic coupling among different phases are currently explored strategies to improve the hydrogen storage properties of traditional materials. In this work, we apply a combination of these methods and synthesize Mg-Pd composite nanoparticles by inert gas condensation of Mg vapors followed by vacuum evaporation of Pd clusters. Irreversible formation of the Mg6Pd intermetallic phase takes place upon vacuum annealing, resulting in Mg/Mg6Pd composite nanoparticles. Their hydrogen storage properties are investigated and connected to the undergoing phase transformations by gas-volumetric techniques and in situ synchrotron radiation powder x-ray diffraction. Mg6Pd transforms reversibly into different Mg-Pd intermetallic compounds upon hydrogen absorption, depending on temperature and pressure. In particular, at 573 K and 1 MPa hydrogen pressure, the metal-hydride transition leads to the formation of Mg3Pd and Mg5Pd2 phases. By increasing the pressure to 5 MPa, the Pd-richer MgPd intermetallic is obtained. Upon hydrogen desorption, the Mg6Pd phase is reversibly recovered. These phase transformations result in a specific hydrogen storage capacity associated with Mg-Pd intermetallics, which attain the maximum value of 3.96 wt % for MgPd and influence both the thermodynamics and kinetics of hydrogen sorption in the composite nanoparticles.
NASA Astrophysics Data System (ADS)
Elias, M. M.; Saidur, R.; Ben-Mansour, R.; Hepbasli, A.; Rahim, N. A.; Jesbains, K.
2018-04-01
Nanofluid is a new class of engineering fluid that has good heat transfer characteristics which is essential to increase the heat transfer performance in various engineering applications such as heat exchangers and cooling of electronics. In this study, experiments were conducted to compare the heat transfer performance and pressure drop characteristics in a plate heat exchanger (PHE) for 30° and 60° chevron angles using water based Al2O3 nanofluid at the concentrations from 0 to 0.5 vol.% for different Reynolds numbers. The thermo-physical properties has been determined and presented in this paper. At 0.5 vol% concentration, the maximum heat transfer coefficient, the overall heat transfer coefficient and the heat transfer rate for 60° chevron angle have attained a higher percentage of 15.14%, 7.8% and 15.4%, respectively in comparison with the base fluid. Consequently, when the volume concentration or Reynolds number increases, the heat transfer coefficient and the overall heat transfer coefficient as well as the heat transfer rate of the PHE (Plate Heat Exchangers) increases respectively. Similarly, the pressure drop increases with the volume concentration. 60° chevron angle showed better performance in comparison with 30° chevron angle.
NASA Astrophysics Data System (ADS)
Pereira, Juliana S. F.; Mello, Paola A.; Moraes, Diogo P.; Duarte, Fábio A.; Dressler, Valderi L.; Knapp, Guenter; Flores, Érico M. M.
2009-06-01
In this study, microwave-induced combustion (MIC) of extra-heavy crude oil is proposed for further chlorine and sulfur determination by inductively coupled plasma optical emission spectrometry (ICP OES). Combustion was carried out under oxygen pressure (20 bar) in quartz vessels using ammonium nitrate (50 µl of 6 mol l - 1 solution) as ignition aid. Samples were wrapped with polyethylene film and placed on a quartz holder positioned inside the quartz vessels. The need for an additional reflux step after combustion and the type and concentration of absorbing solution (water, 0.02 to 0.9 mmol l - 1 H 2O 2, 10 to 100 mmol l - 1 (NH 4) 2CO 3 or 0.1 to 14 mol l - 1 HNO 3) were studied. The influence of sample mass, O 2 pressure and maximum pressure attained during the combustion process were investigated. Recoveries from 92 to 102% were obtained for Cl and S for all absorbing solutions. For comparison, Cl and S determination was also performed by ion chromatography (IC) using 25 mmol l - 1 (NH 4) 2CO 3 as absorbing solution. Using MIC with a reflux step the agreement was better than 95% for certified reference materials of similar composition (crude oil, petroleum coke, coal and residual fuel oil). Microwave-assisted digestion and water extraction in high pressure closed vessels were also evaluated. Using these procedures the maximum recoveries were 30 and 98% for Cl and S, respectively, using microwave-assisted digestion and 70% for Cl and less than 1% for S by water extraction procedure. Limits of detection by ICP OES were 12 and 5 µg g - 1 for Cl and S, respectively, and the corresponding values by IC were 1.2 and 8 µg g - 1 . Using MIC it was possible to digest simultaneously up to eight samples resulting in a solution suitable for the determination of both analytes with a single combustion step.
49 CFR 192.619 - Maximum allowable operating pressure: Steel or plastic pipelines.
Code of Federal Regulations, 2013 CFR
2013-10-01
... 49 Transportation 3 2013-10-01 2013-10-01 false Maximum allowable operating pressure: Steel or... Operations § 192.619 Maximum allowable operating pressure: Steel or plastic pipelines. (a) No person may operate a segment of steel or plastic pipeline at a pressure that exceeds a maximum allowable operating...
49 CFR 192.619 - Maximum allowable operating pressure: Steel or plastic pipelines.
Code of Federal Regulations, 2011 CFR
2011-10-01
... 49 Transportation 3 2011-10-01 2011-10-01 false Maximum allowable operating pressure: Steel or... Operations § 192.619 Maximum allowable operating pressure: Steel or plastic pipelines. (a) No person may operate a segment of steel or plastic pipeline at a pressure that exceeds a maximum allowable operating...
49 CFR 192.619 - Maximum allowable operating pressure: Steel or plastic pipelines.
Code of Federal Regulations, 2012 CFR
2012-10-01
... 49 Transportation 3 2012-10-01 2012-10-01 false Maximum allowable operating pressure: Steel or... Operations § 192.619 Maximum allowable operating pressure: Steel or plastic pipelines. (a) No person may operate a segment of steel or plastic pipeline at a pressure that exceeds a maximum allowable operating...
49 CFR 192.619 - Maximum allowable operating pressure: Steel or plastic pipelines.
Code of Federal Regulations, 2014 CFR
2014-10-01
... 49 Transportation 3 2014-10-01 2014-10-01 false Maximum allowable operating pressure: Steel or... Operations § 192.619 Maximum allowable operating pressure: Steel or plastic pipelines. (a) No person may operate a segment of steel or plastic pipeline at a pressure that exceeds a maximum allowable operating...
Maximum static inspiratory and expiratory pressures with different lung volumes
Lausted, Christopher G; Johnson, Arthur T; Scott, William H; Johnson, Monique M; Coyne, Karen M; Coursey, Derya C
2006-01-01
Background Maximum pressures developed by the respiratory muscles can indicate the health of the respiratory system, help to determine maximum respiratory flow rates, and contribute to respiratory power development. Past measurements of maximum pressures have been found to be inadequate for inclusion in some exercise models involving respiration. Methods Maximum inspiratory and expiratory airway pressures were measured over a range of lung volumes in 29 female and 19 male adults. A commercial bell spirometry system was programmed to occlude airflow at nine target lung volumes ranging from 10% to 90% of vital capacity. Results In women, maximum expiratory pressure increased with volume from 39 to 61 cmH2O and maximum inspiratory pressure decreased with volume from 66 to 28 cmH2O. In men, maximum expiratory pressure increased with volume from 63 to 97 cmH2O and maximum inspiratory pressure decreased with volume from 97 to 39 cmH2O. Equations describing pressures for both sexes are: Pe/Pmax = 0.1426 Ln( %VC) + 0.3402 R2 = 0.95 Pi/Pmax = 0.234 Ln(100 - %VC) - 0.0828 R2 = 0.96 Conclusion These results were found to be consistent with values and trends obtained by other authors. Regression equations may be suitable for respiratory mechanics models. PMID:16677384
Code of Federal Regulations, 2010 CFR
2010-07-01
... Tin Subcategory § 421.293 Effluent limitations guidelines representing the degree of effluent... application of the best available technology economically achievable: (a) Tin smelter SO2 scrubber. BAT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2013 CFR
2013-07-01
... Tin Subcategory § 421.293 Effluent limitations guidelines representing the degree of effluent... application of the best available technology economically achievable: (a) Tin smelter SO2 scrubber. BAT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Tin Subcategory § 421.293 Effluent limitations guidelines representing the degree of effluent... application of the best available technology economically achievable: (a) Tin smelter SO2 scrubber. BAT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Tin Subcategory § 421.293 Effluent limitations guidelines representing the degree of effluent... application of the best available technology economically achievable: (a) Tin smelter SO2 scrubber. BAT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... Tin Subcategory § 421.293 Effluent limitations guidelines representing the degree of effluent... application of the best available technology economically achievable: (a) Tin smelter SO2 scrubber. BAT Limitations for the Secondary Tin Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum...
Code of Federal Regulations, 2013 CFR
2013-07-01
... Uranium Subcategory § 421.323 Effluent limitations guidelines representing the degree of effluent... Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the refinery...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Uranium Subcategory § 421.323 Effluent limitations guidelines representing the degree of effluent... Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the refinery...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Uranium Subcategory § 421.323 Effluent limitations guidelines representing the degree of effluent... Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the refinery...
Code of Federal Regulations, 2014 CFR
2014-07-01
... CATEGORY Secondary Uranium Subcategory § 421.322 Effluent limitations guidelines representing the degree of... filtrate. BPT Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the...
Code of Federal Regulations, 2012 CFR
2012-07-01
... CATEGORY Secondary Uranium Subcategory § 421.322 Effluent limitations guidelines representing the degree of... filtrate. BPT Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the...
Code of Federal Regulations, 2013 CFR
2013-07-01
... CATEGORY Secondary Uranium Subcategory § 421.322 Effluent limitations guidelines representing the degree of... filtrate. BPT Limitations for the Secondary Uranium Subcategory Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of uranium processed in the...
14 CFR 23.441 - Maneuvering loads.
Code of Federal Regulations, 2010 CFR
2010-01-01
... conditions. In computing the loads, the yawing velocity may be assumed to be zero: (1) With the airplane in unaccelerated flight at zero yaw, it is assumed that the rudder control is suddenly displaced to the maximum... attainable steady state sideslip angle, with the rudder at maximum deflection caused by any one of the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... process generated waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity...
Code of Federal Regulations, 2011 CFR
2011-07-01
... waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Oyabu, Chikako; Ushigome, Emi; Matsumoto, Shinobu; Tanaka, Toru; Hasegawa, Goji; Nakamura, Naoto; Ohnishi, Masayoshi; Tsunoda, Sei; Ushigome, Hidetaka; Yokota, Isao; Tanaka, Muhei; Asano, Mai; Yamazaki, Masahiro; Fukui, Michiaki
2017-11-01
Maximum home systolic blood pressure has been shown to predict target organ damage. We aimed to clarify the association between maximum home systolic blood pressure and urine albumin to creatinine ratio, an indicator of early-phase diabetic nephropathy in patients with type 2 diabetes. In 1040 patients, we assessed the relationship of mean or maximum home systolic blood pressure and urine albumin to creatinine ratio, and compared the area under the receiver operating characteristic curve of mean or maximum home systolic blood pressure for diabetic nephropathy (urine albumin to creatinine ratio ⩾30 mg/g Cr). Multivariate linear regression analyses indicated that mean morning systolic blood pressure ( β = 0.010, p < 0.001) and maximum morning systolic blood pressure ( β = 0.008, p < 0.001) were significantly associated with urine albumin to creatinine ratio. Area under the receiver operating characteristic curve (95% confidence interval) for diabetic nephropathy in mean and maximum morning systolic blood pressure was 0.667 (0.634-0.700; p < 0.001) and 0.671 (0.638-0.703; p < 0.001), respectively. Maximum home systolic blood pressure, as well as mean home systolic blood pressure, was significantly associated with diabetic nephropathy in patients with type 2 diabetes.
46 CFR 54.10-5 - Maximum allowable working pressure (reproduces UG-98).
Code of Federal Regulations, 2013 CFR
2013-10-01
... 46 Shipping 2 2013-10-01 2013-10-01 false Maximum allowable working pressure (reproduces UG-98). 54.10-5 Section 54.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING PRESSURE VESSELS Inspection, Reports, and Stamping § 54.10-5 Maximum allowable working pressure (reproduces UG-98). (a) The maximum allowable...
46 CFR 54.10-5 - Maximum allowable working pressure (reproduces UG-98).
Code of Federal Regulations, 2011 CFR
2011-10-01
... 46 Shipping 2 2011-10-01 2011-10-01 false Maximum allowable working pressure (reproduces UG-98). 54.10-5 Section 54.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING PRESSURE VESSELS Inspection, Reports, and Stamping § 54.10-5 Maximum allowable working pressure (reproduces UG-98). (a) The maximum allowable...
46 CFR 54.10-5 - Maximum allowable working pressure (reproduces UG-98).
Code of Federal Regulations, 2014 CFR
2014-10-01
... 46 Shipping 2 2014-10-01 2014-10-01 false Maximum allowable working pressure (reproduces UG-98). 54.10-5 Section 54.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING PRESSURE VESSELS Inspection, Reports, and Stamping § 54.10-5 Maximum allowable working pressure (reproduces UG-98). (a) The maximum allowable...
46 CFR 54.10-5 - Maximum allowable working pressure (reproduces UG-98).
Code of Federal Regulations, 2012 CFR
2012-10-01
... 46 Shipping 2 2012-10-01 2012-10-01 false Maximum allowable working pressure (reproduces UG-98). 54.10-5 Section 54.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING PRESSURE VESSELS Inspection, Reports, and Stamping § 54.10-5 Maximum allowable working pressure (reproduces UG-98). (a) The maximum allowable...
On measurement of the isotropy of the maximum attainable speed
NASA Astrophysics Data System (ADS)
Wojtsekhowski, Bogdan
2015-04-01
A proposal for a precision experiment to investigate possible anisotropy of the maximum attainable speed (MAS) will be presented. It is based on an electron/positron beam with a large Lorentz factor and a 180-degree magnetic arc. The ratio of the momenta at the two ends of the magnetic arc will be used to form an observable which is sensitive to the MAS variation and immune to most of the instabilities of the apparatus. The search will use the sidereal periodicity of a potential signal. The uncertainty of momenta measurement could be greatly reduced by means of the electron and positron beams simultaneously rotating in the same magnetic system. The projected sensitivity of the measurement and the implications will be discussed.
Clinical application of diadenosine tetraphosphate (Ap4A:F-1500) for controlled hypotension.
Kikuta, Y; Ohiwa, E; Okada, K; Watanabe, A; Haruki, S
1999-01-01
In our animal study, it was revealed that diadenosine tetraphosphate (Ap4A:F-1500) has a dose-dependent hypotension effect of up to 60% decrease in mean arterial pressure compared to control value. Furthermore, in healthy male volunteers, the safety of Ap4A up to 4 mg.min-1 was confirmed. In patients who require surgical procedures under general anesthesia together with controlled hypotension, hypotension was induced by Ap4A in order to examine its hypotensive effect and modulating action on the blood pressure. Ten patients who required controlled hypotension and who were scheduled for elective surgery under general anesthesia were studied. Anesthesia was maintained with isoflurane (n = 7) or sevoflurane (n = 3) in oxygen-nitrous oxide. Controlled hypotension was induced by Ap4A administered at a rate of 10-20 micrograms.kg-1.min-1. The dose was adjusted at a maximum rate of 80 micrograms.kg-1.min-1 until the target blood pressure was achieved. Arterial blood pressure and heart rate were monitored. Arterial samples were drawn at 4 separate time points to measure the concentration of Ap4A in the plasma. The time required for attaining the target blood pressure after initiation of Ap4A infusion was about 16 min, and the time lapse between withdrawal of infusion to recovery of blood pressure was about 18 min. No reflex tachycardia was observed during infusion of Ap4A and no rebound hypertension was evident after withdrawal. The plasma Ap4A concentration increased in response to the acceleration rate of Ap4A administration with a tendency of augmented hypotensive effect. As it produces an excellent hypotensive effect together with a modulating action on blood pressure, Ap4A was assessed as useful in producing controlled hypotension.
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS NONFERROUS METALS MANUFACTURING POINT SOURCE... contained in sodium antimonate product Antimony 44.840 20.000 Arsenic 32.650 14.530 Mercury 3.906 1.562... Maximum for any 1 day Maximum for monthly average mg/kg (pounds per million pounds) of antimony metal...
Code of Federal Regulations, 2011 CFR
2011-07-01
... of process waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment. The height difference between the maximum safe surge capacity level and the...
Code of Federal Regulations, 2011 CFR
2011-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS METAL MOLDING AND CASTING POINT SOURCE CATEGORY Zinc Casting... copper, lead, zinc, and total phenols. For non-continuous dischargers, annual average mass limitations....0187 Lead (T) 0.0237 0.0116 Zinc (T) 0.0339 0.0129 Maximum for any 1 day Maximum for monthly average...
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS METAL MOLDING AND CASTING POINT SOURCE CATEGORY Zinc Casting... copper, lead, zinc, and total phenols. For non-continuous dischargers, annual average mass limitations....0187 Lead (T) 0.0237 0.0116 Zinc (T) 0.0339 0.0129 Maximum for any 1 day Maximum for monthly average...
Code of Federal Regulations, 2013 CFR
2013-07-01
... for the finishing water processes at a point source times the following pollutant concentrations: Subpart C [Finishing water] Concentration used to calculate BPT effluent limitations Pollutant or pollutant property Maximum for any 1 day (mg/l) Maximum for monthly average (mg/l) TSS 130 37 pH (1) (1) 1...
Code of Federal Regulations, 2011 CFR
2011-07-01
... finishing water processes at a point source times the following pollutant concentrations: Subpart C [Finishing water] Concentration used to calculate BPT effluent limitations Pollutant or pollutant property Maximum for any 1 day (mg/l) Maximum for monthly average (mg/l) TSS 130 37 pH (1) (1) 1 Within the range...
Code of Federal Regulations, 2012 CFR
2012-07-01
... for the finishing water processes at a point source times the following pollutant concentrations: Subpart C [Finishing water] Concentration used to calculate BPT effluent limitations Pollutant or pollutant property Maximum for any 1 day (mg/l) Maximum for monthly average (mg/l) TSS 130 37 pH (1) (1) 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... for the finishing water processes at a point source times the following pollutant concentrations: Subpart C [Finishing water] Concentration used to calculate BPT effluent limitations Pollutant or pollutant property Maximum for any 1 day (mg/l) Maximum for monthly average (mg/l) TSS 130 37 pH (1) (1) 1...
Ren, Shuai; Cai, Maolin; Shi, Yan; Xu, Weiqing; Zhang, Xiaohua Douglas
2018-03-01
Bronchial diameter is a key parameter that affects the respiratory treatment of mechanically ventilated patients. In this paper, to reveal the influence of bronchial diameter on the airflow dynamics of pressure-controlled mechanically ventilated patients, a new respiratory system model is presented that combines multigeneration airways with lungs. Furthermore, experiments and simulation studies to verify the model are performed. Finally, through the simulation study, it can be determined that in airway generations 2 to 7, when the diameter is reduced to half of the original value, the maximum air pressure (maximum air pressure in lungs) decreases by nearly 16%, the maximum flow decreases by nearly 30%, and the total airway pressure loss (sum of each generation pressure drop) is more than 5 times the original value. Moreover, in airway generations 8 to 16, with increasing diameter, the maximum air pressure, maximum flow, and total airway pressure loss remain almost constant. When the diameter is reduced to half of the original value, the maximum air pressure decreases by 3%, the maximum flow decreases by nearly 5%, and the total airway pressure loss increases by 200%. The study creates a foundation for improvement in respiratory disease diagnosis and treatment. Copyright © 2017 John Wiley & Sons, Ltd.
Advanced engine study for mixed-mode orbit-transfer vehicles
NASA Technical Reports Server (NTRS)
Mellish, J. A.
1978-01-01
Engine design, performance, weight and envelope data were established for three mixed-mode orbit-transfer vehicle engine candidates. Engine concepts evaluated are the tripropellant, dual-expander and plug cluster. Oxygen, RP-1 and hydrogen are the propellants considered for use in these engines. Theoretical performance and propellant properties were established for bipropellant and tripropellant mixes of these propellants. RP-1, hydrogen and oxygen were evaluated as coolants and the maximum attainable chamber pressures were determined for each engine concept within the constraints of the propellant properties and the low cycle thermal fatigue (300 cycles) requirement. The baseline engine design and component operating characteristics are determined at a thrust level of 88,964N (20,000 lbs) and a thrust split of 0.5. The parametric data is generated over ranges of thrust and thrust split of 66.7 to 400kN (15 to 90 klb) and 0.4 to 0.8, respectively.
A New Method to Measure Temperature and Burner Pattern Factor Sensing for Active Engine Control
NASA Technical Reports Server (NTRS)
Ng, Daniel
1999-01-01
The determination of the temperatures of extended surfaces which exhibit non-uniform temperature variation is very important for a number of applications including the "Burner Pattern Factor" (BPF) of turbine engines. Exploratory work has shown that use of BPF to control engine functions can result in many benefits, among them reduction in engine weight, reduction in operating cost, increase in engine life, while attaining maximum engine efficiency. Advanced engines are expected to operate at very high temperature to achieve high efficiency. Brief exposure of engine components to higher than design temperatures due to non-uniformity in engine burner pattern can reduce engine life. The engine BPF is a measure of engine temperature uniformity. Attainment of maximum temperature uniformity and high temperatures is key to maximum efficiency and long life. A new approach to determine through the measurement of just one radiation spectrum by a multiwavelength pyrometer is possible. This paper discusses a new temperature sensing approach and its application to determine the BPF.
The trade-off characteristics of acoustic and pressure sensors for the NASP
NASA Technical Reports Server (NTRS)
Winkler, Martin; Bush, Chuck
1992-01-01
Results of a trade study for the development of pressure and acoustic sensors for use on the National Aerospace Plane (NASP) are summarized. Pressure sensors are needed to operate to 100 psia; acoustic sensors are needed that can give meaningful information about a 200 dB sound pressure level (SPL) environment. Both sensors will have to operate from a high temperature of 2000 F down to absolute zero. The main conclusions of the study are the following: (1) Diaphragm materials limit minimum size and maximum frequency response attainable. (2) No transduction is available to meet all the NASP requirements with existing technology. (3) Capacitive sensors are large relative to the requirement, have limited resolution and frequency response due to noise, and cable length is limited to approximately 20 feet. (4) Eddy current sensors are large relative to the requirement and have limited cable lengths. (5) Fiber optic sensors provide the possibility for a small sensor, even though present developments do not exhibit that characteristic. The need to use sapphire at high temperature complicates the design. Present high temperature research sensors suffer from poor resolution. A significant development effort will be required to realize the potential of fiber optics. (6) Short-term development seems to favor eddy current techniques with the penalty of larger size and reduced dynamic range for acoustic sensors. (7) Long-term development may favor fiber optics with the penalties of cost, schedule, and uncertainty.
NASA Astrophysics Data System (ADS)
Xu, Bing; Hu, Min; Zhang, Junhui
2015-09-01
The current research about the flow ripple of axial piston pump mainly focuses on the effect of the structure of parts on the flow ripple. Therein, the structure of parts are usually designed and optimized at rated working conditions. However, the pump usually has to work in large-scale and time-variant working conditions. Therefore, the flow ripple characteristics of pump and analysis for its test accuracy with respect to variant steady-state conditions and transient conditions in a wide range of operating parameters are focused in this paper. First, a simulation model has been constructed, which takes the kinematics of oil film within friction pairs into account for higher accuracy. Afterwards, a test bed which adopts Secondary Source Method is built to verify the model. The simulation and tests results show that the angular position of the piston, corresponding to the position where the peak flow ripple is produced, varies with the different pressure. The pulsating amplitude and pulsation rate of flow ripple increase with the rise of pressure and the variation rate of pressure. For the pump working at a constant speed, the flow pulsation rate decreases dramatically with the increasing speed when the speed is less than 27.78% of the maximum speed, subsequently presents a small decrease tendency with the speed further increasing. With the rise of the variation rate of speed, the pulsating amplitude and pulsation rate of flow ripple increase. As the swash plate angle augments, the pulsating amplitude of flow ripple increases, nevertheless the flow pulsation rate decreases. In contrast with the effect of the variation of pressure, the test accuracy of flow ripple is more sensitive to the variation of speed. It makes the test accuracy above 96.20% available for the pulsating amplitude of pressure deviating within a range of ±6% from the mean pressure. However, with a variation of speed deviating within a range of ±2% from the mean speed, the attainable test accuracy of flow ripple is above 93.07%. The model constructed in this research proposes a method to determine the flow ripple characteristics of pump and its attainable test accuracy under the large-scale and time-variant working conditions. Meanwhile, a discussion about the variation of flow ripple and its obtainable test accuracy with the conditions of the pump working in wide operating ranges is given as well.
