Sample records for air pressure drop

  1. Drop impact on a solid surface at reduced air pressure

    NASA Astrophysics Data System (ADS)

    Langley, Kenneth; Li, E. Q.; Tian, Y. S.; Hicks, P. D.; Thoroddsen, S. T.

    2017-11-01

    When a drop approaches a solid surface at atmospheric pressure, the lubrication pressure within the air forms a dimple in the bottom of the drop resulting in the entrainment of an air disc upon impact. Reducing the ambient air pressure below atmospheric has been shown to suppress splashing and the compression of the intervening air could be significant on the air disc formation; however, to date there have been no experimental studies showing how the entrainment of the air disc is affected by reducing the ambient pressure. Using ultra-high-speed interferometry, at up to 5 Mfps, we investigate droplet impacts onto dry solid surfaces in reduced ambient air pressures with particular interest in what happens as rarified gas effects become important, i.e. when the thickness of the air layer is of the same magnitude as the mean free path of the air molecules. Experimental data will be presented showing novel phenomena and comparisons will be drawn with theoretical models from the literature.

  2. Air Flow and Pressure Drop Measurements Across Porous Oxides

    NASA Technical Reports Server (NTRS)

    Fox, Dennis S.; Cuy, Michael D.; Werner, Roger A.

    2008-01-01

    This report summarizes the results of air flow tests across eight porous, open cell ceramic oxide samples. During ceramic specimen processing, the porosity was formed using the sacrificial template technique, with two different sizes of polystyrene beads used for the template. The samples were initially supplied with thicknesses ranging from 0.14 to 0.20 in. (0.35 to 0.50 cm) and nonuniform backside morphology (some areas dense, some porous). Samples were therefore ground to a thickness of 0.12 to 0.14 in. (0.30 to 0.35 cm) using dry 120 grit SiC paper. Pressure drop versus air flow is reported. Comparisons of samples with thickness variations are made, as are pressure drop estimates. As the density of the ceramic material increases the maximum corrected flow decreases rapidly. Future sample sets should be supplied with samples of similar thickness and having uniform surface morphology. This would allow a more consistent determination of air flow versus processing parameters and the resulting porosity size and distribution.

  3. Intercooler cooling-air weight flow and pressure drop for minimum drag loss

    NASA Technical Reports Server (NTRS)

    Reuter, J George; Valerino, Michael F

    1944-01-01

    An analysis has been made of the drag losses in airplane flight of cross-flow plate and tubular intercoolers to determine the cooling-air weight flow and pressure drop that give a minimum drag loss for any given cooling effectiveness and, thus, a maximum power-plant net gain due to charge-air cooling. The drag losses considered in this analysis are those due to (1) the extra drag imposed on the airplane by the weight of the intercooler, its duct, and its supports and (2) the drag sustained by the cooling air in flowing through the intercooler and its duct. The investigation covers a range of conditions of altitude, airspeed, lift-drag ratio, supercharger-pressure ratio, and supercharger adiabatic efficiency. The optimum values of cooling air pressure drop and weight flow ratio are tabulated. Curves are presented to illustrate the results of the analysis.

  4. Heat transfer and pressure drop for air flow through enhanced passages

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

    Obot, N.T.; Esen, E.B.

    1992-06-01

    An extensive experimental investigation was carried out to determine the pressure drop and heat transfer characteristics for laminar, transitional and turbulent flow of air through a smooth passage and twenty-three enhanced passages. The internal surfaces of all enhanced passages had spirally shaped geometries; these included fluted, finned/ribbed and indented surfaces. The Reynolds number (Re) was varied between 400 and 50000. The effect of heat transfer (wall cooling or fluid heating) on pressure drop is most significant within the transition region; the recorded pressure drop with heat transfer is much higher than that without heat transfer. The magnitude of this effectmore » depends markedly on the average surface temperature and, to a lesser extent, on the geometric characteristics of the enhanced surfaces. When the pressure drop data are reduced as values of the Fanning friction factor(f), the results are about the same with and without heat transfer for turbulent flow, with moderate differences in the laminar and transition regions.« less

  5. Heat transfer and pressure drop measurements in an air/molten salt direct-contact heat exchanger

    NASA Astrophysics Data System (ADS)

    Bohn, Mark S.

    1988-11-01

    This paper presents a comparison of experimental data with a recently published model of heat exchange in irrigated packed beds. Heat transfer and pressure drop were measured in a 150 mm (ID) column with a 610 mm bed of metal Pall rings. Molten nitrate salt and preheated air were the working fluids with a salt inlet temperature of approximately 440 C and air inlet temperatures of approximately 230 C. A comparison between the experimental data and the heat transfer model is made on the basis of heat transfer from the salt. For the range of air and salt flow rates tested, 0.3 to 1.2 kg/sq m/s air flow and 6 to 18 kg/sq m/s salt flow, the data agree with the model within 22 percent standard deviation. In addition, a model for the column pressure drop was validated, agreeing with the experimental data within 18 percent standard deviation over the range of column pressure drop from 40 to 1250 Pa/m.

  6. Heat transfer and pressure drop for air flow through enhanced passages. Final report

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

    Obot, N.T.; Esen, E.B.

    1992-06-01

    An extensive experimental investigation was carried out to determine the pressure drop and heat transfer characteristics for laminar, transitional and turbulent flow of air through a smooth passage and twenty-three enhanced passages. The internal surfaces of all enhanced passages had spirally shaped geometries; these included fluted, finned/ribbed and indented surfaces. The Reynolds number (Re) was varied between 400 and 50000. The effect of heat transfer (wall cooling or fluid heating) on pressure drop is most significant within the transition region; the recorded pressure drop with heat transfer is much higher than that without heat transfer. The magnitude of this effectmore » depends markedly on the average surface temperature and, to a lesser extent, on the geometric characteristics of the enhanced surfaces. When the pressure drop data are reduced as values of the Fanning friction factor(f), the results are about the same with and without heat transfer for turbulent flow, with moderate differences in the laminar and transition regions.« less

  7. Pressure drop in tubing in aircraft instrument installations

    NASA Technical Reports Server (NTRS)

    Wildhack, W A

    1937-01-01

    The theoretical basis of calculation of pressure drop in tubing is reviewed briefly. The effect of pressure drop in connecting tubing upon the operation and indication of aircraft instruments is discussed. Approximate equations are developed, and charts and tables based upon them are presented for use in designing installations of altimeters, air-speed indicators, rate-of-climb indicators, and air-driven gyroscopic instruments.

  8. Washable antimicrobial polyester/aluminum air filter with a high capture efficiency and low pressure drop.

    PubMed

    Choi, Dong Yun; Heo, Ki Joon; Kang, Juhee; An, Eun Jeong; Jung, Soo-Ho; Lee, Byung Uk; Lee, Hye Moon; Jung, Jae Hee

    2018-06-05

    Here, we introduce a reusable bifunctional polyester/aluminum (PET/Al) air filter for the high efficiency simultaneous capture and inactivation of airborne microorganisms. Both bacteria of Escherichia coli and Staphylococcus epidermidis were collected on the PET/Al filter with a high efficiency rate (∼99.99%) via the electrostatic interactions between the charged bacteria and fibers without sacrificing pressure drop. The PET/Al filter experienced a pressure drop approximately 10 times lower per thickness compared with a commercial high-efficiency particulate air filter. As the Al nanograins grew on the fibers, the antimicrobial activity against airborne E. coli and S. epidermidis improved to ∼94.8% and ∼96.9%, respectively, due to the reinforced hydrophobicity and surface roughness of the filter. Moreover, the capture and antimicrobial performances were stably maintained during a cyclic washing test of the PET/Al filter, indicative of its reusability. The PET/Al filter shows great potential for use in energy-efficient bioaerosol control systems suitable for indoor environments. Copyright © 2018 Elsevier B.V. All rights reserved.

  9. Reducing cyclone pressure drop with evasés

    USDA-ARS?s Scientific Manuscript database

    Cyclones are widely used to separate particles from gas flows and as air emissions control devices. Their cost of operation is proportional to the fan energy required to overcome their pressure drop. Evasés or exit diffusers potentially could reduce exit pressure losses without affecting collection...

  10. Influence of ambient air pressure on effervescent atomization

    NASA Technical Reports Server (NTRS)

    Chen, S. K.; Lefebvre, A. H.; Rollbuhler, J.

    1993-01-01

    The influence of ambient air pressure on the drop-size distributions produced in effervescent atomization is examined in this article. Also investigated are the effects on spray characteristics of variations in air/liquid mass ratio, liquid-injection pressure, and atomizer discharge-orifice diameter at different levels of ambient air pressure. It is found that continuous increase in air pressure above the normal atmospheric value causes the mean drop-size to first increase up to a maximum value and then decline. An explanation for this characteristic is provided in terms of the various contributing factors to the overall atomization process. It is also observed that changes in atomizer geometry and operating conditions have little effect on the distribution of drop-sizes in the spray.

  11. Experimental investigation of air pressure affecting filtration performance of fibrous filter sheet.

    PubMed

    Xu, Bin; Yu, Xiao; Wu, Ya; Lin, Zhongping

    2017-03-01

    Understanding the effect of air pressure on their filtration performance is important for assessing the effectiveness of fibrous filters under different practical circumstances. The effectiveness of three classes of air filter sheets were investigated in laboratory-based measurements at a wide range of air pressures (60-130 KPa). The filtration efficiency was found most sensitive to the air pressure change at smaller particle sizes. As the air pressure increased from 60 to 130 KPa, significant decrease in filtration efficiency (up to 15%) and increase in pressure drop (up to 90 Pa) were observed. The filtration efficiency of the filter sheet with largest fiber diameter and smallest solid volume fraction was affected most, while the pressure drop of the filter sheet with smallest fiber diameter and largest solid volume fraction was affected most. The effect of air pressure on the filtration efficiency was slightly larger at greater filter face air velocity. However, the effect of air pressure on the pressure drop was negligible. The filtration efficiency and pressure drop were explicitly expressed as functions of the air pressure. Two coefficients were empirically derived and successfully accounted for the effects of air pressure on filtration efficiency and pressure drop.

  12. Filter aids influence on pressure drop across a filtration system

    NASA Astrophysics Data System (ADS)

    Hajar, S.; Rashid, M.; Nurnadia, A.; Ammar, M. R.; Hasfalina, C. M.

    2017-06-01

    Filter aids is commonly used to reduce pressure drop across air filtration system as it helps to increase the efficiency of filtration of accumulated filter cake. Filtration velocity is one of the main parameters that affect the performance of filter aids material. In this study, a formulated filter aids consisting of PreKot™ and activated carbon mixture (designated as PrekotAC) was tested on PTFE filter media under various filtration velocities of 5, 6, and 8 m/min at a constant material loading of 0.2 mg/mm2. Results showed that pressure drop is highly influenced by filtration velocity where higher filtration velocity leads to a higher pressure drop across the filter cake. It was found that PrekotAC performed better in terms of reducing the pressure drop across the filter cake even at the highest filtration velocity. The diversity in different particle size distribution of non-uniform particle size in the formulated PrekotAC mixture presents a higher permeability causes a lower pressure drop across the accumulated filter cake. The finding suggests that PrekotAC is a promising filter aids material that helps reducing the pressure drop across fabric filtration system.

  13. Effect of airstream velocity on mean drop diameters of water sprays produced by pressure and air atomizing nozzles

    NASA Technical Reports Server (NTRS)

    Ingebo, R. D.

    1977-01-01

    A scanning radiometer was used to determine the effect of airstream velocity on the mean drop diameter of water sprays produced by pressure atomizing and air atomizing fuel nozzles used in previous combustion studies. Increasing airstream velocity from 23 to 53.4 meters per second reduced the Sauter mean diameter by approximately 50 percent with both types of fuel nozzles. The use of a sonic cup attached to the tip of an air assist nozzle reduced the Sauter mean diameter by approximately 40 percent. Test conditions included airstream velocities of 23 to 53.4 meters per second at 293 K and atmospheric pressure.

  14. Drop transfer between superhydrophobic wells using air logic control.

    PubMed

    Vuong, Thach; Cheong, Brandon Huey-Ping; Huynh, So Hung; Muradoglu, Murat; Liew, Oi Wah; Ng, Tuck Wah

    2015-02-21

    Superhydrophobic surfaces aid biochemical analysis by limiting sample loss. A system based on wells here tolerated tilting up to 20° and allowed air logic transfer with evidence of mixing. Conditions for intact transfer on 15 to 60 μL drops using compressed air pressure operation were also mapped.

  15. Gas Pressure-Drop Experiment

    ERIC Educational Resources Information Center

    Luyben, William L.; Tuzla, Kemal

    2010-01-01

    Most chemical engineering undergraduate laboratories have fluid mechanics experiments in which pressure drops through pipes are measured over a range of Reynolds numbers. The standard fluid is liquid water, which is essentially incompressible. Since density is constant, pressure drop does not depend on the pressure in the pipe. In addition, flow…

  16. Air Entrapment for Liquid Drops Impacting a Solid Substrate

    NASA Astrophysics Data System (ADS)

    Liu, Yuan; Tan, Peng; Xu, Lei

    2012-11-01

    Using high-speed photography coupled with optical interference, we experimentally study the air entrapment during a liquid drop impacting a solid substrate. We observe the formation of a compressed air film before the liquid touches the substrate, with internal pressure considerably higher than the atmospheric value. The degree of compression highly depends on the impact velocity, as explained by balancing the liquid deceleration with the large pressure of compressed air. After contact, the air film expands vertically at the edge, reducing its pressure within a few tens of microseconds and producing a thick rim on the perimeter. This thick-rimmed air film subsequently contracts into an air bubble, governed by the complex interaction between surface tension, inertia and viscous drag. Such a process is universally observed for impacts above a few centimeters high. Hong Kong GRF grant CUHK404211 and direct grant 2060418.

  17. Investigation of pressure drop in capillary tube for mixed refrigerant Joule-Thomson cryocooler

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

    Ardhapurkar, P. M.; Sridharan, Arunkumar; Atrey, M. D.

    2014-01-29

    A capillary tube is commonly used in small capacity refrigeration and air-conditioning systems. It is also a preferred expansion device in mixed refrigerant Joule-Thomson (MR J-T) cryocoolers, since it is inexpensive and simple in configuration. However, the flow inside a capillary tube is complex, since flashing process that occurs in case of refrigeration and air-conditioning systems is metastable. A mixture of refrigerants such as nitrogen, methane, ethane, propane and iso-butane expands below its inversion temperature in the capillary tube of MR J-T cryocooler and reaches cryogenic temperature. The mass flow rate of refrigerant mixture circulating through capillary tube depends onmore » the pressure difference across it. There are many empirical correlations which predict pressure drop across the capillary tube. However, they have not been tested for refrigerant mixtures and for operating conditions of the cryocooler. The present paper assesses the existing empirical correlations for predicting overall pressure drop across the capillary tube for the MR J-T cryocooler. The empirical correlations refer to homogeneous as well as separated flow models. Experiments are carried out to measure the overall pressure drop across the capillary tube for the cooler. Three different compositions of refrigerant mixture are used to study the pressure drop variations. The predicted overall pressure drop across the capillary tube is compared with the experimentally obtained value. The predictions obtained using homogeneous model show better match with the experimental results compared to separated flow models.« less

  18. Effect of airstream velocity on mean drop diameters of water sprays produced by pressure and air atomizing nozzles. [for combustion studies

    NASA Technical Reports Server (NTRS)

    Ingebo, R. D.

    1977-01-01

    A scanning radiometer was used to determine the effect of airstream velocity on the mean drop diameter of water sprays produced by pressure atomizing and air atomizing fuel nozzles used in previous combustion studies. Increasing airstream velocity from 23 to 53.4 meters per second reduced the Sauter mean diameter by approximately 50 percent with both types of fuel nozzles. The use of a sonic cup attached to the tip of an air assist nozzle reduced the Sauter mean diameter by approximately 40 percent. Test conditions included airstream velocities of 23 to 53.4 meters per second at 293 K and atmospheric pressure.

  19. Microfluidic pressure sensing using trapped air compression.

    PubMed

    Srivastava, Nimisha; Burns, Mark A

    2007-05-01

    We have developed a microfluidic method for measuring the fluid pressure head experienced at any location inside a microchannel. The principal component is a microfabricated sealed chamber with a single inlet and no exit; the entrance to the single inlet is positioned at the location where pressure is to be measured. The pressure measurement is then based on monitoring the movement of a liquid-air interface as it compresses air trapped inside the microfabricated sealed chamber and calculating the pressure using the ideal gas law. The method has been used to measure the pressure of the air stream and continuous liquid flow inside microfluidic channels (d approximately 50 microm). Further, a pressure drop has also been measured using multiple microfabricated sealed chambers. For air pressure, a resolution of 700 Pa within a full-scale range of 700-100 kPa was obtained. For liquids, pressure drops as low as 70 Pa were obtained in an operating range from 70 Pa to 10 kPa. Since the method primarily uses a microfluidic sealed chamber, it does not require additional fabrication steps and may easily be incorporated in several lab-on-a-chip fluidic applications for laminar as well as turbulent flow conditions.

  20. Microfluidic pressure sensing using trapped air compression

    PubMed Central

    Srivastava, Nimisha; Burns, Mark A.

    2010-01-01

    We have developed a microfluidic method for measuring the fluid pressure head experienced at any location inside a microchannel. The principal component is a microfabricated sealed chamber with a single inlet and no exit; the entrance to the single inlet is positioned at the location where pressure is to be measured. The pressure measurement is then based on monitoring the movement of a liquid–air interface as it compresses air trapped inside the microfabricated sealed chamber and calculating the pressure using the ideal gas law. The method has been used to measure the pressure of the air stream and continuous liquid flow inside microfluidic channels (d ~ 50 μm). Further, a pressure drop has also been measured using multiple microfabricated sealed chambers. For air pressure, a resolution of 700 Pa within a full-scale range of 700–100 kPa was obtained. For liquids, pressure drops as low as 70 Pa were obtained in an operating range from 70 Pa to 10 kPa. Since the method primarily uses a microfluidic sealed chamber, it does not require additional fabrication steps and may easily be incorporated in several lab-on-a-chip fluidic applications for laminar as well as turbulent flow conditions. PMID:17476384

  1. Experimental study of the effect of drag reducing agent on pressure drop and thermal efficiency of an air cooler

    NASA Astrophysics Data System (ADS)

    Peyghambarzadeh, S. M.; Hashemabadi, S. H.; Saffarian, H.; Shekari, F.

    2016-01-01

    Effect of polymeric drag reduction agents (DRAs) on pressure drop and heat transfer was studied. Aqueous solutions of carboxy methyl cellulose were used inside an air-finned heat exchanger. Despite the previous studies which indicated the importance of drag reduction just in turbulent flow, results of this study in laminar flow indicated that the addition of DRA increases drag reduction, and decreases the overall heat transfer coefficient.

  2. Aerodynamic effect of combustor inlet-air pressure on fuel jet atomization

    NASA Technical Reports Server (NTRS)

    Ingebo, R. D.

    1984-01-01

    Mean drop diameters were measured with a recently developed scanning radiometer in a study of the atomization of liquid jets injected cross stream in high velocity and high pressure airflows. At constant inlet air pressure, reciprocal mean drop diameter, was correlated with airflow mass velocity. Over a combustor inlet-air pressure range of 1 to 21 atmospheres, the ratio of orifice to mean drop diameter, D(O)/D(M), was correlated with the product of Weber and Reynolds number, WeRe, and with the molecular scale momentum transfer ratio of gravitational to inertial forces.

  3. Air cushioning in drop impact

    NASA Astrophysics Data System (ADS)

    de Ruiter, Jolet; Oh, Jung; van den Ende, Dirk; Mugele, Frieder

    2011-11-01

    Liquid drops impacting on solid surfaces deform under the influence of the ambient gas that needs to be squeezed out before a true solid-liquid contact can be established. We demonstrate experimentally the existence of this theoretically predicted air layer and follow its evolution with time for moderate impact speeds (We ~ 1 ... 10) using reflection interference microscopy with a thickness resolution of approximately 10nm. For a wide range of fluid properties (ρ, γ, η) we find a very robust generic behavior that includes the predicted formation of a dimple in the center of the drop with a local minimum of the air film thickness at its boundary. Depending on We as well as the fluid properties, a skating layer of more or less constant thickness as well as a second local minimum of the air film thickness farther away from the drop center develop in time. Eventually, solid-liquid contact is generated via random nucleation event. The nucleation spot spreads across the drop-substrate interface within a few milliseconds. This process can lead to the entrapment of an air bubble.

  4. Aerodynamic effect of combustor inlet-air pressure on fuel jet atomization

    NASA Technical Reports Server (NTRS)

    Ingebo, R. D.

    1984-01-01

    Mean drop diameters were measured with a recently developed scanning radiometer in a study of the atomization of liquid jets injected cross stream in high velocity and high pressure airflows. At constant inlet air pressure, reciprocal mean drop diameter was correlated with airflow mass velocity. Over a combustor inlet-air pressure range of 1 to 21 atmospheres, the ratio of orifice to mean drop diameter, D(O)/D(M), was correlated with the product of Weber and Reynolds number, WeRe, and with the molecular scale momentum transfer ratio of gravitational to inertial forces. Previously announced in STAR as N84-22910

  5. Determination of pressure drop across activated carbon fiber respirator cartridges.

    PubMed

    Balanay, Jo Anne G; Lungu, Claudiu T

    2016-01-01

    Activated carbon fiber (ACF) is considered as an alternative adsorbent to granular activated carbon (GAC) for the development of thinner, lighter, and efficient respirators because of their larger surface area and adsorption capacities, thinner critical bed depth, lighter weight, and fabric form. This study aims to measure the pressure drop across different types of commercially available ACFs in respirator cartridges to determine the ACF composition and density that will result in acceptably breathable respirators. Seven ACF types in cloth (ACFC) and felt (ACFF) forms were tested. ACFs in cartridges were challenged with pre-conditioned constant air flow (43 LPM, 23°C, 50% RH) at different compositions (single- or combination-ACF type) in a test chamber. Pressure drop across ACF cartridges were obtained using a micromanometer, and compared among different cartridge configurations, to those of the GAC cartridge, and to the NIOSH breathing resistance requirements for respirator cartridges. Single-ACF type cartridges filled with any ACFF had pressure drop measurements (23.71-39.93 mmH2O) within the NIOSH inhalation resistance requirement of 40 mmH2O, while those of the ACFC cartridges (85.47±3.67 mmH2O) exceeded twice the limit due possibly to the denser weaving of ACFC fibers. All single ACFF-type cartridges had higher pressure drop compared to the GAC cartridge (23.13±1.14 mmH2O). Certain ACF combinations (2 ACFF or ACFC/ACFF types) resulted to pressure drop (26.39-32.81 mmH2O) below the NIOSH limit. All single-ACFF type and all combination-ACF type cartridges with acceptable pressure drop had much lower adsorbent weights than GAC (≤15.2% of GAC weight), showing potential for light-weight respirator cartridges. 100% ACFC in cartridges may result to respirators with high breathing resistance and, thus, is not recommended. The more dense ACFF and ACFC types may still be possibly used in respirators by combining them with less dense ACFF materials and/or by

  6. Experimental Investigation of Oscillatory Flow Pressure and Pressure Drop Through Complex Geometries

    NASA Technical Reports Server (NTRS)

    Ibrahim, Mounir B.; Wang, Meng; Gedeon, David

    2005-01-01

    A series of experiments have been performed to investigate the oscillatory flow pressure and pressure drop through complex geometries. These experiments were conducted at the CSU-SLRE facility which is a horizontally opposed, two-piston, single-acting engine with a split crankshaft driving mechanism. Flow through a rectangular duct, with no insert (obstruction), was studied first. Then four different inserts were examined: Abrupt, Manifold, Diverging Short and Diverging Long. The inserts were mounted in the center of the rectangular duct to represent different type of geometries that could be encountered in Stirling machines. The pressure and pressure drop of the oscillating flow was studied for: 1) different inserts, 2) different phase angle between the two pistons of the engine (zero, 90 lead, 180, and 90 lag), and 3) for different piston frequencies (5, 10, 15, and 20 Hz). It was found that the pressure drop of the oscillatory flow increases with increasing Reynolds number. The pressure drop was shown to be mainly due to the gas inertia for the case of oscillatory flow through a rectangular duct with no insert. On the other hand, for the cases with different inserts into the rectangular duct, the pressure drop has three sources: inertia, friction, and local losses. The friction pressure drop is only a small fraction of the total pressure drop. It was also shown that the dimensionless pressure drop decreases with increasing kinetic Reynolds number.

  7. Define and Quantify the Physics of Air Flow, Pressure Drop and Aerosol Collection in Nuclear Grade HEPA Filters

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

    Moore, Murray E.

    Objective: Develop a set of peer-review and verified analytical methods to adjust HEPA filter performance to different flow rates, temperatures and altitudes. Experimental testing will measure HEPA filter flow rate, pressure drop and efficiency to verify the analytical approach. Nuclear facilities utilize HEPA (High Efficiency Particulate Air) filters to purify air flow for workspace ventilation. However, the ASME AG-1 technical standard (Code on Nuclear Air and Gas Treatment) does not adequately describe air flow measurement units for HEPA filter systems. Specifically, the AG-1 standard does not differentiate between volumetric air flow in ACFM (actual cubic feet per minute)compared to massmore » flow measured in SCFM (standard cubic feet per minute). More importantly, the AG-1 standard has an overall deficiency for using HEPA filter devices at different air flow rates, temperatures, and altitudes. Technical Approach: The collection efficiency and pressure drops of 18 different HEPA filters will be measured over a range of flow rates, temperatures and altitudes. The experimental results will be compared to analytical scoping calculations. Three manufacturers have allocated six HEPA filters each for this effort. The 18 filters will be tested at two different flow rates, two different temperatures and two different altitudes. The 36 total tests will be conducted at two different facilities: the ATI Test facilities (Baltimore MD) and the Los Alamos National Laboratory (Los Alamos NM). The Radiation Protection RP-SVS group at Los Alamos has an aerosol wind tunnel that was originally designed to evaluate small air samplers. In 2010, modifications were started to convert the wind tunnel for HEPA filter testing. (Extensive changes were necessary for the required aerosol generators, HEPA test fixtures, temperature control devices and measurement capabilities.) To this date, none of these modification activities have been funded through a specific DOE or NNSA program

  8. Antimicrobial nanoparticle-coated electrostatic air filter with high filtration efficiency and low pressure drop.

    PubMed

    Sim, Kyoung Mi; Park, Hyun-Seol; Bae, Gwi-Nam; Jung, Jae Hee

    2015-11-15

    In this study, we demonstrated an antimicrobial nanoparticle-coated electrostatic (ES) air filter. Antimicrobial natural-product Sophora flavescens nanoparticles were produced using an aerosol process, and were continuously deposited onto the surface of air filter media. For the electrostatic activation of the filter medium, a corona discharge electrification system was used before and after antimicrobial treatment of the filter. In the antimicrobial treatment process, the deposition efficiency of S. flavescens nanoparticles on the ES filter was ~12% higher than that on the pristine (Non-ES) filter. In the evaluation of filtration performance using test particles (a nanosized KCl aerosol and submicron-sized Staphylococcus epidermidis bioaerosol), the ES filter showed better filtration efficiency than the Non-ES filter. However, antimicrobial treatment with S. flavescens nanoparticles affected the filtration efficiency of the filter differently depending on the size of the test particles. While the filtration efficiency of the KCl nanoparticles was reduced on the ES filter after the antimicrobial treatment, the filtration efficiency was improved after the recharging process. In summary, we prepared an antimicrobial ES air filter with >99% antimicrobial activity, ~92.5% filtration efficiency (for a 300-nm KCl aerosol), and a ~0.8 mmAq pressure drop (at 13 cm/s). This study provides valuable information for the development of a hybrid air purification system that can serve various functions and be used in an indoor environment. Copyright © 2015 Elsevier B.V. All rights reserved.

  9. Variability among electronic cigarettes in the pressure drop, airflow rate, and aerosol production.

    PubMed

    Williams, Monique; Talbot, Prue

    2011-12-01

    This study investigated the performance of electronic cigarettes (e-cigarettes), compared different models within a brand, compared identical copies of the same model within a brand, and examined performance using different protocols. Airflow rate required to generate aerosol, pressure drop across e-cigarettes, and aerosol density were examined using three different protocols. First 10 puff protocol: The airflow rate required to produce aerosol and aerosol density varied among brands, while pressure drop varied among brands and between the same model within a brand. Total air hole area correlated with pressure drop for some brands. Smoke-out protocol: E-cigarettes within a brand generally performed similarly when puffed to exhaustion; however, there was considerable variation between brands in pressure drop, airflow rate required to produce aerosol, and the total number of puffs produced. With this protocol, aerosol density varied significantly between puffs and gradually declined. CONSECUTIVE TRIAL PROTOCOL: Two copies of one model were subjected to 11 puffs in three consecutive trials with breaks between trials. One copy performed similarly in each trial, while the second copy of the same model produced little aerosol during the third trial. The different performance properties of the two units were attributed to the atomizers. There was significant variability between and within brands in the airflow rate required to produce aerosol, pressure drop, length of time cartridges lasted, and production of aerosol. Variation in performance properties within brands suggests a need for better quality control during e-cigarette manufacture.

  10. Method for reducing pressure drop through filters, and filter exhibiting reduced pressure drop

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

    Sappok, Alexander; Wong, Victor

    Methods for generating and applying coatings to filters with porous material in order to reduce large pressure drop increases as material accumulates in a filter, as well as the filter exhibiting reduced and/or more uniform pressure drop. The filter can be a diesel particulate trap for removing particulate matter such as soot from the exhaust of a diesel engine. Porous material such as ash is loaded on the surface of the substrate or filter walls, such as by coating, depositing, distributing or layering the porous material along the channel walls of the filter in an amount effective for minimizing ormore » preventing depth filtration during use of the filter. Efficient filtration at acceptable flow rates is achieved.« less

  11. A study of pressure losses in residential air distribution systems

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

    Abushakra, Bass; Walker, Iain S.; Sherman, Max H.

    2002-07-01

    An experimental study was conducted to evaluate the pressure drop characteristics of residential duct system components that are either not available or not thoroughly (sometimes incorrectly) described in existing duct design literature. The tests were designed to imitate cases normally found in typical residential and light commercial installations. The study included three different sizes of flexible ducts, under different compression configurations, splitter boxes, supply boots, and a fresh air intake hood. The experimental tests conformed to ASHRAE Standard 120P--''Methods of Testing to Determine Flow Resistance of HVAC Air Ducts and Fittings''. The flexible duct study covered compressibility and bending effectsmore » on the total pressure drop, and the results showed that the available published references tend to underestimate the effects of compression in flexible ducts that can increase pressure drops by up to a factor of nine. The supply boots were tested under different configurations including a setup where a flexible duct elbow connection was considered as an integral part of the supply boot. The supply boots results showed that diffusers can increase the pressure drop by up to a factor of two in exit fittings, and the installation configuration can increase the pressure drop by up to a factor of five. The results showed that it is crucial for designers and contractors to be aware of the compressibility effects of the flexible duct, and the installation of supply boots and diffusers.« less

  12. Flame propagation in heterogeneous mixtures of fuel drops and air

    NASA Technical Reports Server (NTRS)

    Myers, G. D.; Lefebvre, A. H.

    1984-01-01

    Photographic methods are used to measure flame speeds in flowing mixtures of fuel props and air at atmospheric pressure. The fuels employed include a conventional fuel oil plus various blends JP 7 with stocks containing single-ring and mullti-ring aromatics. The results for stoichiometric mixtures show that flame propagation cannot occur in mixtures containing mean drop sizes larger than 300 to 400 microns, depending on the fuel type. For smaller drop sizes, down to around 60 microns, flame speed is inversely proportional to drop size, indicating that evaporation rates are limiting to flame speed. Below around 60 microns, the curves of flame speed versus mean drop size flatten out, thereby demonstrating that for finely atomized sprays flame speeds are much less dependent on evaporation rates, and are governed primarily by mixing and/or chemical reaction rates. The fuels exhibiting the highest flame speeds are those containing multi-ring aromatics. This is attributed to the higher radiative heat flux emanating from their soot-bearing flames which enhances the rate of evaporation of the fuel drops approaching the flame front.

  13. Effects of phosphoric acid sprayed into an incinerator furnace on the flue gas pressure drop at fabric filters.

    PubMed

    Takahashi, Shigetoshi; Hwang, In-Hee; Matsuto, Toshihiko

    2016-06-01

    Fabric filters are widely used to remove dust from flue gas generated by waste incineration. However, a pressure drop occurs at the filters, caused by growth of a dust layer on the filter fabric despite regular cleaning by pulsed-jet air. The pressure drop at the fabric filters leads to energy consumption at induced draft fan to keep the incinerator on negative pressure, so that its proper control is important to operate incineration facility efficiently. The pressure drop at fabric filters decreased whenever phosphoric acid wastewater (PAW) was sprayed into an incinerator for treating industrial waste. Operational data obtained from the incineration facility were analyzed to determine the short- and long-term effects of PAW spraying on the pressure drop. For the short-term effect, it was confirmed that the pressure drop at the fabric filters always decreased to 0.3-1.2kPa within about 5h after spraying PAW. This effect was expected to be obtained by about one third of present PAW spraying amount. However, from the long-term perspective, the pressure drop showed an increase in the periods of PAW spraying compared with periods for which PAW spraying was not performed. The pressure drop increase was particularly noticeable after the initial PAW spraying, regardless of the age and type of fabric filters used. These results suggest that present PAW spraying causes a temporary pressure drop reduction, leading to short-term energy consumption savings; however, it also causes an increase of the pressure drop over the long-term, degrading the overall operating conditions. Thus, appropriate PAW spraying conditions are needed to make effective use of PAW to reduce the pressure drop at fabric filters from a short- and long-term point of view. Copyright © 2016 Elsevier Ltd. All rights reserved.

  14. Air Pressure Responses to Sudden Vocal Tract Pressure Bleeds During Production of Stop Consonants: New Evidence of Aeromechanical Regulation

    PubMed Central

    Zajac, David J.; Weissler, Mark C.

    2011-01-01

    Two studies were conducted to evaluate short-latency vocal tract air pressure responses to sudden pressure bleeds during production of voiceless bilabial stop consonants. It was hypothesized that the occurrence of respiratory reflexes would be indicated by distinct patterns of responses as a function of bleed magnitude. In Study 1, 19 adults produced syllable trains of /pΛ/ using a mouthpiece coupled to a computer-controlled perturbator. The device randomly created bleed apertures that ranged from 0 to 40 mm2 during production of the 2nd or 4th syllable of an utterance. Although peak oral air pressure dropped in a linear manner across bleed apertures, it averaged 2 to 3 cm H2O at the largest bleed. While slope of oral pressure also decreased in a linear trend, duration of the oral pressure pulse remained relatively constant. The patterns suggest that respiratory reflexes, if present, have little effect on oral air pressure levels. In Study 2, both oral and subglottal air pressure responses were monitored in 2 adults while bleed apertures of 20 and 40 mm2 were randomly created. For 1 participant, peak oral air pressure dropped across bleed apertures, as in Study 1. Subglottal air pressure and slope, however, remained relatively stable. These patterns provide some support for the occurrence of respiratory reflexes to regulate subglottal air pressure. Overall, the studies indicate that the inherent physiologic processes of the respiratory system, which may involve reflexes, and passive aeromechanical resistance of the upper airway are capable of developing oral air pressure in the face of substantial pressure bleeds. Implications for understanding speech production and the characteristics of individuals with velopharyngeal dysfunction are discussed. PMID:15324286

  15. Prediction of friction pressure drop for low pressure two-phase flows on the basis of approximate analytical models

    NASA Astrophysics Data System (ADS)

    Zubov, N. O.; Kaban'kov, O. N.; Yagov, V. V.; Sukomel, L. A.

    2017-12-01

    Wide use of natural circulation loops operating at low redused pressures generates the real need to develop reliable methods for predicting flow regimes and friction pressure drop for two-phase flows in this region of parameters. Although water-air flows at close-to-atmospheric pressures are the most widely studied subject in the field of two-phase hydrodynamics, the problem of reliably calculating friction pressure drop can hardly be regarded to have been fully solved. The specific volumes of liquid differ very much from those of steam (gas) under such conditions, due to which even a small change in flow quality may cause the flow pattern to alter very significantly. Frequently made attempts to use some or another universal approach to calculating friction pressure drop in a wide range of steam quality values do not seem to be justified and yield predicted values that are poorly consistent with experimentally measured data. The article analyzes the existing methods used to calculate friction pressure drop for two-phase flows at low pressures by comparing their results with the experimentally obtained data. The advisability of elaborating calculation procedures for determining the friction pressure drop and void fraction for two-phase flows taking their pattern (flow regime) into account is demonstrated. It is shown that, for flows characterized by low reduced pressures, satisfactory results are obtained from using a homogeneous model for quasi-homogeneous flows, whereas satisfactory results are obtained from using an annular flow model for flows characterized by high values of void fraction. Recommendations for making a shift from one model to another in carrying out engineering calculations are formulated and tested. By using the modified annular flow model, it is possible to obtain reliable predictions for not only the pressure gradient but also for the liquid film thickness; the consideration of droplet entrainment and deposition phenomena allows reasonable

  16. Numerical studies on heat transfer and pressure drop characteristics of flat finned tube bundles with various fin materials

    NASA Astrophysics Data System (ADS)

    Peng, Y.; Zhang, S. J.; Shen, F.; Wang, X. B.; Yang, X. R.; Yang, L. J.

    2017-11-01

    The air-cooled heat exchanger plays an important role in the field of industry like for example in thermal power plants. On the other hand, it can be used to remove core decay heat out of containment passively in case of a severe accident circumstance. Thus, research on the performance of fins in air-cooled heat exchangers can benefit the optimal design and operation of cooling systems in nuclear power plants. In this study, a CFD (Computational Fluid Dynamic) method is implemented to investigate the effects of inlet velocity, fin spacing and tube pitch on the flow and the heat transfer characteristics of flat fins constructed of various materials (316L stainless steel, copper-nickel alloy and aluminium). A three dimensional geometric model of flat finned tube bundles with fixed longitudinal tube pitch and transverse tube pitch is established. Results for the variation of the average convective heat transfer coefficient with respect to cooling air inlet velocity, fin spacing, tube pitch and fin material are obtained, as well as for the pressure drop of the cooling air passing through finned tube. It is shown that the increase of cooling air inlet velocity results in enhanced average convective heat transfer coefficient and decreasing pressure drop. Both fin spacing and tube pitch engender positive effects on pressure drop and have negative effects on heat transfer characteristics. Concerning the fin material, the heat transfer performance of copper-nickel alloy is superior to 316L stainless steel and inferior to aluminium.

  17. Falling drops skating on a film of air

    NASA Astrophysics Data System (ADS)

    Rubinstein, Shmuel

    2012-02-01

    When a raindrop hits a window, the surface immediately becomes wet as the water spreads. Indeed, this common observation of a drop impacting a surface is ubiquitous in our everyday experience. I will show that the impact of a drop on a surface is a much richer, more complex phenomenon than our simple experience may suggests: To completely wet the surface the drop must first expel all the air beneath it; however, this does not happened instantaneously. Instead, a very thin film of air, only a few tens of nanometers thick, remains trapped between the falling drop and the surface as the fluid spreads. The thin film of air serves to lubricate the drop enabling the fluid to skate laterally outward at strikingly high velocities. Simultaneously, the wetting fluid spreads inward at a much slower velocity, trapping a bubble of air within the drop. However, these events occur at diminutive length scales and fleeting time scales; therefore, to visualize them we develop new imaging modalities that are sensitive to the behavior right at the surface and that have time resolution superior to even the very fastest cameras. These imaging techniques reveal that the ultimate wetting of the surface occurs through a completely new mechanism, the breakup of the thin film of air through a spinodal like dewetting process that breaks the cylindrical symmetry of the impact and drives an anomalously rapid spreading of a wetting front. These results are in accord with recent theoretical predictions and challenge the prevailing paradigm in which contact between the liquid and solid occurs immediately, and spreading is dominated by the dynamics of a single contact line.

  18. Air entrapment under an impacting drop

    NASA Astrophysics Data System (ADS)

    Thoroddsen, S. T.; Etoh, T. G.; Takehara, K.

    2003-03-01

    When a drop impacts on a liquid surface it entraps a small amount of air under its centre as the two liquid surfaces meet. The contact occurs along a ring enclosing a thin disk of air. We use the next-generation ultra-high-speed video camera, capable of 1 million f.p.s. (Etoh et al. 2002), to study the dynamics of this air sheet as it contracts due to surface tension, to form a bubble or, more frequently, splits into two bubbles. During the contraction of the air disk an azimuthal undulation, resembling a pearl necklace, develops along its edge. The contraction speed of the sheet is accurately described by a balance between inertia and surface tension. The average initial thickness of the air sheet decreases with higher impact Reynolds numbers, becoming less than one micron. The total volume of air entrapped depends strongly on the bottom curvature of the drop at impact. A sheet of micro-bubbles is often observed along the original interface. Oguz Prosperetti bubble rings are also observed. For low Weber numbers (We<20) a variety of other entrapment phenomena appear.

  19. Skating on a Film of Air: Drops Impacting on a Surface

    NASA Astrophysics Data System (ADS)

    Kolinski, John M.; Rubinstein, Shmuel M.; Mandre, Shreyas; Brenner, Michael P.; Weitz, David A.; Mahadevan, L.