Razus, D; Brinzea, V; Mitu, M; Movileanu, C; Oancea, D
2011-06-15
The maximum rates of pressure rise during closed vessel explosions of propane-air mixtures are reported, for systems with various initial concentrations, pressures 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 pressure rise is examined against the adiabatic deflagration index, K(G, ad), computed from normal burning velocities and peak explosion pressures. At constant temperature and fuel/oxygen ratio, both the maximum rates of pressure rise and the deflagration indices are linear functions of total initial pressure, as reported for other fuel-air mixtures. At constant initial pressure and composition, the maximum rates of pressure rise and deflagration indices are slightly influenced by the initial temperature; some influence of the initial temperature on maximum rates of pressure rise is observed only for propane-air mixtures far from stoichiometric composition. The differentiated temperature influence on the normal burning velocities and the peak explosion pressures might explain this behaviour. Copyright © 2011 Elsevier B.V. All rights reserved.
Law of damage accumulation and fracture criteria in highly filled polymer materials
NASA Astrophysics Data System (ADS)
Bykov, D. L.; Kazakov, A. V.; Konovalov, D. N.; Mel'nikov, V. P.; Milyokhin, Yu. M.; Peleshko, V. A.; Sadovnichii, D. N.
2014-09-01
We present the results of a large series of experiments aimed at the study of laws of damage accumulation and fracture in highly filled polymer materials under loading conditions of various types: monotone, repeated, low- and high-cycle, with varying type of stress state, dynamic (in general, more than 50 programs implemented on specimens from one lot of material). The data obtained in these test allow one to make conclusions about the constitutive role of the attained maximum of strain intensity when estimating the accumulated damage in the process of uniaxial tension by various programs (in particular, an additional cyclic deformation below the preliminary attained strain maximum does not affect the limit values of strain and stress in the subsequent active extension), about the strong influence of the stress state on the deformation and fracture, about the specific features of the nonlinear behavior of the material under the shock loading conditions and its influence on the repeated deformation. All tests are described (with an accuracy acceptable in practical calculations, both with respect to stresses and strains in the process of loading and at the moment of fracture) in the framework of the same model of nonlinear viscoelasticity with the same set of constants. The constants of the proposed model are calculated according to a relatively simple algorithm by using the results of standard uniaxial tension tests with constant values of the strain rate and hydrostatic pressure (each test for 2-3 levels of these parameters chosen from the ranges proposed in applications, each loading lasts until the fracture occurs, and one of the tests contains an intermediate interval of total loading and repeated loading) and one axial shock compression test if there are dynamic problems in the applications. The model is based on the use of the criterion fracture parameter which, in the class of proportional loading processes, is the sum of partial increments of the strain intensity on active segments of the process (where the strain intensity is at its historical maximum) with the form of the stress state and the intensity of strain rates taken into account.
49 CFR 195.406 - Maximum operating pressure.
Code of Federal Regulations, 2010 CFR
2010-10-01
... HAZARDOUS LIQUIDS BY PIPELINE Operation and Maintenance § 195.406 Maximum operating pressure. (a) Except for surge pressures and other variations from normal operations, no operator may operate a pipeline at a... 49 Transportation 3 2010-10-01 2010-10-01 false Maximum operating pressure. 195.406 Section 195...
49 CFR 195.406 - Maximum operating pressure.
Code of Federal Regulations, 2012 CFR
2012-10-01
... HAZARDOUS LIQUIDS BY PIPELINE Operation and Maintenance § 195.406 Maximum operating pressure. (a) Except for surge pressures and other variations from normal operations, no operator may operate a pipeline at a... 49 Transportation 3 2012-10-01 2012-10-01 false Maximum operating pressure. 195.406 Section 195...
49 CFR 195.406 - Maximum operating pressure.
Code of Federal Regulations, 2014 CFR
2014-10-01
... HAZARDOUS LIQUIDS BY PIPELINE Operation and Maintenance § 195.406 Maximum operating pressure. (a) Except for surge pressures and other variations from normal operations, no operator may operate a pipeline at a... 49 Transportation 3 2014-10-01 2014-10-01 false Maximum operating pressure. 195.406 Section 195...
49 CFR 195.406 - Maximum operating pressure.
Code of Federal Regulations, 2011 CFR
2011-10-01
... HAZARDOUS LIQUIDS BY PIPELINE Operation and Maintenance § 195.406 Maximum operating pressure. (a) Except for surge pressures and other variations from normal operations, no operator may operate a pipeline at a... 49 Transportation 3 2011-10-01 2011-10-01 false Maximum operating pressure. 195.406 Section 195...
49 CFR 195.406 - Maximum operating pressure.
Code of Federal Regulations, 2013 CFR
2013-10-01
... HAZARDOUS LIQUIDS BY PIPELINE Operation and Maintenance § 195.406 Maximum operating pressure. (a) Except for surge pressures and other variations from normal operations, no operator may operate a pipeline at a... 49 Transportation 3 2013-10-01 2013-10-01 false Maximum operating pressure. 195.406 Section 195...
Code of Federal Regulations, 2014 CFR
2014-07-01
... renewable resources and approach the maximum attainable recycling of depletable resources. (b) As an.... Consideration must be given to reasonable alternative means of achieving the purpose and need for the proposed...
Code of Federal Regulations, 2011 CFR
2011-07-01
... renewable resources and approach the maximum attainable recycling of depletable resources. (b) As an.... Consideration must be given to reasonable alternative means of achieving the purpose and need for the proposed...
Code of Federal Regulations, 2013 CFR
2013-07-01
... renewable resources and approach the maximum attainable recycling of depletable resources. (b) As an.... Consideration must be given to reasonable alternative means of achieving the purpose and need for the proposed...
Code of Federal Regulations, 2012 CFR
2012-07-01
... renewable resources and approach the maximum attainable recycling of depletable resources. (b) As an.... Consideration must be given to reasonable alternative means of achieving the purpose and need for the proposed...
Code of Federal Regulations, 2010 CFR
2010-07-01
... renewable resources and approach the maximum attainable recycling of depletable resources. (b) As an.... Consideration must be given to reasonable alternative means of achieving the purpose and need for the proposed...
NASA Astrophysics Data System (ADS)
Alsing, Justin; Silva, Hector O.; Berti, Emanuele
2018-07-01
We infer the mass distribution of neutron stars in binary systems using a flexible Gaussian mixture model and use Bayesian model selection to explore evidence for multimodality and a sharp cut-off in the mass distribution. We find overwhelming evidence for a bimodal distribution, in agreement with previous literature, and report for the first time positive evidence for a sharp cut-off at a maximum neutron star mass. We measure the maximum mass to be 2.0 M⊙ < mmax < 2.2 M⊙ (68 per cent), 2.0 M⊙ < mmax < 2.6 M⊙ (90 per cent), and evidence for a cut-off is robust against the choice of model for the mass distribution and to removing the most extreme (highest mass) neutron stars from the data set. If this sharp cut-off is interpreted as the maximum stable neutron star mass allowed by the equation of state of dense matter, our measurement puts constraints on the equation of state. For a set of realistic equations of state that support >2 M⊙ neutron stars, our inference of mmax is able to distinguish between models at odds ratios of up to 12:1, whilst under a flexible piecewise polytropic equation-of-state model our maximum mass measurement improves constraints on the pressure at 3-7× the nuclear saturation density by ˜ 30-50 per cent compared to simply requiring mmax > 2 M⊙. We obtain a lower bound on the maximum sound speed attained inside the neutron star of c_ s^max > 0.63c (99.8 per cent), ruling out c_ s^max < c/√{3} at high significance. Our constraints on the maximum neutron star mass strengthen the case for neutron star-neutron star mergers as the primary source of short gamma-ray bursts.
46 CFR 151.03-37 - Maximum allowable working pressure.
Code of Federal Regulations, 2013 CFR
2013-10-01
... 46 Shipping 5 2013-10-01 2013-10-01 false Maximum allowable working pressure. 151.03-37 Section 151.03-37 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) CERTAIN BULK DANGEROUS CARGOES BARGES CARRYING BULK LIQUID HAZARDOUS MATERIAL CARGOES Definitions § 151.03-37 Maximum allowable working pressure. The maximum allowable working...
46 CFR 151.03-37 - Maximum allowable working pressure.
Code of Federal Regulations, 2012 CFR
2012-10-01
... 46 Shipping 5 2012-10-01 2012-10-01 false Maximum allowable working pressure. 151.03-37 Section 151.03-37 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) CERTAIN BULK DANGEROUS CARGOES BARGES CARRYING BULK LIQUID HAZARDOUS MATERIAL CARGOES Definitions § 151.03-37 Maximum allowable working pressure. The maximum allowable working...
46 CFR 151.03-37 - Maximum allowable working pressure.
Code of Federal Regulations, 2011 CFR
2011-10-01
... 46 Shipping 5 2011-10-01 2011-10-01 false Maximum allowable working pressure. 151.03-37 Section 151.03-37 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) CERTAIN BULK DANGEROUS CARGOES BARGES CARRYING BULK LIQUID HAZARDOUS MATERIAL CARGOES Definitions § 151.03-37 Maximum allowable working pressure. The maximum allowable working...
46 CFR 151.03-37 - Maximum allowable working pressure.
Code of Federal Regulations, 2010 CFR
2010-10-01
... 46 Shipping 5 2010-10-01 2010-10-01 false Maximum allowable working pressure. 151.03-37 Section 151.03-37 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) CERTAIN BULK DANGEROUS CARGOES BARGES CARRYING BULK LIQUID HAZARDOUS MATERIAL CARGOES Definitions § 151.03-37 Maximum allowable working pressure. The maximum allowable working...
46 CFR 151.03-37 - Maximum allowable working pressure.
Code of Federal Regulations, 2014 CFR
2014-10-01
... 46 Shipping 5 2014-10-01 2014-10-01 false Maximum allowable working pressure. 151.03-37 Section 151.03-37 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) CERTAIN BULK DANGEROUS CARGOES BARGES CARRYING BULK LIQUID HAZARDOUS MATERIAL CARGOES Definitions § 151.03-37 Maximum allowable working pressure. The maximum allowable working...
NASA Technical Reports Server (NTRS)
Beke, Andrew; Allen, J L
1953-01-01
Aerodynamic and performance characteristics of a conical spike nacelle-type inlet with two bypasses are presented at Mach numbers of 1.6, 1.8, and 2.0 for angles of attach up to 90 degrees. The bypasses were located 6 inlet diameters downstream of the inlet and were designed to discharge the bypass mass flow outward from the body axis. The inlet was designed to attain a mass-flow ratio of unity at a Mach number of 2.0. It is shown that discharging the bypass mass flow outward from the body nearly doubles the critical drag of a similar configuration but with bypass discharge in an axial direction. As a result of this greater drag, the net force on the model in the flight direction is reduced when comparison is made with the axial discharge case. The lift and pitching-moment coefficients are slightly higher than those for a configuration without bypasses. Approximately 25 % of the maximum inlet mass flow was discharged through the bypasses, and the pressure-recovery and mass-flow characteristics were in qualitative and quantitative agreement with the results of an investigation of a similar configuration with axial discharge.
Requirements for long-life operation of inert gas hollow cathodes: Preliminary report
NASA Technical Reports Server (NTRS)
Verhey, Timothy R.; Macrae, Gregory S.
1990-01-01
An experimental investigation was initiated to establish conditioning procedures for reliable hollow cathode operation via the characterization of critical parameters in a representative cathode test facility. From vacuum pumpdown rates, it was found that approximately 1.5 hours were required to achieve pressure levels within 5 percent of the lowest attainable pressure for this facility, depending on the purge conditions. The facility atmosphere was determined by a residual gas analyzer to be composed of primarily air and water vapor. The effects of vacuum pumping and inert gas purging were evaluated. A maximum effective leakage rate of 2.0 x 10(exp -3)sccm was observed and its probable causes were examined. An extended test of a 0.64 cm diameter Mo-Re hollow cathode was successfully completed. This test ran for 504 hours at an emission current of 23.0 amperes and a xenon flow rate of 6.1 sccm. Discharge voltage rose continuously from 15 to 21 volts over the course of the test. The temperature of the cathode body during the test was relatively stable at 1160 C. Post-test examination revealed ion-bombardment texturing of the orifice plate to be the only detectable sign of wear on the hollow cathode.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Music, Denis, E-mail: music@mch.rwth-aachen.de; Geyer, Richard W.; Hans, Marcus
2016-07-28
To increase the thermoelectric efficiency and reduce the thermal fatigue upon cyclic heat loading, alloying of amorphous NbO{sub 2} with all 3d and 5d transition metals has systematically been investigated using density functional theory. It was found that Ta fulfills the key design criteria, namely, enhancement of the Seebeck coefficient and positive Cauchy pressure (ductility gauge). These quantum mechanical predictions were validated by assessing the thermoelectric and elastic properties on combinatorial thin films, which is a high-throughput approach. The maximum power factor is 2813 μW m{sup −1} K{sup −2} for the Ta/Nb ratio of 0.25, which is a hundredfold increment compared to puremore » NbO{sub 2} and exceeds many oxide thermoelectrics. Based on the elasticity measurements, the consistency between theory and experiment for the Cauchy pressure was attained within 2%. On the basis of the electronic structure analysis, these configurations can be perceived as metallic, which is consistent with low electrical resistivity and ductile behavior. Furthermore, a pronounced quantum confinement effect occurs, which is identified as the physical origin for the Seebeck coefficient enhancement.« less
Code of Federal Regulations, 2010 CFR
2010-07-01
... for any 1 day Maximum for monthly average mg/troy ounce of precious metals, including silver.../troy ounce of precious metals in the granulated raw material Copper 0.819 0.390 Cyanide (total) 0.128 0... Maximum for monthly average mg/troy ounce of gold produced by cyanide stripping Copper 4.736 2.257 Cyanide...
Code of Federal Regulations, 2014 CFR
2014-07-01
... emulsion. Subpart J—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average... process wastewater pollutants. (g) Sawing or grinding spent emulsion. Subpart J—BPT Pollutant or pollutant... powder metallurgy parts sawed or ground with emulsion Copper 0.035 0.018 Cyanide 0.005 0.002 Lead 0.008 0...
Code of Federal Regulations, 2013 CFR
2013-07-01
... emulsion. Subpart J—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average... process wastewater pollutants. (g) Sawing or grinding spent emulsion. Subpart J—BPT Pollutant or pollutant... powder metallurgy parts sawed or ground with emulsion Copper 0.035 0.018 Cyanide 0.005 0.002 Lead 0.008 0...
Code of Federal Regulations, 2012 CFR
2012-07-01
... emulsion. Subpart J—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average... process wastewater pollutants. (g) Sawing or grinding spent emulsion. Subpart J—BPT Pollutant or pollutant... powder metallurgy parts sawed or ground with emulsion Copper 0.035 0.018 Cyanide 0.005 0.002 Lead 0.008 0...
Federal Register 2010, 2011, 2012, 2013, 2014
2011-12-22
... posting of the availability of the submittal on EPA's Adequacy Web site (at http://www.epa.gov/otaq... average annual fourth-highest daily maximum 8-hour average ozone concentration), if it had a 1-hour design... ozone standard is attained when the three-year average of the annual fourth-highest daily maximum 8-hour...
Code of Federal Regulations, 2010 CFR
2010-07-01
... Maximum for monthly average mg/kg (pounds per million pounds) of concentrate digested Lead .174 .081 Zinc... monthly average mg/Kg (pounds per million pounds) of concentrate digested Lead 2.592 1.203 Zinc 9.442 3... Maximum for monthly average mg/kg (pounds per million pounds) of concentrate digested Lead .069 .032 Zinc...
Code of Federal Regulations, 2011 CFR
2011-07-01
... Maximum for monthly average mg/kg (pounds per million pounds) of concentrate digested Lead .174 .081 Zinc... monthly average mg/Kg (pounds per million pounds) of concentrate digested Lead 2.592 1.203 Zinc 9.442 3... Maximum for monthly average mg/kg (pounds per million pounds) of concentrate digested Lead .069 .032 Zinc...
40 CFR 147.1803 - Existing Class I and III wells authorized by rule-maximum injection pressure.
Code of Federal Regulations, 2010 CFR
2010-07-01
... authorized by rule-maximum injection pressure. 147.1803 Section 147.1803 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) WATER PROGRAMS (CONTINUED) STATE, TRIBAL, AND EPA-ADMINISTERED...—maximum injection pressure. The owner or operator shall limit injection pressure to the lesser of: (a) A...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Pal, Karoly F.; Vertesi, Tamas
2010-08-15
The I{sub 3322} inequality is the simplest bipartite two-outcome Bell inequality beyond the Clauser-Horne-Shimony-Holt (CHSH) inequality, consisting of three two-outcome measurements per party. In the case of the CHSH inequality the maximal quantum violation can already be attained with local two-dimensional quantum systems; however, there is no such evidence for the I{sub 3322} inequality. In this paper a family of measurement operators and states is given which enables us to attain the maximum quantum value in an infinite-dimensional Hilbert space. Further, it is conjectured that our construction is optimal in the sense that measuring finite-dimensional quantum systems is not enoughmore » to achieve the true quantum maximum. We also describe an efficient iterative algorithm for computing quantum maximum of an arbitrary two-outcome Bell inequality in any given Hilbert space dimension. This algorithm played a key role in obtaining our results for the I{sub 3322} inequality, and we also applied it to improve on our previous results concerning the maximum quantum violation of several bipartite two-outcome Bell inequalities with up to five settings per party.« less
French, B; Potter, I C; Hesp, S A; Coulson, P G; Hall, N G
2014-01-01
Key biological characteristics of the harlequin fish Othos dentex, a representative of a monospecific genus of the Anthiinae (Serranidae), were determined from samples collected around reefs on the south coast of Western Australia. The females of this relatively long-lived species (maximum recorded age in this study = 37 years) attained only a slightly greater maximum total length and age than males and neither the length nor the age-frequency distributions showed a conspicuous sex-based bimodality. Furthermore, gonads from a wide size and age range of O. dentex were shown by histology, at several locations along their length, to always comprise exclusively either ovarian or testicular tissues. Thus, O. dentex is a gonochorist, a sexual pattern only previously recorded definitively for one other anthiine serranid, i.e. Epinephelides armatus, which also occurs in south-western Australia. Similar to E. armatus, O. dentex possesses 'solid' testes with a central sperm duct, thereby differing in structure from those typically found in serranids, in which there is a central membrane-bound 'ovarian' lumen and peripherally located sperm sinuses. The gonadal characteristics and sexual pattern of these two gonochoristic anthiines are not consistent with a recent proposal for the trends exhibited by the evolution of gonochorism and protogyny within the Serranidae. Othos dentex has indeterminate fecundity and a protracted spawning period (7 months) and, on the basis of underwater observations and a low gonado-somatic index (I(G)) for males, is a pair spawner, which is unusual for a gonochorist of a serranid or member of a related family. While the large spots on the lower half of the body of O. dentex are shown quantitatively to be similarly yellow in juveniles and adult females, they then become blue in males at maturity and this intensifies during the spawning period, when they presumably play an important role in agonistic interactions among males and courtship with females. The attainment of maturity and rapid growth by O. dentex early in life may reflect selection pressures to reduce predation mortality during that period. Total mortality in the population is moderately low during later life, implying that the current fishing pressure on O. dentex is relatively light. © 2014 The Fisheries Society of the British Isles.
NASA Technical Reports Server (NTRS)
Proctor, M. P.; Tien, J. S.
1985-01-01
A stainless steel, two-dimensional (rectangular), center-dump, premixed-prevaporized combustor with quartz window sidewalls for visual access was designed, built, and used to study flashback. A parametric study revealed that the flashback equivalence ratio decreased slightly as the inlet air temperature increased. It also indicated that the average premixer velocity and premixer wall temperature were not governing parameters of flashback. The steady-state velocity balance concept as the flashback mechanism was not supported. From visual observation several stages of burning were identified. High speed photography verified upstream flame propagation with the leading edge of the flame front near the premixer wall. Combustion instabilities (spontaneous pressure oscillations) were discovered during combustion at the dump plane and during flashback. The pressure oscillation frequency ranged from 40 to 80 Hz. The peak-to-peak amplitude (up to 1.4 psi) increased as the fuel/air equivalence ratio was increased attaining a maximum value just before flashback. The amplitude suddenly decreased when the flame stabilized in the premixer. The pressure oscillations were large enough to cause a local flow reversal. A simple test using ceramic fiber tufts indicated flow reversals existed at the premixer exit during flickering. It is suspected that flashback occurs through the premixer wall boundary layer flow reversal caused by combustion instability. A theoretical analysis of periodic flow in the premixing channel has been made. The theory supports the flow reversal mechanism.
40 CFR 63.7944 - How do I determine the maximum HAP vapor pressure of my remediation material?
Code of Federal Regulations, 2010 CFR
2010-07-01
... vapor pressure of my remediation material? 63.7944 Section 63.7944 Protection of Environment... Pollutants: Site Remediation Performance Tests § 63.7944 How do I determine the maximum HAP vapor pressure of my remediation material? (a) You must determine the maximum HAP vapor pressure of your remediation...
Utanohara, Yuri; Hayashi, Ryo; Yoshikawa, Mineka; Yoshida, Mitsuyoshi; Tsuga, Kazuhiro; Akagawa, Yasumasa
2008-09-01
It is clinically important to evaluate tongue function in terms of rehabilitation of swallowing and eating ability. We have developed a disposable tongue pressure measurement device designed for clinical use. In this study we used this device to determine standard values of maximum tongue pressure in adult Japanese. Eight hundred fifty-three subjects (408 male, 445 female; 20-79 years) were selected for this study. All participants had no history of dysphagia and maintained occlusal contact in the premolar and molar regions with their own teeth. A balloon-type disposable oral probe was used to measure tongue pressure by asking subjects to compress it onto the palate for 7 s with maximum voluntary effort. Values were recorded three times for each subject, and the mean values were defined as maximum tongue pressure. Although maximum tongue pressure was higher for males than for females in the 20-49-year age groups, there was no significant difference between males and females in the 50-79-year age groups. The maximum tongue pressure of the seventies age group was significantly lower than that of the twenties to fifties age groups. It may be concluded that maximum tongue pressures were reduced with primary aging. Males may become weaker with age at a faster rate than females; however, further decreases in strength were in parallel for male and female subjects.
McKinney, Timothy B; Babin, Elizabeth A; Ciolfi, Veronica; McKinney, Cynthia R; Shah, Nima
2018-04-01
Air-charged (AC) and water-perfused (WP) catheters have been evaluated for differences in measuring pressures for voiding dysfunction. Typically, a two-catheter system was used. We believe that simultaneous pressure measurements with AC and WP in a single catheter will provide analogous pressures for coughs, Valsalvas, and maximum pressures in voiding pressure 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 pressure 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 pressures. At maximum bladder capacity, VPS was done and maximum voiding pressure was recorded. Comparing coughs and Valsalva maneuvers pressures, 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 pressure measurements and had a strong correlation. Cystometrogram and maximum voiding pressure measurements done with either water or air charged catheters will yield similarly accurate results and are comparable. Results suggest more variability at low bladder volumes <50 mL. © 2018 Wiley Periodicals, Inc.
Kaczmarek, Maria; Stawińska-Witoszyńska, Barbara; Krzyżaniak, Alicja; Krzywińska-Wiewiorowska, Małgorzata; Siwińska, Aldona
2015-11-01
In Poland, there is no data on parental socioeconomic status (SES) as a potent risk factor in adolescent elevated blood pressure, although social differences in somatic growth and maturation of children and adolescents have been recorded since the 1980s. This study aimed to evaluate the association between parental SES and blood pressure levels of their adolescent offspring. A cross-sectional survey was carried out between 2009 and 2010 on a sample of 4941 students (2451 boys and 2490 girls) aged 10-18, participants in the ADOPOLNOR study. The depended outcome variable was the level of blood pressure (optimal, pre- and hypertension) and explanatory variables included place of residence and indicators of parental SES: family size, parental educational attainments and occupation status, income adequacy and family wealth. The final selected model of the multiple multinomial logistic regression analysis (MLRA) with backward elimination procedure revealed the multifactorial dependency of blood pressure levels on maternal educational attainment, paternal occupation and income adequacy interrelated to urbanization category of the place of residence after controlling for family history of hypertension, an adolescent's sex, age and weight status. Consistent rural-to-urban and socioeconomic gradients were found in prevalence of elevated blood pressure, which increased with continuous lines from large cities through small- to medium-sized cities to villages and from high-SES to low-SES familial environments. The adjusted likelihood of developing systolic and diastolic hypertension decreased with each step increase in maternal educational attainment and increased urbanization category. The likelihood of developing prehypertension decreased with increased urbanization category, maternal education, paternal employment status and income adequacy. Weight status appeared to be the strongest confounder of adolescent blood pressure level and, at the same time, a mediator between their blood pressure and parental SES. The findings of the present study confirmed socioeconomic disparities in blood pressure levels among adolescents. This calls for regularly performed blood pressure assessment and monitoring in the adolescent population. It is recommended to focus on obesity prevention and socioeconomic health inequalities by further trying to improve living and working conditions in adverse rural environments.
Running humans attain optimal elastic bounce in their teens.
Legramandi, Mario A; Schepens, Bénédicte; Cavagna, Giovanni A
2013-01-01
In an ideal elastic bounce of the body, the time during which mechanical energy is released during the push equals the time during which mechanical energy is absorbed during the brake, and the maximal upward velocity attained by the center of mass equals the maximal downward velocity. Deviations from this ideal model, prolonged push duration and lower upward velocity, have found to be greater in older than in younger adult humans. However it is not known how similarity to the elastic bounce changes during growth and whether an optimal elastic bounce is attained at some age. Here we show that similarity with the elastic bounce is minimal at 2 years and increases with age attaining a maximum at 13-16 years, concomitant with a mirror sixfold decrease of the impact deceleration peak following collision of the foot with the ground. These trends slowly reverse during the course of the lifespan.
Running humans attain optimal elastic bounce in their teens
Legramandi, Mario A.; Schepens, Bénédicte; Cavagna, Giovanni A.
2013-01-01
In an ideal elastic bounce of the body, the time during which mechanical energy is released during the push equals the time during which mechanical energy is absorbed during the brake, and the maximal upward velocity attained by the center of mass equals the maximal downward velocity. Deviations from this ideal model, prolonged push duration and lower upward velocity, have found to be greater in older than in younger adult humans. However it is not known how similarity to the elastic bounce changes during growth and whether an optimal elastic bounce is attained at some age. Here we show that similarity with the elastic bounce is minimal at 2 years and increases with age attaining a maximum at 13-16 years, concomitant with a mirror sixfold decrease of the impact deceleration peak following collision of the foot with the ground. These trends slowly reverse during the course of the lifespan. PMID:23419705
Code of Federal Regulations, 2011 CFR
2011-07-01
... Metallurgical Acid Plants Subcategory § 421.93 Effluent limitations guidelines representing the degree of...—Metallurgical Acid Plant—BAT Effluent Limitations Pollutant or pollutant property Maximum for any 1 day Maximum... 1.584 Cadmium 0.511 0.204 Copper 3.269 1.558 Lead 0.715 0.332 Zinc 2.605 1.073 Fluoride 1 89.390 50...
Code of Federal Regulations, 2010 CFR
2010-07-01
... Metallurgical Acid Plants Subcategory § 421.93 Effluent limitations guidelines representing the degree of...—Metallurgical Acid Plant—BAT Effluent Limitations Pollutant or pollutant property Maximum for any 1 day Maximum... 1.584 Cadmium 0.511 0.204 Copper 3.269 1.558 Lead 0.715 0.332 Zinc 2.605 1.073 Fluoride 1 89.390 50...
Code of Federal Regulations, 2011 CFR
2011-07-01
... 1.45 Silver 0.120 0.0351 Tin 0.409 0.120 Titanium 0.0947 0.0618 Vanadium 0.218 0.0662 Zinc 2.87 0.641 1 mg/L (ppm). 2 Within the range 6 to 9. (b) The following in-plant limitations apply to metal-bearing wastewater containing cyanide: In-Plant Limitations Regulatedparameter Maximum daily 1 Maximum...
Code of Federal Regulations, 2012 CFR
2012-07-01
... at all times. (p) Alkaline cleaning spent baths. Subpart D—BPT Pollutant or pollutant property... metals alkaline cleaned Cadmium 0.021 0.009 Copper 0.114 0.060 Cyanide 0.018 0.007 Silver 0.025 0.010 Oil...) Alkaline cleaning rinse. Subpart D—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for...
Code of Federal Regulations, 2013 CFR
2013-07-01
... at all times. (p) Alkaline cleaning spent baths. Subpart D—BPT Pollutant or pollutant property... metals alkaline cleaned Cadmium 0.021 0.009 Copper 0.114 0.060 Cyanide 0.018 0.007 Silver 0.025 0.010 Oil...) Alkaline cleaning rinse. Subpart D—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for...
Code of Federal Regulations, 2011 CFR
2011-07-01
....151 (j) Alkaline cleaning spent baths. Subpart H—BAT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/off-kg (pounds per million off-pounds) of zinc alkaline cleaned Chromium 0.002 0.0006 Copper 0.005 0.002 Cyanide 0.0007 0.0003 Zinc 0.004 0.002 (k) Alkaline cleaning rinse...
Code of Federal Regulations, 2014 CFR
2014-07-01
... at all times. (p) Alkaline cleaning spent baths. Subpart D—BPT Pollutant or pollutant property... metals alkaline cleaned Cadmium 0.021 0.009 Copper 0.114 0.060 Cyanide 0.018 0.007 Silver 0.025 0.010 Oil...) Alkaline cleaning rinse. Subpart D—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for...
Code of Federal Regulations, 2010 CFR
2010-07-01
....151 (j) Alkaline cleaning spent baths. Subpart H—BAT Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/off-kg (pounds per million off-pounds) of zinc alkaline cleaned Chromium 0.002 0.0006 Copper 0.005 0.002 Cyanide 0.0007 0.0003 Zinc 0.004 0.002 (k) Alkaline cleaning rinse...
Code of Federal Regulations, 2010 CFR
2010-07-01
... at all times. (p) Alkaline cleaning spent baths. Subpart D—BPT Pollutant or pollutant property... metals alkaline cleaned Cadmium 0.021 0.009 Copper 0.114 0.060 Cyanide 0.018 0.007 Silver 0.025 0.010 Oil...) Alkaline cleaning rinse. Subpart D—BPT Pollutant or pollutant property Maximum for any 1 day Maximum for...
Fournier, R.O.
1991-01-01
Pore-fluid pressure (Pf) > Ph has been encountered at the bottom of 3 geothermal exploration wells that attained temperatures > 370??C (at Larderello, Italy, at Nesjavellir, Iceland, and at The Geysers, California). Chemical sealing by deposition of minerals in veins appears to have allowed the development of the high Pf encountered in the above wells. The upper limit for the magnitude of Pf that can be attained is controlled by either the onset of shear fracturing (where differential stress is relatively high) that reopens clogged veins, or the hydraulic opening of new or old fractures (at relatively low values of differential stress). -from Author
NASA Astrophysics Data System (ADS)
Aamir, Muhammad; Liao, Qiang; Hong, Wang; Xun, Zhu; Song, Sihong; Sajid, Muhammad
2017-02-01
High heat transfer performance of spray cooling on structured surface might be an additional measure to increase the safety of an installation against any threat caused by rapid increase in the temperature. The purpose of present experimental study is to explore heat transfer performance of structured surface under different spray conditions and surface temperatures. Two cylindrical stainless steel samples were used, one with pyramid pins structured surface and other with smooth surface. Surface heat flux of 3.60, 3.46, 3.93 and 4.91 MW/m2 are estimated for sample initial average temperature of 600, 700, 800 and 900 °C, respectively for an inlet pressure of 1.0 MPa. A maximum cooling rate of 507 °C/s was estimated for an inlet pressure of 0.7 MPa at 900 °C for structured surface while for smooth surface maximum cooling rate of 356 °C/s was attained at 1.0 MPa for 700 °C. Structured surface performed better to exchange heat during spray cooling at initial sample temperature of 900 °C with a relative increase in surface heat flux by factor of 1.9, 1.56, 1.66 and 1.74 relative to smooth surface, for inlet pressure of 0.4, 0.7, 1.0 and 1.3 MPa, respectively. For smooth surface, a decreasing trend in estimated heat flux is observed, when initial sample temperature was increased from 600 to 900 °C. Temperature-based function specification method was utilized to estimate surface heat flux and surface temperature. Limited published work is available about the application of structured surface spray cooling techniques for safety of stainless steel structures at very high temperature scenario such as nuclear safety vessel and liquid natural gas storage tanks.
NASA Astrophysics Data System (ADS)
Targino, Admir Créso; Krecl, Patricia; Coraiola, Guilherme Conor
2014-07-01
Air temperature was monitored at 13 sites across the urban perimeter of a Brazilian midsize city in winter 2011. In this study, we show that the urban heat island (UHI) develops only at night and under certain weather conditions, and its intensity depends not only on the site's land cover but also on the meteorological setting. The urban heat island intensity was largest (6.6 °C) under lingering high-pressure conditions, milder (3.0 °C) under cold anticyclones and almost vanished (1.0 °C) during the passage of cold fronts. The cooling rates were calculated to monitor the growth and decay of the UHI over each specific synoptic setting. Over four contiguous days under the effect of a lingering high-pressure event, we observed that the onset of cooling was always at about 2 h before sunset. The reference site attained mean cooling rate of -2.6 °C h-1 at sunset, whilst the maximum urban rate was -1.2 °C h-1. Under a 3-day cold anticyclone episode, cooling also started about 2 h before sunset, and the difference between maximum rural (-2.0 °C h-1) and urban (-1.0 °C h-1) cooling rates diminished. Under cold-front conditions, the cooling rate was homogeneous for all sites and swang about zero throughout the day. The air temperature has a memory effect under lingering high-pressure conditions which intensified the UHI, in addition to the larger heat storage in the urban area. Cold anticyclone conditions promoted the development of the UHI; however, the cold air pool and relatively light winds smoothed out its intensity. Under the influence of cold fronts, the urban fabric had little effect on the city's air temperature field, and the UHI was imperceptible.
NASA Technical Reports Server (NTRS)
Grebowsky, J. M.; Hoegy, W. R.; Chen, T. C.
1993-01-01
Using a comprehensive ionospheric data set comprised of all available ion composition and plasma temperature measurements from satellites, the vertical distributions of ion composition and plasma temperatures are defined from middle latitudes up into the polar cap for summer conditions for altitudes below about 1200 km. These data are sufficient to allow a numerical estimation of the latitudinal variation of the light ion outflows from within the plasmasphere to the polar wind regions. The altitude at which significant light ion outflow begins is found to be lower during solar minimum conditions than during solar maximum. The H(+) outward speeds are of the order of 1 km/s near 1100 km during solar maximum but attain several km/s speeds for solar minimum. He(+) shows a similar altitude development of flow but attains polar cap speeds much less than 1 km/s at altitudes below 1100 km, particularly under solar maximum conditions. Outward flows are also found in the topside F-region for noontime magnetic flux tubes within the plasmasphere.
Maximum of the modulus of kernels in Gauss-Turan quadratures
NASA Astrophysics Data System (ADS)
Milovanovic, Gradimir V.; Spalevic, Miodrag M.; Pranic, Miroslav S.
2008-06-01
We study the kernels K_{n,s}(z) in the remainder terms R_{n,s}(f) of the Gauss-Turan quadrature formulae for analytic functions on elliptical contours with foci at pm 1 , when the weight omega is a generalized Chebyshev weight function. For the generalized Chebyshev weight of the first (third) kind, it is shown that the modulus of the kernel \\vert K_{n,s}(z)\\vert attains its maximum on the real axis (positive real semi-axis) for each ngeq n_0, n_0Dn_0(rho,s) . It was stated as a conjecture in [Mathematics of Computation 72 (2003), 1855-1872]. For the generalized Chebyshev weight of the second kind, in the case when the number of the nodes n in the corresponding Gauss-Turan quadrature formula is even, it is shown that the modulus of the kernel attains its maximum on the imaginary axis for each ngeq n_0, n_0Dn_0(rho,s) . Numerical examples are included. Retrieve articles in all Journals with MSC (1991): [41]41A55, [42]65D30, [43]65D32
49 CFR 192.619 - Maximum allowable operating pressure: Steel or plastic pipelines.
Code of Federal Regulations, 2010 CFR
2010-10-01
... plastic pipelines. 192.619 Section 192.619 Transportation Other Regulations Relating to Transportation... Operations § 192.619 Maximum allowable operating pressure: Steel or plastic pipelines. (a) No person may operate a segment of steel or plastic pipeline at a pressure that exceeds a maximum allowable operating...
NASA Astrophysics Data System (ADS)
Abir, Ahmed Musafi
Spacer grids are used in Pressurized Water Reactors (PWRs) fuel assemblies which enhances heat transfer from fuel rods. However, there remain regions of low turbulence in between the spacer grids. To enhance turbulence in these regions surface roughness is applied on the fuel rod walls. Meyer [1] used empirical correlations to predict heat transfer and friction factor for artificially roughened fuel rod bundles at High Performance Light Water Reactors (LWRs). Their applicability was tested by Carrilho at University of South Carolina's (USC) Single Heated Element Loop Tester (SHELT). He attained a heat transfer and friction factor enhancement of 50% and 45% respectively, using Inconel nuclear fuel rods with square transverse ribbed surface. Following him Najeeb conducted a similar study due to three dimensional diamond shaped blocks in turbulent flow. He recorded a maximum heat transfer enhancement of 83%. At present, several types of materials are being used for fuel rod cladding including Zircaloy, Uranium oxide, etc. But researchers are actively searching for new material that can be a more practical alternative. Silicon Carbide (SiC) has been identified as a material of interest for application as fuel rod cladding [2]. The current study deals with the experimental investigation to find out the friction factor increase of a SiC fuel rod with 3D surface roughness. The SiC rod was tested at USC's SHELT loop. The experiment was conducted in turbulent flowing Deionized (DI) water at steady state conditions. Measurements of Flow rate and pressure drop were made. The experimental results were also validated by Computational Fluid Dynamics (CFD) analysis in ANSYS Fluent. To simplify the CFD analysis and to save computational resources the 3D roughness was approximated as a 2D one. The friction factor results of the CFD investigation was found to lie within +/-8% of the experimental results. A CFD model was also run with the energy equation turned on, and a heat generation of 8 kW applied to the rod. A maximum heat transfer enhancement of 18.4% was achieved at the highest flow rate investigated (i.e. Re=109204).
Code of Federal Regulations, 2012 CFR
2012-10-01
... distribution systems. (a) No person may operate a low-pressure distribution system at a pressure high enough to...) No person may operate a low pressure distribution system at a pressure lower than the minimum... 49 Transportation 3 2012-10-01 2012-10-01 false Maximum and minimum allowable operating pressure...
Code of Federal Regulations, 2011 CFR
2011-10-01
... distribution systems. (a) No person may operate a low-pressure distribution system at a pressure high enough to...) No person may operate a low pressure distribution system at a pressure lower than the minimum... 49 Transportation 3 2011-10-01 2011-10-01 false Maximum and minimum allowable operating pressure...
Code of Federal Regulations, 2013 CFR
2013-10-01
... distribution systems. (a) No person may operate a low-pressure distribution system at a pressure high enough to...) No person may operate a low pressure distribution system at a pressure lower than the minimum... 49 Transportation 3 2013-10-01 2013-10-01 false Maximum and minimum allowable operating pressure...
Code of Federal Regulations, 2014 CFR
2014-10-01
... distribution systems. (a) No person may operate a low-pressure distribution system at a pressure high enough to...) No person may operate a low pressure distribution system at a pressure lower than the minimum... 49 Transportation 3 2014-10-01 2014-10-01 false Maximum and minimum allowable operating pressure...
Code of Federal Regulations, 2010 CFR
2010-10-01
... distribution systems. (a) No person may operate a low-pressure distribution system at a pressure high enough to...) No person may operate a low pressure distribution system at a pressure lower than the minimum... 49 Transportation 3 2010-10-01 2010-10-01 false Maximum and minimum allowable operating pressure...
Code of Federal Regulations, 2010 CFR
2010-07-01
... all mechanical barking installations: There shall be no discharge of process wastewater pollutants... hydraulic barking installations: Subpart A Pollutant or pollutant property BPT effluent limitations Maximum...
Code of Federal Regulations, 2011 CFR
2011-07-01
... all mechanical barking installations: There shall be no discharge of process wastewater pollutants... hydraulic barking installations: Subpart A Pollutant or pollutant property BPT effluent limitations Maximum...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS SUGAR PROCESSING POINT SOURCE CATEGORY Beet Sugar... beet sugar processing operation. Effluent characteristic Effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2011 CFR
2011-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS SUGAR PROCESSING POINT SOURCE CATEGORY Beet Sugar... beet sugar processing operation. Effluent characteristic Effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Calcium Chloride Production Subcategory § 415.42 Effluent limitations guidelines... available (BPT): Subpart D—Calcium Chloride Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2012 CFR
2012-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS SUGAR PROCESSING POINT SOURCE CATEGORY Beet Sugar... beet sugar processing operation. Effluent characteristic Effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2014 CFR
2014-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS SUGAR PROCESSING POINT SOURCE CATEGORY Beet Sugar... beet sugar processing operation. Effluent characteristic Effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2013 CFR
2013-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS SUGAR PROCESSING POINT SOURCE CATEGORY Beet Sugar... beet sugar processing operation. Effluent characteristic Effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS ORGANIC CHEMICALS, PLASTICS, AND SYNTHETIC FIBERS Thermoplastic... concentration listed in the following table. Effluent characteristics BPT Effluent Limitations 1 Maximum for any...
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS ORGANIC CHEMICALS, PLASTICS, AND SYNTHETIC FIBERS Thermosetting... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any...
Factors Relating to Student Grade Obsession: A Quantitative Correlational Study
ERIC Educational Resources Information Center
Thomas, Jacqueline
2011-01-01
The intense focus of students on grades attained in academia reflects a contemporary issue in higher education. The internal pressure that students experience regarding academics fuels student grade obsession. Researchers suggest that in addition to internal pressure, financial anxiety, the need to receive academic recognition and parental…
Magnetic resonance imaging of boiling induced by high intensity focused ultrasound
Khokhlova, Tatiana D.; Canney, Michael S.; Lee, Donghoon; Marro, Kenneth I.; Crum, Lawrence A.; Khokhlova, Vera A.; Bailey, Michael R.
2009-01-01
Both mechanically induced acoustic cavitation and thermally induced boiling can occur during high intensity focused ultrasound (HIFU) medical therapy. The goal was to monitor the temperature as boiling was approached using magnetic resonance imaging (MRI). Tissue phantoms were heated for 20 s in a 4.7-T magnet using a 2-MHz HIFU source with an aperture and radius of curvature of 44 mm. The peak focal pressure was 27.5 MPa with corresponding beam width of 0.5 mm. The temperature measured in a single MRI voxel by water proton resonance frequency shift attained a maximum value of only 73 °C after 7 s of continuous HIFU exposure when boiling started. Boiling was detected by visual observation, by appearance on the MR images, and by a marked change in the HIFU source power. Nonlinear modeling of the acoustic field combined with a heat transfer equation predicted 100 °C after 7 s of exposure. Averaging of the calculated temperature field over the volume of the MRI voxel (0.3×0.5×2 mm3) yielded a maximum of 73 °C that agreed with the MR thermometry measurement. These results have implications for the use of MRI-determined temperature values to guide treatments with clinical HIFU systems. PMID:19354416
Impact of Cubic Pin Finned Surface Structure Geometry upon Spray Cooling Heat Transfer
NASA Technical Reports Server (NTRS)
Silk, Eric A.; Kim, Jungho; Kiger, Ken
2005-01-01
Experiments were conducted to study the effects of enhanced surface structures on heat flux using spray cooling. The surface enhancements consisted of cubic pin fins machined on the top surface of copper heater blocks. The structure height, pitch, and width were parametrically vaned. Each copper block had a projected cross-sectional area of 2.0 sq cm. Measurements were also obtained on a heater block with a flat surface for baseline comparison purposes. A 2 x 2 nozzle array was used with PF-5060 as the working fluid. Thermal performance data were obtained under nominally degassed (chamber pressure of 41.4 kPa) and gassy conditions (chamber with N2 gas at 100.7 kPa) with a bulk fluid temperature of 20.5 C. Results for both the degassed and gassy cases show that structure width and separation distance have a dominant effect upon the heat transfer for the size ranges used. Cubic pin fin height had little impact upon heat flux. The maximum critical heat flux (CHF) attained for any of the surfaces was 121 W/sq cm, giving an enhancement of 51% relative to the flat surface case under nominally degassed conditions. The gassy case had a maximum CHF of 149 W/sq cm, giving an enhancement of 38% relative to the flat surface case.
Code of Federal Regulations, 2011 CFR
2011-07-01
... Copper 9.58 5.04 Cyanide 1.46 0.605 Lead 2.12 1.01 (b) Sizing spent emulsions. Subpart J—BAT Pollutant or... grinding spent emulsions. Subpart J—BAT Pollutant or pollutant property Maximum for any 1 day Maximum for... emulsions Copper 0.0035 0.018 Cyanide 0.005 0.002 Lead 0.008 0.004 (h) Sawing or grinding contact cooling...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Copper 9.58 5.04 Cyanide 1.46 0.605 Lead 2.12 1.01 (b) Sizing spent emulsions. Subpart J—BAT Pollutant or... grinding spent emulsions. Subpart J—BAT Pollutant or pollutant property Maximum for any 1 day Maximum for... emulsions Copper 0.0035 0.018 Cyanide 0.005 0.002 Lead 0.008 0.004 (h) Sawing or grinding contact cooling...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Copper 9.58 5.04 Cyanide 1.46 0.605 Lead 2.12 1.01 (b) Sizing spent emulsions. Subpart J—BAT Pollutant or... grinding spent emulsions. Subpart J—BAT Pollutant or pollutant property Maximum for any 1 day Maximum for... emulsions Copper 0.0035 0.018 Cyanide 0.005 0.002 Lead 0.008 0.004 (h) Sawing or grinding contact cooling...
Extreme values and the level-crossing problem: An application to the Feller process
NASA Astrophysics Data System (ADS)
Masoliver, Jaume
2014-04-01
We review the question of the extreme values attained by a random process. We relate it to level crossings to one boundary (first-passage problems) as well as to two boundaries (escape problems). The extremes studied are the maximum, the minimum, the maximum absolute value, and the range or span. We specialize in diffusion processes and present detailed results for the Wiener and Feller processes.
46 CFR 52.01-55 - Increase in maximum allowable working pressure.
Code of Federal Regulations, 2011 CFR
2011-10-01
... 46 Shipping 2 2011-10-01 2011-10-01 false Increase in maximum allowable working pressure. 52.01-55 Section 52.01-55 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING POWER BOILERS General Requirements § 52.01-55 Increase in maximum allowable working pressure. (a) When...
46 CFR 52.01-55 - Increase in maximum allowable working pressure.
Code of Federal Regulations, 2012 CFR
2012-10-01
... 46 Shipping 2 2012-10-01 2012-10-01 false Increase in maximum allowable working pressure. 52.01-55 Section 52.01-55 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING POWER BOILERS General Requirements § 52.01-55 Increase in maximum allowable working pressure. (a) When...
46 CFR 52.01-55 - Increase in maximum allowable working pressure.
Code of Federal Regulations, 2010 CFR
2010-10-01
... 46 Shipping 2 2010-10-01 2010-10-01 false Increase in maximum allowable working pressure. 52.01-55 Section 52.01-55 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING POWER BOILERS General Requirements § 52.01-55 Increase in maximum allowable working pressure. (a) When...
46 CFR 52.01-55 - Increase in maximum allowable working pressure.
Code of Federal Regulations, 2014 CFR
2014-10-01
... 46 Shipping 2 2014-10-01 2014-10-01 false Increase in maximum allowable working pressure. 52.01-55 Section 52.01-55 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING POWER BOILERS General Requirements § 52.01-55 Increase in maximum allowable working pressure. (a) When...
46 CFR 52.01-55 - Increase in maximum allowable working pressure.
Code of Federal Regulations, 2013 CFR
2013-10-01
... 46 Shipping 2 2013-10-01 2013-10-01 false Increase in maximum allowable working pressure. 52.01-55 Section 52.01-55 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING POWER BOILERS General Requirements § 52.01-55 Increase in maximum allowable working pressure. (a) When...