    2012-02-01

    The commonly accepted description of drops impacting on a surface typically ignores the essential role of the air that is trapped between the impacting drop and the surface. Here we describe a new imaging modality that is sensitive to the behavior right at the surface. We show that a very thin film of air, only a few tens of nanometers thick, remains trapped between the falling drop and the surface as the drop spreads. The thin film of air serves to lubricate the drop enabling the fluid to skate on the air film laterally outward at surprisingly high velocities, consistent with theoretical predictions. Eventually this thin film of air breaks down as the fluid wets the surface via a spinodal-like mechanism. Our results show that the dynamics of impacting drops are much more complex than previously thought, with a rich array of unexpected phenomena that require rethinking classic paradigms.

  20. Microseismicity Induced by Fluid Pressure Drop (Laboratory Study)

    NASA Astrophysics Data System (ADS)

    Turuntaev, Sergey; Zenchenko, Evgeny; Melchaeva, Olga

    2013-04-01

    Pore pressure change in saturated porous rocks may result in its fracturing (Maury et Fourmaintraux, 1993) and corresponding microseismic event occurrences. Microseismicity due to fluid injection is considered in numerous papers (Maxwell, 2010, Shapiro et al., 2005). Another type of the porous medium fracturing is related with rapid pore pressure drop at some boundary. The mechanism of such fracturing was considered by (Khristianovich, 1985) as a model of sudden coal blowing and by (Alidibirov, Panov, 1998) as a model of volcano eruptions. If the porous saturated medium has a boundary where it directly contacted with fluid under the high pressure (in a hydraulic fracture or in a borehole), and the pressure at that boundary is dropped, the conditions for tensile cracks can be achieved at some distance from the boundary. In the paper, the results of experimental study of saturated porous sample fracturing due to pore pressure rapid drop are discussed. The samples (82 mm high, ∅60 mm) were made of quartz sand, which was cemented by "liquid glass" glue with mass fraction 1%. The sample (porosity 35%, uniaxial unconfined compression strength 2.5 MPa) was placed in a mould and saturated by oil. The upper end of the sample contacted with the mould upper lid, the lower end contacted with fluid. The fluid pressure was increased to 10 MPa and then discharged through the bottom nipple. The pressure increases/drops were repeated 30-50 times. Pore pressure and acoustic emission (AE) were registered by transducers mounted into upper and bottom lids of the mould. It was found, that AE sources (corresponded to microfracturing) were spreading from the open end to the closed end of the sample, and that maximal number of AE events was registered at some distance from the opened end. The number of AE pulses increased with every next pressure drop, meanwhile the number of pulses with high amplitudes diminished. It was found that AE maximal rate corresponded to the fluid pressure

  1. Pressure, temperature and density drops along supercritical fluid chromatography columns in different thermal environments. III. Mixtures of carbon dioxide and methanol as the mobile phase.

    PubMed

    Poe, Donald P; Veit, Devon; Ranger, Megan; Kaczmarski, Krzysztof; Tarafder, Abhijit; Guiochon, Georges

    2014-01-03

    The pressure, temperature and density drops along SFC columns eluted with a CO2/methanol mobile phase were measured and compared with theoretical values. For columns packed with 3- and 5-μm particles the pressure and temperature drops were measured using a mobile phase of 95% CO2 and 5% methanol at a flow rate of 5mL/min, at temperatures from 20 to 100°C, and outlet pressures from 80 to 300bar. The density drop was calculated based on the temperature and pressure at the column inlet and outlet. The columns were suspended in a circulating air bath, either bare or covered with foam insulation. The experimental measurements were compared to theoretical results obtained by numerical simulation. For the convective air condition at outlet pressures above 100bar the average difference between the experimental and calculated temperature drops and pressure drops were 0.1°C and 0.7% for the bare 3-μm column, respectively, and were 0.6°C and 4.1% for the insulated column. The observed temperature drops for the insulated columns are consistent with those predicted by the Joule-Thomson coefficients for isenthalpic expansion. The dependence of the temperature and the pressure drops on the Joule-Thomson coefficient and kinematic viscosity are described for carbon dioxide mobile phases containing up to 20% methanol. Copyright © 2013 Elsevier B.V. All rights reserved.

  2. Flow rate-pressure drop relation for deformable shallow microfluidic channels

    NASA Astrophysics Data System (ADS)

    Christov, Ivan C.; Cognet, Vincent; Shidhore, Tanmay C.; Stone, Howard A.

    2018-04-01

    Laminar flow in devices fabricated from soft materials causes deformation of the passage geometry, which affects the flow rate--pressure drop relation. For a given pressure drop, in channels with narrow rectangular cross-section, the flow rate varies as the cube of the channel height, so deformation can produce significant quantitative effects, including nonlinear dependence on the pressure drop [{Gervais, T., El-Ali, J., G\\"unther, A. \\& Jensen, K.\\ F.}\\ 2006 Flow-induced deformation of shallow microfluidic channels.\\ \\textit{Lab Chip} \\textbf{6}, 500--507]. Gervais et. al. proposed a successful model of the deformation-induced change in the flow rate by heuristically coupling a Hookean elastic response with the lubrication approximation for Stokes flow. However, their model contains a fitting parameter that must be found for each channel shape by performing an experiment. We present a perturbation approach for the flow rate--pressure drop relation in a shallow deformable microchannel using the theory of isotropic quasi-static plate bending and the Stokes equations under a lubrication approximation (specifically, the ratio of the channel's height to its width and of the channel's height to its length are both assumed small). Our result contains no free parameters and confirms Gervais et. al.'s observation that the flow rate is a quartic polynomial of the pressure drop. The derived flow rate--pressure drop relation compares favorably with experimental measurements.

  3. Modeling pressure relationships of inspired air into the human lung bifurcations through simulations

    NASA Astrophysics Data System (ADS)

    Aghasafari, Parya; Ibrahim, Israr B. M.; Pidaparti, Ramana

    2018-03-01

    Applied pressure on human lung wall has great importance on setting up protective ventilatory strategies, therefore, estimating pressure relationships in terms of specific parameters would provide invaluable information specifically during mechanical ventilation (MV). A three-dimensional model from a healthy human lung MRI is analyzed by computational fluid dynamic (CFD), and results for pressure are curve fitted to estimate relationships that associate pressure to breathing time, cross section and generation numbers of intended locations. Among all possible functions, it is observed that exponential and polynomial pressure functions present most accurate results for normal breathing (NB) and MV, respectively. For validation, pressure-location curves from CFD and results from this study are compared and good correlations are found. Also, estimated pressure values are used to calculate pressure drop and airway resistance to the induced air into the lung bifurcations. It is concluded that maximum pressure drop appeared in generation number 2 and medium sized airways show higher resistance to air flow and that resistance decreased as cross sectional area increased through the model. Results from this study are in good agreement with previous studies and provide potentials for further studies on influence of air pressure on human lung tissue and reducing lung injuries during MV.

  4. A systematic search of sudden pressure drops on Gale crater during two Martian years derived from MSL/REMS data

    NASA Astrophysics Data System (ADS)

    Ordonez-Etxeberria, Iñaki; Hueso, Ricardo; Sánchez-Lavega, Agustín

    2018-01-01

    The Mars Science Laboratory (MSL) rover carries a suite of meteorological detectors that constitute the Rover Environmental Monitoring Station (REMS) instrument. REMS investigates the meteorological conditions at Gale crater by obtaining high-frequency data of pressure, air and ground temperature, relative humidity, UV flux at the surface and wind intensity and direction with some limitations in the wind data. We have run a search of atmospheric pressure drops of short duration (< 25 s) and we present a statistical study of the frequency of these events in the REMS pressure data during its first 1417 sols (more than two Martian years). The identified daytime pressure drops could be caused by the close passages of warm vortices and dust devils. Previous systematic searches of warm vortices from REMS pressure data (Kahanpää et al., 2016; Steakley and Murphy, 2016) cover about one Martian year. We show that sudden pressure drops are twice more abundant in the second Martian year [sols 671-1339] than in the first one analyzed in previous works. The higher number of detections could be linked to a combination of different topography, higher altitudes (120 m above the landing site) and true inter-annual meteorological variability. We found 1129 events with a pressure drop larger than 0.5 Pa. Of these, 635 occurred during the local daytime (∼56%) and 494 were nocturnal. The most intense pressure drop (4.2 Pa) occurred at daytime on sol 1417 (areocentric solar longitude Ls = 195°) and was accompanied by a simultaneous decrease in the UV signal of 7.1%, pointing to a true dust devil. We also discuss similar but less intense simultaneous pressure and UV radiation drops that constitute 0.7% of all daytime events. Most of the intense daytime pressure drops with variations larger than 1.0 Pa occur when the difference between air and ground temperature is larger than 15 K. Statistically, the frequency of daytime pressure drops peaks close to noon (12:00-13:00 Local True

  5. Condensation heat transfer and pressure drop of R-410A in flat aluminum multi-port tubes

    NASA Astrophysics Data System (ADS)

    Kim, Nae-Hyun

    2018-02-01

    Brazed heat exchangers with aluminum flat multi-port tubes are being used as condensers of residential air-conditioners. In this study, R-410A condensation tests were conducted in four multi-port tubes having a range of hydraulic diameter (0.78 ≤ Dh ≤ 0.95 mm). The test range covered the mass flux from 100 to 400 kg/m2 s and the heat flux at 3 kW/m2, which are typical operating conditions of residential air conditioners. Results showed that both the heat transfer coefficient and the pressure drop increased as the hydraulic diameter decreased. The effect of hydraulic diameter on condensation heat transfer was much larger than the predictions of existing correlations for the range of investigation. Comparison of the data with the correlations showed that some macro-channel tube correlations and mini-channel tube correlations reasonably predicted the heat transfer coefficient. However, macro-channel correlations highly overpredicted the pressure drop data.

  6. Liquid jet response to internal modulated ultrasonic radiation pressure and stimulated drop production.

    PubMed

    Lonzaga, Joel B; Osterhoudt, Curtis F; Thiessen, David B; Marston, Philip L

    2007-06-01

    Experimental evidence shows that a liquid jet in air is an acoustic waveguide having a cutoff frequency inversely proportional to the jet diameter. Ultrasound applied to the jet supply liquid can propagate within the jet when the acoustic frequency is near to or above the cutoff frequency. Modulated radiation pressure is used to stimulate large amplitude deformations and the breakup of the jet into drops. The jet response to the modulated internal ultrasonic radiation pressure was monitored along the jet using (a) an optical extinction method and (b) images captured by a video camera. The jet profile oscillates at the frequency of the radiation pressure modulation and where the response is small, the amplitude was found to increase in proportion to the square of the acoustic pressure amplitude as previously demonstrated for oscillating drops [P.L. Marston and R.E. Apfel, J. Acoust. Soc. Am. 67, 27-37 (1980)]. Small amplitude deformations initially grow approximately exponentially with axial distance along the jet. Though aspects of the perturbation growth can be approximated from Rayleigh's analysis of the capillary instability, some detailed features of the observed jet response to modulated ultrasound are unexplained neglecting the effects of gravity.

  7. On the collapse pressure of armored bubbles and drops.

    PubMed

    Pitois, O; Buisson, M; Chateau, X

    2015-05-01

    Drops and bubbles wrapped in dense monolayers of hydrophobic particles are known to sustain a significant decrease of their internal pressure. Through dedicated experiments we investigate the collapse behavior of such armored water drops as a function of the particle-to-drop size ratio in the range 0.02-0.2. We show that this parameter controls the behavior of the armor during the deflation: at small size ratios the drop shrinkage proceeds through the soft crumpling of the monolayer, at intermediate ratios the drop becomes faceted, and for the largest studied ratios the armor behaves like a granular arch. The results show that each of the three morphological regimes is characterized by an increasing magnitude of the collapse pressure. This increase is qualitatively modeled thanks to a mechanism involving out-of-plane deformations and particle disentanglement in the armor.

  8. Spume Drops: Their Potential Role in Air-Sea Gas Exchange

    NASA Astrophysics Data System (ADS)

    Monahan, Edward C.; Staniec, Allison; Vlahos, Penny

    2017-12-01

    After summarizing the time scales defining the change of the physical properties of spume and other droplets cast up from the sea surface, the time scales governing drop-atmosphere gas exchange are compared. Following a broad review of the spume drop production functions described in the literature, a subset of these functions is selected via objective criteria, to represent typical, upper bound, and lower bound production functions. Three complementary mechanisms driving spume-atmosphere gas exchange are described, and one is then used to estimate the relative importance, over a broad range of wind speeds, of this spume drop mechanism compared to the conventional, diffusional, sea surface mechanism in air-sea gas exchange. While remaining uncertainties in the wind dependence of the spume drop production flux, and in the immediate sea surface gas flux, preclude a definitive conclusion, the findings of this study strongly suggest that, at high wind speeds (>20 m s-1 for dimethyl sulfide and >30 m s-1 for gases such a carbon dioxide), spume drops do make a significant contribution to air-sea gas exchange.Plain Language SummaryThis paper evaluates the existing spume <span class="hlt">drop</span> generation functions available to date and selects a reasonable upper, lower and mid range function that are reasonable for use in <span class="hlt">air</span> sea exchange models. Based on these the contribution of spume <span class="hlt">drops</span> to overall <span class="hlt">air</span> sea gas exchange at different wind speeds is then evaluated to determine the % contribution of spume. Generally below 20ms-1 spume <span class="hlt">drops</span> contribute <1% of gas exchange but may account for a significant amount of gas exchange at higher wind speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28478944','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28478944"><span>Theoretical and experimental evaluation of the effects of an argon gas mixture on the <span class="hlt">pressure</span> <span class="hlt">drop</span> through adult tracheobronchial airway replicas.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Litwin, Patrick D; Reis Dib, Anna Luisa; Chen, John; Noga, Michelle; Finlay, Warren H; Martin, Andrew R</p> <p>2017-06-14</p> <p>Argon has the potential to be a novel inhaled therapeutic agent, owing to the neuroprotective and organoprotective properties demonstrated in preclinical studies. Before human trials are performed, an understanding of varying gas properties on airway resistance during inhalation is essential. This study predicts the effect of an 80% argon/20% oxygen gas mixture on the <span class="hlt">pressure</span> <span class="hlt">drop</span> through conducting airways, and by extension the airway resistance, and then verifies these predictions experimentally using 3-D printed adult tracheobronchial airway replicas. The predicted <span class="hlt">pressure</span> <span class="hlt">drop</span> was calculated using established analytical models of airway resistance, incorporating the change in viscosity and density of the 80% argon/20% oxygen mixture versus that of <span class="hlt">air</span>. Predicted <span class="hlt">pressure</span> <span class="hlt">drop</span> for the argon mixture increased by approximately 29% compared to that for <span class="hlt">air</span>. The experimental results were consistent with this prediction for inspiratory flows ranging from 15 to 90slpm. These results indicate that established analytical models may be used to predict increases in conducting airway resistance for argon/oxygen mixtures, compared with <span class="hlt">air</span>. Such predictions are valuable in predicting average patient response to breathing argon/oxygen mixtures, and in selecting or designing delivery systems for use in administration of argon/oxygen mixtures to critically ill or injured patients. Copyright © 2017 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012APS..DFD.G8004M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012APS..DFD.G8004M"><span>Measuring the force of drag on <span class="hlt">air</span> sheared sessile <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Milne, Andrew J. B.; Fleck, Brian; Amirfazli, Alidad</p> <p>2012-11-01</p> <p>To blow a <span class="hlt">drop</span> along or off of a surface (i.e. to shed the <span class="hlt">drop</span>), the drag force on the <span class="hlt">drop</span> (based on flow conditions, <span class="hlt">drop</span> shape, and fluid properties) must overcome the adhesion force between the <span class="hlt">drop</span> and the surface (based on surface tension, <span class="hlt">drop</span> shape, and contact angle). While the shedding of sessile <span class="hlt">drops</span> by shear flow has been studied [Milne, A. J. B. & Amirfazli, A. Langmuir 25, 14155 (2009).], no independent measurements of the drag or adhesion forces have been made. Likewise, analytic predictions are limited to hemispherical <span class="hlt">drops</span> and low <span class="hlt">air</span> velocities. We present, therefore, measurements of the drag force on sessile <span class="hlt">drops</span> at <span class="hlt">air</span> velocities up to the point of incipient motion. Measurements were made using a modified floating element shear sensor in a laminar low speed wind tunnel to record drag force over the surface with the <span class="hlt">drop</span> absent, and over the combined system of the surface and <span class="hlt">drop</span> partially immersed in the boundary layer. Surfaces of different wettabilities were used to study the effects of <span class="hlt">drop</span> shape and contact angles, with <span class="hlt">drop</span> volume ranged between approximately 10 and 100 microlitres. The drag force for incipient motion (which by definition equals the maximum of the adhesion force) is compared to simplified models for <span class="hlt">drop</span> adhesion such as that of Furmidge</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880000475&hterms=hanging+drop&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dhanging%2Bdrop','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880000475&hterms=hanging+drop&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dhanging%2Bdrop"><span>Controlling Vapor <span class="hlt">Pressure</span> In Hanging-<span class="hlt">Drop</span> Crystallization</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Carter, Daniel C.; Smith, Robbie</p> <p>1988-01-01</p> <p>Rate of evaporation adjusted to produce larger crystals. Device helps to control vapor <span class="hlt">pressure</span> of water and other solvents in vicinity of hanging <span class="hlt">drop</span> of solution containing dissolved enzyme protein. Well of porous frit (sintered glass) holds solution in proximity to <span class="hlt">drop</span> of solution containing protein or enzyme. Vapor from solution in frit controls evaporation of solvent from <span class="hlt">drop</span> to control precipitation of protein or enzyme. With device, rate of nucleation limited to decrease number and increase size (and perhaps quality) of crystals - large crystals of higher quality needed for x-ray diffraction studies of macromolecules.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000031620','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000031620"><span>System for Manipulating <span class="hlt">Drops</span> and Bubbles Using Acoustic Radiation <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Oeftering, Richard C. (Inventor)</p> <p>1999-01-01</p> <p>The manipulation and control of <span class="hlt">drops</span> of liquid and gas bubbles is achieved using high intensity acoustics in the form of and/or acoustic radiation <span class="hlt">pressure</span> and acoustic streaming. generated by a controlled wave emission from a transducer. Acoustic radiation <span class="hlt">pressure</span> is used to deploy or dispense <span class="hlt">drops</span> into a liquid or a gas or bubbles into a liquid at zero or near zero velocity from the discharge end of a needle such as a syringe needle. Acoustic streaming is useful in manipulating the <span class="hlt">drop</span> or bubble during or after deployment. Deployment and discharge is achieved by focusing the acoustic radiation <span class="hlt">pressure</span> on the discharge end of the needle, and passing the acoustic waves through the fluid in the needle. through the needle will itself, or coaxially through the fluid medium surrounding the needle. Alternatively, the acoustic waves can be counter-deployed by focusing on the discharge end of the needle from a transducer axially aligned with the needle, but at a position opposite the needle, to prevent premature deployment of the <span class="hlt">drop</span> or bubble. The acoustic radiation <span class="hlt">pressure</span> can also be used for detecting the presence or absence of a <span class="hlt">drop</span> or a bubble at the tip of a needle or for sensing various physical characteristics of the <span class="hlt">drop</span> or bubble such as size or density.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22521956','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22521956"><span><span class="hlt">Pressure</span>, temperature and density <span class="hlt">drops</span> along supercritical fluid chromatography columns. I. Experimental results for neat carbon dioxide and columns packed with 3- and 5-micron particles.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Poe, Donald P; Veit, Devon; Ranger, Megan; Kaczmarski, Krzysztof; Tarafder, Abhijit; Guiochon, Georges</p> <p>2012-08-10</p> <p>The <span class="hlt">pressure</span> <span class="hlt">drop</span> and temperature <span class="hlt">drop</span> on columns packed with 3- and 5-micron particles were measured using neat CO(2) at a flow rate of 5 mL/min, at temperatures from 20°C to 100°C, and outlet <span class="hlt">pressures</span> from 80 to 300 bar. The density <span class="hlt">drop</span> was calculated based on the temperature and <span class="hlt">pressure</span> at the column inlet and outlet. The columns were suspended in a circulating <span class="hlt">air</span> bath either bare or covered with foam insulation. The results show that the <span class="hlt">pressure</span> <span class="hlt">drop</span> depends on the outlet <span class="hlt">pressure</span>, the operating temperature, and the thermal environment. A temperature <span class="hlt">drop</span> was observed for all conditions studied. The temperature <span class="hlt">drop</span> was relatively small (less than 3°C) for combinations of low temperature and high <span class="hlt">pressure</span>. Larger temperature <span class="hlt">drops</span> and density <span class="hlt">drops</span> occurred at higher temperatures and low to moderate <span class="hlt">pressures</span>. Covering the column with thermal insulation resulted in larger temperature <span class="hlt">drops</span> and corresponding smaller density <span class="hlt">drops</span>. At 20°C the temperature <span class="hlt">drop</span> was never more than a few degrees. The largest temperature <span class="hlt">drops</span> occurred for both columns when insulated at 80°C and 80 bar, reaching a maximum value of 21°C for the 5-micron column, and 26°C for the 3-micron column. For an adiabatic column, the temperature <span class="hlt">drop</span> depends on the <span class="hlt">pressure</span> <span class="hlt">drop</span>, the thermal expansion coefficient, and the density and the heat capacity of the mobile phase fluid, and can be described by a simple mathematical relationship. For a fixed operating temperature and outlet <span class="hlt">pressure</span>, the temperature <span class="hlt">drop</span> increases monotonically with the <span class="hlt">pressure</span> <span class="hlt">drop</span>. Copyright © 2012 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23261298','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23261298"><span>Estimation of methacrylate monolith binding capacity from <span class="hlt">pressure</span> <span class="hlt">drop</span> data.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Podgornik, Aleš; Smrekar, Vida; Krajnc, Peter; Strancar, Aleš</p> <p>2013-01-11</p> <p>Convective chromatographic media comprising of membranes and monoliths represent an important group of chromatographic supports due to their flow-unaffected chromatographic properties and consequently fast separation and purification even of large biological macromolecules. Consisting of a single piece of material, common characterization procedures based on analysis of a small sample assuming to be representative for the entire batch, cannot be applied. Because of that, non-invasive characterization methods are preferred. In this work <span class="hlt">pressure</span> <span class="hlt">drop</span> was investigated for an estimation of dynamic binding capacity (DBC) of proteins and plasmid DNA for monoliths with different pore sizes. It was demonstrated that methacrylate monolith surface area is reciprocally proportional to pore diameter and that <span class="hlt">pressure</span> <span class="hlt">drop</span> on monolith is reciprocally proportional to square pore size demonstrating that methacrylate monolith microstructure is preserved by changing pore size. Based on these facts mathematical formalism has been derived predicting that DBC is in linear correlation with the square root of <span class="hlt">pressure</span> <span class="hlt">drop</span>. This was experimentally confirmed for ion-exchange and hydrophobic interactions for proteins and plasmid DNA. Furthermore, <span class="hlt">pressure</span> <span class="hlt">drop</span> was also applied for an estimation of DBC in grafted layers of different thicknesses as estimated from the <span class="hlt">pressure</span> <span class="hlt">drop</span> data. It was demonstrated that the capacity is proportional to the estimated grafted layer thickness. Copyright © 2012 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT...tmp..107K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT...tmp..107K"><span>Selective laser melting in heat exchanger development - experimental investigation of heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristics of wavy fins</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kuehndel, J.; Kerler, B.; Karcher, C.</p> <p>2018-04-01</p> <p>To improve performance of heat exchangers for vehicle applications, it is necessary to increase the <span class="hlt">air</span> side heat transfer. Selective laser melting gives rise to be applied for fin development due to: i) independency of conventional tooling ii) a fast way to conduct essential experimental studies iii) high dimensional accuracy iv) degrees of freedom in design. Therefore, heat exchanger elements with wavy fins were examined in an experimental study. Experiments were conducted for <span class="hlt">air</span> side Reynolds number range of 1400-7400, varying wavy amplitude and wave length of the fins at a constant water flow rate of 9.0 m3/h. Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristics were evaluated with Nusselt Number Nu and Darcy friction factor ψ as functions of Reynolds number. Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> correlations were derived from measurement data obtained by regression analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20020060500','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20020060500"><span>Effect of External <span class="hlt">Pressure</span> <span class="hlt">Drop</span> on Loop Heat Pipe Operating Temperature</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jentung, Ku; Ottenstein, Laura; Rogers, Paul; Cheung, Kwok; Obenschain, Arthur F. (Technical Monitor)</p> <p>2002-01-01</p> <p>This paper discusses the effect of the <span class="hlt">pressure</span> <span class="hlt">drop</span> on the operating temperature in a loop heat pipe (LHP). Because the evaporator and the compensation chamber (CC) both contain two-phase fluid, a thermodynamic constraint exists between the temperature difference and the <span class="hlt">pressure</span> <span class="hlt">drop</span> for these two components. As the <span class="hlt">pressure</span> <span class="hlt">drop</span> increases, so will the temperature difference. The temperature difference in turn causes an increase of the heat leak from the evaporator to the CC, resulting in a higher CC temperature. Furthermore, the heat leak strongly depends on the vapor void fraction inside the evaporator core. Tests were conducted by installing a valve on the vapor line so as to vary the <span class="hlt">pressure</span> <span class="hlt">drop</span>, and by charging the LHP with various amounts of fluid. Test results verify that the LHP operating temperature increases with an increasing differential <span class="hlt">pressure</span>, and the temperature increase is a strong function of the fluid inventory in the loop.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19870046666&hterms=different+body+size&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Ddifferent%2Bbody%2Bsize','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870046666&hterms=different+body+size&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Ddifferent%2Bbody%2Bsize"><span><span class="hlt">Drop</span> size distribution and <span class="hlt">air</span> velocity measurements in <span class="hlt">air</span> assist swirl atomizer sprays</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mao, C.-P.; Oechsle, V.; Chigier, N.</p> <p>1987-01-01</p> <p>Detailed measurements of mean <span class="hlt">drop</span> size (SMD) and size distribution parameters have been made using a Fraunhofer diffraction particle sizing instrument in a series of sprays generated by an <span class="hlt">air</span> assist swirl atomizer. Thirty-six different combinations of fuel and <span class="hlt">air</span> mass flow rates were examined with liquid flow rates up to 14 lbm/hr and atomizing <span class="hlt">air</span> flow rates up to 10 lbm/hr. Linear relationships were found between SMD and liquid to <span class="hlt">air</span> mass flow rate ratios. SMD increased with distance downstream along the center line and also with radial distance from the axis. Increase in obscuration with distance downstream was due to an increase in number density of particles as the result of deceleration of <span class="hlt">drops</span> and an increase in the exposed path length of the laser beam. Velocity components of the atomizing <span class="hlt">air</span> flow field measured by a laser anemometer show swirling jet <span class="hlt">air</span> flow fields with solid body rotation in the core and free vortex flow in the outer regions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170008803','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170008803"><span>International Space Station (ISS) Bacterial Filter Elements (BFEs): Filter Efficiency and <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Testing of Returned Units</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Green, Robert D.; Agui, Juan H.; Vijayakumar, R.; Berger, Gordon M.; Perry, Jay L.</p> <p>2017-01-01</p> <p>The <span class="hlt">air</span> quality control equipment aboard the International Space Station (ISS) and future deep space exploration vehicles provide the vital function of maintaining a clean cabin environment for the crew and the hardware. This becomes a serious challenge in <span class="hlt">pressurized</span> space compartments since no outside <span class="hlt">air</span> ventilation is possible, and a larger particulate load is imposed on the filtration system due to lack of sedimentation. The ISS Environmental Control and Life Support (ECLS) system architecture in the U.S. Segment uses a distributed particulate filtration approach consisting of traditional High-Efficiency Particulate <span class="hlt">Air</span> (HEPA) filters deployed at multiple locations in each U.S. Seg-ment module; these filters are referred to as Bacterial Filter Elements, or BFEs. In our previous work, we presented results of efficiency and <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements for a sample set of two returned BFEs with a service life of 2.5 years. In this follow-on work, we present similar efficiency, <span class="hlt">pressure</span> <span class="hlt">drop</span>, and leak tests results for a larger sample set of six returned BFEs. The results of this work can aid the ISS Program in managing BFE logistics inventory through the stations planned lifetime as well as provide insight for managing filter element logistics for future exploration missions. These results also can provide meaningful guidance for particulate filter designs under consideration for future deep space exploration missions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT...tmp..125H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT...tmp..125H"><span>Two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in a helical coil flow boiling system</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hardik, B. K.; Prabhu, S. V.</p> <p>2018-05-01</p> <p>The objective of the present work is to study the two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in helical coils. Literature on the two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in a helical coil suggests the complexity in flow boiling inside a helical coil due to secondary flow. Most of correlations reported in the literature on the two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in a helical coil are limited to a specific operating range. No general correlation is available for a helical coil which is applicable for all fluids. In the present study, an experimental databank collected containing a total of 832 data points includes the data from the present study and from the literature. The data includes diabatic <span class="hlt">pressure</span> <span class="hlt">drop</span> of two fluids namely water and R123. Data covers a range of parameters namely a mass flux of 120-2058 kg/m2 s, a heat flux of 18-2831 kW/m2, an exit quality of 0.03-1, a density ratio of 32-1404 and a coil to tube diameter ratio of 14-58. The databank is compared with eighteen empirical correlations which include well referred correlations of straight tubes and the available correlations of helical coils. The straight tube correlations are not working well for the present data set. The helical coil correlations work reasonably well for the present databank. A correlation is suggested to predict the two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in helical coils. The present study suggests that the influence of a helical coil is completely included in the single phase <span class="hlt">pressure</span> <span class="hlt">drop</span> correlation for helical coils.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1994PhFl....6.3554L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1994PhFl....6.3554L"><span>Static shape of an acoustically levitated <span class="hlt">drop</span> with wave-<span class="hlt">drop</span> interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lee, C. P.; Anilkumar, A. V.; Wang, T. G.</p> <p>1994-11-01</p> <p>The static shape of a <span class="hlt">drop</span> levitated and flattened by an acoustic standing wave field in <span class="hlt">air</span> is calculated, requiring self-consistency between the <span class="hlt">drop</span> shape and the wave. The wave is calculated for a given shape using the boundary integral method. From the resulting radiation stress on the <span class="hlt">drop</span> surface, the shape is determined by solving the Young-Laplace equation, completing an iteration cycle. The iteration is continued until both the shape and the wave converge. Of particular interest are the shapes of large <span class="hlt">drops</span> that sustain equilibrium, beyond a certain degree of flattening, by becoming more flattened at a decreasing sound <span class="hlt">pressure</span> level. The predictions for flattening versus acoustic radiation stress, for <span class="hlt">drops</span> of different sizes, compare favorably with experimental data.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_1");'>1</a></li> <li><a href="#" onclick='return showDiv("page_2");'>2</a></li> <li class="active"><span>3</span></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_3 --> <div id="page_4" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_2");'>2</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li class="active"><span>4</span></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="61"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HMT...tmp...66F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HMT...tmp...66F"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of condensation of hydrocarbons in tubes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fries, Simon; Skusa, Severin; Luke, Andrea</p> <p>2018-03-01</p> <p>The heat transfer coefficient and <span class="hlt">pressure</span> <span class="hlt">drop</span> are investigated for propane. Two different mild steel plain tubes and saturation <span class="hlt">pressures</span> are considered for varying mass flux and vapour quality. The <span class="hlt">pressure</span> <span class="hlt">drop</span> is compared to the Friedel-Correlation with two different approaches to determine the friction factor. The first is calculation as proposed by Friedel and the second is through single phase <span class="hlt">pressure</span> <span class="hlt">drop</span> investigations. For lower vapour qualities the experimental results are in better agreement with the approach of the calculated friction factor. For higher vapour qualities the experimental friction factor is more precise. The <span class="hlt">pressure</span> <span class="hlt">drop</span> increases for a decreasing tube diameter and saturation <span class="hlt">pressure</span>. The circumferential temperature profile and heat transfer coefficients are shown for a constant vapour quality at varying mass fluxes. The subcooling is highest for the bottom of the tube and lowest for the top. The average subcooling as well as the circumferential deviation decreases for rising mass fluxes. The averaged heat transfer coefficients are compared to the model proposed by Thome and Cavallini. The experimental results are in good agreement with both correlations, however the trend is better described with the correlation from Thome. The experimental heat transfer coefficients are under predicted by Thome and over predicted by Cavallini.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018E%26ES..108e2113L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018E%26ES..108e2113L"><span>Correction of <span class="hlt">Pressure</span> <span class="hlt">Drop</span> in Steam and Water System in Performance Test of Boiler</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Jinglong; Zhao, Xianqiao; Hou, Fanjun; Wu, Xiaowu; Wang, Feng; Hu, Zhihong; Yang, Xinsen</p> <p>2018-01-01</p> <p>Steam and water <span class="hlt">pressure</span> <span class="hlt">drop</span> is one of the most important characteristics in the boiler performance test. As the measuring points are not in the guaranteed position and the test condition fluctuation exsits, the <span class="hlt">pressure</span> <span class="hlt">drop</span> test of steam and water system has the deviation of measuring point position and the deviation of test running parameter. In order to get accurate <span class="hlt">pressure</span> <span class="hlt">drop</span> of steam and water system, the corresponding correction should be carried out. This paper introduces the correction method of steam and water <span class="hlt">pressure</span> <span class="hlt">drop</span> in boiler performance test.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18074287','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18074287"><span>Effects of <span class="hlt">pressure</span> <span class="hlt">drop</span> and superficial velocity on the bubbling fluidized bed incinerator.