46 CFR 154.408 - Cargo tank external pressure load.
Code of Federal Regulations, 2010 CFR
2010-10-01
... minimum internal pressure (maximum vacuum), and the maximum external pressure to which any portion of the... 46 Shipping 5 2010-10-01 2010-10-01 false Cargo tank external pressure load. 154.408 Section 154... Equipment Cargo Containment Systems § 154.408 Cargo tank external pressure load. For the calculation...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY.... The height difference between the maximum safe surge capacity level and the normal operating level...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY.... The height difference between the maximum safe surge capacity level and the normal operating level...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY.... The height difference between the maximum safe surge capacity level and the normal operating level...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY.... The height difference between the maximum safe surge capacity level and the normal operating level...
Code of Federal Regulations, 2014 CFR
2014-07-01
... SOURCE CATEGORY Aluminum Sulfate Production Subcategory § 415.22 Effluent limitations guidelines...—Aluminum Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2011 CFR
2011-07-01
... SOURCE CATEGORY Aluminum Sulfate Production Subcategory § 415.22 Effluent limitations guidelines...—Aluminum Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2012 CFR
2012-07-01
... SOURCE CATEGORY Aluminum Sulfate Production Subcategory § 415.22 Effluent limitations guidelines...—Aluminum Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Aluminum Sulfate Production Subcategory § 415.22 Effluent limitations guidelines...—Aluminum Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2014 CFR
2014-07-01
... CATEGORY Hydrogen Cyanide Production Subcategory § 415.423 Effluent limitations guidelines representing the...): Subpart AP—Hydrogen Cyanide Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2013 CFR
2013-07-01
... CATEGORY Hydrogen Cyanide Production Subcategory § 415.423 Effluent limitations guidelines representing the...): Subpart AP—Hydrogen Cyanide Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2010 CFR
2010-07-01
...—Calcium Oxide Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily... SOURCE CATEGORY Calcium Oxide Production Subcategory § 415.52 Effluent limitations guidelines...
Perimeter Barrier Selection Guide
DOT National Transportation Integrated Search
1989-05-01
This document provides a methodology to determine the magnitude of the threat from attack vehicles to the perimeter of a facility. The threat is determined by the penetration tolerance and the maximum speed attainable. After the threat is defined thi...
Code of Federal Regulations, 2014 CFR
2014-07-01
... SOURCE CATEGORY Potassium Sulfate Production Subcategory § 415.132 Effluent limitations guidelines...—Potassium Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2013 CFR
2013-07-01
... SOURCE CATEGORY Potassium Sulfate Production Subcategory § 415.132 Effluent limitations guidelines...—Potassium Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Potassium Sulfate Production Subcategory § 415.132 Effluent limitations guidelines...—Potassium Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2012 CFR
2012-07-01
... SOURCE CATEGORY Potassium Sulfate Production Subcategory § 415.132 Effluent limitations guidelines...—Potassium Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2011 CFR
2011-07-01
... SOURCE CATEGORY Potassium Sulfate Production Subcategory § 415.132 Effluent limitations guidelines...—Potassium Sulfate Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Code of Federal Regulations, 2012 CFR
2012-07-01
... SOURCE CATEGORY Silver Nitrate Production Subcategory § 415.532 Effluent limitations guidelines... available (BPT): Subpart BA—Silver Nitrate Pollutant or pollutant property BPT limitations Maximum for any 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... SOURCE CATEGORY Silver Nitrate Production Subcategory § 415.532 Effluent limitations guidelines... available (BPT): Subpart BA—Silver Nitrate Pollutant or pollutant property BPT limitations Maximum for any 1...
Code of Federal Regulations, 2013 CFR
2013-07-01
... SOURCE CATEGORY Silver Nitrate Production Subcategory § 415.532 Effluent limitations guidelines... available (BPT): Subpart BA—Silver Nitrate Pollutant or pollutant property BPT limitations Maximum for any 1...
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS ORGANIC CHEMICALS, PLASTICS, AND SYNTHETIC FIBERS Other Fibers... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any...
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS ORGANIC CHEMICALS, PLASTICS, AND SYNTHETIC FIBERS Rayon Fibers... concentration listed in the following table. Effluent characteristics BPT effluent limitations 1 Maximum for any...
Objects of Maximum Electromagnetic Chirality
NASA Astrophysics Data System (ADS)
Fernandez-Corbaton, Ivan; Fruhnert, Martin; Rockstuhl, Carsten
2016-07-01
We introduce a definition of the electromagnetic chirality of an object and show that it has an upper bound. Reciprocal objects attain the upper bound if and only if they are transparent for all the fields of one polarization handedness (helicity). Additionally, electromagnetic duality symmetry, i.e., helicity preservation upon interaction, turns out to be a necessary condition for reciprocal objects to attain the upper bound. We use these results to provide requirements for the design of such extremal objects. The requirements can be formulated as constraints on the polarizability tensors for dipolar objects or on the material constitutive relations for continuous media. We also outline two applications for objects of maximum electromagnetic chirality: a twofold resonantly enhanced and background-free circular dichroism measurement setup, and angle-independent helicity filtering glasses. Finally, we use the theoretically obtained requirements to guide the design of a specific structure, which we then analyze numerically and discuss its performance with respect to maximal electromagnetic chirality.
49 CFR 192.621 - Maximum allowable operating pressure: High-pressure distribution systems.
Code of Federal Regulations, 2012 CFR
2012-10-01
... STANDARDS Operations § 192.621 Maximum allowable operating pressure: High-pressure distribution systems. (a) No person may operate a segment of a high pressure distribution system at a pressure that exceeds the... segment of a distribution system otherwise designed to operate at over 60 p.s.i. (414 kPa) gage, unless...
49 CFR 192.621 - Maximum allowable operating pressure: High-pressure distribution systems.
Code of Federal Regulations, 2011 CFR
2011-10-01
... STANDARDS Operations § 192.621 Maximum allowable operating pressure: High-pressure distribution systems. (a) No person may operate a segment of a high pressure distribution system at a pressure that exceeds the... segment of a distribution system otherwise designed to operate at over 60 p.s.i. (414 kPa) gage, unless...
49 CFR 192.621 - Maximum allowable operating pressure: High-pressure distribution systems.
Code of Federal Regulations, 2010 CFR
2010-10-01
... STANDARDS Operations § 192.621 Maximum allowable operating pressure: High-pressure distribution systems. (a) No person may operate a segment of a high pressure distribution system at a pressure that exceeds the... segment of a distribution system otherwise designed to operate at over 60 p.s.i. (414 kPa) gage, unless...
49 CFR 192.621 - Maximum allowable operating pressure: High-pressure distribution systems.
Code of Federal Regulations, 2014 CFR
2014-10-01
... STANDARDS Operations § 192.621 Maximum allowable operating pressure: High-pressure distribution systems. (a) No person may operate a segment of a high pressure distribution system at a pressure that exceeds the... segment of a distribution system otherwise designed to operate at over 60 p.s.i. (414 kPa) gage, unless...
49 CFR 192.621 - Maximum allowable operating pressure: High-pressure distribution systems.
Code of Federal Regulations, 2013 CFR
2013-10-01
... STANDARDS Operations § 192.621 Maximum allowable operating pressure: High-pressure distribution systems. (a) No person may operate a segment of a high pressure distribution system at a pressure that exceeds the... segment of a distribution system otherwise designed to operate at over 60 p.s.i. (414 kPa) gage, unless...
Ultrapressure materials science
NASA Technical Reports Server (NTRS)
Ruoff, A. L.
1984-01-01
Three active areas of research at ultra pressure are pursued, i.e., diffraction studies with the Cornell High Energy Synchrotron Source (CHESS), band gap and absorption edge effects, indentor-anvil experiments and theory and research to attain higher pressures. The range over which X-ray diffraction data and absorption edge data are obtained is extended to 700 kbars. Using the indentor technique pressures of 2.1 Mbars are obtained. Research results and methods are discussed.
Polymer Claw: Instant Underwater Adhesive
2012-08-27
technology is the use of pressure sensitive microcapsules , which release reactive amine crosslinkers into an adhesive putty when pressed against the surface...CLEANING AGENT RHEOLOGY 3 3.3 PRESSURE-ACTIVATED ADHESIVE 5 3.3.1 PROCESSING IMPROVEMENTS 5 3.3.2 MICROCAPSULE DIAMETER 5 3.3.3 MICROCAPSULE /RESIN...to attain a reasonable shelf life (- l wk.). The microcapsule diameter has been halved in order to improve mixing in the pressure-activated
High methane natural gas/air explosion characteristics in confined vessel.
Tang, Chenglong; Zhang, Shuang; Si, Zhanbo; Huang, Zuohua; Zhang, Kongming; Jin, Zebing
2014-08-15
The explosion characteristics of high methane fraction natural gas were investigated in a constant volume combustion vessel at different initial conditions. Results show that with the increase of initial pressure, the peak explosion pressure, the maximum rate of pressure rise increase due to a higher amount (mass) of flammable mixture, which delivers an increased amount of heat. The increased total flame duration and flame development time result as a consequence of the higher amount of flammable mixture. With the increase of the initial temperature, the peak explosion pressures decrease, but the pressure increase during combustion is accelerated, which indicates a faster flame speed and heat release rate. The maximum value of the explosion pressure, the maximum rate of pressure rise, the minimum total combustion duration and the minimum flame development time is observed when the equivalence ratio of the mixture is 1.1. Additionally, for higher methane fraction natural gas, the explosion pressure and the maximum rate of pressure rise are slightly decreased, while the combustion duration is postponed. The combustion phasing is empirically correlated with the experimental parameters with good fitting performance. Furthermore, the addition of dilute gas significantly reduces the explosion pressure, the maximum rate of pressure rise and postpones the flame development and this flame retarding effect of carbon dioxide is stronger than that of nitrogen. Copyright © 2014 Elsevier B.V. All rights reserved.
1951-02-01
the pressure switch (16) is activated. This causes the-electrical circuit to open valve (11) and start the igniter (17). The nitrogen pressure...activates the pressure switch (11) at approximately 7 psi before it flows through the Injector (9) into the chamber. ATI-85«’ - -A 11...precluded. Accordingly, pressure switch (11) is inserted in the system in parallel (electrically) with the flow indicator (17), and the circuit may
Iuchi, Terumi; Nakajima, Yukari; Fukuda, Moriyoshi; Matsuo, Junko; Okamoto, Hiroyuki; Sanada, Hiromi; Sugama, Junko
2014-05-01
Bed sheets generate high surface tension across the support surface and increase pressure to the body through a process known as the hammock effect. Using an anatomical model and a loading device characterized by extreme bony prominences, the present study compared pressure distributions on support surfaces across different bed making methods and bed sheet materials to determine the factors that influence pressure distribution. The model was placed on a pressure mapping system (CONFORMat; NITTA Corp., Osaka, Japan), and interface pressure was measured. Bed sheet elasticity and friction between the support surface and the bed sheets were also measured. For maximum interface pressure, the relative values of the following methods were higher than those of the control method, which did not use any bed sheets: cotton sheets with hospital corners (1.28, p = 0.02), polyester with no corners (1.29, p = 0.01), cotton with no corners (1.31, p = 0.003), and fitted polyester sheets (1.35, p = 0.002). Stepwise multiple regression analysis indicated that maximum interface pressure was negatively correlated with bed sheet elasticity (R(2) = 0.74). A statistically significant negative correlation was observed between maximum interface pressure and immersion depth, which was measured using the loading device (r = -0.40 and p = 0.04). We found that several combinations of bed making methods and bed sheet materials induced maximum interface pressures greater than those observed for the control method. Bed sheet materials influenced maximum interface pressure, and bed sheet elasticity was particularly important in reducing maximum interface pressure. Copyright © 2014 Tissue Viability Society. Published by Elsevier Ltd. All rights reserved.
33 CFR 156.170 - Equipment tests and inspections.
Code of Federal Regulations, 2014 CFR
2014-07-01
... distort under static liquid pressure at least 11/2 times the maximum allowable working pressure; and (iv... static liquid pressure test is successfully completed in the presence of the COTP. The test medium is not... static liquid pressure at least 11/2 times the maximum allowable working pressure; and (5) Each item of...
33 CFR 156.170 - Equipment tests and inspections.
Code of Federal Regulations, 2012 CFR
2012-07-01
... distort under static liquid pressure at least 11/2 times the maximum allowable working pressure; and (iv... static liquid pressure test is successfully completed in the presence of the COTP. The test medium is not... static liquid pressure at least 11/2 times the maximum allowable working pressure; and (5) Each item of...
33 CFR 156.170 - Equipment tests and inspections.
Code of Federal Regulations, 2013 CFR
2013-07-01
... distort under static liquid pressure at least 11/2 times the maximum allowable working pressure; and (iv... static liquid pressure test is successfully completed in the presence of the COTP. The test medium is not... static liquid pressure at least 11/2 times the maximum allowable working pressure; and (5) Each item of...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Hall, C.E.; Hungerford, S.
1982-05-01
The acute pressor effect of intraperitoneally administered cadmium was explored over the dose range 0.015-2 mg/kg in both pentobarbital-anesthetized and conscious rats. The former first respondent at 0.031 mg/kg, and successive doublings of that dosage increased the highest pressures attained in a stepwise fashion until a dosage of 0.25 mg/kg, the maximally effective quantity, was reached. Arterial pressure did not rise in conscious rats until a dose of 1 mg/kg, which gave the maximum response within the range examined. Heart-rate changes with Cd were slight, and rarely significant at a given dosage, but pentobarbital invariably caused tachycardia. Anesthetized rats thusmore » gave a graded response, while conscious animals reacted in an all-or-none fashion. The increased pressor responsiveness of rats under pentobarbital can not be ascribed to its cardiac parasympatholytic effects, since sensitivity was not conferred upon conscious rats when pretreated with atropine at a dose producing even greater tachycardia than that caused by pentobarbital. Nifedipine, which blocks calcium entry into smooth muscle cells, prevented the pressor response to cadmium when given as pretreatment and terminated an ongoing response when give intercurrently. Possible mechanisms to account for the observed behavior are considered.« less
NASA Astrophysics Data System (ADS)
Noro, Atsushi; Hayashi, Mikihiro
We prepared block copolymer-based supramolecular elastomers with high extensibility and large stress generation capability. Reversible addition fragmentation chain transfer polymerizations were conducted under normal pressure and high pressure to synthesize several large molecular weight polystyrene-b-[poly(butyl acrylate)-co-polyacrylamide]-b-polystyrene (S-Ba-S) block copolymers. Tensile tests revealed that the largest S-Ba-S with middle block molecular weight of 3140k achieved a breaking elongation of over 2000% with a maximum tensile stress of 3.6 MPa and a toughness of 28 MJ/m3 while the reference sample without any middle block hydrogen bonds, polystyrene-b-poly(butyl acrylate)-b-polystyrene with almost the same molecular weight, was merely viscous and not self-standing. Hence, incorporation of hydrogen bonds into a long soft middle block was found to be beneficial to attain high extensibility and large stress generation capability probably due to concerted combination of entropic changes and internal potential energy changes originaing from the dissociation of multiple hydrogen bonds by elongation. This work was supported by JSPS KAKENHI Grant Numbers 13J02357, 24685035, 15K13785, and 23655213 for M.H. and A.N. A.N. also expresses his gratitude for Tanaka Rubber Science & Technology Award by Enokagaku-Shinko Foundation, Japan.
Code of Federal Regulations, 2011 CFR
2011-07-01
... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS TEXTILE MILLS POINT SOURCE CATEGORY Low Water Use Processing... 9.0 at all times. Water Jet Weaving Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2011 CFR
2011-07-01
... silver smelted Lead 0.546 0.260 Mercury 0.325 0.130 Silver 0.533 0.221 Zinc 1.898 0.793 Gold 0.130 Oil... monthly average mg/troy ounce of silver reduced in solution Lead 0.168 0.080 Mercury 0.100 0.040 Silver 0... property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold refined electrolytically...
Code of Federal Regulations, 2010 CFR
2010-07-01
... copper, lead, zinc, and total phenols. For non-continuous dischargers, annual average mass limitations....0771 0.0421 Lead (T) 0.0791 0.039 Zinc (T) 0.114 0.0431 Maximum for any 1 day Maximum for monthly average Annual average 1 (mg/l) 2 (mg/l) 2 Copper (T) 0.77 0.42 0.017 Lead (T) 0.79 0.39 0.022 Zinc (T) 1...
Code of Federal Regulations, 2011 CFR
2011-07-01
... copper, lead, zinc, and total phenols. For non-continuous dischargers, annual average mass limitations....0771 0.0421 Lead (T) 0.0791 0.039 Zinc (T) 0.114 0.0431 Maximum for any 1 day Maximum for monthly average Annual average 1 (mg/l) 2 (mg/l) 2 Copper (T) 0.77 0.42 0.017 Lead (T) 0.79 0.39 0.022 Zinc (T) 1...
Direct measurements of the pressure distribution along the contact area during droplet impact
NASA Astrophysics Data System (ADS)
Nguyen, Thanh-Vinh; Matsumoto, Kiyoshi; Shimoyama, Isao
2016-11-01
We report direct measurements of the pressure distribution on the contact area during the impact of a droplet on a micropillar array. The measurements were realized using an array of MEMS-based force sensors fabricated underneath the micropillars. We show that immediately after the droplet hits the surface, the pressure becomes maximum at the center of the contact area and this maximum pressure value is more than 10 times larger than the dynamic pressure. This result emphasizes the effect of water-hammer-type pressure during the early stage of the impact. Furthermore, our measurement results demonstrate that the critical pressure associated with Cassie-Wenzel transition agrees well with the maximum capillary pressure of the micropillar array.
Wang, Hongyu; Chen, Zhouzhou; Miao, Jia; Li, Yaozhong
2016-06-01
Membrane fouling alleviation by addition of poly dimethyl diallyl ammonium chloride (PDMDAAC) and magnetic powder (Fe3O4) was investigated. It was found that magnetic powder associated with PDMDAAC had a good performance on mitigation of membrane fouling, improvement in dehydrogenase activity and enhancement of biomass growth. The optimal dose of PDMDAAC was determined by using constant pressure dead-end filtration unit. Maximum permeate flux was attained at 400mg/L of PDMDAAC addition. Continuous experiment was conducted in a submerged membrane bioreactor (MBR) system and biomass parameters such as soluble microbial products (SMP), extracellular polymeric substances (EPS), dehydrogenase activity, zeta potential, and capillary suction time (CST) were analyzed. Best results were obtained with a combination of 120mg/L of magnetic powder and 400mg/L of PDMDAAC. This study results demonstrated that PDMDAAC played a major role in SMPc and EPSc reduction, whereas magnetic powder had better performance in decreasing SMPc and EPSp. Copyright © 2016 Elsevier Ltd. All rights reserved.
NASA Technical Reports Server (NTRS)
Kamhawi, Hani; Huang, Wensheng; Haag, Thomas; Shastry, Rohit; Thomas, Robert; Yim, John; Herman, Daniel; Williams, George; Myers, James; Hofer, Richard;
2015-01-01
NASA's Space Technology Mission Directorate (STMD) Solar Electric Propulsion Technology Demonstration Mission (SEP/TDM) project is funding the development of a 12.5-kW Hall thruster system to support future NASA missions. The thruster designated Hall Effect Rocket with Magnetic Shielding (HERMeS) is a 12.5-kW Hall thruster with magnetic shielding incorporating a centrally mounted cathode. HERMeS was designed and modeled by a NASA GRC and JPL team and was fabricated and tested in vacuum facility 5 (VF5) at NASA GRC. Tests at NASA GRC were performed with the Technology Development Unit 1 (TDU1) thruster. TDU1's magnetic shielding topology was confirmed by measurement of anode potential and low electron temperature along the discharge chamber walls. Thermal characterization tests indicated that during full power thruster operation at peak magnetic field strength, the various thruster component temperatures were below prescribed maximum allowable limits. Performance characterization tests demonstrated the thruster's wide throttling range and found that the thruster can achieve a peak thruster efficiency of 63% at 12.5 kW 500 V and can attain a specific impulse of 3,000 s at 12.5 kW and a discharge voltage of 800 V. Facility background pressure variation tests revealed that the performance, operational characteristics, and magnetic shielding effectiveness of the TDU1 design were mostly insensitive to increases in background pressure.
Nayak, Chitresh; Singh, Amit; Chaudhary, Himanshu; Unune, Deepak Rajendra
2017-10-23
Technological advances in prosthetics have attracted the curiosity of researchers in monitoring design and developments of the sockets to sustain maximum pressure without any soft tissue damage, skin breakdown, and painful sores. Numerous studies have been reported in the area of pressure measurement at the limb/socket interface, though, the relation between amputee's physiological parameters and the pressure developed at the limb/socket interface is still not studied. Therefore, the purpose of this work is to investigate the effects of patient-specific physiological parameters viz. height, weight, and stump length on the pressure development at the transtibial prosthetic limb/socket interface. Initially, the pressure values at the limb/socket interface were clinically measured during stance and walking conditions for different patients using strain gauges placed at critical locations of the stump. The measured maximum pressure data related to patient's physiological parameters was used to develop an artificial neural network (ANN) model. The effects of physiological parameters on the pressure development at the limb/socket interface were examined using the ANN model. The analyzed results indicated that the weight and stump length significantly affects the maximum pressure values. The outcomes of this work could be an important platform for the design and development of patient-specific prosthetic socket which can endure the maximum pressure conditions at stance and ambulation conditions.
A Pressure-Based Analysis of Vortex Ring Pinch-Off
NASA Astrophysics Data System (ADS)
Schlueter, Kristy; Braun, Noah; Dabiri, John
2014-11-01
This study investigated the development of vortex rings over a range of maximum stroke ratios, and analyzed vorticity and pressure data for clues to the physical mechanisms underlying vortex pinch-off. An impulsive piston velocity profile and Reynolds number of 3000 were used for all cases. The formation number was consistently found to be 3.6 +/-0.3. A recently developed algorithm was used to generate pressure fields by integrating the pressure gradient along several paths through the velocity field and taking the median to get explicit values for pressure. The formation time at the occurrence of a local maximum in the pressure between the vortex ring and the lip of the nozzle, known as the trailing pressure maximum, was found to occur concurrently with the formation number for each case, within the error associated with the temporal resolution of the data. This suggests that the trailing pressure maximum is an indicator of vortex ring pinch-off. This is consistent with the results of Lawson and Dawson (2014), who found that the appearance of the trailing pressure maximum was coincident with the formation number. This pressure based approach to determining vortex ring pinch-off will be applied to a biological flow to examine the efficiency of such a flow. This research was partially supported by the Department of Defense (DoD) through the National Defense Science & Engineering Graduate Fellowship (NDSEG) Program.
14 CFR 25.365 - Pressurized compartment loads.
Code of Federal Regulations, 2010 CFR
2010-01-01
... Pressurized compartment loads. For airplanes with one or more pressurized compartments the following apply: (a... differential loads from zero up to the maximum relief valve setting. (b) The external pressure distribution in... zero up to the maximum allowed during landing. (d) The airplane structure must be designed to be able...
46 CFR 151.50-13 - Propylene oxide.
Code of Federal Regulations, 2012 CFR
2012-10-01
...) Pressure vessel cargo tanks shall meet the requirements of Class II pressure vessels. (2) Cargo tanks shall be designed for the maximum pressure expected to be encountered during loading, storing and... cargo piping shall be subjected to a hydrostatic test of 11/2 times the maximum pressure to which they...
46 CFR 151.50-13 - Propylene oxide.
Code of Federal Regulations, 2014 CFR
2014-10-01
...) Pressure vessel cargo tanks shall meet the requirements of Class II pressure vessels. (2) Cargo tanks shall be designed for the maximum pressure expected to be encountered during loading, storing and... cargo piping shall be subjected to a hydrostatic test of 11/2 times the maximum pressure to which they...
46 CFR 151.50-13 - Propylene oxide.
Code of Federal Regulations, 2010 CFR
2010-10-01
...) Pressure vessel cargo tanks shall meet the requirements of Class II pressure vessels. (2) Cargo tanks shall be designed for the maximum pressure expected to be encountered during loading, storing and... cargo piping shall be subjected to a hydrostatic test of 11/2 times the maximum pressure to which they...