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wang, Feng-Jehng; Chen, Suming; Lei, Perng-Kwei; Wu, Chung-Hsing</p> <p>2007-12-01</p> <p>Since performance and operational conditions, such as superficial velocity, <span class="hlt">pressure</span> <span class="hlt">drop</span>, particles viodage, and terminal velocity, are difficult to measure on an incinerator, this study used computational fluid dynamics (CFD) to determine numerical solutions. The effects of <span class="hlt">pressure</span> <span class="hlt">drop</span> and superficial velocity on a bubbling fluidized bed incinerator (BFBI) were evaluated. Analytical results indicated that simulation models were able to effectively predict the relationship between superficial velocity and <span class="hlt">pressure</span> <span class="hlt">drop</span> over bed height in the BFBI. Second, the models in BFBI were simplified to simulate scale-up beds without excessive computation time. Moreover, simulation and experimental results showed that minimum fluidization velocity of the BFBI must be controlled in at 0.188-3.684 m/s and <span class="hlt">pressure</span> <span class="hlt">drop</span> was mainly caused by bed particles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000057062','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000057062"><span>Validation of an All-<span class="hlt">Pressure</span> Fluid <span class="hlt">Drop</span> Model: Heptane Fluid <span class="hlt">Drops</span> in Nitrogen</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Harstad, K.; Bellan, J.; Bulzan, Daniel L. (Technical Monitor)</p> <p>2000-01-01</p> <p>Despite the fact that supercritical fluids occur both in nature and in industrial situations, the fundamentals of their behavior is poorly understood because supercritical fluids combine the characteristics of both liquids and gases, and therefore their behavior is not intuitive. There are several specific reasons for the lack of understanding: First, data from (mostly optical) measurements can be very misleading because regions of high density thus observed are frequently identified with liquids. A common misconception is that if in an experiment one can optically identify "<span class="hlt">drops</span>" and "ligaments", the observed fluid must be in a liquid state. This inference is incorrect because in fact optical measurements detect any large change (i.e. gradients) in density. Thus, the density ratio may be well below Omicron(10(exp 3)) that characterizes its liquid/gas value, but the measurement will still identify a change in the index of refraction providing that the change is sudden (steep gradients). As shown by simulations of supercritical fluids, under certain conditions the density gradients may remain large during the supercritical binary fluids mixing, thus making them optically identifiable. Therefore, there is no inconsistency between the optical observation of high density regions and the fluids being in a supercritical state. A second misconception is that because a fluid has a liquid-like density, it is appropriate to model it as a liquid. However, such fluids may have liquid-like densities while their transport properties differ from those of a liquid. Considering that the critical <span class="hlt">pressure</span> of most fuel hydrocarbons used in Diesel and gas turbine engines is in the range of 1.5 - 3 MPa, and the fact that the maximum <span class="hlt">pressure</span> attained in these engines is about 6 Mps, it is clear that the fuel in the combustion chamber will experience both subcritical and supercritical conditions. Studies of <span class="hlt">drop</span> behavior over a wide range of <span class="hlt">pressures</span> were performed in the past</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/21137948-experimental-investigation-ice-slurry-flow-pressure-drop-horizontal-tubes','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/21137948-experimental-investigation-ice-slurry-flow-pressure-drop-horizontal-tubes"><span>Experimental investigation of ice slurry flow <span class="hlt">pressure</span> <span class="hlt">drop</span> in horizontal tubes</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Grozdek, Marino; Khodabandeh, Rahmatollah; Lundqvist, Per</p> <p>2009-01-15</p> <p><span class="hlt">Pressure</span> <span class="hlt">drop</span> behaviour of ice slurry based on ethanol-water mixture in circular horizontal tubes has been experimentally investigated. The secondary fluid was prepared by mixing ethyl alcohol and water to obtain initial alcohol concentration of 10.3% (initial freezing temperature -4.4 C). The <span class="hlt">pressure</span> <span class="hlt">drop</span> tests were conducted to cover laminar and slightly turbulent flow with ice mass fraction varying from 0% to 30% depending on test conditions. Results from flow tests reveal much higher <span class="hlt">pressure</span> <span class="hlt">drop</span> for higher ice concentrations and higher velocities in comparison to the single phase flow. However for ice concentrations of 15% and higher, certain velocitymore » exists at which ice slurry <span class="hlt">pressure</span> <span class="hlt">drop</span> is same or even lower than for single phase flow. It seems that higher ice concentration delay flow pattern transition moment (from laminar to turbulent) toward higher velocities. In addition experimental results for <span class="hlt">pressure</span> <span class="hlt">drop</span> were compared to the analytical results, based on Poiseulle and Buckingham-Reiner models for laminar flow, Blasius, Darby and Melson, Dodge and Metzner, Steffe and Tomita for turbulent region and general correlation of Kitanovski which is valid for both flow regimes. For laminar flow and low buoyancy numbers Buckingham-Reiner method gives good agreement with experimental results while for turbulent flow best fit is provided with Dodge-Metzner and Tomita methods. Furthermore, for transport purposes it has been shown that ice mass fraction of 20% offers best ratio of ice slurry transport capability and required pumping power. (author)« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/4818266-comparison-pressure-drop-produced-spiral-wraps-cookie-cutters-other-rod-bundle-spacers','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/4818266-comparison-pressure-drop-produced-spiral-wraps-cookie-cutters-other-rod-bundle-spacers"><span>COMPARISON OF <span class="hlt">PRESSURE</span> <span class="hlt">DROP</span> PRODUCED BY SPIRAL WRAPS, COOKIE CUTTERS AND OTHER ROD BUNDLE SPACERS</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Noyes, R.C.</p> <p></p> <p>The problem of predicting <span class="hlt">pressure</span> <span class="hlt">drop</span> due to various fuel bundle spacers is considered in some detail. Three sets of experimental data are reviewed and presented in reduced form. These data are compared to several semitheoretical approaches to <span class="hlt">pressure</span> <span class="hlt">drop</span> prediction and a best method is selected to make the required predictions. The comparison between predictions for the ASCR spiral wrap spacer and cookie cutter spacer shows that both types of spacers produce about the same <span class="hlt">pressure</span> <span class="hlt">drop</span>. Spacer <span class="hlt">pressure</span> <span class="hlt">drop</span> is shown to be strongly dependent on spacer frontal area and pitch. (auth)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvF...3e3601V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvF...3e3601V"><span>Boiling regimes of impacting <span class="hlt">drops</span> on a heated substrate under reduced <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>van Limbeek, Michiel A. J.; Hoefnagels, Paul B. J.; Shirota, Minori; Sun, Chao; Lohse, Detlef</p> <p>2018-05-01</p> <p>We experimentally investigate the boiling behavior of impacting ethanol <span class="hlt">drops</span> on a heated smooth sapphire substrate at <span class="hlt">pressures</span> ranging from P =0.13 bar to atmospheric <span class="hlt">pressure</span>. We employ frustrated total internal reflection imaging to study the wetting dynamics of the contact between the <span class="hlt">drop</span> and the substrate. The spreading <span class="hlt">drop</span> can be in full contact (contact boiling), it can partially touch (transition boiling), or the <span class="hlt">drop</span> can be fully levitated (Leidenfrost boiling). We show that the temperature of the boundary between contact and transition boiling shows at most a weak dependence on the impact velocity, but a significant decrease with decreasing ambient gas <span class="hlt">pressure</span>. A striking correspondence is found between the temperature of this boundary and the static Leidenfrost temperature for all <span class="hlt">pressures</span>. We therefore conclude that both phenomena share the same mechanism and are dominated by the dynamics taking place at the contact line. On the other hand, the boundary between transition boiling and Leidenfrost boiling, i.e., the dynamic Leidenfrost temperature, increases for increasing impact velocity for all ambient gas <span class="hlt">pressures</span>. Moreover, the dynamic Leidenfrost temperature coincides for <span class="hlt">pressures</span> between P =0.13 and 0.54 bar, whereas for atmospheric <span class="hlt">pressure</span> the dynamic Leidenfrost temperature is slightly elevated. This indicates that the dynamic Leidenfrost temperature is at most weakly dependent on the enhanced evaporation by the lower saturation temperature of the liquid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28499454','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28499454"><span>Risk for intracranial <span class="hlt">pressure</span> increase related to enclosed <span class="hlt">air</span> in post-craniotomy patients during <span class="hlt">air</span> ambulance transport: a retrospective cohort study with simulation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Brändström, Helge; Sundelin, Anna; Hoseason, Daniela; Sundström, Nina; Birgander, Richard; Johansson, Göran; Winsö, Ola; Koskinen, Lars-Owe; Haney, Michael</p> <p>2017-05-12</p> <p>Post-craniotomy intracranial <span class="hlt">air</span> can be present in patients scheduled for <span class="hlt">air</span> ambulance transport to their home hospital. We aimed to assess risk for in-flight intracranial <span class="hlt">pressure</span> (ICP) increases related to observed intracranial <span class="hlt">air</span> volumes, hypothetical sea level pre-transport ICP, and different potential flight levels and cabin <span class="hlt">pressures</span>. A cohort of consecutive subdural hematoma evacuation patients from one University Medical Centre was assessed with post-operative intracranial <span class="hlt">air</span> volume measurements by computed tomography. Intracranial <span class="hlt">pressure</span> changes related to estimated intracranial <span class="hlt">air</span> volume effects of changing atmospheric <span class="hlt">pressure</span> (simulating flight and cabin <span class="hlt">pressure</span> changes up to 8000 ft) were simulated using an established model for intracranial <span class="hlt">pressure</span> and volume relations. Approximately one third of the cohort had post-operative intracranial <span class="hlt">air</span>. Of these, approximately one third had intracranial <span class="hlt">air</span> volumes less than 11 ml. The simulation estimated that the expected changes in intracranial <span class="hlt">pressure</span> during 'flight' would not result in intracranial hypertension. For intracranial <span class="hlt">air</span> volumes above 11 ml, the simulation suggested that it was possible that intracranial hypertension could develop 'inflight' related to cabin <span class="hlt">pressure</span> <span class="hlt">drop</span>. Depending on the pre-flight intracranial <span class="hlt">pressure</span> and <span class="hlt">air</span> volume, this could occur quite early during the assent phase in the flight profile. DISCUSSION: These findings support the idea that there should be radiographic verification of the presence or absence of intracranial <span class="hlt">air</span> after craniotomy for patients planned for long distance <span class="hlt">air</span> transport. Very small amounts of <span class="hlt">air</span> are clinically inconsequential. Otherwise, <span class="hlt">air</span> transport with maintained ground-level cabin <span class="hlt">pressure</span> should be a priority for these patients.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820015566','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820015566"><span>Resonances, radiation <span class="hlt">pressure</span> and optical scattering phenomena of <span class="hlt">drops</span> and bubbles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Marston, P. L.; Goosby, S. G.; Langley, D. S.; Loporto-Arione, S. E.</p> <p>1982-01-01</p> <p>Acoustic levitation and the response of fluid spheres to spherical harmonic projections of the radiation <span class="hlt">pressure</span> are described. Simplified discussions of the projections are given. A relationship between the tangential radiation stress and the Konstantinov effect is introduced and fundamental streaming patterns for <span class="hlt">drops</span> are predicted. Experiments on the forced shape oscillation of <span class="hlt">drops</span> are described and photographs of <span class="hlt">drop</span> fission are displayed. Photographs of critical angle and glory scattering by bubbles and rainbow scattering by <span class="hlt">drops</span> are displayed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1030245-fibrous-filter-efficiency-pressure-drop-viscous-inertial-transition-flow-regime','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1030245-fibrous-filter-efficiency-pressure-drop-viscous-inertial-transition-flow-regime"><span>Fibrous filter efficiency and <span class="hlt">pressure</span> <span class="hlt">drop</span> in the viscous-inertial transition flow regime.</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sanchez, Andres L.; Brockmann, John E.; Dellinger, Jennifer Gwynne</p> <p>2011-10-01</p> <p>Fibrous filter <span class="hlt">pressure</span> <span class="hlt">drop</span> and aerosol collection efficiency were measured at low <span class="hlt">air</span> <span class="hlt">pressures</span> (0.2 to 0.8 atm) and high face velocities (5 to 20 meters per second) to give fiber Reynolds numbers in the viscous-inertial transition flow regime (1 to 16). In this regime, contemporary filtration theory based on Kuwabara's viscous flow through an ensemble of fibers under-predicts single fiber impaction by several orders of magnitude. Streamline curvature increases substantially as inertial forces become dominant. Dimensionless <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements followed the viscous-inertial theory of Robinson and Franklin rather than Darcy's linear <span class="hlt">pressure</span>-velocity relationship (1972). Sodium chloride and iron nano-agglomeratemore » test aerosols were used to evaluate the effects of particle density and shape factor. Total filter efficiency collapsed when plotted against the particle Stokes and fiber Reynolds numbers. Efficiencies were then fitted with an impactor type equation where the cutpoint Stokes number and a steepness parameter described data well in the sharply increasing portion of the curve (20% to 80% efficiency). The cutpoint Stokes number was a linearly decreasing function of fiber Reynolds number. Single fiber efficiencies were calculated from total filter efficiencies and compared to contemporary viscous flow impaction theory (Stechkina et al. 1969), and numerical simulations from the literature. Existing theories under-predicted measured single fiber efficiencies although the assumption of uniform flow conditions for each successive layer of fibers is questionable; the common exponential relationship between single fiber efficiency and total filter efficiency may not be appropriate in this regime.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012ArTh...33...47E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012ArTh...33...47E"><span>Experimental investigation of the two-phase flow regimes and <span class="hlt">pressure</span> <span class="hlt">drop</span> in horizontal mini-size rectangular test section</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Elazhary, Amr Mohamed; Soliman, Hassan M.</p> <p>2012-10-01</p> <p>An experimental study was conducted in order to investigate two-phase flow regimes and fully developed <span class="hlt">pressure</span> <span class="hlt">drop</span> in a mini-size, horizontal rectangular channel. The test section was machined in the form of an impacting tee junction in an acrylic block (in order to facilitate visualization) with a rectangular cross-section of 1.87-mm height on 20-mm width on the inlet and outlet sides. <span class="hlt">Pressure</span> <span class="hlt">drop</span> measurement and flow regime identification were performed on all three sides of the junction. <span class="hlt">Air</span>-water mixtures at 200 kPa (abs) and room temperature were used as the test fluids. Four flow regimes were identified visually: bubbly, plug, churn, and annular over the ranges of gas and liquid superficial velocities of 0.04 ≤ JG ≤ 10 m/s and 0.02 ≤ JL ≤ 0.7 m/s, respectively, and a flow regime map was developed. Accuracy of the <span class="hlt">pressure</span>-measurement technique was validated with single-phase, laminar and turbulent, fully developed data. Two-phase experiments were conducted for eight different inlet conditions and various mass splits at the junction. Comparisons were conducted between the present data and former correlations for the fully developed two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> in rectangular channels with similar sizes. Wide deviations were found among these correlations, and the correlations that agreed best with the present data were identified.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993AIPC..271..981W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993AIPC..271..981W"><span>An investigation of two phase flow <span class="hlt">pressure</span> <span class="hlt">drops</span> in a reduced acceleration environment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wheeler, Montgomery W.; Best, Frederick R.; Reinarts, Thomas R.</p> <p>1993-01-01</p> <p>Thermal systems for space applications based on two phase flow have several advantages over single phase systems. Two phase thermal energy management and dynamic power conversion system advantages include the capability of achieving high specific power levels. Before two phase systems for space applications can be designed effectively, knowledge of the flow behavior in a reduced acceleration environment is necessary. To meet these needs, two phase flow experiments were conducted aboard the National Aeronautic and Space Administration's KC-135 using R12 as the working fluid. Annular flow two phase <span class="hlt">pressure</span> <span class="hlt">drops</span> were measured through 10.41-mm ID 1.251-m long glass tubing during periods with acceleration levels in the range ±0.05 G. The experiments were conducted with emphasis on achieving data with a high level of accuracy. The reduced acceleration annular flow <span class="hlt">pressure</span> <span class="hlt">drops</span> were compred with <span class="hlt">pressure</span> <span class="hlt">drops</span> measured in a 1-G environment for similar flow conditions. The reduced acceleration <span class="hlt">pressure</span> <span class="hlt">drops</span> were found to be 45% greater than the 1-G <span class="hlt">pressure</span> <span class="hlt">drops</span>. In addition, the reduced acceleration annular flow interfacial friction factors were compared with models for vertical up-flow in a 1-G environment. The reduced acceleration interfacial friction factor data was not predicted by the 1-G models.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17030418','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17030418"><span>Predicting <span class="hlt">pressure</span> <span class="hlt">drop</span> in venturi scrubbers with artificial neural networks.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nasseh, S; Mohebbi, A; Jeirani, Z; Sarrafi, A</p> <p>2007-05-08</p> <p>In this study a new approach based on artificial neural networks (ANNs) has been used to predict <span class="hlt">pressure</span> <span class="hlt">drop</span> in venturi scrubbers. The main parameters affecting the <span class="hlt">pressure</span> <span class="hlt">drop</span> are mainly the gas velocity in the throat of venturi scrubber (V(g)(th)), liquid to gas flow rate ratio (L/G), and axial distance of the venturi scrubber (z). Three sets of experimental data from five different venturi scrubbers have been applied to design three independent ANNs. Comparing the results of these ANNs and the calculated results from available models shows that the results of ANNs have a better agreement with experimental data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29193159','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29193159"><span>Investigation of the quality of stored red blood cells after simulated <span class="hlt">air</span> <span class="hlt">drop</span> in the maritime environment.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Meli, Athinoula; Hancock, Vicky; Doughty, Heidi; Smedley, Steve; Cardigan, Rebecca; Wiltshire, Michael</p> <p>2018-02-01</p> <p>Maritime medical capability may be compromised by blood resupply. <span class="hlt">Air-dropped</span> red blood cells (RBCs) is a possible mitigation factor. This study set out to evaluate RBC storage variables after a simulated parachute <span class="hlt">air</span> <span class="hlt">drop</span> into the sea, as limited data exist. The <span class="hlt">air</span> load construction for the <span class="hlt">air</span> <span class="hlt">drop</span> of blood was subject to static <span class="hlt">drop</span> assessment to simulate a worst-case parachute <span class="hlt">drop</span> scenario. One control and two test Golden Hour shipping containers were each packaged with 10 RBC units. The control box was not <span class="hlt">dropped</span>; Test Boxes 1 and 2 were further reinforced with waterproof boxes and underwent a simulated <span class="hlt">air</span> <span class="hlt">drop</span> on Day 7 or Day 8 postdonation, respectively. One day after the <span class="hlt">drop</span> and once a week thereafter until Day 43 of storage, RBCs from each box were sampled and tested for full blood counts, hemolysis, adenosine triphosphate, 2,3-diphosphoglycerate, pH, extracellular potassium, glucose, lactate, deformability, and RBC microvesicles. The packaging configuration completed the <span class="hlt">air</span> <span class="hlt">drop</span> with no water ingress or physical damage. All units met UK specifications for volume, hemoglobin, and hemolysis. There were no significant differences for any of the variables studied between RBCs in the control box compared to RBCs in Test Boxes 1 and 2 combined over storage. The test proved that the packaging solution and the impact of a maritime <span class="hlt">air</span> <span class="hlt">drop</span> as performed in this study, on Day 7 or Day 8 postdonation, did not affect the in vitro quality of RBCs in SAGM over storage for 35 days. © 2017 AABB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010PhLA..374.2301S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010PhLA..374.2301S"><span>Parametric resonance in acoustically levitated water <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shen, C. L.; Xie, W. J.; Wei, B.</p> <p>2010-05-01</p> <p>Liquid <span class="hlt">drops</span> can be suspended in <span class="hlt">air</span> with acoustic levitation method. When the sound <span class="hlt">pressure</span> is periodically modulated, the levitated <span class="hlt">drop</span> is usually forced into an axisymmetric oscillation. However, a transition from axisymmetric oscillation into sectorial oscillation occurs when the modulation frequency approaches some specific values. The frequency of the sectorial oscillation is almost exactly half of the modulation frequency. It is demonstrated that this transition is induced by the parametric resonance of levitated <span class="hlt">drop</span>. The natural frequency of sectorial oscillation is found to decrease with the increase of <span class="hlt">drop</span> distortion extent.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1295510-negative-pressures-spallation-water-drops-subjected-nanosecond-shock-waves','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1295510-negative-pressures-spallation-water-drops-subjected-nanosecond-shock-waves"><span>Negative <span class="hlt">pressures</span> and spallation in water <span class="hlt">drops</span> subjected to nanosecond shock waves</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Stan, Claudiu A.; Willmott, Philip R.; Stone, Howard A.; ...</p> <p>2016-05-16</p> <p>Most experimental studies of cavitation in liquid water at negative <span class="hlt">pressures</span> reported cavitation at tensions significantly smaller than those expected for homogeneous nucleation, suggesting that achievable tensions are limited by heterogeneous cavitation. We generated tension pulses with nanosecond rise times in water by reflecting cylindrical shock waves, produced by X-ray laser pulses, at the internal surface of <span class="hlt">drops</span> of water. Depending on the X-ray pulse energy, a range of cavitation phenomena occurred, including the rupture and detachment, or spallation, of thin liquid layers at the surface of the <span class="hlt">drop</span>. When spallation occurred, we evaluated that negative <span class="hlt">pressures</span> below –100 MPamore » were reached in the <span class="hlt">drops</span>. As a result, we model the negative <span class="hlt">pressures</span> from shock reflection experiments using a nucleation-and-growth model that explains how rapid decompression could outrun heterogeneous cavitation in water, and enable the study of stretched water close to homogeneous cavitation <span class="hlt">pressures</span>.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..278a2128K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..278a2128K"><span>Study of nitrogen two-phase flow <span class="hlt">pressure</span> <span class="hlt">drop</span> in horizontal and vertical orientation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Koettig, T.; Kirsch, H.; Santandrea, D.; Bremer, J.</p> <p>2017-12-01</p> <p>The large-scale liquid argon Short Baseline Neutrino Far-detector located at Fermilab is designed to detect neutrinos allowing research in the field of neutrino oscillations. It will be filled with liquid argon and operate at almost ambient <span class="hlt">pressure</span>. Consequently, its operation temperature is determined at about 87 K. The detector will be surrounded by a thermal shield, which is actively cooled with boiling nitrogen at a <span class="hlt">pressure</span> of about 2.8 bar absolute, the respective saturation <span class="hlt">pressure</span> of nitrogen. Due to strict temperature gradient constraints, it is important to study the two-phase flow <span class="hlt">pressure</span> <span class="hlt">drop</span> of nitrogen along the cooling circuit of the thermal shield in different orientations of the flow with respect to gravity. An experimental setup has been built in order to determine the two-phase flow <span class="hlt">pressure</span> <span class="hlt">drop</span> in nitrogen in horizontal, vertical upward and vertical downward direction. The measurements have been conducted under quasi-adiabatic conditions and at a saturation <span class="hlt">pressure</span> of 2.8 bar absolute. The mass velocity has been varied in the range of 20 kg·m-2·s-1 to 70 kg·m-2·s-1 and the <span class="hlt">pressure</span> <span class="hlt">drop</span> data has been recorded scanning the two-phase region from vapor qualities close to zero up to 0.7. The experimental data will be compared with several established predictions of <span class="hlt">pressure</span> <span class="hlt">drop</span> e.g. Mueller-Steinhagen and Heck by using the void fraction correlation of Rouhani.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24594638','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24594638"><span>Effect of flow rate and temperature on transmembrane blood <span class="hlt">pressure</span> <span class="hlt">drop</span> in an extracorporeal artificial lung.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Park, M; Costa, E L V; Maciel, A T; Barbosa, E V S; Hirota, A S; Schettino, G de P; Azevedo, L C P</p> <p>2014-11-01</p> <p>Transmembrane <span class="hlt">pressure</span> <span class="hlt">drop</span> reflects the resistance of an artificial lung system to blood transit. Decreased resistance (low transmembrane <span class="hlt">pressure</span> <span class="hlt">drop</span>) enhances blood flow through the oxygenator, thereby, enhancing gas exchange efficiency. This study is part of a previous one where we observed the behaviour and the modulation of blood <span class="hlt">pressure</span> <span class="hlt">drop</span> during the passage of blood through artificial lung membranes. Before and after the induction of multi-organ dysfunction, the animals were instrumented and analysed for venous-venous extracorporeal membrane oxygenation, using a pre-defined sequence of blood flows. Blood flow and revolutions per minute (RPM) of the centrifugal pump varied in a linear fashion. At a blood flow of 5.5 L/min, pre- and post-pump blood <span class="hlt">pressures</span> reached -120 and 450 mmHg, respectively. Transmembrane <span class="hlt">pressures</span> showed a significant spread, particularly at blood flows above 2 L/min; over the entire range of blood flow rates, there was a positive association of <span class="hlt">pressure</span> <span class="hlt">drop</span> with blood flow (0.005 mmHg/mL/minute of blood flow) and a negative association of <span class="hlt">pressure</span> <span class="hlt">drop</span> with temperature (-4.828 mmHg/(°Celsius). These associations were similar when blood flows of below and above 2000 mL/minute were examined. During its passage through the extracorporeal system, blood is exposed to <span class="hlt">pressure</span> variations from -120 to 450 mmHg. At high blood flows (above 2 L/min), the <span class="hlt">drop</span> in transmembrane <span class="hlt">pressure</span> becomes unpredictable and highly variable. Over the entire range of blood flows investigated (0-5500 mL/min), the <span class="hlt">drop</span> in transmembrane <span class="hlt">pressure</span> was positively associated with blood flow and negatively associated with body temperature. © The Author(s) 2014.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20090025293','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20090025293"><span>Altitude Cooling Investigation of the R-2800-21 Engine in the P-47G Airplane. IV - Engine Cooling-<span class="hlt">Air</span> <span class="hlt">Pressure</span> Distribution</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kaufman, Samuel J.; Staudt, Robert C.; Valerino, Michael F.</p> <p>1947-01-01</p> <p>A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane was made to determine the effect of the flight variables on the engine cooling-<span class="hlt">air</span> <span class="hlt">pressure</span> distribution. The investigation consisted of level flights at altitudes from 5000 to 35,000 feet for the normal range of engine and airplane operation. The data showed that the average engine front <span class="hlt">pressures</span> ranged from 0.73 to 0.82 of the impact <span class="hlt">pressure</span> (velocity head). The average engine rear <span class="hlt">pressures</span> ranged from 0.50 to 0.55 of the impact <span class="hlt">pressure</span> for closed cowl flaps and from 0.10 to 0.20 for full-open cowl flaps. In general, the highest front <span class="hlt">pressures</span> were obtained at the bottom of the engine. The rear <span class="hlt">pressures</span> for the rear-row cylinders were .lower and the <span class="hlt">pressure</span> <span class="hlt">drops</span> correspondingly higher than for the front-row cylinders. The rear-<span class="hlt">pressure</span> distribution was materially affected by cowl-flap position in that the differences between the rear <span class="hlt">pressures</span> of the front-row and rear-row cylinders markedly increased as the cowl flaps were opened. For full-open cowl flaps, the <span class="hlt">pressure</span> <span class="hlt">drops</span> across the rear-row cylinders were in the order of 0.2 of the impact <span class="hlt">pressure</span> greater than across the front-row cylinders. Propeller speed and altitude had little effect on the -coolingair <span class="hlt">pressure</span> distribution, Increase in angle of inclination of the thrust axis decreased the front ?<span class="hlt">pressures</span> for the cylinders at the top of the engine and increased them for the cylinders at the bottom of the engine. As more auxiliary <span class="hlt">air</span> was taken from the engine cowling, the front <span class="hlt">pressures</span> and, to a lesser extent, the rear <span class="hlt">pressures</span> for the cylinders at the bottom of the engine decreased. No correlation existed between the cooling-<span class="hlt">air</span> <span class="hlt">pressure-drop</span> distribution and the cylinder-temperature distribution.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014Cryo...64..260H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014Cryo...64..260H"><span>A steady state <span class="hlt">pressure</span> <span class="hlt">drop</span> model for screen channel liquid acquisition devices</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hartwig, J. W.; Darr, S. R.; McQuillen, J. B.; Rame, E.; Chato, D. J.</p> <p>2014-11-01</p> <p>This paper presents the derivation of a simplified one dimensional (1D) steady state <span class="hlt">pressure</span> <span class="hlt">drop</span> model for flow through a porous liquid acquisition device (LAD) inside a cryogenic propellant tank. Experimental data is also presented from cryogenic LAD tests in liquid hydrogen (LH2) and liquid oxygen (LOX) to compare against the simplified model and to validate the model at cryogenic temperatures. The purpose of the experiments was to identify the various <span class="hlt">pressure</span> <span class="hlt">drop</span> contributions in the analytical model which govern LAD channel behavior during dynamic, steady state outflow. LH2 pipe flow of LAD screen samples measured the second order flow-through-screen (FTS) <span class="hlt">pressure</span> <span class="hlt">drop</span>, horizontal LOX LAD outflow tests determined the relative magnitude of the third order frictional and dynamic losses within the channel, while LH2 inverted vertical outflow tests determined the magnitude of the first order hydrostatic <span class="hlt">pressure</span> loss and validity of the full 1D model. When compared to room temperature predictions, the FTS <span class="hlt">pressure</span> <span class="hlt">drop</span> is shown to be temperature dependent, with a significant increase in flow resistance at LH2 temperatures. Model predictions of frictional and dynamic losses down the channel compare qualitatively with LOX LADs data. Meanwhile, the 1D model predicted breakdown points track the trends in the LH2 inverted outflow experimental results, with discrepancies being due to a non-uniform injection velocity across the LAD screen not accounted for in the model.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_2");'>2</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li class="active"><span>4</span></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_4 --> <div id="page_5" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li class="active"><span>5</span></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="81"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFDH15009K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFDH15009K"><span>Effects of vascular structures on the <span class="hlt">pressure</span> <span class="hlt">drop</span> in stenotic coronary arteries</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Jaerim; Choi, Haecheon; Kweon, Jihoon; Kim, Young-Hak; Yang, Dong Hyun; Kim, Namkug</p> <p>2016-11-01</p> <p>A stenosis, which is a narrowing of a blood vessel, of the coronary arteries restricts the flow to the heart and it may lead to sudden cardiac death. Therefore, the accurate determination of the severity of a stenosis is a critical issue. Due to the convenience of visual assessments, geometric parameters such as the diameter stenosis and area stenosis have been used, but the decision based on them sometimes under- or overestimates the functional severity of a stenosis, i.e., <span class="hlt">pressure</span> <span class="hlt">drop</span>. In this study, patient-specific models that have similar area stenosis but different <span class="hlt">pressure</span> <span class="hlt">drops</span> are considered, and their geometries are reconstructed from the coronary computed tomography angiography (CCTA). Both steady and pulsatile inflows are considered for the simulations. Comparison between two models that have a bifurcation right after a stenosis shows that the parent to daughter vessel angle results in different secondary flow patterns and wall shear stress distributions which affect the <span class="hlt">pressure</span> downstream. Thus, the structural features of the lower and upper parts of a stenosis significantly affect the <span class="hlt">pressure</span> <span class="hlt">drop</span>. Supported by 20152020105600.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5397859','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5397859"><span>Estimating the irreversible <span class="hlt">pressure</span> <span class="hlt">drop</span> across a stenosis by quantifying turbulence production using 4D Flow MRI</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Ha, Hojin; Lantz, Jonas; Ziegler, Magnus; Casas, Belen; Karlsson, Matts; Dyverfeldt, Petter; Ebbers, Tino</p> <p>2017-01-01</p> <p>The <span class="hlt">pressure</span> <span class="hlt">drop</span> across a stenotic vessel is an important parameter in medicine, providing a commonly used and intuitive metric for evaluating the severity of the stenosis. However, non-invasive estimation of the <span class="hlt">pressure</span> <span class="hlt">drop</span> under pathological conditions has remained difficult. This study demonstrates a novel method to quantify the irreversible <span class="hlt">pressure</span> <span class="hlt">drop</span> across a stenosis using 4D Flow MRI by calculating the total turbulence production of the flow. Simulation MRI acquisitions showed that the energy lost to turbulence production can be accurately quantified with 4D Flow MRI within a range of practical spatial resolutions (1–3 mm; regression slope = 0.91, R2 = 0.96). The quantification of the turbulence production was not substantially influenced by the signal-to-noise ratio (SNR), resulting in less than 2% mean bias at SNR > 10. <span class="hlt">Pressure</span> <span class="hlt">drop</span> estimation based on turbulence production robustly predicted the irreversible <span class="hlt">pressure</span> <span class="hlt">drop</span>, regardless of the stenosis severity and post-stenosis dilatation (regression slope = 0.956, R2 = 0.96). In vitro validation of the technique in a 75% stenosis channel confirmed that <span class="hlt">pressure</span> <span class="hlt">drop</span> prediction based on the turbulence production agreed with the measured <span class="hlt">pressure</span> <span class="hlt">drop</span> (regression slope = 1.15, R2 = 0.999, Bland-Altman agreement = 0.75 ± 3.93 mmHg). PMID:28425452</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005JFM...545..203T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005JFM...545..203T"><span>The <span class="hlt">air</span> bubble entrapped under a <span class="hlt">drop</span> impacting on a solid surface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Thoroddsen, S. T.; Etoh, T. G.; Takehara, K.; Ootsuka, N.; Hatsuki, Y.</p> <p>2005-12-01</p> <p>We present experimental observations of the disk of <span class="hlt">air</span> caught under a <span class="hlt">drop</span> impacting onto a solid surface. By imaging the impact through an acrylic plate with an ultra-high-speed video camera, we can follow the evolution of the <span class="hlt">air</span> disk as it contracts into a bubble under the centre of the <span class="hlt">drop</span>. The initial size and contraction speed of the disk were measured for a range of impact Weber and Reynolds numbers. The size of the initial disk is related to the bottom curvature of the <span class="hlt">drop</span> at the initial contact, as measured in free-fall. The initial contact often leaves behind a ring of micro-bubbles, marking its location. The <span class="hlt">air</span> disk contracts at a speed comparable to the corresponding <span class="hlt">air</span> disks caught under a <span class="hlt">drop</span> impacting onto a liquid surface. This speed also seems independent of the wettability of the liquid, which only affects the azimuthal shape of the contact line. For some impact conditions, the dynamics of the contraction leaves a small droplet at the centre of the bubble. This arises from a capillary wave propagating from the edges of the contracting disk towards the centre. As the wave converges its amplitude grows until it touches the solid substrate, thereby pinching off the micro-droplet at the plate, in the centre of the bubble. The effect of increasing liquid viscosity is to slow down the contraction speed and to produce a more irregular contact line leaving more micro-bubbles along the initial ring.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011ExFl...51..731R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011ExFl...51..731R"><span>Experimental investigation into vortex structure and <span class="hlt">pressure</span> <span class="hlt">drop</span> across microcavities in 3D integrated electronics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Renfer, Adrian; Tiwari, Manish K.; Brunschwiler, Thomas; Michel, Bruno; Poulikakos, Dimos</p> <p>2011-09-01</p> <p>Hydrodynamics in microcavities with cylindrical micropin fin arrays simulating a single layer of a water-cooled electronic chip stack is investigated experimentally. Both inline and staggered pin arrangements are investigated using <span class="hlt">pressure</span> <span class="hlt">drop</span> and microparticle image velocimetry (μPIV) measurements. The <span class="hlt">pressure</span> <span class="hlt">drop</span> across the cavity shows a flow transition at pin diameter-based Reynolds numbers ( Re d ) ~200. Instantaneous μPIV, performed using a pH-controlled high seeding density of tracer microspheres, helps visualize vortex structure unreported till date in microscale geometries. The post-transition flow field shows vortex shedding and flow impingement onto the pins explaining the <span class="hlt">pressure</span> <span class="hlt">drop</span> increase. The flow fluctuations start at the chip outlet and shift upstream with increasing Re d . No fluctuations are observed for a cavity with pin height-to-diameter ratio h/ d = 1 up to Re d ~330; however, its <span class="hlt">pressure</span> <span class="hlt">drop</span> was higher than for a cavity with h/d = 2 due to pronounced influence of cavity walls.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29522889','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29522889"><span>Role of regression analysis and variation of rheological data in calculation of <span class="hlt">pressure</span> <span class="hlt">drop</span> for sludge pipelines.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Farno, E; Coventry, K; Slatter, P; Eshtiaghi, N</p> <p>2018-06-15</p> <p>Sludge pumps in wastewater treatment plants are often oversized due to uncertainty in calculation of <span class="hlt">pressure</span> <span class="hlt">drop</span>. This issue costs millions of dollars for industry to purchase and operate the oversized pumps. Besides costs, higher electricity consumption is associated with extra CO 2 emission which creates huge environmental impacts. Calculation of <span class="hlt">pressure</span> <span class="hlt">drop</span> via current pipe flow theory requires model estimation of flow curve data which depends on regression analysis and also varies with natural variation of rheological data. This study investigates impact of variation of rheological data and regression analysis on variation of <span class="hlt">pressure</span> <span class="hlt">drop</span> calculated via current pipe flow theories. Results compare the variation of calculated <span class="hlt">pressure</span> <span class="hlt">drop</span> between different models and regression methods and suggest on the suitability of each method. Copyright © 2018 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFMPP31A2258S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFMPP31A2258S"><span>Measuring Ancient <span class="hlt">Air</span> <span class="hlt">Pressure</span> Using Fossilized Cyanobacteria</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Silverman, S. N.; Som, S. M.; Gordon, R.; Bebout, B.</p> <p>2016-12-01</p> <p>The evolution of Earth's atmosphere has been governed by biological evolution. The dominant <span class="hlt">air</span> component, nitrogen, has undergone substantial variation over geological time. Today, the partial <span class="hlt">pressure</span> of nitrogen is 0.79 bar, but this value could have been much higher during early Earth1. The nitrogen partial <span class="hlt">pressure</span> is postulated to have <span class="hlt">dropped</span> to a maximum of 0.5 bar before the Great Oxidation Event 2.4 billion years ago, and subsequently recovered to the 0.8 bar value of our modern atmosphere over the next 330 million years2. We are placing constraints on the trajectory of this recovery by investigating how nitrogen partial <span class="hlt">pressure</span> influences the morphology of a certain species of filamentous cyanobacteria that has been found fossilized in 2 billion year old rocks. These filamentous cyanobacteria convert nitrogen from its dissolved gaseous state (N2) to a biologically useful state (i.e. NH3) when the latter is present at growth-limiting concentrations in their aquatic environment. Such cyanobacteria develop heterocysts (specialized, visually distinct cells), which fix the nitrogen and laterally distribute it to neighboring cells along the one-dimensional filament. We suggest that the distance between heterocysts reflects the nitrogen partial <span class="hlt">pressure</span> dissolved in water, which is related to atmospheric pN2 by Henry's law. In the laboratory, we are quantifying the relationship between heterocyst distance, variance and covariance to atmospheric pN2 by subjecting cyanobacteria (in media devoid of nitrate) to different partial <span class="hlt">pressures</span> of N2 at a constant temperature and lighting for the representative species Anabaena variabilis. As far as we know, such experiments have not been previously conducted. This new geobarometer will complement existing methods of quantifying ancient nitrogen partial <span class="hlt">pressure</span>. 1Goldblatt, Colin, et al. "Nitrogen-enhanced greenhouse warming on early Earth." Nature Geoscience 2 (2009): 891-896. 2Som, S., et al. "Earth's <span class="hlt">air</span> <span class="hlt">pressure</span> 2</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhFl...28e4102Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhFl...28e4102Z"><span>Influence of surfactant on the <span class="hlt">drop</span> bag breakup in a continuous <span class="hlt">air</span> jet stream</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhao, Hui; Zhang, Wen-Bin; Xu, Jian-Liang; Li, Wei-Feng; Liu, Hai-Feng</p> <p>2016-05-01</p> <p>The deformation and breakup of surfactant-laden <span class="hlt">drops</span> is a common phenomenon in nature and numerous practical applications. We investigate influence of surfactant on the <span class="hlt">drop</span> bag breakup in a continuous <span class="hlt">air</span> jet stream. The airflow would induce the advection diffusion of surfactant between interface and bulk of <span class="hlt">drop</span>. Experiments indicate that the convective motions of deforming <span class="hlt">drop</span> would induce the non-equilibrium distribution of surfactant, which leads to the change of surface tension. When the surfactant concentration is smaller than critical micelle concentration (CMC), with the increase of surface area of <span class="hlt">drop</span>, the surface tension of liquid-<span class="hlt">air</span> interface and the critical Weber number will increase. When the surfactant concentration is bigger than CMC, the micelle can be considered as the source term, which can supply the monomers. So in the presence of surfactant, there would be the significant nonlinear variation on the critical Weber number of bag breakup. We build the dynamic non-monotonic relationship between concentrations of surfactant and critical Weber number theoretically. In the range of parameters studied, the experimental results are consistent with the model estimates.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013PhDT.......140S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013PhDT.......140S"><span>The effect of passive mixing on <span class="hlt">pressure</span> <span class="hlt">drop</span> and oxygen mass fraction using opposing channel flow field design in a Proton Exchange Membrane Fuel Cell</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Singh, Anant Bir</p> <p></p> <p>This study investigates a flow field with opposing channel design. Previous studies on flow field designs have been focused on improving fuel utilization which often leads to increased <span class="hlt">pressure</span> <span class="hlt">drop</span>. This increased <span class="hlt">pressure</span> <span class="hlt">drop</span> is typical because standard designs employ either a single flow channel to clear blockages or dead end condition to force the flow through the gas diffusion layer. The disadvantage with these designs is the increased resistance to the flow which requires higher <span class="hlt">pressure</span>, which becomes a parasitic loss that lowers the system efficiency. For this study the focus was to reduce the <span class="hlt">pressure</span> <span class="hlt">drop</span> by providing a less resistive path to the flow. To achieve a less resistive path, the inlet channel was split into two opposing channels. These channels are then recombined only to be split again for the next leg. Therefore, the split channel design should reduce the <span class="hlt">pressure</span> <span class="hlt">drop</span> which reduces the parasitic load and ultimately contributes to higher system efficiency. In addition the recombining of the streams at each leg should induce mixing. Having opposing channels should also increase cross flow under the lands to reduce mass transfer loses. The cathode side of the fuel cell is especially sensitive to the mass transport losses since <span class="hlt">air</span> (oxygen mixed with nitrogen) is used for supplying oxygen unlike the anode side which uses pure hydrogen. To test the hypothesis of having benefits from an opposing channel design, both an experimental and analytical approach was taken. For the experiment, a serpentine flow field and opposing channel flow field plates were compared over several flow rates with compressed <span class="hlt">air</span>. To test the hypothesis of increased mass transfer, the two flow fields were modeled using a CFD software package, COMSOL. It was found that the opposing channel configuration for high flow rate with multiple entry and exit conditions exhibited significant improvement over the single serpentine channel. <span class="hlt">Pressure</span> <span class="hlt">drop</span> was ⅓ less than the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080006635','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080006635"><span>Heat Transfer and <span class="hlt">Pressure</span> <span class="hlt">Drop</span> in Concentric Annular Flows of Binary Inert Gas Mixtures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Reid, R. S.; Martin, J. J.; Yocum, D. J.; Stewart, E. T.</p> <p>2007-01-01</p> <p>Studies of heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of binary inert gas mixtures flowing through smooth concentric circular annuli, tubes with fully developed velocity profiles, and constant heating rate are described. There is a general lack of agreement among the constant property heat transfer correlations for such mixtures. No inert gas mixture data exist for annular channels. The intent of this study was to develop highly accurate and benchmarked <span class="hlt">pressure</span> <span class="hlt">drop</span> and heat transfer correlations that can be used to size heat exchangers and cores for direct gas Brayton nuclear power plants. The inside surface of the annular channel is heated while the outer surface of the channel is insulated. Annulus ratios range 0.5 < r* < 0.83. These smooth tube data may serve as a reference to the heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> performance in annuli, tubes, and channels having helixes or spacer ribs, or other surfaces.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AIPC.1737d0007N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AIPC.1737d0007N"><span>Effect of superficial velocity on vaporization <span class="hlt">pressure</span> <span class="hlt">drop</span> with propane in horizontal circular tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Novianto, S.; Pamitran, A. S.; Nasruddin, Alhamid, M. I.</p> <p>2016-06-01</p> <p>Due to its friendly effect on the environment, natural refrigerants could be the best alternative refrigerant to replace conventional refrigerants. The present study was devoted to the effect of superficial velocity on vaporization <span class="hlt">pressure</span> <span class="hlt">drop</span> with propane in a horizontal circular tube with an inner diameter of 7.6 mm. The experiments were conditioned with 4 to 10 °C for saturation temperature, 9 to 20 kW/m2 for heat flux, and 250 to 380 kg/m2s for mass flux. It is shown here that increased heat flux may result in increasing vapor superficial velocity, and then increasing <span class="hlt">pressure</span> <span class="hlt">drop</span>. The present experimental results were evaluated with some existing correlations of <span class="hlt">pressure</span> <span class="hlt">drop</span>. The best prediction was evaluated by Lockhart-Martinelli (1949) with MARD 25.7%. In order to observe the experimental flow pattern, the present results were also mapped on the Wang flow pattern map.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015ThEng..62..423S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015ThEng..62..423S"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> in rectangular channels with crossing fins (a Review)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sokolov, N. P.; Polishchuk, V. G.; Andreev, K. D.; Rassokhin, V. A.; Zabelin, N. A.</p> <p>2015-06-01</p> <p>Channels with crossing finning find wide use in the cooling paths of high-temperature gas turbine blade systems. At different times, different institutions carried out experimental investigations of heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> in channels with coplanar finning of opposite walls for obtaining semiempirical dependences of Nusselt criteria (dimensionless heat-transfer coefficients) and <span class="hlt">pressure</span> <span class="hlt">drop</span> coefficients on the operating Reynolds number and relative geometrical parameters (or their complexes). The shape of experimental channels, the conditions of experiments, and the used variables were selected so that they would be most suited for solving particular practical tasks. Therefore, the results obtained in processing the experimental data have large scatter and limited use. This article considers the results from experimental investigations of different authors. In comparing the results, additional calculations were carried out for bringing the mathematical correlations to the form of dependences from the same variables. Generalization of the results is carried out. In the final analysis, universal correlations are obtained for determining the <span class="hlt">pressure</span> <span class="hlt">drop</span> coefficients and Nusselt number values for the flow of working medium in channels with coplanar finning.