46 CFR 151.50-13 - Propylene oxide.
Code of Federal Regulations, 2013 CFR
2013-10-01
...) Pressure vessel cargo tanks shall meet the requirements of Class II pressure vessels. (2) Cargo tanks shall be designed for the maximum pressure expected to be encountered during loading, storing and... cargo piping shall be subjected to a hydrostatic test of 11/2 times the maximum pressure to which they...
46 CFR 151.50-13 - Propylene oxide.
Code of Federal Regulations, 2011 CFR
2011-10-01
...) Pressure vessel cargo tanks shall meet the requirements of Class II pressure vessels. (2) Cargo tanks shall be designed for the maximum pressure expected to be encountered during loading, storing and... cargo piping shall be subjected to a hydrostatic test of 11/2 times the maximum pressure to which they...
Code of Federal Regulations, 2010 CFR
2010-07-01
... point source subject to this subpart and using the milk of lime process must achieve the following... Lime Process Pollutant or pollutant property BPT limitations Maximum for any 1 day Average of daily...
Calorific values and combustion chemistry of animal manure
USDA-ARS?s Scientific Manuscript database
Combustion chemistry and calorific value analyses are the fundamental information for evaluating different biomass waste-to-energy conversion operations. Specific chemical exergy of manure and other biomass feedstock will provide a measure for the theoretically maximum attainable energy. The specifi...
NASA Astrophysics Data System (ADS)
Patton, Henry; Hubbard, Alun; Andreassen, Karin; Winsborrow, Monica; Stroeven, Arjen P.
2016-12-01
The Eurasian ice-sheet complex (EISC) was the third largest ice mass during the Last Glacial Maximum (LGM), after the Antarctic and North American ice sheets. Despite its global significance, a comprehensive account of its evolution from independent nucleation centres to its maximum extent is conspicuously lacking. Here, a first-order, thermomechanical model, robustly constrained by empirical evidence, is used to investigate the dynamics of the EISC throughout its build-up to its maximum configuration. The ice flow model is coupled to a reference climate and applied at 10 km spatial resolution across a domain that includes the three main spreading centres of the Celtic, Fennoscandian and Barents Sea ice sheets. The model is forced with the NGRIP palaeo-isotope curve from 37 ka BP onwards and model skill is assessed against collated flowsets, marginal moraines, exposure ages and relative sea-level history. The evolution of the EISC to its LGM configuration was complex and asynchronous; the western, maritime margins of the Fennoscandian and Celtic ice sheets responded rapidly and advanced across their continental shelves by 29 ka BP, yet the maximum aerial extent (5.48 × 106 km2) and volume (7.18 × 106 km3) of the ice complex was attained some 6 ka later at c. 22.7 ka BP. This maximum stand was short-lived as the North Sea and Atlantic margins were already in retreat whilst eastern margins were still advancing up until c. 20 ka BP. High rates of basal erosion are modelled beneath ice streams and outlet glaciers draining the Celtic and Fennoscandian ice sheets with extensive preservation elsewhere due to frozen subglacial conditions, including much of the Barents and Kara seas. Here, and elsewhere across the Norwegian shelf and North Sea, high pressure subglacial conditions would have promoted localised gas hydrate formation.
Ashizawa, K; Takahashi, C; Yanagisawa, S
1978-09-01
Longitudinal survey data of stature and body weight from age 7 to 17 were obtained for 100 boys and 100 girls during World War II. The growth rates and the average annual increments were compared with those of children born after the war. Growth attained at age 7 as a percentage of that at age 17 is larger in children of the control group, presumably as a result of an improved environment affecting the growth increment. The age at maximum velocity is six months to one year earlier for the current group of children. Although the maximum velocities for both items and sexes are nearly the same in the groups compared, the total increments are larger in the current group of children. Age, distance, and maximum velocity at adolescent growth spurt were obtained for each child. The mean values were compared according to growth patterns and growth attained at age 7. The "increasing type" growth group has the highest velocity at the greatest distance and the oldest age for stature. Children who were taller or heavier at age 7 have velocity peaks with greater distances.
40 CFR Appendix I to Subpart B of... - Appendix I to Subpart B of Part 205
Code of Federal Regulations, 2011 CFR
2011-07-01
...: Acceleration Test: Deceleration Test: Acceleration Test Run No. 1 2 3 4 5 dBA Left Right Highest RPM attained in End Zone Calculated Sound Pressure dBA Deceleration Test with Exhaust Brake Applied dBA Left Right Calculated Sound Pressure dBA TEST Personnel: (Name) Recorded By: Date:......... (Signature) Supervisor...
40 CFR Appendix I to Subpart B of... - Appendix I to Subpart B of Part 205
Code of Federal Regulations, 2010 CFR
2010-07-01
...: Acceleration Test: Deceleration Test: Acceleration Test Run No. 1 2 3 4 5 dBA Left Right Highest RPM attained in End Zone Calculated Sound Pressure dBA Deceleration Test with Exhaust Brake Applied dBA Left Right Calculated Sound Pressure dBA TEST Personnel: (Name) Recorded By: Date:......... (Signature) Supervisor...
Dunkel, Trisha M; Davidson, Denise; Qurashi, Shaji
2010-01-01
Younger and older Muslim and non-Muslim women living in the United States completed questionnaires about body satisfaction and their internalization of Western standards of beauty (thin-ideal). Younger Muslim women wearing non-Western clothing and a head veil were significantly less likely to express drive for thinness or pressure to attain a thin-ideal standard of beauty than women wearing Western dress or younger women wearing non-Western dress without a head veil. Older women, while expressing greater discrepancy between their ideal body shape and their current body shape, and less satisfaction with their bodies than younger women, reported less drive for thinness and less pressure to attain the Western thin-ideal standard of beauty than younger women. These results are discussed in terms of how factors such as age and religion may serve as protective factors against a strong or unhealthy drive for thinness or thin-ideal standard. Copyright 2009 Elsevier Ltd. All rights reserved.
40 CFR 60.116b - Monitoring of operations.
Code of Federal Regulations, 2012 CFR
2012-07-01
... greater than or equal to 151 m3 storing a liquid with a maximum true vapor pressure greater than or equal... liquid with a maximum true vapor pressure greater than or equal to 15.0 kPa shall maintain a record of... than or equal to 75 m3 but less than 151 m3 storing a liquid with a maximum true vapor pressure that is...
40 CFR 60.116b - Monitoring of operations.
Code of Federal Regulations, 2014 CFR
2014-07-01
... greater than or equal to 151 m3 storing a liquid with a maximum true vapor pressure greater than or equal... liquid with a maximum true vapor pressure greater than or equal to 15.0 kPa shall maintain a record of... than or equal to 75 m3 but less than 151 m3 storing a liquid with a maximum true vapor pressure that is...
40 CFR 60.116b - Monitoring of operations.
Code of Federal Regulations, 2011 CFR
2011-07-01
... greater than or equal to 151 m3 storing a liquid with a maximum true vapor pressure greater than or equal... liquid with a maximum true vapor pressure greater than or equal to 15.0 kPa shall maintain a record of... than or equal to 75 m3 but less than 151 m3 storing a liquid with a maximum true vapor pressure that is...
40 CFR 60.116b - Monitoring of operations.
Code of Federal Regulations, 2013 CFR
2013-07-01
... greater than or equal to 151 m3 storing a liquid with a maximum true vapor pressure greater than or equal... liquid with a maximum true vapor pressure greater than or equal to 15.0 kPa shall maintain a record of... than or equal to 75 m3 but less than 151 m3 storing a liquid with a maximum true vapor pressure that is...
Shafagoj, Yanal A; Mohammed, Faisal I
2002-08-01
The physiological effects of cigarette smoking have been widely studied, however, little is known regarding the effects of smoking hubble-bubble. We examined the acute effects of hubble-bubble smoking on heart rate, systolic, diastolic, and mean arterial blood pressure and maximum end-expiratory carbon monoxide. This study was carried out in the student laboratory, School of Medicine, Department of Physiology, University of Jordan, Amman, Jordan, during the summer of 1999. In 18 healthy habitual hubble-bubble smokers, heart rate, blood pressure, and maximum end-expiratory carbon monoxide was measured before, during and post smoking of one hubble-bubble run (45 minutes). Compared to base line (time zero), at the end of smoking heart rate, systolic blood pressure, diastolic blood pressure, mean arterial blood pressure, and maximum end-expiratory carbon monoxide were increased 16 2.4 beats per minute, 6.7 2.5 mm Hg, 4.4 1.6 mm Hg, 5.2 1.7 mm Hg, and 14.2 1.8 ppm, (mean standard error of mean, P<.05). Acute short-term active hubble-bubble smoking elicits a modest increase in heart rate, systolic blood pressure, diastolic blood pressure, mean arterial blood pressure and maximum end-expiratory carbon monoxide in healthy hubble-bubble smokers.
Enhanced oil recovery using flash-driven steamflooding
Roark, Steven D.
1990-01-01
The present invention is directed to a novel steamflooding process which utilizes three specific stages of steam injection for enhanced oil recovery. The three stages are as follows: As steam is being injected into an oil-bearing reservoir through an injection well, the production rate of a production well located at a distance from the injection well is gradually restricted to a point that the pressure in the reservoir increases at a predetermined rate to a predetermined maximum value. After the maximum pressure has been reached, the production rate is increased to a value such that the predetermined maximum pressure value is maintained. Production at maximum pressure is continued for a length of time that will be unique for each individual reservoir. In some cases, this step of the steamflooding process of the invention may be omitted entirely. In the third stage of the steamflooding process of the invention, production rates at the producing well are increased gradually to allow the pressure to decrease down from the maximum pressure value to the original pressure value at the producing well. The rate of pressure reduction will be unique for each reservoir. After completing stage three, the three stages can be repeated or the steamflood may be terminated as considered desirable.
Comparison of masticatory performance and tongue pressure between children and young adults.
Fujita, Yuko; Ichikawa, Maika; Hamaguchi, Ayako; Maki, Kenshi
2018-04-01
The aims of the present study were to evaluate whether there are significant differences in masticatory performance by gender and dental stage. We also determined the factors directly associated with the masticatory performance in children, and those directly associated with masticatory performance in young adults. The study included 180 subjects, ranging in age from 6 to 12 years or 20 to 33 years. The subjects were divided into three groups according to the Hellman developmental stage (III A, III B, or VA); the groups were the subdivided according to gender. The body mass index (BMI), maximum tongue pressure, and sum of decayed, missing, and filled teeth (DMFT) were determined in all subjects. To investigate masticatory performance, the total number and maximum projected area of chewed particles of the jelly materials were measured. Masticatory performance had the highest values at Stage VA in both males and females. Regarding the maximum tongue pressure in females, Stage III B had the highest value of all stages. Multiple regression analysis showed that masticatory performance was associated with DMFT index, maximum tongue pressure, and BMI in children. Among young adults, masticatory performance was associated with DMFT index and maximum tongue pressure. Better masticatory performance is directly associated with better dental status, a higher BMI, and tongue pressure in schoolchildren. Additionally, masticatory performance was well-correlated with tongue pressure in young adults, although maximum tongue pressure reached its peak before Stage VA in females. We suggest that females need training with respect to tongue pressure, by the mixed dentition stage.
Sea-Ice Conditions in the Norwegian, Barents, and White Seas
1976-08-01
pack, aided by relatively warm water from the Murman coast current, would reduce the maximum ice thickness predicted by the equation used for...THICKNESS With the aid of the ice growth model in the appendix, it is pos- sible to relate the maximum ice thickness attained during a winter season to a...inserted merely to aid the reader in discerning differences between individual winter seasons. As was the case for the 12-month mean temperatures
Code of Federal Regulations, 2013 CFR
2013-07-01
... Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.546 0.260 Mercury 0.325 0.130 Silver 0.533 0.221 Zinc 1.898 0.793 Gold 0.130 Oil....164 0.068 Zinc 0.584 0.244 Gold 0.040 Oil and grease 8.000 4.800 Total suspended solids 16.400 7.800 p...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.546 0.260 Mercury 0.325 0.130 Silver 0.533 0.221 Zinc 1.898 0.793 Gold 0.130 Oil....164 0.068 Zinc 0.584 0.244 Gold 0.040 Oil and grease 8.000 4.800 Total suspended solids 16.400 7.800 p...
Code of Federal Regulations, 2014 CFR
2014-07-01
... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.364 0.169 Mercury 0.195 0.078 Silver 0.377 0.156 Zinc 1.326 0.546 Gold 0.130 (b) Silver... reduced in solution Lead 0.112 0.052 Mercury 0.060 0.024 Silver 0.116 0.048 Zinc 0.408 0.168 Gold 0.040 (c...
Code of Federal Regulations, 2012 CFR
2012-07-01
... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.364 0.169 Mercury 0.195 0.078 Silver 0.377 0.156 Zinc 1.326 0.546 Gold 0.130 (b) Silver... reduced in solution Lead 0.112 0.052 Mercury 0.060 0.024 Silver 0.116 0.048 Zinc 0.408 0.168 Gold 0.040 (c...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Pollutant or pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.546 0.260 Mercury 0.325 0.130 Silver 0.533 0.221 Zinc 1.898 0.793 Gold 0.130 Oil....164 0.068 Zinc 0.584 0.244 Gold 0.040 Oil and grease 8.000 4.800 Total suspended solids 16.400 7.800 p...
Code of Federal Regulations, 2013 CFR
2013-07-01
... pollutant property Maximum for any 1 day Maximum for monthly average mg/troy ounce of gold and silver smelted Lead 0.364 0.169 Mercury 0.195 0.078 Silver 0.377 0.156 Zinc 1.326 0.546 Gold 0.130 (b) Silver... reduced in solution Lead 0.112 0.052 Mercury 0.060 0.024 Silver 0.116 0.048 Zinc 0.408 0.168 Gold 0.040 (c...
Altitude-Related Change in Endotracheal Tube Cuff Pressures in Helicopter EMS
Weisberg, Stacy N.; McCall, Jonathan C.; Tennyson, Joseph
2017-01-01
Introduction Over-inflation of endotracheal tube (ETT) cuffs has the potential to lead to scarring and stenosis of the trachea.1, 2,3, 4 The air inside an ETT cuff is subject to expansion as atmospheric pressure decreases, as happens with an increase in altitude. Emergency medical services helicopters are not pressurized, thereby providing a good environment for studying the effects of altitude changes ETT cuff pressures. This study aims to explore the relationship between altitude and ETT cuff pressures in a helicopter air-medical transport program. Methods ETT cuffs were initially inflated in a nonstandardized manner and then adjusted to a pressure of 25 cmH2O. The pressure was again measured when the helicopter reached maximum altitude. A final pressure was recorded when the helicopter landed at the receiving facility. Results We enrolled 60 subjects in the study. The mean for initial tube cuff pressures was 70 cmH2O. Maximum altitude for the program ranged from 1,000–3,000 feet above sea level, with a change in altitude from 800–2,480 feet. Mean cuff pressure at altitude was 36.52 ± 8.56 cmH2O. Despite the significant change in cuff pressure at maximum altitude, there was no relationship found between the maximum altitude and the cuff pressures measured. Conclusion Our study failed to demonstrate the expected linear relationship between ETT cuff pressures and the maximum altitude achieved during typical air-medical transportation in our system. At altitudes less than 3,000 feet above sea level, the effect of altitude change on ETT pressure is minimal and does not require a change in practice to saline-filled cuffs. PMID:28611883
Altitude-Related Change in Endotracheal Tube Cuff Pressures in Helicopter EMS.
Weisberg, Stacy N; McCall, Jonathan C; Tennyson, Joseph
2017-06-01
Over-inflation of endotracheal tube (ETT) cuffs has the potential to lead to scarring and stenosis of the trachea.1, 2,3, 4 The air inside an ETT cuff is subject to expansion as atmospheric pressure decreases, as happens with an increase in altitude. Emergency medical services helicopters are not pressurized, thereby providing a good environment for studying the effects of altitude changes ETT cuff pressures. This study aims to explore the relationship between altitude and ETT cuff pressures in a helicopter air-medical transport program. ETT cuffs were initially inflated in a nonstandardized manner and then adjusted to a pressure of 25 cmH 2 O. The pressure was again measured when the helicopter reached maximum altitude. A final pressure was recorded when the helicopter landed at the receiving facility. We enrolled 60 subjects in the study. The mean for initial tube cuff pressures was 70 cmH 2 O. Maximum altitude for the program ranged from 1,000-3,000 feet above sea level, with a change in altitude from 800-2,480 feet. Mean cuff pressure at altitude was 36.52 ± 8.56 cmH 2 O. Despite the significant change in cuff pressure at maximum altitude, there was no relationship found between the maximum altitude and the cuff pressures measured. Our study failed to demonstrate the expected linear relationship between ETT cuff pressures and the maximum altitude achieved during typical air-medical transportation in our system. At altitudes less than 3,000 feet above sea level, the effect of altitude change on ETT pressure is minimal and does not require a change in practice to saline-filled cuffs.
Triboelectric, Corona, and Induction Charging of Insulators as a Function of Pressure
NASA Technical Reports Server (NTRS)
Hogue, Michael D.; Mucciolo, Eduardo R.; Calle, Carlos I.
2006-01-01
Theoretical and experimental research has been performed that shows that the surface charge on an insulator after triboelectric charging with another insulator is rapidly dissipated with lowered atmospheric pressure. This pressure discharge is consistent with surface ions being evaporated off the surface once their vapor pressure is attained. In this paper we will report on the results of three different charging techniques (triboelectric, corona, and induction) performed on selected polymers with varying atmospheric pressure. This data will show that ion exchange between the polymer samples is the mechanism responsible for most of the surface charge on the polymer surfaces.
Code of Federal Regulations, 2010 CFR
2010-07-01
... technology currently available (BPT). Except as provided in 40 CFR 125.30 through 125.32, any existing point... available (BPT): Subpart BA—Silver Nitrate Pollutant or pollutant property BPT limitations Maximum for any 1...
Code of Federal Regulations, 2011 CFR
2011-07-01
... technology currently available (BPT). Except as provided in 40 CFR 125.30 through 125.32, any existing point... available (BPT): Subpart BA—Silver Nitrate Pollutant or pollutant property BPT limitations Maximum for any 1...
The Influences of Lamination Angles on the Interior Noise Levels of an Aircraft
NASA Technical Reports Server (NTRS)
Fernholz, Christian M.; Robinson, Jay H.
1996-01-01
The feasibility of reducing the interior noise levels of an aircraft passenger cabin through optimization of the composite lay up of the fuselage is investigated. MSC/NASTRAN, a commercially available finite element code, is used to perform the dynamic analysis and subsequent optimization of the fuselage. The numerical calculation of sensitivity of acoustic pressure to lamination angle is verified using a simple thin, cylindrical shell with point force excitations as noise sources. The thin shell used represents a geometry similar to the fuselage and analytic solutions are available for the cylindrical thin shell equations of motion. Optimization of lamination angle for the reduction of interior noise is performed using a finite element model of an actual aircraft fuselage. The aircraft modeled for this study is the Beech Starship. Point forces simulate the structure borne noise produced by the engines and are applied to the fuselage at the wing mounting locations. These forces are the noise source for the optimization problem. The acoustic pressure response is reduced at a number of points in the fuselage and over a number of frequencies. The objective function is minimized with the constraint that it be larger than the maximum sound pressure level at the response points in the passenger cabin for all excitation frequencies in the range of interest. Results from the study of the fuselage model indicate that a reduction in interior noise levels is possible over a finite frequency range through optimal configuration of the lamination angles in the fuselage. Noise reductions of roughly 4 dB were attained. For frequencies outside the optimization range, the acoustic pressure response may increase after optimization. The effects of changing lamination angle on the overall structural integrity of the airframe are not considered in this study.
A Study of the Response of the Human Cadaver Head to Impact
Hardy, Warren N.; Mason, Matthew J.; Foster, Craig D.; Shah, Chirag S.; Kopacz, James M.; Yang, King H.; King, Albert I.; Bishop, Jennifer; Bey, Michael; Anderst, William; Tashman, Scott
2008-01-01
High-speed biplane x-ray and neutral density targets were used to examine brain displacement and deformation during impact. Relative motion, maximum principal strain, maximum shear strain, and intracranial pressure were measured in thirty-five impacts using eight human cadaver head and neck specimens. The effect of a helmet was evaluated. During impact, local brain tissue tends to keep its position and shape with respect to the inertial frame, resulting in relative motion between the brain and skull and deformation of the brain. The local brain motions tend to follow looping patterns. Similar patterns are observed for impact in different planes, with some degree of posterior-anterior and right-left symmetry. Peak coup pressure and pressure rate increase with increasing linear acceleration, but coup pressure pulse duration decreases. Peak average maximum principal strain and maximum shear are on the order of 0.09 for CFC 60 Hz data for these tests. Peak average maximum principal strain and maximum shear increase with increasing linear acceleration, coup pressure, and coup pressure rate. Linear and angular acceleration of the head are reduced with use of a helmet, but strain increases. These results can be used for the validation of finite element models of the human head. PMID:18278591
Recent advances in lightweight, filament-wound composite pressure vessel technology
NASA Technical Reports Server (NTRS)
Lark, R. F.
1977-01-01
A review of recent advances is presented for lightweight, high performance composite pressure vessel technology that covers the areas of design concepts, fabrication procedures, applications, and performance of vessels subjected to single cycle burst and cyclic fatigue loading. Filament wound fiber/epoxy composite vessels were made from S glass, graphite, and Kevlar 49 fibers and were equipped with both structural and nonstructural liners. Pressure vessels structural efficiencies were attained which represented weight savings, using different liners, of 40 to 60 percent over all titanium pressure vessels. Significant findings in each area are summarized.
Exhaust-Gas Pressure and Temperature Survey of F404-GE-400 Turbofan Engine
NASA Technical Reports Server (NTRS)
Walton, James T.; Burcham, Frank W., Jr.
1986-01-01
An exhaust-gas pressure and temperature survey of the General Electric F404-GE-400 turbofan engine was conducted in the altitude test facility of the NASA Lewis Propulsion System Laboratory. Traversals by a survey rake were made across the exhaust-nozzle exit to measure the pitot pressure and total temperature. Tests were performed at Mach 0.87 and a 24,000-ft altitude and at Mach 0.30 and a 30,000-ft altitude with various power settings from intermediate to maximum afterburning. Data yielded smooth pressure and temperature profiles with maximum jet temperatures approximately 1.4 in. inside the nozzle edge and maximum jet temperatures from 1 to 3 in. inside the edge. A low-pressure region located exactly at engine center was noted. The maximum temperature encountered was 3800 R.
The coronal structure of active regions
NASA Technical Reports Server (NTRS)
Landini, M.; Monsignori Fossi, B. C.; Krieger, A.; Vaiana, G. S.
1975-01-01
A four-parameter model, which assumes a Gaussian dependence of both temperature and pressure on distance from center, is used to fit the compact part of coronal active regions as observed in X-ray photographs from a rocket experiment. The four parameters are the maximum temperature, the maximum pressure, the width of the pressure distribution, and the width of the temperature distribution. The maximum temperature ranges from 2.2 to 2.8 million K, and the maximum density from 2 to 9 by 10 to the 9th power per cu cm. The range of the pressure-distribution width is from 2 to 4 by 10 to the 9th power cm and that of the temperature-distribution width from 2 to 7.
Sound absorption by subwavelength membrane structures: A geometric perspective
NASA Astrophysics Data System (ADS)
Yang, Min; Li, Yong; Meng, Chong; Fu, Caixing; Mei, Jun; Yang, Zhiyu; Sheng, Ping
2015-12-01
Decorated membranes comprising a thin layer of elastic film with small rigid platelets fixed on top have been found to be efficient absorbers of low-frequency sound. In this work we consider the problem of sound absorption from a perspective aimed at deriving upper bounds under different scenarios, i.e., whether the sound is incident from one side only or from both sides, and whether there is a reflecting surface on the back side of the membrane. By considering the negligible thickness of the membrane, usually on the order of a fraction of one millimeter, we derive a relation showing that the sum of the incoming sound waves' (complex) pressure amplitudes, averaged over the area of the membrane, must be equal to that of the outgoing waves. By using this relation, and without going to any details of the wave solutions, it is shown that the maximum absorption achievable from one-sided incidence is 50%, while the maximum absorption with a back-reflecting surface can reach 100%. The latter was attained by the hybridized resonances. All the results are shown to be in excellent agreement with the experiments. This generalized perspective, when used together with the Green function's formalism, can be useful in gaining insights into the constraints on what are achievable in scatterings and absorption by thin film structures and delineating them.