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1989Cryo...29..503M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1989Cryo...29..503M"><span><span class="hlt">Pressure</span> <span class="hlt">drop</span> and He II flow through fine mesh screens</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Maddocks, J. R.; van Sciver, S. W.</p> <p>1989-05-01</p> <p>Fluid acquisition systems for He II transfer devices will utilize gallery arms to ensure that the fluid encounters the pump inlet. In near term experiments such as Superfluid Helium on Orbit Transfer (SHOOT), the preferred configuration consists of several rectangular channels which have one side made from a Dutch weave stainless steel screen having 325 x 2300 wires per inch. The effective pore diameter for this screen is about 5 microns. The present paper reports on measurements of <span class="hlt">pressure</span> <span class="hlt">drop</span> across a screen when it is subjected to a flow of liquid helium. The experiment measures the time rate of change of the level in two different helium reservoirs connected by a screen-blocked channel. Results with normal helium are compared with predictions based on the Armour-Cannon (1968) equations. The He II data show considerable deviation from the classical result. A discussion of the He II <span class="hlt">pressure</span> <span class="hlt">drop</span> results in terms of two fluid hydrodynamics is included.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19910043907&hterms=UNDER+ARMOUR&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DUNDER%2BARMOUR','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19910043907&hterms=UNDER+ARMOUR&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DUNDER%2BARMOUR"><span><span class="hlt">Pressure</span> <span class="hlt">drop</span> and He II flow through fine mesh screens</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Maddocks, J. R.; Van Sciver, S. W.</p> <p>1989-01-01</p> <p>Fluid acquisition systems for He II transfer devices will utilize gallery arms to ensure that the fluid encounters the pump inlet. In near term experiments such as Superfluid Helium on Orbit Transfer (SHOOT), the preferred configuration consists of several rectangular channels which have one side made from a Dutch weave stainless steel screen having 325 x 2300 wires per inch. The effective pore diameter for this screen is about 5 microns. The present paper reports on measurements of <span class="hlt">pressure</span> <span class="hlt">drop</span> across a screen when it is subjected to a flow of liquid helium. The experiment measures the time rate of change of the level in two different helium reservoirs connected by a screen-blocked channel. Results with normal helium are compared with predictions based on the Armour-Cannon (1968) equations. The He II data show considerable deviation from the classical result. A discussion of the He II <span class="hlt">pressure</span> <span class="hlt">drop</span> results in terms of two fluid hydrodynamics is included.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1987abe..symp..193W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1987abe..symp..193W"><span>Influence of fuel temperature on atomization performance of <span class="hlt">pressure</span>-swirl atomizers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, X. F.; Lefebvre, A. H.</p> <p></p> <p>The influence of fuel temperature on mean <span class="hlt">drop</span> size and <span class="hlt">drop</span>-size distribution is examined for aviation gasoline and diesel oil, using three <span class="hlt">pressure</span>-swirl simplex nozzles. Spray characteristics are measured over wide ranges of fuel injection <span class="hlt">pressure</span> and ambient <span class="hlt">air</span> <span class="hlt">pressure</span> using a Malvern spray analyzer. Fuel temperatures are varied from -20 C to +50 C. Over this range of temperature, the overall effect of an increase in fuel temperature is to reduce the mean <span class="hlt">drop</span> size and broaden the distribution of <span class="hlt">drop</span> sizes in the spray. Generally, it is found that the influence of fuel temperature on mean <span class="hlt">drop</span> size is far more pronounced for diesel oil than for gasoline. For both fuels the beneficial effect of higher fuel temperatures on atomization quality is sensibly independent of ambient <span class="hlt">air</span> <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017SPIE10328E..18T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017SPIE10328E..18T"><span>Probing the nanoscale with high-speed interferometry of an impacting <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Thoroddsen, S. T.; Li, E. Q.; Vakarelski, I. U.; Langley, K.</p> <p>2017-02-01</p> <p>The simple phenomenon of a water <span class="hlt">drop</span> falling onto a glass plate may seem like a trivial fluid mechanics problem. However, detailed imaging has shown that this process is highly complex and a small <span class="hlt">air</span>-bubble is always entrapped under the <span class="hlt">drop</span> when it makes contact with the solid. This bubble can interfere with the uniformity of spray coatings and degrade inkjet fabrication of displays etc. We will describe how we use high-speed interferometry at 5 million frames per second to understand the details of this process. As the impacting <span class="hlt">drop</span> approaches the solid, the dynamics are characterized by a balance between the lubrication <span class="hlt">pressure</span> in the thin <span class="hlt">air</span> layer and the inertia of the bot-tom of the <span class="hlt">drop</span>. This deforms the <span class="hlt">drop</span>, forming a dimple at its bottom and making the <span class="hlt">drop</span> touch the surface along a ring, thereby entrapping the <span class="hlt">air</span>-layer, which is typically 1-3 μm thick. This <span class="hlt">air</span>-layer can be highly compressed and the deceleration of the bottom of the <span class="hlt">drop</span> can be as large as 300,000 g. We describe how the thickness evolution of the lubricating <span class="hlt">air</span>-layer is extracted from following the interference fringes between frames. Two-color interferometry is also used to extract absolute layer thicknesses. Finally, we identify the effects of nanometric surface roughness on the first contact of the <span class="hlt">drop</span> with the substrate. Here we need to resolve the 100 nm thickness changes occurring during 200 ns intervals, requiring these state of the art high-speed cameras. Surprisingly, we see a ring of micro-bubbles marking the first contact of the <span class="hlt">drop</span> with the glass, only for microscope slides, which have a typical roughness of 20 nm, while such rings are absent for <span class="hlt">drop</span> impacts onto molecularly smooth mica surfaces.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMMR11A0295Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMMR11A0295Y"><span>Study on Transfer Rules of Coal Reservoir <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Based on Coalbed Methane Well Drainage Experiments</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yuhang, X.</p> <p>2017-12-01</p> <p>A pumping test was carried out to explore the transfer rules of <span class="hlt">pressure</span> <span class="hlt">drop</span> in coal reservoir during the drainage. The experiment was divided into three stages. In the first stage, the pump displacement of 3m3/h was used to reduce the bottom hole flowing <span class="hlt">pressure</span> and stopped until the continuous gas phase was produced; Undertaking the first stage, in the second stage, when the gas phase was continuously produced, the pump was stopped immediately. As the bottom hole flowing <span class="hlt">pressure</span> going up without gas phase, pumping started again for a week. In the third stage ,the well pumping was carried out at the bottom hole <span class="hlt">pressure</span> <span class="hlt">drop</span> rate of 30Kpa/d after two months' recovery. Combined with the data of regional geology and fractured well, taking the characteristics of macroscopic coal rocks, development of pore and fracture in coal and isothermal adsorption test as the background, the features of reservoir output in each stage of the experiment were analyzed and compared, and then the transfer rules of <span class="hlt">pressure</span> <span class="hlt">drop</span> contained in the differences of the output was studied further. In the first and third stage of the experiment, the output of liquid phase was much larger than the space volume of coal reservoir pore and fracture in the range of 100m2. In the second stage, the output of the continuous gas phase appeared around 0.7Mpa when the continuous gas phase appears below the critical desorption <span class="hlt">pressure</span> of 0.25Mpa during the whole experiment. The results indicate that, the transfer of <span class="hlt">pressure</span> <span class="hlt">drop</span> in the coal reservoir of this well is mainly horizontal, and the liquid phase produced in the reservoir mainly comes from the recharge of the reservoir at the far end of the relative high <span class="hlt">pressure</span> area; the adsorption space of coalbed methane in the coal matrix as well as the main migration channel of fluid in the reservoir doesn't belong to the same <span class="hlt">pressure</span> system and there exists the communication barrier between them. In addition, the increasing of the effective stress</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA457145','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA457145"><span>Evaluation of Low-<span class="hlt">Pressure</span> <span class="hlt">Drop</span> Antimicrobial and Hybrid <span class="hlt">Air</span> Filters</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2006-09-01</p> <p>purification of aerosol- contaminated <span class="hlt">air</span> streams has been performed by mechanical filtration. Existing particle filters will stop bacterial and viral...or hybrid low-∆P antimicrobial particulate filter materials. 1.2 Background Traditional purification of aerosol- contaminated <span class="hlt">air</span> streams has...Plastics, Lima , Ohio). Each path runs through a test article and thence through one AGI-30 all-glass impinger (Chemglass, Vineland, N.J.) partially</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16290596','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16290596"><span>Development of a constant surface <span class="hlt">pressure</span> penetration langmuir balance based on axisymmetric <span class="hlt">drop</span> shape analysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wege, H A; Holgado-Terriza, J A; Cabrerizo-Vílchez, M A</p> <p>2002-05-15</p> <p>A new constant <span class="hlt">pressure</span> pendant-<span class="hlt">drop</span> penetration surface balance has been developed combining a pendant-<span class="hlt">drop</span> surface balance, a rapid-subphase-exchange technique, and a fuzzy logic control algorithm. Beside the determination of insoluble monolayer compression-expansion isotherms, it allows performance of noninvasive kinetic studies of the adsorption of surfactants added to the new subphase onto the free surface and of the adsorption/penetration/reaction of the former onto/into/with surface layers, respectively. The interfacial <span class="hlt">pressure</span> pi is a fundamental parameter in these studies: by working at constant pi one controls the height of the energy barrier to adsorption/penetration and can select different regimes and steps of the adsorption/penetration process. In our device a solution <span class="hlt">drop</span> is formed at the tip of a coaxial double capillary, connected to a double microinjector. <span class="hlt">Drop</span> profiles are extracted from digital <span class="hlt">drop</span> micrographs and fitted to the equation of capillarity, yielding pi, the <span class="hlt">drop</span> volume V, and the interfacial area A. pi is varied changing V (and hence A) with the microinjector. Control is based on a case-adaptable modulated fuzzy-logic PID algorithm able to maintain constant pi (or A) under a wide range of experimental conditions. The <span class="hlt">drop</span> subphase liquid can be exchanged quantitatively by the coaxial capillaries. The adsorption/penetration/reaction kinetics at constant pi are then studied monitoring A(t), i.e., determining the relative area change necessary at each instant to compensate the <span class="hlt">pressure</span> variation due to the interaction of the surfactant in the subsurface with the surface layer. A fully Windows-integrated program manages the whole setup. Examples of experimental protein adsorption and monolayer penetration kinetics are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1995AIPC..324...53L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1995AIPC..324...53L"><span>Two-phase adiabatic <span class="hlt">pressure</span> <span class="hlt">drop</span> experiments and modeling under micro-gravity conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Longeot, Matthieu J.; Best, Frederick R.</p> <p>1995-01-01</p> <p>Thermal systems for space applications based on two phase flow have several advantages over single phase systems. Two phase thermal energy management and dynamic power conversion systems have the capability of achieving high specific power levels. However, before two phase systems for space applications can be designed effectively, knowledge of the flow behavior in a ``0-g'' acceleration environment is necessary. To meet this need, two phase flow experiments were conducted by the Interphase Transport Phenomena Laboratory Group (ITP) aboard the National Aeronautics and Space Administration's (NASA) KC-135, using R12 as the working fluid. The present work is concerned with modeling of two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> under 0-g conditions, for bubbly and slug flow regimes. The set of data from the ITP group includes 3 bubbly points, 9 bubbly/slug points and 6 slug points. These two phase <span class="hlt">pressure</span> <span class="hlt">drop</span> data were collected in 1991 and 1992. A methodology to correct and validate the data was developed to achieve high levels of confidence. A homogeneous model was developed to predict the <span class="hlt">pressure</span> <span class="hlt">drop</span> for particular flow conditions. This model, which uses the Blasius Correlation, was found to be accurate for bubbly and bubbly/slug flows, with errors not larger than 28%. For slug flows, however, the errors are greater, attaining values up to 66%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009JPS...188..163Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009JPS...188..163Y"><span>The critical <span class="hlt">pressure</span> <span class="hlt">drop</span> for the purge process in the anode of a fuel cell</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yu, Xiao; Pingwen, Ming; Ming, Hou; Baolian, Yi; Shao, Zhi-Gang</p> <p></p> <p>Purge operation is an effective way to remove the accumulated liquid water in the anode of proton exchange membrane fuel cells (PEMFCs). This paper studies the phenomenon of the two-phase flow as well as the <span class="hlt">pressure</span> <span class="hlt">drop</span> fluctuation inside the flow field of a single cell during the purge process. The flow patterns are identified as intermittent purge and annular purge, and the two purge processes are contrastively analyzed and discussed. The intermittent purge greatly affects the fuel cell performance and thus it is not suitable for the in situ application. The annular purge process requires a higher <span class="hlt">pressure</span> <span class="hlt">drop</span>, and the critical <span class="hlt">pressure</span> <span class="hlt">drop</span> is calculated from the annular purge model. Furthermore, this value is quantitatively analyzed and validated by experiments. The results show that the annular purge is appropriate for removing liquid water out of the anode in the fuel cell.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li class="active"><span>5</span></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_5 --> <div id="page_6" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="101"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25288476','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25288476"><span><span class="hlt">Air</span> filtration in the free molecular flow regime: a review of high-efficiency particulate <span class="hlt">air</span> filters based on carbon nanotubes.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Li, Peng; Wang, Chunya; Zhang, Yingying; Wei, Fei</p> <p>2014-11-01</p> <p><span class="hlt">Air</span> filtration in the free molecular flow (FMF) regime is important and challenging because a higher filtration efficiency and lower <span class="hlt">pressure</span> <span class="hlt">drop</span> are obtained when the fiber diameter is smaller than the gas mean free path in the FMF regime. In previous studies, FMF conditions have been obtained by increasing the gas mean free path through reducing the <span class="hlt">pressure</span> and increasing the temperature. In the case of carbon nanotubes (CNTs) with nanoscale diameters, it is possible to filtrate in the FMF regime under normal conditions. This paper reviews recent progress in theoretical and experimental studies of <span class="hlt">air</span> filtration in the FMF regime. Typical structure models of high-efficiency particulate (HEPA) <span class="hlt">air</span> filters based on CNTs are introduced. The <span class="hlt">pressure</span> <span class="hlt">drop</span> in <span class="hlt">air</span> filters operated in the FMF regime is less than that predicted by the conventional <span class="hlt">air</span> filtration theory. The thinnest HEPA filters fabricated from single-walled CNT films have an extremely low <span class="hlt">pressure</span> <span class="hlt">drop</span>. CNT <span class="hlt">air</span> filters with a gradient nanostructure are shown to give a much better filtration performance in dynamic filtration. CNT <span class="hlt">air</span> filters with a hierarchical structure and an agglomerated CNT fluidized bed <span class="hlt">air</span> filter are also introduced. Finally, the challenges and opportunities for the application of CNTs in <span class="hlt">air</span> filtration are discussed. © 2014 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16615688','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16615688"><span>Testing of heat exchangers in membrane oxygenators using <span class="hlt">air</span> <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hamilton, Carole; Stein, Jutta; Seidler, Rainer; Kind, Robert; Beck, Karin; Tosok, Jürgen; Upterfofel, Jörg</p> <p>2006-03-01</p> <p>All heat exchangers (HE) in membrane oxygenators are tested by the manufacturer for water leaks during the production phase. However, for safety reasons, it is highly recommended that HEs be tested again before clinical use. The most common method is to attach the heater-cooler to the HE and allow the water to recirculate for at least 10 min, during which time a water leak should be evident. To improve the detection of water leaks, a test was devised using a <span class="hlt">pressure</span> manometer with an integrated bulb used to <span class="hlt">pressurize</span> the HE with <span class="hlt">air</span>. The cardiopulmonary bypass system is set up as per protocol. A <span class="hlt">pressure</span> manometer adapted to a 1/2" tubing is connected to the water inlet side of the oxygenator. The water outlet side is blocked with a short piece of 1/2" deadend tubing. The HE is <span class="hlt">pressurized</span> with 250 mmHg for at least 30 sec and observed for any <span class="hlt">drop</span>. Over the last 2 years, only one oxygenator has been detected with a water leak in which the <span class="hlt">air</span>-method leaktest was performed. This unit was sent back to the manufacturer who confirmed the failure. Even though the incidence of water leaks is very low, it does occur and it is, therefore, important that all HEs are tested before they are used clinically. This method of using a <span class="hlt">pressure</span> manometer offers many advantages, as the HE can be tested outside of the operating room (OR), allowing earlier testing of the oxygenator, no water contact is necessary, and it is simple, easy and quick to perform.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012IJT....33.1726M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012IJT....33.1726M"><span><span class="hlt">Pressure-Drop</span> Considerations in the Characterization of Dew-Point Transfer Standards at High Temperatures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mitter, H.; Böse, N.; Benyon, R.; Vicente, T.</p> <p>2012-09-01</p> <p>During calibration of precision optical dew-point hygrometers (DPHs), it is usually necessary to take into account the <span class="hlt">pressure</span> <span class="hlt">drop</span> induced by the gas flow between the "point of reference" and the "point of use" (mirror or measuring head of the DPH) either as a correction of the reference dew-point temperature or as part of the uncertainty estimation. At dew-point temperatures in the range of ambient temperature and below, it is sufficient to determine the <span class="hlt">pressure</span> <span class="hlt">drop</span> for the required gas flow, and to keep the volumetric flow constant during the measurements. In this case, it is feasible to keep the dry-gas flow into the dew-point generator constant or to measure the flow downstream the DPH at ambient temperature. In normal operation, at least one DPH in addition to the monitoring DPH are used, and this operation has to be applied to each instrument. The situation is different at high dew-point temperatures up to 95 °C, the currently achievable upper limit reported in this paper. With increasing dew-point temperatures, the reference gas contains increasing amounts of water vapour and a constant dry-gas flow will lead to a significant enhanced volume flow at the conditions at the point of use, and therefore, to a significantly varying <span class="hlt">pressure</span> <span class="hlt">drop</span> depending on the applied dew-point temperature. At dew-point temperatures above ambient temperature, it is also necessary to heat the reference gas and the mirror head of the DPH sufficiently to avoid condensation which will additionally increase the volume flow and the <span class="hlt">pressure</span> <span class="hlt">drop</span>. In this paper, a method is provided to calculate the dry-gas flow rate needed to maintain a known wet-gas flow rate through a chilled mirror for a range of temperature and <span class="hlt">pressures</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993KvanE..20...51V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993KvanE..20...51V"><span>Laser plasma at low <span class="hlt">air</span> <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vas'kovskii, Iu. M.; Moiseev, V. N.; Rovinskii, R. E.; Tsenina, I. S.</p> <p>1993-01-01</p> <p>The ambient-<span class="hlt">pressure</span> dependences of the dynamic and optical characteristics of a laser plasma generated by CO2-laser irradiation of an obstacle are investigated experimentally. The change of the sample's surface roughness after irradiation is investigated as a function of <span class="hlt">air</span> <span class="hlt">pressure</span>. It is concluded that the transition from the <span class="hlt">air</span> plasma to the erosion plasma takes place at an <span class="hlt">air</span> <span class="hlt">pressure</span> of about 1 mm Hg. The results confirm the existing theory of plasma formation near the surface of an obstacle under the CO2-laser pulse effect in <span class="hlt">air</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000055585','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000055585"><span>A Validated All-<span class="hlt">Pressure</span> Fluid <span class="hlt">Drop</span> Model and Lewis Number Effects for a Binary Mixture</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Harstad, K.; Bellan, J.</p> <p>1999-01-01</p> <p>The differences between subcritical liquid <span class="hlt">drop</span> and supercritical fluid <span class="hlt">drop</span> behavior are discussed. Under subcritical, evaporative high emission rate conditions, a film layer is present in the inner part of the <span class="hlt">drop</span> surface which contributes to the unique determination of the boundary conditions; it is this film layer which contributes to the solution's convective-diffusive character. In contrast, under supercritical condition as the boundary conditions contain a degree of arbitrariness due to the absence of a surface, and the solution has then a purely diffusive character. Results from simulations of a free fluid <span class="hlt">drop</span> under no-gravity conditions are compared to microgravity experimental data from suspended, large <span class="hlt">drop</span> experiments at high, low and intermediary temperatures and in a range of <span class="hlt">pressures</span> encompassing the sub-and supercritical regime. Despite the difference between the conditions of the simulations and experiments (suspension vs. free floating), the time rate of variation of the <span class="hlt">drop</span> diameter square is remarkably well predicted in the linear curve regime. The <span class="hlt">drop</span> diameter is determined in the simulations from the location of the maximum density gradient, and agrees well with the data. It is also shown that the classical calculation of the Lewis number gives qualitatively erroneous results at supercritical conditions, but that an effective Lewis number previously defined gives qualitatively correct estimates of the length scales for heat and mass transfer at all <span class="hlt">pressures</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017Cryo...81...60O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017Cryo...81...60O"><span><span class="hlt">Pressure</span> <span class="hlt">drop</span> reduction and heat transfer deterioration of slush nitrogen in triangular and circular pipe flows</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ohira, Katsuhide; Kurose, Kizuku; Okuyama, Jun; Saito, Yutaro; Takahashi, Koichi</p> <p>2017-01-01</p> <p>Slush fluids such as slush hydrogen and slush nitrogen are characterized by superior properties as functional thermal fluids due to their density and heat of fusion. In addition to allowing efficient hydrogen transport and storage, slush hydrogen can serve as a refrigerant for high-temperature superconducting (HTS) equipment using MgB2, with the potential for synergistic effects. In this study, <span class="hlt">pressure</span> <span class="hlt">drop</span> reduction and heat transfer deterioration experiments were performed on slush nitrogen flowing in a horizontal triangular pipe with sides of 20 mm under the conditions of three different cross-sectional orientations. Experimental conditions consisted of flow velocity (0.3-4.2 m/s), solid fraction (0-25 wt.