The Trajectory, Orbit and Preliminary Fall Data of the JUNE BOOTID Superbolide of July 23, 2008
NASA Technical Reports Server (NTRS)
Konovalova, N. A.; Madiedo, J. M.; Trigo-Rodriguez, J. M.
2011-01-01
The results of the atmospheric trajectory, radiant, orbit and preliminary fall data calculations of an extremely bright slow-moving fireball are presented. The fireball had a -20.7 maximum absolute magnitude and the spectacular long-persistence dust trail (Fig 1 and 2) was observed in a widespread region of Tajikistan twenty eight minutes after sunset, precisely at 14h 45m 25s UT on July 23, 2008. The bolide was first recorded at a height of 38.2 km, and attained its maximum brightness at a height of 35.0 km and finished at a height of 19.6 km. These values are very much in line with other well-known fireballs producing meteorites. The first break-up must have occurred under an aerodynamic pressure Pdyn of about 1.5 MPa, similar to those derived from the study of atmospheric break-ups of previously reported meteorite-dropping bolides. Our trajectory, and dynamic results suggest that one might well expect to find meteorites on the ground in this case. The heliocentric orbit of the meteoroid determined from the observations is very similar to the mean orbit of the June Bootid meteor shower, whose parental comet is 7P/Pons-Winnecke (Lindblad et al. 2003). If the parent was indeed a comet, this has implications for the internal structure of comets, and for the survivability of cometary meteorites.
OCEAN OUTFALLS. II: SPATIAL EVOLUTION OF SUBMERGED WASTEFIELD
Some of the basic features of submerged wastefield formation in stratified currents are reported in this paper. ilution increased with distance from the diffuser in the initial mixing region until it attained a maximum value, which is the initial dilution, after which it remained...
The Child and Adolescent Psychiatry Trials Network
ERIC Educational Resources Information Center
March, John S.; Silva, Susan G.; Compton, Scott; Anthony, Ginger; DeVeaugh-Geiss, Joseph; Califf, Robert; Krishnan, Ranga
2004-01-01
Objective: The current generation of clinical trials in pediatric psychiatry often fails to maximize clinical utility for practicing clinicians, thereby diluting its impact. Method: To attain maximum clinical relevance and acceptability, the Child and Adolescent Psychiatry Trials Network (CAPTN) will transport to pediatric psychiatry the practical…
Code of Federal Regulations, 2010 CFR
2010-07-01
... exceed— Total phosphorus (as P) 105 35 Fluoride 75 25 TSS 150 50 The total suspended solid limitation set...) Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus...
Code of Federal Regulations, 2011 CFR
2011-07-01
... exceed— Total phosphorus (as P) 105 35 Fluoride 75 25 TSS 150 50 The total suspended solid limitation set...) Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus...
Code of Federal Regulations, 2012 CFR
2012-07-01
... 38 Pensions, Bonuses, and Veterans' Relief 2 2012-07-01 2012-07-01 false Policy. 26.4 Section 26.4 Pensions, Bonuses, and Veterans' Relief DEPARTMENT OF VETERANS AFFAIRS (CONTINUED) ENVIRONMENTAL EFFECTS OF... toward the maximum attainable recycling of nonrenewable resources. (b) VA elements shall: (1) Interpret...
Code of Federal Regulations, 2014 CFR
2014-07-01
... 38 Pensions, Bonuses, and Veterans' Relief 2 2014-07-01 2014-07-01 false Policy. 26.4 Section 26.4 Pensions, Bonuses, and Veterans' Relief DEPARTMENT OF VETERANS AFFAIRS (CONTINUED) ENVIRONMENTAL EFFECTS OF... toward the maximum attainable recycling of nonrenewable resources. (b) VA elements shall: (1) Interpret...
Code of Federal Regulations, 2013 CFR
2013-07-01
... 38 Pensions, Bonuses, and Veterans' Relief 2 2013-07-01 2013-07-01 false Policy. 26.4 Section 26.4 Pensions, Bonuses, and Veterans' Relief DEPARTMENT OF VETERANS AFFAIRS (CONTINUED) ENVIRONMENTAL EFFECTS OF... toward the maximum attainable recycling of nonrenewable resources. (b) VA elements shall: (1) Interpret...
Code of Federal Regulations, 2010 CFR
2010-07-01
... 38 Pensions, Bonuses, and Veterans' Relief 2 2010-07-01 2010-07-01 false Policy. 26.4 Section 26.4 Pensions, Bonuses, and Veterans' Relief DEPARTMENT OF VETERANS AFFAIRS (CONTINUED) ENVIRONMENTAL EFFECTS OF... toward the maximum attainable recycling of nonrenewable resources. (b) VA elements shall: (1) Interpret...
Code of Federal Regulations, 2011 CFR
2011-07-01
... 38 Pensions, Bonuses, and Veterans' Relief 2 2011-07-01 2011-07-01 false Policy. 26.4 Section 26.4 Pensions, Bonuses, and Veterans' Relief DEPARTMENT OF VETERANS AFFAIRS (CONTINUED) ENVIRONMENTAL EFFECTS OF... toward the maximum attainable recycling of nonrenewable resources. (b) VA elements shall: (1) Interpret...
Code of Federal Regulations, 2011 CFR
2011-07-01
... concentrations: Subpart A [Contact cooling and heating water] Concentration used to calculate BPT effluent limitations Pollutant or pollutant property Maximum for any 1 day (mg/l) BOD5 26 Oil and grease 29 TSS 19 pH...
14 CFR 23.925 - Propeller clearance.
Code of Federal Regulations, 2010 CFR
2010-01-01
... deflected and in the level, normal takeoff, or taxing attitude, whichever is most critical. In addition, for... attitude with the critical tire completely deflated and the corresponding landing gear strut bottomed... the runway surface when the airplane is in the maximum pitch attitude attainable during normal...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Freon, A.; Berry, J.; Coste, J.-P.
1959-02-01
Some recordings of the variations of intensity of cosmic neutrons, made since October 1956 at the observatory of the Pic du Midi and since July 1957 on the Kerguelen Islands, have shown the existence, since the beginning of the observations and during at least 20 solar rotations, of a cyclic variation with a stable period equal to 27.35 plus or minus 0.1 solar days and a maximum amplitude of 2.2% attained in October 1957. (tr-auth)
NASA Astrophysics Data System (ADS)
Chen, Yihang; Xiao, Chijie; Yang, Xiaoyi; Wang, Tianbo; Xu, Tianchao; Yu, Yi; Xu, Min; Wang, Long; Lin, Chen; Wang, Xiaogang
2017-10-01
The Laser-driven Ion beam trace probe (LITP) is a new diagnostic method for measuring poloidal magnetic field (Bp) and radial electric field (Er) in tokamaks. LITP injects a laser-driven ion beam into the tokamak, and Bp and Er profiles can be reconstructed using tomography methods. A reconstruction code has been developed to validate the LITP theory, and both 2D reconstruction of Bp and simultaneous reconstruction of Bp and Er have been attained. To reconstruct from experimental data with noise, Maximum Entropy and Gaussian-Bayesian tomography methods were applied and improved according to the characteristics of the LITP problem. With these improved methods, a reconstruction error level below 15% has been attained with a data noise level of 10%. These methods will be further tested and applied in the following LITP experiments. Supported by the ITER-CHINA program 2015GB120001, CHINA MOST under 2012YQ030142 and National Natural Science Foundation Abstract of China under 11575014 and 11375053.
Sound field inside acoustically levitated spherical drop
NASA Astrophysics Data System (ADS)
Xie, W. J.; Wei, B.
2007-05-01
The sound field inside an acoustically levitated small spherical water drop (radius of 1mm) is studied under different incident sound pressures (amplitude p0=2735-5643Pa). The transmitted pressure ptr in the drop shows a plane standing wave, which varies mainly in the vertical direction, and distributes almost uniformly in the horizontal direction. The maximum of ptr is always located at the lowermost point of the levitated drop. Whereas the secondary maximum appears at the uppermost point if the incident pressure amplitude p0 is higher than an intermediate value (3044Pa), in which there exists a pressure nodal surface in the drop interior. The value of the maximum ptr lies in a narrow range of 2489-3173Pa, which has a lower limit of 2489Pa when p0=3044Pa. The secondary maximum of ptr is rather small and only remarkable at high incident pressures.
Alm-Roijer, Carin; Stagmo, Martin; Udén, Giggi; Erhardt, Leif
2004-12-01
Many patients with coronary heart disease (CHD) are not managed adequately, and we often fail to reach treatment targets. To investigate if knowledge of risk factors for CHD, measured by a questionnaire, would show any relation to advice to compliance to lifestyle changes to attain treatment goals and adherence to drug therapy. Men and women <71 years who had had a cardiac event were screened consecutively (509) from the medical records. Responders (392) were interviewed, examined and received a questionnaire. Three hundred and forty-seven patients answered the questionnaire regarding their general knowledge of risk factors for CHD, compliance to lifestyle changes to attain treatment goals and adherence to drug therapy. There were statistically significant correlations between general knowledge about risk factors for CHD and compliance to certain lifestyle changes: weight, physical activity, stress management, diet, attainment of lipid level goals and the likelihood of taking prescribed blood pressure-lowering drugs. General knowledge of risk factors had no correlation to blood glucose or blood pressure levels nor on smoking habits or treatment patterns for prescribed lipid- and blood glucose-lowering drugs. Knowledge correlates to patient behaviour with respect to some risk factors, which should be recognised in preventive programs.
Solar-Power System Produces High-Pressure Steam
NASA Technical Reports Server (NTRS)
Lansing, F. L.
1985-01-01
Combination of three multistaged solar collectors produces highpressure steam for large-scale continuously operating turbines for generating mechanical or electrical energy. Superheated water vapor drives turbines, attaining an overall system efficiency about 22 percent.
Cerebellar pressor response in the dog
NASA Technical Reports Server (NTRS)
Dormer, K. J.; Stone, H. L.
1976-01-01
A fastigial pressor response has been elicited in the anesthetized mongrel dog. Stimulation within the rostral portions of this nucleus results in mean arterial pressure rises up to 150 mmHg above control. A proportional tachycardia is simultaneously evoked which may rapidly attain heart rates of 190 beats/min above control levels. Peak tachycardias immediately subside and often the heart rate declines below control values during stimulation while arterial pressure remains elevated. When either the carotid sinuses were isolated by ligation or a bilateral vagotomy was performed, the fastigial tachycardia was sustained. The response could still be attained when submaximal doses of alpha-chloralose anesthesia or high levels of barbiturates (30-40 mg/kg) were given. Both portions of the response result from widespread sympathetic activation; however, buffering of the response through the baroreceptor reflexes is only demonstrated in the cardiac segment of the response.
Cushion System for Multi-Use Child Safety Seat
NASA Technical Reports Server (NTRS)
Dabney, Richard W. (Inventor); Elrod, Susan V. (Inventor)
2007-01-01
A cushion system for use with a child safety seat has a plurality of bladders assembled to form a seat cushion that cooperates with the seat's safety harness. One or more sensors coupled to the safety harness sense tension therein and generate a signal indicative of the tension. Each of the bladders is individually pressurized by a pressurization system to define a support configuration of the seat cushion. The pressurization system is disabled when tension in the safety harness has attained a threshold level.
Cushion system for multi-use child safety seat
NASA Technical Reports Server (NTRS)
Elrod, Susan V. (Inventor); Dabney, Richard W. (Inventor)
2007-01-01
A cushion system for use with a child safety seat has a plurality of bladders assembled to form a seat cushion that cooperates with the seat's safety harness. One or more sensors coupled to the safety harness sense tension therein and generate a signal indicative of the tension. Each of the bladders is individually pressurized by a pressurization system to define a support configuration of the seat cushion. The pressurization system is disabled when tension in the safety harness has attained a threshold level.
40 CFR Table 4 to Subpart Ooo of... - Operating Parameter Levels
Code of Federal Regulations, 2012 CFR
2012-07-01
... temperature Maximum temperature Carbon absorber Total regeneration steam or nitrogen flow, or pressure (gauge or absolute) a during carbon bed regeneration cycle; and temperature of the carbon bed after regeneration (and within 15 minutes of completing any cooling cycle(s)) Maximum flow or pressure; and maximum...
Phrommintikul, Arintaya; Krittayaphong, Rungroj; Wongcharoen, Wanwarang; Boonyaratavej, Smonporn; Wongvipaporn, Chaiyasith; Tiyanon, Woraporn; Dinchuthai, Pakaphan; Kunjara-Na-Ayudhya, Rapeephon; Tatsanavivat, Pyatat; Sritara, Piyamitr
2016-12-01
Coronary artery disease (CAD) is a leading cause of death in elderly because aging is the important non-modifiable risk factors of atherosclerosis and also a predictor of poor outcomes. Underuse of guideline directed therapy may contribute to suboptimal risk factor control and worse outcomes in the elderly. We aimed to explore the management of CAD, risk factors control as well as goal attainment in elderly compared to nonelderly CAD patients. The CORE-Thailand is an ongoing multicenter, prospective, observational registry of patients with high atherosclerotic risk in Thailand. The data of 4120 CAD patients enrolled in this cohort was analyzed comparing between the elderly (age ≥ 65 years) vs. nonelderly (age < 65 years). There were 2172 elderly and 1948 nonelderly patients. The elderly CAD patients had higher prevalence of hypertension, dyslipidemia, atrial fibrillation and chronic kidney disease. The proportion of patients who received coronary revascularization was not different between the elderly and nonelderly CAD patients. Antiplatelets were prescribed less in the elderly while statin was prescribed in the similar proportion. Goal attainments of risk factor control of glycemic control, low density lipoprotein cholesterol, and smoking cessation except the blood pressure goal were higher in the elderly CAD patients. The CORE-Thailand registry showed the equity in the treatment of CAD between elderly and non-elderly. Elderly CAD patients had higher rate of goal attainment in risk factor control except blood pressure goal. The effects of goal attainment on cardiovascular outcomes will be demonstrated from ongoing cohort.
46 CFR 28.880 - Hydraulic equipment.
Code of Federal Regulations, 2011 CFR
2011-10-01
... times the system's maximum operating pressure. (c) Each hydraulic system must be equipped with at least... sudden loss of control due to loss of hydraulic system pressure. A system is considered to be fail-safe... catalog number and maximum allowable working pressure. (k) Existing hydraulic piping, nonmetallic hose...
46 CFR 28.880 - Hydraulic equipment.
Code of Federal Regulations, 2013 CFR
2013-10-01
... times the system's maximum operating pressure. (c) Each hydraulic system must be equipped with at least... sudden loss of control due to loss of hydraulic system pressure. A system is considered to be fail-safe... catalog number and maximum allowable working pressure. (k) Existing hydraulic piping, nonmetallic hose...
46 CFR 28.880 - Hydraulic equipment.
Code of Federal Regulations, 2014 CFR
2014-10-01
... times the system's maximum operating pressure. (c) Each hydraulic system must be equipped with at least... sudden loss of control due to loss of hydraulic system pressure. A system is considered to be fail-safe... catalog number and maximum allowable working pressure. (k) Existing hydraulic piping, nonmetallic hose...
46 CFR 28.880 - Hydraulic equipment.
Code of Federal Regulations, 2012 CFR
2012-10-01
... times the system's maximum operating pressure. (c) Each hydraulic system must be equipped with at least... sudden loss of control due to loss of hydraulic system pressure. A system is considered to be fail-safe... catalog number and maximum allowable working pressure. (k) Existing hydraulic piping, nonmetallic hose...
Code of Federal Regulations, 2011 CFR
2011-07-01
... values for 30 consecutive days shall not exceed— Total phosphorus (as P) 105 35 Fluoride (as F) 75 25 (d... Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus...
Code of Federal Regulations, 2010 CFR
2010-07-01
... values for 30 consecutive days shall not exceed— Total phosphorus (as P) 105 35 Fluoride (as F) 75 25 (d... Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus...
Federal Register 2010, 2011, 2012, 2013, 2014
2011-01-21
... accordance with requirements for a 1-year extension, the Philadelphia Area's 4th highest daily 8-hour...) The maximum 4th highest daily 8-hour monitored value at any monitoring site in the Philadelphia area...
Wang, H; Tang, Y; Zhang, Y; Xu, K; Zhao, J B
2018-05-10
Objective: To investigate the relationship between the maximum blood pressure fluctuation within 24 hours after admission and the prognosis at discharge. Methods: The patients with ischemic stroke admitted in Department of Neurology of the First Affiliated Hospital of Harbin Medical University within 24 hours after onset were consecutively selected from April 2016 to March 2017. The patients were grouped according to the diagnostic criteria of hypertension. Ambulatory blood pressure of the patients within 24 hours after admission were measured with bedside monitors and baseline data were collected. The patients were scored by NIHSS at discharge. The relationships between the maximum values of systolic blood pressure (SBP) or diastolic blood pressure (DBP) and the prognosis at discharge were analyzed. Results: A total of 521 patients with acute ischemic stroke were enrolled. They were divided into normal blood pressure group (82 cases) and hypertension group(439 cases). In normal blood pressure group, the maximum values of SBP and DBP were all in normal distribution ( P >0.05). The maximum value of SBP fluctuation was set at 146.6 mmHg. After adjustment for potential confounders, the OR for poor prognosis at discharge in patients with SBP fluctuation ≥146.6 mmHg was 2.669 (95 %CI : 0.594-11.992) compared with those with SBP fluctuation <146.6 mmHg. The maximum value of DBP fluctuation was set at 90.0 mmHg, and the adjusted OR for poor prognosis at discharge in patients with DBP fluctuation ≥90.0 mmHg was 0.416 (95 %CI : 0.087-1.992) compared with those with DBP fluctuation <90.0 mmHg. In hypertension group, the maximum values of SBP and DBP were not in normal distribution ( P <0.05). The maximum value of SBP fluctuation was set at median 171.0 mmHg. After adjustment for the confounders, the greater the maximum of SBP, the greater the risk of poor prognosis at discharge was, the OR was 1.636 (95 %CI : 1.014-2.641). The maximum value of DBP fluctuation was set at median 98.0 mmHg. After adjustment for the confounders, the greater the maximum of DBP, the greater the risk of poor prognosis at discharge was, the OR was 1.645 (95 %CI : 1.003-2.697). Conclusion: In acute ischemic stroke patients with normal blood pressure at admission, the maximum values of SBP and DBP within 24 hours after admission had no relationship with prognosis at discharge. In acute ischemic stroke patients with hypertension at admission, the maximum values of SBP and DBP within 24 hours after admission were associated with poor prognosis at discharge.
Tissue interface pressure and skin integrity in critically ill, mechanically ventilated patients.
Grap, Mary Jo; Munro, Cindy L; Wetzel, Paul A; Schubert, Christine M; Pepperl, Anathea; Burk, Ruth S; Lucas, Valentina
2017-02-01
To describe tissue interface pressure, time spent above critical pressure levels and the effect on skin integrity at seven anatomical locations. Descriptive, longitudinal study in critically ill mechanically ventilated adults, from Surgical Trauma ICU-STICU; Medical Respiratory ICU-MRICU; Neuroscience ICU-NSICU in a Mid-Atlantic urban university medical centre. Subjects were enroled in the study within 24hours of intubation. Tissue interface pressure was measured continuously using the XSENSOR pressure mapping system (XSENSOR Technology Corporation, Calgary, Canada). Skin integrity was observed at all sites, twice daily, using the National Pressure Ulcer Advisory Panel staging system, for the first seven ICU days and at day 10 and 14. Of the 132 subjects, 90.9% had no observed changes in skin integrity. Maximum interface pressure was above 32mmHg virtually 100% of the time for the sacrum, left and right trochanter. At the 45mmHg level, the left and right trochanter had the greatest amount of time above this level (greater than 95% of the time), followed by the sacrum, left and right scapula, and the left and right heels. Similarly, at levels above 60mmHg, the same site order applied. For those six subjects with sacral skin integrity changes, maximum pressures were greater than 32mmHg 100% of the time. Four of the six sacral changes were associated with greater amounts of time above both 45mmHg and 60mmHg than the entire sample. Maximum tissue interface pressure was above critical levels for the majority of the documented periods, especially in the sacrum, although few changes in skin integrity were documented. Time spent above critical levels for mean pressures were considerably less compared to maximum pressures. Maximum pressures may have reflected pressure spikes, but the large amount of time above the critical pressure levels remains substantial. Copyright © 2016 Elsevier Ltd. All rights reserved.
Tissue interface pressure and skin integrity in critically ill, mechanically ventilated patients☆
Grap, Mary Jo; Munro, Cindy L.; Wetzel, Paul A.; Schubert, Christine M.; Pepperl, Anathea; Burk, Ruth S.; Lucas, Valentina
2016-01-01
Summary Objective To describe tissue interface pressure, time spent above critical pressure levels and the effect on skin integrity at seven anatomical locations. Design, setting, patients Descriptive, longitudinal study in critically ill mechanically ventilated adults, from Surgical Trauma ICU-STICU; Medical Respiratory ICU-MRICU; Neuroscience ICU-NSICU in a Mid-Atlantic urban university medical centre. Subjects were enroled in the study within 24 hours of intubation. Measurements Tissue interface pressure was measured continuously using the XSENSOR pressure mapping system (XSENSOR Technology Corporation, Calgary, Canada). Skin integrity was observed at all sites, twice daily, using the National Pressure Ulcer Advisory Panel staging system, for the first seven ICU days and at day 10 and 14. Results Of the 132 subjects, 90.9% had no observed changes in skin integrity. Maximum interface pressure was above 32 mmHg virtually 100% of the time for the sacrum, left and right trochanter. At the 45 mmHg level, the left and right trochanter had the greatest amount of time above this level (greater than 95% of the time), followed by the sacrum, left and right scapula, and the left and right heels. Similarly, at levels above 60 mmHg, the same site order applied. For those six subjects with sacral skin integrity changes, maximum pressures were greater than 32 mmHg100% of the time. Four of the six sacral changes were associated with greater amounts of time above both 45 mmHg and 60 mmHg than the entire sample. Conclusions Maximum tissue interface pressure was above critical levels for the majority of the documented periods, especially in the sacrum, although few changes in skin integrity were documented. Time spent above critical levels for mean pressures were considerably less compared to maximum pressures. Maximum pressures may have reflected pressure spikes, but the large amount of time above the critical pressure levels remains substantial. PMID:27836262
49 CFR 236.701 - Application, brake; full service.
Code of Federal Regulations, 2010 CFR
2010-10-01
... a split reduction in brake pipe pressure at a service rate until maximum brake cylinder pressure is developed. As applied to an automatic or electro-pneumatic brake with speed governor control, an application other than emergency which develops the maximum brake cylinder pressure, as determined by the design of...
Federal Register 2010, 2011, 2012, 2013, 2014
2011-01-10
... profile that is dependent upon the pipelines attributes, its geographical location, design, operating... type of threats posed by the pipeline segment, including consideration of the age, design, pipe... calculation. There are several methods available for establishing MAOP or MOP. A hydrostatic pressure test...
Growth and Maximum Size of Tiger Sharks (Galeocerdo cuvier) in Hawaii
Meyer, Carl G.; O'Malley, Joseph M.; Papastamatiou, Yannis P.; Dale, Jonathan J.; Hutchinson, Melanie R.; Anderson, James M.; Royer, Mark A.; Holland, Kim N.
2014-01-01
Tiger sharks (Galecerdo cuvier) are apex predators characterized by their broad diet, large size and rapid growth. Tiger shark maximum size is typically between 380 & 450 cm Total Length (TL), with a few individuals reaching 550 cm TL, but the maximum size of tiger sharks in Hawaii waters remains uncertain. A previous study suggested tiger sharks grow rather slowly in Hawaii compared to other regions, but this may have been an artifact of the method used to estimate growth (unvalidated vertebral ring counts) compounded by small sample size and narrow size range. Since 1993, the University of Hawaii has conducted a research program aimed at elucidating tiger shark biology, and to date 420 tiger sharks have been tagged and 50 recaptured. All recaptures were from Hawaii except a single shark recaptured off Isla Jacques Cousteau (24°13′17″N 109°52′14″W), in the southern Gulf of California (minimum distance between tag and recapture sites = approximately 5,000 km), after 366 days at liberty (DAL). We used these empirical mark-recapture data to estimate growth rates and maximum size for tiger sharks in Hawaii. We found that tiger sharks in Hawaii grow twice as fast as previously thought, on average reaching 340 cm TL by age 5, and attaining a maximum size of 403 cm TL. Our model indicates the fastest growing individuals attain 400 cm TL by age 5, and the largest reach a maximum size of 444 cm TL. The largest shark captured during our study was 464 cm TL but individuals >450 cm TL were extremely rare (0.005% of sharks captured). We conclude that tiger shark growth rates and maximum sizes in Hawaii are generally consistent with those in other regions, and hypothesize that a broad diet may help them to achieve this rapid growth by maximizing prey consumption rates. PMID:24416287
Growth and maximum size of tiger sharks (Galeocerdo cuvier) in Hawaii.
Meyer, Carl G; O'Malley, Joseph M; Papastamatiou, Yannis P; Dale, Jonathan J; Hutchinson, Melanie R; Anderson, James M; Royer, Mark A; Holland, Kim N
2014-01-01
Tiger sharks (Galecerdo cuvier) are apex predators characterized by their broad diet, large size and rapid growth. Tiger shark maximum size is typically between 380 & 450 cm Total Length (TL), with a few individuals reaching 550 cm TL, but the maximum size of tiger sharks in Hawaii waters remains uncertain. A previous study suggested tiger sharks grow rather slowly in Hawaii compared to other regions, but this may have been an artifact of the method used to estimate growth (unvalidated vertebral ring counts) compounded by small sample size and narrow size range. Since 1993, the University of Hawaii has conducted a research program aimed at elucidating tiger shark biology, and to date 420 tiger sharks have been tagged and 50 recaptured. All recaptures were from Hawaii except a single shark recaptured off Isla Jacques Cousteau (24°13'17″N 109°52'14″W), in the southern Gulf of California (minimum distance between tag and recapture sites = approximately 5,000 km), after 366 days at liberty (DAL). We used these empirical mark-recapture data to estimate growth rates and maximum size for tiger sharks in Hawaii. We found that tiger sharks in Hawaii grow twice as fast as previously thought, on average reaching 340 cm TL by age 5, and attaining a maximum size of 403 cm TL. Our model indicates the fastest growing individuals attain 400 cm TL by age 5, and the largest reach a maximum size of 444 cm TL. The largest shark captured during our study was 464 cm TL but individuals >450 cm TL were extremely rare (0.005% of sharks captured). We conclude that tiger shark growth rates and maximum sizes in Hawaii are generally consistent with those in other regions, and hypothesize that a broad diet may help them to achieve this rapid growth by maximizing prey consumption rates.
Limits on the maximum attainable efficiency for solid-state lighting
NASA Astrophysics Data System (ADS)
Coltrin, Michael E.; Tsao, Jeffrey Y.; Ohno, Yoshi
2008-03-01
Artificial lighting for general illumination purposes accounts for over 8% of global primary energy consumption. However, the traditional lighting technologies in use today, i.e., incandescent, fluorescent, and high-intensity discharge lamps, are not very efficient, with less than about 25% of the input power being converted to useful light. Solid-state lighting is a rapidly evolving, emerging technology whose efficiency of conversion of electricity to visible white light is likely to approach 50% within the next years. This efficiency is significantly higher than that of traditional lighting technologies, with the potential to enable a marked reduction in the rate of world energy consumption. There is no fundamental physical reason why efficiencies well beyond 50% could not be achieved, which could enable even greater world energy savings. The maximum achievable luminous efficacy for a solid-state lighting source depends on many different physical parameters, for example the color rendering quality that is required, the architecture employed to produce the component light colors that are mixed to produce white, and the efficiency of light sources producing each color component. In this article, we discuss in some detail several approaches to solid-state lighting and the maximum luminous efficacy that could be attained, given various constraints such as those listed above.
33 CFR Appendix A to Part 154 - Guidelines for Detonation Flame Arresters
Code of Federal Regulations, 2010 CFR
2010-07-01
... (CG-522). 1. Scope 1.1This standard provides the minimum requirements for design, construction.../Circ. 373/Rev. 1—Revised Standards for the Design, Testing and Locating of Devices to Prevent the... maximum design pressure drop for that maximum flow rate. 6.1.10Maximum operating pressure. 7. Materials 7...
NASA Astrophysics Data System (ADS)
Balitsky, V. S.; Balitskaya, L. V.; Penteley, S. V.; Novikova, M. A.
2012-02-01
The compositions and phase conditions of water-hydrocarbon fluids in synthetic quartz inclusions were studied by the methods of microthermometry, local IR spectroscopy, and gas-liquid chromatography. Synthetic quartz was grown in near-neutral fluoride, low-alkali bicarbonate, and alkali carbonate solutions with crude oil and its major fractions. The crystals with fluid inclusions were grown under thermal gradient conditions at relatively low temperatures (240-280°C) and pressures (6-45 MPa). After the study, the inclusions of grown crystals were subject to thermal processing in autoclaves at 350-380°C and 80-125 MPa. As a result, the initial water-hydrocarbon inclusions underwent significant changes. Hydrocarbon gases, largely methane and residual solid bitumens, appeared in their composition; the gasoline-kerosene fraction content increased substantially in liquid hydrocarbons (HCs). These changes are caused, first of all, by crude oil cracking, which is manifested already at 330°C and attains its maximum activity at 350-500°C (pressure of saturated vapor and higher). In natural conditions with increase in depths and, thus, the thermobaric parameters, this process is inevitable. According to the obtained experimental data, this very phenomenon and the existence of real thermal and baric gradients in the Earth's interior provide for the formation of vertical zoning in the distribution of hydrocarbon deposits of different types.
Tůma, Petr; Gojda, Jan
2015-08-01
A CE method with contactless conductivity detection has been developed for the clinical determination of the branched chain amino acids (BCAAs) valine, isoleucine and leucine in human blood plasma. The CE separation was performed in an optimised BGE with composition of 3.2 M acetic acid in 20% v/v methanol, pH 2.0. The achieved separation time was 125 s when using a capillary with an effective length of 14.7 cm, electric field intensity of 0.96 kV/cm and simultaneous application of a hydrodynamic pressure of 50 mbar. The separation efficiency in blood plasma equalled 461 000 theoretical plates/m for valine and isoleucine, and 455 000 theoretical plates/m for leucine; the detection limits are equal to 0.4 μM for all three amino acids. The RSD values for repeatability of the migration time equalled 0.1% for measurements during a single day and 0.3% for measurements on different days; the RSD values for repeatability of the peak areas equalled 2.3-2.6% for measurements during a single day and 2.7-4.6% for measurements on different days. It followed from the performed tests that the plasmatic levels of BCAAs attain a maximum 60 min after intravenous application of an infusion of BCAAs. © 2015 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim.
Advanced natural laminar flow airfoil with high lift to drag ratio
NASA Technical Reports Server (NTRS)
Viken, Jeffrey K.; Pfenninger, Werner; Mcghee, Robert J.
1986-01-01
An experimental verification of a high performance natural laminar flow (NLF) airfoil for low speed and high Reynolds number applications was completed in the Langley Low Turbulence Pressure Tunnel (LTPT). Theoretical development allowed for the achievement of 0.70 chord laminar flow on both surfaces by the use of accelerated flow as long as tunnel turbulence did not cause upstream movement of transition with increasing chord Reynolds number. With such a rearward pressure recovery, a concave type deceleration was implemented. Two-dimensional theoretical analysis indicated that a minimum profile drag coefficient of 0.0026 was possible with the desired laminar flow at the design condition. With the three-foot chord two-dimensional model constructed for the LTPT experiment, a minimum profile drag coefficient of 0.0027 was measured at c sub l = 0.41 and Re sub c = 10 x 10 to the 6th power. The low drag bucket was shifted over a considerably large c sub l range by the use of the 12.5 percent chord trailing edge flap. A two-dimensional lift to drag ratio (L/D) was 245. Surprisingly high c sub l max values were obtained for an airfoil of this type. A 0.20 chort split flap with 60 deg deflection was also implemented to verify the airfoil's lift capabilities. A maximum lift coefficient of 2.70 was attained at Reynolds numbers of 3 and 6 million.
NASA Technical Reports Server (NTRS)
Sanders, J. C.; Mendelson, Alexander
1945-01-01
Small high-speed single-cylinder compression-ignition engines were tested to determine their performance characteristics under high supercharging. Calculations were made on the energy available in the exhaust gas of the compression-ignition engines. The maximum power at any given maximum cylinder pressure was obtained when the compression pressure was equal to the maximum cylinder pressure. Constant-pressure combustion was found possible at an engine speed of 2200 rpm. Exhaust pressures and temperatures were determined from an analysis of indicator cards. The analysis showed that, at rich mixtures with the exhaust back pressure equal to the inlet-air pressure, there is excess energy available for driving a turbine over that required for supercharging. The presence of this excess energy indicates that a highly supercharged compression-ignition engine might be desirable as a compressor and combustion chamber for a turbine.
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 410.63 Section 410.63 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 410.13 Section 410.13 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 410.13 Section 410.13 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 410.13 Section 410.13 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 410.13 Section 410.13 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 410.63 Section 410.63 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 410.63 Section 410.63 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 410.63 Section 410.63 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... technology economically achievable (BAT): Pollutant or pollutant property BAT limitations Maximum for any 1...
Code of Federal Regulations, 2010 CFR
2010-07-01
...) Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus... exceed— Total phosphorus (as P) 105 35 Fluoride 75 25 [39 FR 12836, Apr. 8, 1974, as amended at 41 FR...
Code of Federal Regulations, 2011 CFR
2011-07-01
...) Maximum for any 1 day Average of daily values for 30 consecutive days shall not exceed— Total phosphorus... exceed— Total phosphorus (as P) 105 35 Fluoride 75 25 [39 FR 12836, Apr. 8, 1974, as amended at 41 FR...
Code of Federal Regulations, 2012 CFR
2012-07-01
... SOURCE CATEGORY Hydrogen Peroxide Production Subcategory § 415.92 Effluent limitations guidelines... point source subject to this subpart and manufacturing hydrogen peroxide by the oxidation of alkyl...—Hydrogen Peroxide Organic Process Pollutant or pollutant property BPT limitations Maximum for any 1 day...
Code of Federal Regulations, 2014 CFR
2014-07-01
... SOURCE CATEGORY Hydrogen Peroxide Production Subcategory § 415.92 Effluent limitations guidelines... point source subject to this subpart and manufacturing hydrogen peroxide by the oxidation of alkyl...—Hydrogen Peroxide Organic Process Pollutant or pollutant property BPT limitations Maximum for any 1 day...
Code of Federal Regulations, 2013 CFR
2013-07-01
... SOURCE CATEGORY Hydrogen Peroxide Production Subcategory § 415.92 Effluent limitations guidelines... point source subject to this subpart and manufacturing hydrogen peroxide by the oxidation of alkyl...—Hydrogen Peroxide Organic Process Pollutant or pollutant property BPT limitations Maximum for any 1 day...
Code of Federal Regulations, 2011 CFR
2011-07-01
... SOURCE CATEGORY Hydrogen Peroxide Production Subcategory § 415.92 Effluent limitations guidelines... point source subject to this subpart and manufacturing hydrogen peroxide by the oxidation of alkyl...—Hydrogen Peroxide Organic Process Pollutant or pollutant property BPT limitations Maximum for any 1 day...
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Hydrogen Peroxide Production Subcategory § 415.92 Effluent limitations guidelines... point source subject to this subpart and manufacturing hydrogen peroxide by the oxidation of alkyl...—Hydrogen Peroxide Organic Process Pollutant or pollutant property BPT limitations Maximum for any 1 day...
49 CFR 210.31 - Operation standards (stationary locomotives at 30 meters).
Code of Federal Regulations, 2010 CFR
2010-10-01
... stationary locomotives at load cells: (1) Each noise emission test shall begin after the engine of the locomotive has attained the normal cooling water operating temperature as prescribed by the locomotive manufacturer. (2) Noise emission testing in idle or maximum throttle setting shall start after a 40 second...
Forest research notes, Pacific Northwest Forest Experiment Station, No. 27, May 1, 1939.
Thornton T. Munger; Donald N. Matthews; Douglas C. Welch; Theodore Kachin; Loyd Bransford; Ernest L. Kolbe; Donald F. McKay; Leo A. Isaac
1939-01-01
Security from fire is the all-important prerequisite for timber growing after clear-cut logging in this region. Maximum security from fire is attained only when the land is again covered with a continuous cover of trees 20 to 30 or more years old.
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Ammonium Chloride Production Subcategory § 415.242 Effluent limitations guidelines... point source subject to this subpart and reacting anhydrous ammonia with hydrogen chloride gas must...): Subpart X—Ammonium Chloride Solvay Process Pollutant or pollutant property BPT limitations Maximum for any...
Evolutionary Scheduler for the Deep Space Network
NASA Technical Reports Server (NTRS)
Guillaume, Alexandre; Lee, Seungwon; Wang, Yeou-Fang; Zheng, Hua; Chau, Savio; Tung, Yu-Wen; Terrile, Richard J.; Hovden, Robert
2010-01-01
A computer program assists human schedulers in satisfying, to the maximum extent possible, competing demands from multiple spacecraft missions for utilization of the transmitting/receiving Earth stations of NASA s Deep Space Network. The program embodies a concept of optimal scheduling to attain multiple objectives in the presence of multiple constraints.
40 CFR 63.7944 - How do I determine the maximum HAP vapor pressure of my remediation material?
Code of Federal Regulations, 2014 CFR
2014-07-01
... vapor pressure of my remediation material? 63.7944 Section 63.7944 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) AIR PROGRAMS (CONTINUED) NATIONAL EMISSION STANDARDS FOR HAZARDOUS... Pollutants: Site Remediation Performance Tests § 63.7944 How do I determine the maximum HAP vapor pressure of...
40 CFR 63.7944 - How do I determine the maximum HAP vapor pressure of my remediation material?
Code of Federal Regulations, 2012 CFR
2012-07-01
... vapor pressure of my remediation material? 63.7944 Section 63.7944 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) AIR PROGRAMS (CONTINUED) NATIONAL EMISSION STANDARDS FOR HAZARDOUS... Pollutants: Site Remediation Performance Tests § 63.7944 How do I determine the maximum HAP vapor pressure of...
40 CFR 63.7944 - How do I determine the maximum HAP vapor pressure of my remediation material?
Code of Federal Regulations, 2013 CFR
2013-07-01
... vapor pressure of my remediation material? 63.7944 Section 63.7944 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) AIR PROGRAMS (CONTINUED) NATIONAL EMISSION STANDARDS FOR HAZARDOUS... Pollutants: Site Remediation Performance Tests § 63.7944 How do I determine the maximum HAP vapor pressure of...
40 CFR 63.7944 - How do I determine the maximum HAP vapor pressure of my remediation material?
Code of Federal Regulations, 2011 CFR
2011-07-01
... vapor pressure of my remediation material? 63.7944 Section 63.7944 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) AIR PROGRAMS (CONTINUED) NATIONAL EMISSION STANDARDS FOR HAZARDOUS... Pollutants: Site Remediation Performance Tests § 63.7944 How do I determine the maximum HAP vapor pressure of...
49 CFR 229.49 - Main reservoir system.
Code of Federal Regulations, 2014 CFR
2014-10-01
... least one safety valve that shall prevent an accumulation of pressure of more than 15 pounds per square... or unloads and loads the air compressor within 5 pounds per square inch above or below the maximum... pressure is not less than 15 pounds per square inch above the maximum brake pipe pressure fixed by the...
49 CFR 229.49 - Main reservoir system.
Code of Federal Regulations, 2010 CFR
2010-10-01
... least one safety valve that shall prevent an accumulation of pressure of more than 15 pounds per square... or unloads and loads the air compressor within 5 pounds per square inch above or below the maximum... pressure is not less than 15 pounds per square inch above the maximum brake pipe pressure fixed by the...
NASA Technical Reports Server (NTRS)
Hertel, Heinrich
1930-01-01
This report is intended to furnish bases for load assumptions in the designing of airplane controls. The maximum control forces and quickness of operation are determined. The maximum forces for a strong pilot with normal arrangement of the controls is taken as 1.25 times the mean value obtained from tests with twelve persons. Tests with a number of persons were expected to show the maximum forces that a man of average strength can exert on the control stick in operating the elevator and ailerons and also on the rudder bar. The effect of fatigue, of duration and of the nature (static or dynamic) of the force, as also the condition of the test subject (with or without belt) were also considered.
[Acoustic conditions in open plan offices - Pilot test results].
Mikulski, Witold
The main source of noise in open plan office are conversations. Office work standards in such premises are attained by applying specific acoustic adaptation. This article presents the results of pilot tests and acoustic evaluation of open space rooms. Acoustic properties of 6 open plan office rooms were the subject of the tests. Evaluation parameters, measurement methods and criterial values were adopted according to the following standards: PN-EN ISO 3382- 3:2012, PN-EN ISO 3382-2:2010, PN-B-02151-4:2015-06 and PN-B-02151-3:2015-10. The reverberation time was 0.33- 0.55 s (maximum permissible value in offices - 0.6 s; the criterion was met), sound absorption coefficient in relation to 1 m2 of the room's plan was 0.77-1.58 m2 (minimum permissible value - 1.1 m2; 2 out of 6 rooms met the criterion), distraction distance was 8.5-14 m (maximum permissible value - 5 m; none of the rooms met the criterion), A-weighted sound pressure level of speech at a distance of 4 m was 43.8-54.7 dB (maximum permissible value - 48 dB; 2 out of 6 rooms met the criterion), spatial decay rate of the speech was 1.8-6.3 dB (minimum permissible value - 7 dB; none of the rooms met the criterion). Standard acoustic treatment, containing sound absorbing suspended ceiling, sound absorbing materials on the walls, carpet flooring and sound absorbing workplace barriers, is not sufficient. These rooms require specific advanced acoustic solutions. Med Pr 2016;67(5):653-662. This work is available in Open Access model and licensed under a CC BY-NC 3.0 PL license.
Oliveira, Marcio Aparecido; Vidotto, Milena Carlos; Nascimento, Oliver Augusto; Almeida, Renato; Santoro, Ilka Lopes; Sperandio, Evandro Fornias; Jardim, José Roberto; Gazzotti, Mariana Rodrigues
2015-01-01
Studies have shown that physiopathological changes to the respiratory system can occur following thoracic and abdominal surgery. Laminectomy is considered to be a peripheral surgical procedure, but it is possible that thoracic spinal surgery exerts a greater influence on lung function. The aim of this study was to evaluate the pulmonary volumes and maximum respiratory pressures of patients undergoing cervical, thoracic or lumbar spinal surgery. Prospective study in a tertiary-level university hospital. Sixty-three patients undergoing laminectomy due to diagnoses of tumors or herniated discs were evaluated. Vital capacity, tidal volume, minute ventilation and maximum respiratory pressures were evaluated preoperatively and on the first and second postoperative days. Possible associations between the respiratory variables and the duration of the operation, surgical diagnosis and smoking status were investigated. Vital capacity and maximum inspiratory pressure presented reductions on the first postoperative day (20.9% and 91.6%, respectively) for thoracic surgery (P = 0.01), and maximum expiratory pressure showed reductions on the first postoperative day in cervical surgery patients (15.3%; P = 0.004). The incidence of pulmonary complications was 3.6%. There were reductions in vital capacity and maximum respiratory pressures during the postoperative period in patients undergoing laminectomy. Surgery in the thoracic region was associated with greater reductions in vital capacity and maximum inspiratory pressure, compared with cervical and lumbar surgery. Thus, surgical manipulation of the thoracic region appears to have more influence on pulmonary function and respiratory muscle action.
NASA Technical Reports Server (NTRS)
Hauser, Cavour H; Plohr, Henry W
1951-01-01
The nature of the flow at the exit of a row of turbine blades for the range of conditions represented by four different blade configurations was evaluated by the conservation-of-momentum principle using static-pressure surveys and by analysis of Schlieren photographs of the flow. It was found that for blades of the type investigated, the maximum exit tangential-velocity component is a function of the blade geometry only and can be accurately predicted by the method of characteristics. A maximum value of exit velocity coefficient is obtained at a pressure ratio immediately below that required for maximum blade loading followed by a sharp drop after maximum blade loading occurs.
A Balanced Diaphragm Type of Maximum Cylinder Pressure Indicator
NASA Technical Reports Server (NTRS)
Spanogle, J A; Collins, John H , Jr
1930-01-01
A balanced diaphragm type of maximum cylinder pressure indicator was designed to give results consistent with engine operating conditions. The apparatus consists of a pressure element, a source of controlled high pressure and a neon lamp circuit. The pressure element, which is very compact, permits location of the diaphragm within 1/8 inch of the combustion chamber walls without water cooling. The neon lamp circuit used for indicating contact between the diaphragm and support facilitates the use of the apparatus with multicylinder engines.
Time Variation of the Distance Separating Bomb and Dive Bomber Subsequent to Bomb Release
NASA Technical Reports Server (NTRS)
Mathews, Charles W.
1952-01-01
A study has been made of the variation of the distance separating bomb and aircraft with time after release as applied to dive-bombing operations, Separation distances determined from this study are presented in terms of two variables only, dive angle and maximum airplane accelerometer reading; the values of separation distance include the effects of delay in initiation of the pull-out and lag in attainment of the maximum normal acceleration.Contains analysis and calculations of the separation distances between bomb and dive bomber following bomb release, Separation distances as determined by the dive angle and the maximum airplane accelerometer reading are presented in a single chart.
A new family of low cost momentum/reaction wheels
NASA Astrophysics Data System (ADS)
Bialke, Bill
In order to satisfy the tight budgets and stringent power requirements of small and medium sized satellites, a new series of momentum/reaction wheels has been developed by ITHACO, Inc. The T-WHEEL integrates state-of-the-art ball bearing technology with flight-proven materials and conventional fabrication techniques to produce a reliable and manufacturable wheel assembly. Maximum performance is attained by using an optimized ball bearing suspension system and an ironless armature brushless dc motor for low power dissipation and minimum weight. In addition to summaries of the tradeoff studies performed, the results of the development effort include the application of a low vapor pressure synthetic hydrocarbon lubricant in the ball bearing suspension system, and performance data from the ironless armature brushless dc motor and driver. The original 4 N-m-s version (Type A) has been enlarged to increase the momentum storage capacity to 19.5 N-m-s (Type B), using the same suspension system and design baseline. A 68 N-m-s version is currently under development to broaden the product family.
Spray Cooling Trajectory Angle Impact Upon Heat Flux Using a Straight Finned Enhanced Surface
NASA Technical Reports Server (NTRS)
Silk, Eric A.; Kim, Jungho; Kiger, Ken
2005-01-01
Experiments were conducted to study the effects of spray trajectory angles upon heat flux for flat and enhanced surface spray cooling. The surface enhancement consisted of straight fins machined on the top surface of a copper heater block. Spray cooling curves were obtained with the straight fin surface aligned both parallel (axial) and perpendicular (transverse) to the spray axis. Measurements were also obtained on a flat surface heater block for comparison purposes. Each copper block had a cross-sectional area of 2.0 sq cm. A 2x2 nozzle array was used with PF-5060 as the working fluid. Thermal performance data was obtained under nominally degassed (chamber pressure of 41.4 kPa) conditions. Results show that the maximum CHF in all cases was attained for a trajectory angle of 30' from the surface normal. Furthermore, trajectory angles applied to straight finned surfaces can have a critical heat flux (CHF) enhancement as much as 75% (heat flux value of 140 W/sq cm) relative to the vertical spray orientation for the analogous flat surface case under nominally degassed conditions.
Anisotropic etching of amorphous perfluoropolymer films in oxygen-based inductively coupled plasmas
DOE Office of Scientific and Technical Information (OSTI.GOV)
Ono, Takao; Akagi, Takanori; Center for NanoBio Integration, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656
2009-01-01
An amorphous perfluoropolymer, 'Cytop' (Asahi Glass Co., Ltd.), is a preferable material for the fabrication of micro total analysis system devices because of its superior optical transparency over a wide wavelength range and low refractive index of 1.34, which is almost the same as that of water, as well as excellent chemical stability. To establish the precise microfabrication technology for this unique resin, the dry etching of the amorphous perfluoropolymer in Ar/O{sub 2} low-pressure inductively coupled plasma has been studied. A relatively high etch rate of approximately 6.3 {mu}m/min at maximum and highly anisotropic etched features was attained. Plasma measurementsmore » by a single Langmuir probe technique and actinometry revealed that etching is dominated by ion-assisted surface desorption above a 10%O{sub 2} mixing ratio, whereas the supply of active oxygen species is the rate-limiting process below 10%. Moreover, angled x-ray photoelectron spectroscopy measurements of an etched trench pattern revealed that a high anisotropy is attributed to the formation of a carbon-rich sidewall protection layer.« less
Hollow cathode lamp based Faraday anomalous dispersion optical filter.
Pan, Duo; Xue, Xiaobo; Shang, Haosen; Luo, Bin; Chen, Jingbiao; Guo, Hong
2016-07-15
The Faraday anomalous dispersion optical filter (FADOF), which has acquired wide applications, is mainly limited to some gaseous elements and low melting-point metals before, for the restriction of the attainable atomic density. In conventional FADOF systems a high atomic density is usually achieved by thermal equilibrium at the saturated vapor pressure, hence for elements with high melting-points a high temperature is required. To avoid this restriction, we propose a scheme of FADOF based on the hollow cathode lamp (HCL), instead of atomic vapor cells. Experimental results in strontium atoms verified this scheme, where a transmission peak corresponding to the (88)Sr (5s(2))(1)S0 - (5s5p)(1)P1 transition (461 nm) is obtained, with a maximum transmittance of 62.5% and a bandwith of 1.19 GHz. The dependence of transmission on magnetic field and HCL discharge current is also studied. Since the state-of-art commercial HCLs cover about 70 elements, this scheme can greatly expand the applications of FADOFs, and the abundant atomic transitions they provide bring the HCL based FADOFs potential applications for frequency stabilization.
Hollow cathode lamp based Faraday anomalous dispersion optical filter
NASA Astrophysics Data System (ADS)
Pan, Duo; Xue, Xiaobo; Shang, Haosen; Luo, Bin; Chen, Jingbiao; Guo, Hong
2016-07-01
The Faraday anomalous dispersion optical filter (FADOF), which has acquired wide applications, is mainly limited to some gaseous elements and low melting-point metals before, for the restriction of the attainable atomic density. In conventional FADOF systems a high atomic density is usually achieved by thermal equilibrium at the saturated vapor pressure, hence for elements with high melting-points a high temperature is required. To avoid this restriction, we propose a scheme of FADOF based on the hollow cathode lamp (HCL), instead of atomic vapor cells. Experimental results in strontium atoms verified this scheme, where a transmission peak corresponding to the 88Sr (5s2)1S0 - (5s5p)1P1 transition (461 nm) is obtained, with a maximum transmittance of 62.5% and a bandwith of 1.19 GHz. The dependence of transmission on magnetic field and HCL discharge current is also studied. Since the state-of-art commercial HCLs cover about 70 elements, this scheme can greatly expand the applications of FADOFs, and the abundant atomic transitions they provide bring the HCL based FADOFs potential applications for frequency stabilization.
Drag reduction by polymers in wall bounded turbulence.
L'vov, Victor S; Pomyalov, Anna; Procaccia, Itamar; Tiberkevich, Vasil
2004-06-18
We elucidate the mechanism of drag reduction by polymers in turbulent wall-bounded flows: while momentum is produced at a fixed rate by the forcing, polymer stretching results in the suppression of momentum flux to the wall. On the basis of the equations of fluid mechanics we develop the phenomenology of the "maximum drag reduction asymptote" which is the maximum drag reduction attained by polymers. Based on Newtonian information only we demonstrate the existence of drag reduction, and with one experimental parameter we reach agreement with the experimental measurements.
Code of Federal Regulations, 2013 CFR
2013-07-01
... 0.446 TSS 1.7 0.67 pH (1) (1) 1 Within the range of 7.0 to 10.0 at all times. Maximum for any 1 day....39 0.0098 Zinc (T) 1.14 0.43 0.0121 Oil and grease 30 10 0.223 TSS 38 15 0.446 pH (3) (3) (3) 1 kg... TTS 0.328 0.13 pH (1) (1) 1 Within the range of 7.0 to 10.0 at all times. Maximum for any 1 day...
CFD predictions of near-field pressure signatures of a low-boom aircraft
NASA Technical Reports Server (NTRS)
Fouladi, Kamran; Baize, Daniel G.
1992-01-01
A three dimensional Euler marching code has been utilized to predict near-field pressure signatures of an aircraft with low boom characteristics. Computations were extended to approximately six body lengths aft of the aircraft in order to obtain pressure data at three body lengths below the aircraft for a cruise Mach number of 1.6. The near-field pressure data were extrapolated to the ground using a Whitham based method. The distance below the aircraft where the pressure data are attained is defined in this paper as the 'separation distance.' The influences of separation distances and the still highly three-dimensional flow field on the predicted ground pressure signatures and boom loudness are presented in this paper.
Grimm, Richard; Malik, Mobin; Yunis, Carla; Sutradhar, Santosh; Kursun, Attila
2010-01-01
TOGETHER investigated whether targeting multiple cardiovascular (CV) risk factors using single-pill amlodipine/atorvastatin (AML/ATO) and therapeutic lifestyle changes (TLC) results in greater blood pressure (BP)/lipid control and additional reduction in estimated cardiovascular disease (CVD) risk compared with blood pressure intervention only using amlodipine (AML) + TLC. TOGETHER was a 6-week, randomized, double-blind, double-dummy trial using hypertensive participants with additional CV risk factors without CVD/diabetes. Participants were randomized to either AML/ATO (5 to 10/20 mg) + TLC or AML (5 to 10 mg) + TLC. The primary end point was the difference in proportion of participants attaining both BP (<140/90 mm Hg) and low-density lipoprotein cholesterol (LDL-C) (<100 mg/dL) goals at week 6. At week 6, 67.8% of participants receiving AML/ATO + TLC attained the combined BP/LDL-C goal versus 9.6% with AML + TLC (RD [A–B]: 58.2; 95% CI [48.1 to 68.4] P < 0.001; OR: 19.0; 95% CI 9.1 to 39.6; P < 0.001). Significant reductions from baseline in LDL-C, total cholesterol and triglycerides and estimated 10-year Framingham risk were also observed. Treatment with AML/ATO was well tolerated. In conclusion, a multifactorial CV management approach is more effective in achieving combined BP/LDL-C targets as well as CV risk reduction compared with BP intervention only in this patient population. PMID:20479948
Development of a gas-pressurized high-pressure μSR setup at the RIKEN-RAL Muon Facility
NASA Astrophysics Data System (ADS)
Watanabe, I.; Ishii, Y.; Kawamata, T.; Suzuki, T.; Pratt, F. L.; Done, R.; Chowdhury, M.; Goodway, C.; Dreyer, J.; Smith, C.; Southern, M.
2009-04-01
The development and testing of a gas-pressurized μSR setup for the RIKEN-RAL Muon Facility is reported. In collaboration with the high-pressure group of the ISIS Facility at the Rutherford Appleton Laboratory, a gas-pressurized setup for a pulsed muon beam at the RIKEN-RAL Muon Facility has been constructed in 2008. The sample is pressurized by helium gas and the designed maximum pressure is 6.4 kbar. The high-pressure cell can be cooled down to 2 K using an existing cryostat. Tests were made injecting the double-pulsed muon beam into a high-purity sample of Sn powder, which confirmed that the maximum pressure achieved at 2 K was close to the designed pressure.
Endotracheal Tube Cuff Pressures in Patients Intubated Prior to Helicopter EMS Transport.
Tennyson, Joseph; Ford-Webb, Tucker; Weisberg, Stacy; LeBlanc, Donald
2016-11-01
Endotracheal intubation is a common intervention in critical care patients undergoing helicopter emergency medical services (HEMS) transportation. Measurement of endotracheal tube (ETT) cuff pressures is not common practice in patients referred to our service. Animal studies have demonstrated an association between the pressure of the ETT cuff on the tracheal mucosa and decreased blood flow leading to mucosal ischemia and scarring. Cuff pressures greater than 30 cmH 2 O impede mucosal capillary blood flow. Multiple prior studies have recommended 30 cmH 2 O as the maximum safe cuff inflation pressure. This study sought to evaluate the inflation pressures in ETT cuffs of patients presenting to HEMS. We enrolled a convenience sample of patients presenting to UMass Memorial LifeFlight who were intubated by the sending facility or emergency medical services (EMS) agency. Flight crews measured the ETT cuff pressures using a commercially available device. Those patients intubated by the flight crew were excluded from this analysis as the cuff was inflated with the manometer to a standardized pressure. Crews logged the results on a research form, and we analyzed the data using Microsoft Excel and an online statistical analysis tool. We analyzed data for 55 patients. There was a mean age of 57 years (range 18-90). The mean ETT cuff pressure was 70 (95% CI= [61-80]) cmH 2 O. The mean lies 40 cmH 2 O above the maximum accepted value of 30 cmH 2 O (p<0.0001). Eighty-four percent (84%) of patients encountered had pressures above the recommended maximum. The most frequently recorded pressure was >120 cmH 2 O, the maximum pressure on the analog gauge. Patients presenting to HEMS after intubation by the referral agency (EMS or hospital) have ETT cuffs inflated to pressures that are, on average, more than double the recommended maximum. These patients are at risk for tracheal mucosal injury and scarring from decreased mucosal capillary blood flow. Hospital and EMS providers should use ETT cuff manometry to ensure that they inflate ETT cuffs to safe pressures.
Endotracheal Tube Cuff Pressures in Patients Intubated Prior to Helicopter EMS Transport
Tennyson, Joseph; Ford-Webb, Tucker; Weisberg, Stacy; LeBlanc, Donald
2016-01-01
Introduction Endotracheal intubation is a common intervention in critical care patients undergoing helicopter emergency medical services (HEMS) transportation. Measurement of endotracheal tube (ETT) cuff pressures is not common practice in patients referred to our service. Animal studies have demonstrated an association between the pressure of the ETT cuff on the tracheal mucosa and decreased blood flow leading to mucosal ischemia and scarring. Cuff pressures greater than 30 cmH2O impede mucosal capillary blood flow. Multiple prior studies have recommended 30 cmH2O as the maximum safe cuff inflation pressure. This study sought to evaluate the inflation pressures in ETT cuffs of patients presenting to HEMS. Methods We enrolled a convenience sample of patients presenting to UMass Memorial LifeFlight who were intubated by the sending facility or emergency medical services (EMS) agency. Flight crews measured the ETT cuff pressures using a commercially available device. Those patients intubated by the flight crew were excluded from this analysis as the cuff was inflated with the manometer to a standardized pressure. Crews logged the results on a research form, and we analyzed the data using Microsoft Excel and an online statistical analysis tool. Results We analyzed data for 55 patients. There was a mean age of 57 years (range 18–90). The mean ETT cuff pressure was 70 (95% CI= [61–80]) cmH2O. The mean lies 40 cmH2O above the maximum accepted value of 30 cmH2O (p<0.0001). Eighty-four percent (84%) of patients encountered had pressures above the recommended maximum. The most frequently recorded pressure was >120 cmH2O, the maximum pressure on the analog gauge. Conclusion Patients presenting to HEMS after intubation by the referral agency (EMS or hospital) have ETT cuffs inflated to pressures that are, on average, more than double the recommended maximum. These patients are at risk for tracheal mucosal injury and scarring from decreased mucosal capillary blood flow. Hospital and EMS providers should use ETT cuff manometry to ensure that they inflate ETT cuffs to safe pressures. PMID:27833679
Recent advances in lightweight, filament-wound composite pressure vessel technology
NASA Technical Reports Server (NTRS)
Lark, R. F.
1977-01-01
A review of recent advances is presented for lightweight, high-performance composite pressure vessel technology that covers the areas of design concepts, fabrication procedures, applications, and performance of vessels subjected to single-cycle burst and cyclic fatigue loading. Filament-wound fiber/epoxy composite vessels were made from S-glass, graphite, and Kevlar 49 fibers and were equipped with both structural and nonstructural liners. Pressure vessel structural efficiencies were attained which represented weight savings, using different liners, of 40 to 60 percent over all-titanium pressure vessels. Significant findings in each area are summarized including data from current NASA-Lewis Research Center contractual and in-house programs.
The shouted voice: A pilot study of laryngeal physiology under extreme aerodynamic pressure.
Lagier, Aude; Legou, Thierry; Galant, Camille; Amy de La Bretèque, Benoit; Meynadier, Yohann; Giovanni, Antoine
2017-12-01
The objective was to study the behavior of the larynx during shouted voice production, when the larynx is exposed to extremely high subglottic pressure. The study involved electroglottographic, acoustic, and aerodynamic analyses of shouts produced at maximum effort by three male participants. Under a normal speaking voice, the voice sound pressure level (SPL) is proportional to the subglottic pressure. However, when the subglottic pressure reached high levels, the voice SPL reached a maximum value and then decreased as subglottic pressure increased further. Furthermore, the electroglottographic signal sometimes lost its periodicity during the shout, suggesting irregular vocal fold vibration.
Magnetization at high pressure in CeP
NASA Astrophysics Data System (ADS)
Naka, T.; Matsumoto, T.; Okayama, Y.; Môri, N.; Haga, Y.; Suzuki, T.
1995-02-01
We have investigated the pressure dependence of magnetization below 60 K up to 1.6 GPa in the low-carrier concentration system CeP showing two step transitions at T = TL and TH under high pressure. At high pressure, M( P, T) exhibits a maximum at around the lower transition temperature TL. This behavior implies that the magnetic state changes at TL. The pressure dependence of isothermal magnetization M( P) is different above and below TL. In fact, M( P) below TL exhibits a maximum at around 1.4 GPa, whereas M( P) above TL increases steeply with pressure up to 1.6 GPa.
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... discharged from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
Code of Federal Regulations, 2010 CFR
2010-07-01
... AGENCY (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS MINERAL MINING AND PROCESSING POINT SOURCE CATEGORY... from that impoundment. The height difference between the maximum safe surge capacity level and the normal operating level must be greater than the inches of rain representing the 10-year, 24-hour rainfall...
The Productivity of Pell Grant Spending: Enrollment versus Attainment
ERIC Educational Resources Information Center
Martinez, Ignacio; Turner, Sarah
2015-01-01
The Pell grant program is the largest source of need-based federal financial aid available to low-income students, currently providing a maximum of $5500 in grants to undergraduate students. The program is a major investment of public money, and policymakers have a responsibility to ensure that the investment yields results. Because low-income…
Code of Federal Regulations, 2012 CFR
2012-07-01
... limitations apply to all dischargers in the calcium-, magnesium-, or sodium-based sulfite pulp segment: Subpart E [Production of Calcium-, Magnesium-, or Sodium-based Sulfite Pulps] Pollutant or pollutant... [Supplemental BAT effluent limitations] Pollutant or pollutant property Maximum for any 1 day kg/kkg (or pounds...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 410.23 Section 410.23 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30 through 125.32... economically achievable (BAT): Pollutant or pollutant property BAT limitation Maximum for any 1 day Average of...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 420.83 Section 420.83 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... and plate. Subpart H Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 420.83 Section 420.83 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... and plate. Subpart H Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 420.103 Section 420.103 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... stand. Subpart J Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day Average...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 420.103 Section 420.103 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... stand. Subpart J Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day Average...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 410.23 Section 410.23 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30 through 125.32... economically achievable (BAT): Pollutant or pollutant property BAT limitation Maximum for any 1 day Average of...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 420.43 Section 420.43 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125...-suppressed combustion. Subpart D Pollutant or pollutant property BAT effluent limitations Maximum for any 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.64 Section 430.64 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... by the application of the best available technology economically achievable (BAT). Except as provided... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 420.43 Section 420.43 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125...-suppressed combustion. Subpart D Pollutant or pollutant property BAT effluent limitations Maximum for any 1...
Code of Federal Regulations, 2013 CFR
2013-07-01
... (BAT). 433.14 Section 433.14 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... the best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... economically achievable (BAT): BAT Effluent Limitations Pollutant or pollutant property Maximum for any 1 day...
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 410.23 Section 410.23 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30 through 125.32... economically achievable (BAT): Pollutant or pollutant property BAT limitation Maximum for any 1 day Average of...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 420.43 Section 420.43 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125...-suppressed combustion. Subpart D Pollutant or pollutant property BAT effluent limitations Maximum for any 1...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 420.83 Section 420.83 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... and plate. Subpart H Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 410.23 Section 410.23 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30 through 125.32... economically achievable (BAT): Pollutant or pollutant property BAT limitation Maximum for any 1 day Average of...
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 420.103 Section 420.103 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... stand. Subpart J Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day Average...
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.64 Section 430.64 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... by the application of the best available technology economically achievable (BAT). Except as provided... achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass limitations in kg...
Code of Federal Regulations, 2012 CFR
2012-07-01
... achievable (BAT). 420.33 Section 420.33 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... pollutant property BAT effluent limitations Maximum for any 1 day Average of daily values for 30 consecutive...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 420.103 Section 420.103 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... stand. Subpart J Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day Average...
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 420.33 Section 420.33 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... pollutant property BAT effluent limitations Maximum for any 1 day Average of daily values for 30 consecutive...
Code of Federal Regulations, 2013 CFR
2013-07-01
... achievable (BAT). 430.104 Section 430.104 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... (BAT). Except as provided in 40 CFR 125.30 through 125.32, any existing point source subject to this... economically achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 430.104 Section 430.104 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY... (BAT). Except as provided in 40 CFR 125.30 through 125.32, any existing point source subject to this... economically achievable (BAT). Non-continuous dischargers shall not be subject to the maximum day mass...
Code of Federal Regulations, 2011 CFR
2011-07-01
... achievable (BAT). 420.33 Section 420.33 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... pollutant property BAT effluent limitations Maximum for any 1 day Average of daily values for 30 consecutive...
Code of Federal Regulations, 2014 CFR
2014-07-01
... achievable (BAT). 420.33 Section 420.33 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... pollutant property BAT effluent limitations Maximum for any 1 day Average of daily values for 30 consecutive...
Code of Federal Regulations, 2010 CFR
2010-07-01
... achievable (BAT). 420.83 Section 420.83 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... application of the best available technology economically achievable (BAT). Except as provided in 40 CFR 125... and plate. Subpart H Pollutant or pollutant property BAT effluent limitations Maximum for any 1 day...
Code of Federal Regulations, 2014 CFR
2014-07-01
... (BAT). 433.14 Section 433.14 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED... the best available technology economically achievable (BAT). (a) Except as provided in 40 CFR 125.30... economically achievable (BAT): BAT Effluent Limitations Pollutant or pollutant property Maximum for any 1 day...
Code of Federal Regulations, 2014 CFR
2014-07-01
... point source subject to this subpart and using borax produced by the Trona process must achieve the... remined borax must achieve the following effluent limitations representing the degree of effluent...): Subpart AB—Boric Acid Mined Borax Process Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2010 CFR
2010-07-01
... point source subject to this subpart and using borax produced by the Trona process must achieve the... remined borax must achieve the following effluent limitations representing the degree of effluent...): Subpart AB—Boric Acid Mined Borax Process Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2012 CFR
2012-07-01
... point source subject to this subpart and using borax produced by the Trona process must achieve the... remined borax must achieve the following effluent limitations representing the degree of effluent...): Subpart AB—Boric Acid Mined Borax Process Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2013 CFR
2013-07-01
... point source subject to this subpart and using borax produced by the Trona process must achieve the... remined borax must achieve the following effluent limitations representing the degree of effluent...): Subpart AB—Boric Acid Mined Borax Process Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2011 CFR
2011-07-01
... point source subject to this subpart and using borax produced by the Trona process must achieve the... remined borax must achieve the following effluent limitations representing the degree of effluent...): Subpart AB—Boric Acid Mined Borax Process Pollutant or pollutant property BPT limitations Maximum for any...
Code of Federal Regulations, 2014 CFR
2014-07-01
... operations not employing wet air emissions control scrubbers there shall be no discharge of process generated waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged...
Code of Federal Regulations, 2013 CFR
2013-07-01
... operations not employing wet air emissions control scrubbers there shall be no discharge of process generated waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged...
Code of Federal Regulations, 2012 CFR
2012-07-01
... operations not employing wet air emissions control scrubbers there shall be no discharge of process generated waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged...
Skills and Knowledge Needed to Serve as Mobile Technology Consultants for Information Organizations
ERIC Educational Resources Information Center
Potnis, Devendra; Regenstreif-Harms, Reynard; Deosthali, Kanchan; Cortez, Ed; Allard, Suzie
2016-01-01
Libraries often lack the in-house information technology (IT) expertise required to (1) implement mobile applications and related technologies (MAT); (2) attain maximum return on investment including patron satisfaction for using MAT; and (3) reduce reliance on expensive IT consultants. Based on secondary analysis of the experiences and advice…
Code of Federal Regulations, 2011 CFR
2011-07-01
... practicable control technology currently available (BPT): there shall be no discharge of process waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment...
Code of Federal Regulations, 2011 CFR
2011-07-01
... practicable control technology currently available (BPT): there shall be no discharge of process waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment...
Code of Federal Regulations, 2011 CFR
2011-07-01
... practicable control technology currently available (BPT): there shall be no discharge of process waste water pollutants into navigable waters. (b) Only that volume of water resulting from precipitation that exceeds the maximum safe surge capacity of a process waste water impoundment may be discharged from that impoundment...
USDA-ARS?s Scientific Manuscript database
The Florida bass (Micropterus floridanus) is a species endemic to peninsular Florida that is held in high esteem by bass anglers for its tendency to attain a larger maximum size than its sister taxon, the Northern largemouth bass, Micropterus salmoides. Stocking of Florida bass outside of their nat...
Code of Federal Regulations, 2013 CFR
2013-07-01
... located beyond 3 miles from shore: Water-based drilling fluids and associated drill cuttings Free Oil No... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS (CONTINUED) OIL AND GAS EXTRACTION POINT SOURCE CATEGORY... parameter BCT effluent limitation Produced water Oil & grease The maximum for any one day shall not exceed...
Code of Federal Regulations, 2012 CFR
2012-07-01
... located beyond 3 miles from shore: Water-based drilling fluids and associated drill cuttings Free Oil No... (CONTINUED) EFFLUENT GUIDELINES AND STANDARDS (CONTINUED) OIL AND GAS EXTRACTION POINT SOURCE CATEGORY... parameter BCT effluent limitation Produced water Oil & grease The maximum for any one day shall not exceed...
Code of Federal Regulations, 2014 CFR
2014-07-01
... technology currently available (BPT). (The fluoride and lead limitations are applicable to the abrasive polishing and acid polishing waste water streams while the TSS, oil, and pH limitations are applicable to the entire process waste water stream): Effluent characteristic Effluent limitations Maximum for any 1...
Code of Federal Regulations, 2012 CFR
2012-07-01
... technology currently available (BPT). (The fluoride and lead limitations are applicable to the abrasive polishing and acid polishing waste water streams while the TSS, oil, and pH limitations are applicable to the entire process waste water stream): Effluent characteristic Effluent limitations Maximum for any 1...
Code of Federal Regulations, 2013 CFR
2013-07-01
... technology currently available (BPT). (The fluoride and lead limitations are applicable to the abrasive polishing and acid polishing waste water streams while the TSS, oil, and pH limitations are applicable to the entire process waste water stream): Effluent characteristic Effluent limitations Maximum for any 1...
LITTLE JOE II - LIFTOFF - WHITE SANDS MISSILE RANGE (WSMR), NM
1963-08-28
S63-15701 (28 August 1963) --- All seven motors of Little Joe II, ignited simultaneously at launch, with a total thrust of about 310,000 pounds. A maximum height of 24,000 feet was attained as Little Joe II traveled 47,000 feet north on the White Sands Test Range.
Code of Federal Regulations, 2011 CFR
2011-07-01
... Zinc Subcategory § 421.83 Effluent limitations guidelines representing the degree of effluent reduction... of the best available technology economically achievable: (a) Subpart H—Zinc Reduction Furnace Wet... Maximum for monthly average mg/kg (pounds per million pounds) of zinc reduced Cadmium .334 .134 Copper 2...
Code of Federal Regulations, 2010 CFR
2010-07-01
... SOURCE CATEGORY Sodium Chloride Production Subcategory § 415.162 Effluent limitations guidelines... added to the bitterns during the production of sodium chloride. (b) Except as provided in 40 CFR 125.30...—Sodium Chloride Brine Mining Process Pollutant or pollutant property BPT limitations Maximum for any 1...
Federal Register 2010, 2011, 2012, 2013, 2014
2012-12-07
... (NOAA), Commerce. ACTION: Proposed rule. SUMMARY: NMFS proposes to implement the annual catch limit (ACL...) Fishery Management Plan (FMP). The proposed 2012-2013 ACL or maximum HG for Pacific mackerel is 40,514... the fishery attains the ACT, the directed fishery will close, reserving the difference between the ACL...