%), and heat flux (0, 10, and 20 kW/m2). <span class="hlt">Pressure</span> <span class="hlt">drop</span> reduction became apparent at flow velocities exceeding about 1.3-1.8 m/s, representing a maximum amount of reduction of 16-19% in comparison with liquid nitrogen, regardless of heating. Heat transfer deterioration was seen at flow velocities of over 1.2-1.8 m/s, for a maximum amount of deterioration of 13-16%. The authors of the current study compared the results for <span class="hlt">pressure</span> <span class="hlt">drop</span> reduction and heat transfer deterioration in triangular pipe with those obtained previously for circular and square pipes, clarifying differences in flow and heat transfer properties. Also, a correlation equation was obtained between the slush Reynolds number and the pipe friction factor, which is important in the estimation of <span class="hlt">pressure</span> <span class="hlt">drop</span> in unheated triangular pipe. Furthermore, a second correlation equation was derived between the modified slush Reynolds number and the pipe friction factor, enabling the integrated prediction of <span class="hlt">pressure</span> <span class="hlt">drop</span> in both unheated triangular and circular pipes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFDL20007C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFDL20007C"><span>Calculation of <span class="hlt">pressure</span> <span class="hlt">drop</span> in the developmental stages of the medaka fish heart and microvasculature</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chakraborty, Sreyashi; Vlachos, Pavlos</p> <p>2016-11-01</p> <p>Peristaltic contraction of the developing medaka fish heart produces temporally and spatially varying <span class="hlt">pressure</span> <span class="hlt">drop</span> across the atrioventricular (AV) canal. Blood flowing through the tail vessels experience a slug flow across the developmental stages. We have performed a series of live imaging experiments over 14 days post fertilization (dpf) of the medaka fish egg and cross-correlated the red blood cell (RBC) pattern intensities to obtain the two-dimensional velocity fields. Subsequently we have calculated the <span class="hlt">pressure</span> field by integrating the <span class="hlt">pressure</span> gradient in the momentum equation. Our calculations show that the <span class="hlt">pressure</span> <span class="hlt">drop</span> across the AV canal increases from 0.8mm Hg during 3dpf to 2.8 mm Hg during 14dpf. We have calculated the time-varying wall shear stress for the blood vessels by assuming a spatially constant velocity magnitude in each vessel. The calculated wall shear stress matches the wall shear stress sensed by human endothelial cells (10-12 dyne/sq. cm). The <span class="hlt">pressure</span> <span class="hlt">drop</span> per unit length of the vessel is obtained by doing a control volume analysis of flow in the caudal arteries and veins. The current results can be extended to investigate the effect of the fluid dynamic parameters on the vascular and cardiac morphogenesis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790042654&hterms=B-52&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DB-52','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790042654&hterms=B-52&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DB-52"><span>Space Shuttle Solid Rocket Booster decelerator subsystem - <span class="hlt">Air</span> <span class="hlt">drop</span> test vehicle/B-52 design</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Runkle, R. E.; Drobnik, R. F.</p> <p>1979-01-01</p> <p>The <span class="hlt">air</span> <span class="hlt">drop</span> development test program for the Space Shuttle Solid Rocket Booster Recovery System required the design of a large <span class="hlt">drop</span> test vehicle that would meet all the stringent requirements placed on it by structural loads, safety considerations, flight recovery system interfaces, and sequence. The <span class="hlt">drop</span> test vehicle had to have the capability to test the drogue and the three main parachutes both separately and in the total flight deployment sequence and still be low-cost to fit in a low-budget development program. The design to test large ribbon parachutes to loads of 300,000 pounds required the detailed investigation and integration of several parameters such as carrier aircraft mechanical interface, <span class="hlt">drop</span> test vehicle ground transportability, impact point ground penetration, salvageability, <span class="hlt">drop</span> test vehicle intelligence, flight design hardware interfaces, and packaging fidelity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol6/pdf/CFR-2014-title49-vol6-sec570-57.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol6/pdf/CFR-2014-title49-vol6-sec570-57.pdf"><span>49 CFR 570.57 - <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake subsystem.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... <span class="hlt">pressure</span> <span class="hlt">drop</span> in psi per minute with brakes released and with brakes fully applied. (d) <span class="hlt">Air</span>-over-hydraulic... 49 Transportation 6 2014-10-01 2014-10-01 false <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake... STANDARDS Vehicles With GVWR of More Than 10,000 Pounds § 570.57 <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title49-vol6/pdf/CFR-2010-title49-vol6-sec570-57.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title49-vol6/pdf/CFR-2010-title49-vol6-sec570-57.pdf"><span>49 CFR 570.57 - <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake subsystem.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-10-01</p> <p>... <span class="hlt">pressure</span> <span class="hlt">drop</span> in psi per minute with brakes released and with brakes fully applied. (d) <span class="hlt">Air</span>-over-hydraulic... 49 Transportation 6 2010-10-01 2010-10-01 false <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake... STANDARDS Vehicles With GVWR of More Than 10,000 Pounds § 570.57 <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol6/pdf/CFR-2012-title49-vol6-sec570-57.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol6/pdf/CFR-2012-title49-vol6-sec570-57.pdf"><span>49 CFR 570.57 - <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake subsystem.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... <span class="hlt">pressure</span> <span class="hlt">drop</span> in psi per minute with brakes released and with brakes fully applied. (d) <span class="hlt">Air</span>-over-hydraulic... 49 Transportation 6 2012-10-01 2012-10-01 false <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake... STANDARDS Vehicles With GVWR of More Than 10,000 Pounds § 570.57 <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol6/pdf/CFR-2013-title49-vol6-sec570-57.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol6/pdf/CFR-2013-title49-vol6-sec570-57.pdf"><span>49 CFR 570.57 - <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake subsystem.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... <span class="hlt">pressure</span> <span class="hlt">drop</span> in psi per minute with brakes released and with brakes fully applied. (d) <span class="hlt">Air</span>-over-hydraulic... 49 Transportation 6 2013-10-01 2013-10-01 false <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic brake... STANDARDS Vehicles With GVWR of More Than 10,000 Pounds § 570.57 <span class="hlt">Air</span> brake system and <span class="hlt">air</span>-over-hydraulic...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740008500','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740008500"><span>Fundamental study of transpiration cooling. [<span class="hlt">pressure</span> <span class="hlt">drop</span> and heat transfer data from porous metals</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Koh, J. C. Y.; Dutton, J. L.; Benson, B. A.</p> <p>1973-01-01</p> <p>Isothermal and non-isothermal <span class="hlt">pressure</span> <span class="hlt">drop</span> data and heat transfer data generated on porous 304L stainless steel wire forms, sintered spherical stainless steel powder, and sintered spherical OFHC copper powder are reported and correlated. <span class="hlt">Pressure</span> <span class="hlt">drop</span> data was collected over a temperature range from 500 R to 2000 R and heat transfer data collected over a heat flux range from 5 to 15 BTU/in2/sec. It was found that flow data could be correlated independently of transpirant temperature and type (i.e., H2, N2). It was also found that no simple relation between heat transfer coefficient and specimen porosity was obtainable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPS...385..100S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPS...385..100S"><span>An optimized microstructure to minimizing in-plane and through-plane <span class="hlt">pressure</span> <span class="hlt">drops</span> of fibrous materials: Counter-intuitive reduction of gas diffusion layer permeability with porosity</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sadeghifar, Hamidreza</p> <p>2018-05-01</p> <p>The present study experimentally investigates the realistic functionality of in-plane and through-plane <span class="hlt">pressure</span> <span class="hlt">drops</span> of layered fibrous media with porosity, fiber diameter, fiber spacing, fiber-fiber angles and fiber-flow angles. The study also reveals that <span class="hlt">pressure</span> <span class="hlt">drop</span> may increase with porosity and fiber diameter under specific circumstances. This counter-intuitive point narrows down the validity range of widely-used permeability-porosity-diameter models or correlations. It is found that, for fibrous materials, the most important parameter that impacts the in-plane <span class="hlt">pressure</span> <span class="hlt">drop</span> is not their porosities but the number of fibers extended in the flow direction. It is also concluded that in-plane <span class="hlt">pressure</span> <span class="hlt">drop</span> is highly dependent upon the flow direction (fiber-flow angles), especially at lower porosities. Contrary to in-plane <span class="hlt">pressure</span> <span class="hlt">drop</span>, through-plane <span class="hlt">pressure</span> <span class="hlt">drop</span> is a weak function of fiber-fiber angles but is strongly impacted by fiber spacing, especially at lower porosities. At a given porosity, low through-plane <span class="hlt">pressure</span> <span class="hlt">drops</span> occur if fiber spacing does not change practically from one layer to another. Through-plane <span class="hlt">pressure</span> <span class="hlt">drop</span> also, insignificantly, increases with the intersecting angles between fibers. An optimized microstructure of fibrous media resulting in minimal in-plane and through-plane <span class="hlt">pressure</span> <span class="hlt">drops</span> is also offered for the first time in this work.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29620373','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29620373"><span>Contact Line Instability Caused by <span class="hlt">Air</span> Rim Formation under Nonsplashing Droplets.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pack, Min; Kaneelil, Paul; Kim, Hyoungsoo; Sun, Ying</p> <p>2018-05-01</p> <p><span class="hlt">Drop</span> impact is fundamental to various natural and industrial processes such as rain-induced soil erosion and spray-coating technologies. The recent discovery of the role of <span class="hlt">air</span> entrainment between the droplet and the impacting surface has produced numerous works, uncovering the unique physics that correlates the <span class="hlt">air</span> film dynamics with the <span class="hlt">drop</span> impact outcomes. In this study, we focus on the post-failure <span class="hlt">air</span> entrainment dynamics for We numbers well below the splash threshold under different ambient <span class="hlt">pressures</span> and elucidate the interfacial instabilities formed by <span class="hlt">air</span> entrainment at the wetting front of impacting droplets on perfectly smooth, viscous films of constant thickness. A high-speed total internal reflection microscopy technique accounting for the Fresnel reflection at the <span class="hlt">drop-air</span> interface allows for in situ measurements of an entrained <span class="hlt">air</span> rim at the wetting front. The presence of an <span class="hlt">air</span> rim is found to be a prerequisite to the interfacial instability which is formed when the capillary <span class="hlt">pressure</span> in the vicinity of the contact line can no longer balance the increasing gas <span class="hlt">pressure</span> near the wetting front. A critical capillary number for the <span class="hlt">air</span> rim formation is experimentally identified above which the wetting front becomes unstable where this critical capillary number inversely scales with the ambient <span class="hlt">pressure</span>. The contact line instabilities at relatively low We numbers ( We ∼ O(10)) observed in this study provide insight into the conventional understanding of hydrodynamic instabilities under <span class="hlt">drop</span> impact which usually require We ≫ 10.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=4&id=EJ522892','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=4&id=EJ522892"><span>Intraoral <span class="hlt">Air</span> <span class="hlt">Pressure</span> of Alaryngeal Speakers during a No-<span class="hlt">Air</span> Insufflation Maneuver.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Gorham, Mary M.; And Others</p> <p>1996-01-01</p> <p>Intraoral <span class="hlt">air</span> <span class="hlt">pressure</span> was recorded during the production of consonant cognate pairs by 8 esophageal speakers (mean age 67 years) under 2 experimental conditions: after the insufflation of <span class="hlt">air</span> and without <span class="hlt">air</span> insufflation. Results revealed that peak intraoral <span class="hlt">air</span> <span class="hlt">pressure</span> magnitudes were significantly greater following the insufflation of <span class="hlt">air</span> than…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24746019','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24746019"><span>Geometry-based <span class="hlt">pressure</span> <span class="hlt">drop</span> prediction in mildly diseased human coronary arteries.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Schrauwen, J T C; Wentzel, J J; van der Steen, A F W; Gijsen, F J H</p> <p>2014-06-03</p> <p><span class="hlt">Pressure</span> <span class="hlt">drop</span> (△p) estimations in human coronary arteries have several important applications, including determination of appropriate boundary conditions for CFD and estimation of fractional flow reserve (FFR). In this study a △p prediction was made based on geometrical features derived from patient-specific imaging data. Twenty-two mildly diseased human coronary arteries were imaged with computed tomography and intravascular ultrasound. Each artery was modelled in three consecutive steps: from straight to tapered, to stenosed, to curved model. CFD was performed to compute the additional △p in each model under steady flow for a wide range of Reynolds numbers. The correlations between the added geometrical complexity and additional △p were used to compute a predicted △p. This predicted △p based on geometry was compared to CFD results. The mean △p calculated with CFD was 855±666Pa. Tapering and curvature added significantly to the total △p, accounting for 31.4±19.0% and 18.0±10.9% respectively at Re=250. Using tapering angle, maximum area stenosis and angularity of the centerline, we were able to generate a good estimate for the predicted △p with a low mean but high standard deviation: average error of 41.1±287.8Pa at Re=250. Furthermore, the predicted △p was used to accurately estimate FFR (r=0.93). The effect of the geometric features was determined and the <span class="hlt">pressure</span> <span class="hlt">drop</span> in mildly diseased human coronary arteries was predicted quickly based solely on geometry. This <span class="hlt">pressure</span> <span class="hlt">drop</span> estimation could serve as a boundary condition in CFD to model the impact of distal epicardial vessels. Copyright © 2014 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27553299','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27553299"><span>Effects of instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span> process on physical and sensory properties of puffed wheat snack.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Yağcı, Sibel</p> <p>2017-04-01</p> <p>In this study, research on the development of a puffed wheat snack using the instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span> (DIC) process was carried out. Snack products were produced by expanding moistened wheat under various DIC processing conditions in order to obtain adequate puffing, followed by drying in a hot <span class="hlt">air</span> dryer. The effects of operational variables such as wheat initial moisture content (11-23% w/w, wet basis), processing <span class="hlt">pressure</span> (3-5 × 10 2 kPa) and processing time (3-11 min) on the physical (density, color and textural characteristics) and sensory properties of the product were investigated. The physical properties of the wheat snack were most affected by changes in processing <span class="hlt">pressure</span>, followed by processing time and wheat moisture content. Increasing processing <span class="hlt">pressure</span> and time often improved expansion and textural properties but led to darkening of the raw wheat color. The most acceptable snack in terms of physical properties was obtained at the lowest wheat moisture content. Sensory analysis suggested that consumer acceptability was optimal for wheat snacks produced at higher processing <span class="hlt">pressure</span>, medium processing time and lower moisture content. The most desirable conditions for puffed wheat snack production using the DIC process were determined as 11% (w/w) of wheat moisture content, 5 × 10 2 kPa of processing <span class="hlt">pressure</span> and 7 min of processing time. © 2016 Society of Chemical Industry. © 2016 Society of Chemical Industry.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/14560234','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/14560234"><span>Prospective evaluation of chronic venous insufficiency based on foot venous <span class="hlt">pressure</span> measurements and <span class="hlt">air</span> plethysmography findings.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Fukuoka, Masato; Sugimoto, Takaki; Okita, Yutaka</p> <p>2003-10-01</p> <p>The purpose of this study was to evaluate lower extremity venous function in patients with chronic venous insufficiency, with foot venous <span class="hlt">pressure</span> (FVP) measurements and <span class="hlt">air</span> plethysmography (APG). Eighty-five limbs of 63 patients with a history of chronic venous insufficiency (CVI) from 1995 to 1999 were studied. FVP parameters studied included ambulatory venous <span class="hlt">pressure</span> (AVP), percent decrease in FVP with manual calf compression (%<span class="hlt">drop</span>), ratio of increase in FVP over 4 seconds after release of compression (4SR%), and time to 90% recovery of FVP were measured. APG parameters studied included functional venous volume, 90% refilling time (VFT90), venous filling index, ejection fraction, and residual volume fraction. Venous filling index and 90% refilling time were significantly decreased in limbs with stasis syndrome compared with the control group. AVP, %<span class="hlt">drop</span>, and 4SR% also showed significantly decrease in limbs with stasis syndrome compared with those without it. AVP, %<span class="hlt">drop</span>, and 4SR% were significantly different for the primary group compared with the secondary group, whereas no differences were found with regard to any APG parameter. APG enables prediction of the presence of CVI, whereas FVP measurements are more useful for evaluation of clinical severity of CVI.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040053564','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040053564"><span>High-<span class="hlt">Pressure</span> Transport Properties Of Fluids: Theory And Data From Levitated <span class="hlt">Drops</span> At Combustion-Relevant Temperatures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bellan, Josette; Harstad, Kenneth; Ohsaka, Kenichi</p> <p>2003-01-01</p> <p>Although the high <span class="hlt">pressure</span> multicomponent fluid conservation equations have already been derived and approximately validated for binary mixtures by this PI, the validation of the multicomponent theory is hampered by the lack of existing mixing rules for property calculations. Classical gas dynamics theory can provide property mixing-rules at low <span class="hlt">pressures</span> exclusively. While thermal conductivity and viscosity high-<span class="hlt">pressure</span> mixing rules have been documented in the literature, there is no such equivalent for the diffusion coefficients and the thermal diffusion factors. The primary goal of this investigation is to extend the low <span class="hlt">pressure</span> mixing rule theory to high <span class="hlt">pressures</span> and validate the new theory with experimental data from levitated single <span class="hlt">drops</span>. The two properties that will be addressed are the diffusion coefficients and the thermal diffusion factors. To validate/determine the property calculations, ground-based experiments from levitated <span class="hlt">drops</span> are being conducted.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_6 --> <div id="page_7" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="121"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014PhRvL.113s4501K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014PhRvL.113s4501K"><span>Universal Behavior of the Initial Stage of <span class="hlt">Drop</span> Impact</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Klaseboer, Evert; Manica, Rogerio; Chan, Derek Y. C.</p> <p>2014-11-01</p> <p>During the early stages of the impact of a <span class="hlt">drop</span> on a solid surface, <span class="hlt">pressure</span> builds up in the intervening thin lubricating <span class="hlt">air</span> layer and deforms the <span class="hlt">drop</span>. The extent of the characteristic deformation is determined by the competition between capillary, gravitational, and inertial forces that has been encapsulated in a simple analytic scaling law. For millimetric <span class="hlt">drops</span>, variations of the observed deformation with impact velocity V exhibit a maximum defined by the Weber and Eötvös numbers: We =1 +Eo . The deformation scales as V1 /2 at the low-velocity capillary regime and as V-1 /2 at the high-velocity inertia regime, in excellent agreement with a variety of experimental systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014SPIE.9232E..0GC','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014SPIE.9232E..0GC"><span>Micro-explosion of compound <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Chun-Kuei; Lin, Ta-Hui</p> <p>2014-08-01</p> <p>Introducing water into spray combustion systems, by either water-in-oil emulsification or supplementary water injection, is one of the major techniques for combustion improvement and NOx reduction. Plentiful researches are available on combustion of water-in-oil emulsion fuel <span class="hlt">drops</span>. The emulsified liquid is a heterogeneous mixture of immiscible liquids. One component forms the continuous phase and the other component forms the discrete phase. The discrete phase consists of globules of the one fluid that are suspended in the continuous phase fluid. Water-in-oil emulsions are commonly considered for combustion applications because emulsions can result in micro-explosion, thereby reducing the average <span class="hlt">drop</span> diameter to enhance liquid vaporization, and suppressing the formation of soot and NOx. However, the water addition generally does not exceed about 20% for smooth engine operations[!, 21. The combustion characteristics and micro-explosion of emulsion <span class="hlt">drop</span> were studied by many researchers. The micro-explosion of water in fuel emulsion <span class="hlt">drops</span> was caused by very fast growth of superheated water vapor bubbles, its superheat limits must be lower than the boiling point temperature of the fuel. These bubbles were primarily governed by the <span class="hlt">pressure</span> difference between the superheated vapor and the liquid, and by the inertia imparted to the liquid by the motion of the bubble surface[3 6 In this study, we used a coaxial nozzle to generation the multi-component <span class="hlt">drop</span>. The different type of water-in-oil fuel <span class="hlt">drops</span> called the compound <span class="hlt">drops</span>. Unlike an emulsion <span class="hlt">drop</span>, a compound <span class="hlt">drop</span> consists of a water core and a fuel shell, which can originate from the phase separation of emulsion[7, 81 or a water <span class="hlt">drop</span> colliding with a fuel <span class="hlt">drop</span>[9, 101 Burning and micro-explosion of compound <span class="hlt">drops</span> have been found to be distinct from those of emulsion <span class="hlt">drops</span>[9-111 Wang et al.[9 , 101 studied the combustion characteristics of collision merged alkane-water <span class="hlt">drops</span>. The merged <span class="hlt">drops</span> appeared in adhesive</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013JMiMi..23e5023V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013JMiMi..23e5023V"><span>A novel generation of 3D SAR-based passive micromixer: efficient mixing and low <span class="hlt">pressure</span> <span class="hlt">drop</span> at a low Reynolds number</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Viktorov, Vladimir; Nimafar, Mohammad</p> <p>2013-05-01</p> <p>This study introduces a novel generation of 3D splitting and recombination (SAR) passive micromixer with microstructures placed on the top and bottom floors of microchannels called a ‘chain mixer’. Both experimental verification and numerical analysis of the flow structure of this type of passive micromixer have been performed to evaluate the mixing performance and <span class="hlt">pressure</span> <span class="hlt">drop</span> of the microchannel, respectively. We propose here two types of chain mixer—chain 1 and chain 2—and compare their mixing performance and <span class="hlt">pressure</span> <span class="hlt">drop</span> with other micromixers, T-, o- and tear-<span class="hlt">drop</span> micromixers. Experimental tests carried out in the laminar flow regime with a low Reynolds number range, 0.083 ≤ Re ≤ 4.166, and image-based techniques are used to evaluate the mixing efficiency. Also, the computational fluid dynamics code, ANSYS FLUENT-13.0 has been used to analyze the flow and <span class="hlt">pressure</span> <span class="hlt">drop</span> in the microchannel. Experimental results show that the chain and tear-<span class="hlt">drop</span> mixer's efficiency is very high because of the SAR process: specifically, an efficiency of up to 98% can be achieved at the tested Reynolds number. The results also show that chain mixers have a lower required <span class="hlt">pressure</span> <span class="hlt">drop</span> in comparison with a tear-<span class="hlt">drop</span> micromixer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4371919','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4371919"><span>Kelvin–Helmholtz instability in an ultrathin <span class="hlt">air</span> film causes <span class="hlt">drop</span> splashing on smooth surfaces</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Liu, Yuan; Tan, Peng; Xu, Lei</p> <p>2015-01-01</p> <p>When a fast-moving <span class="hlt">drop</span> impacts onto a smooth substrate, splashing will be produced at the edge of the expanding liquid sheet. This ubiquitous phenomenon lacks a fundamental understanding. Combining experiment with model, we illustrate that the ultrathin <span class="hlt">air</span> film trapped under the expanding liquid front triggers splashing. Because this film is thinner than the mean free path of <span class="hlt">air</span> molecules, the interior airflow transfers momentum with an unusually high velocity comparable to the speed of sound and generates a stress 10 times stronger than the airflow in common situations. Such a large stress initiates Kelvin–Helmholtz instabilities at small length scales and effectively produces splashing. Our model agrees quantitatively with experimental verifications and brings a fundamental understanding to the ubiquitous phenomenon of <span class="hlt">drop</span> splashing on smooth surfaces. PMID:25713350</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012HMT....48..735S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012HMT....48..735S"><span>Flow structure, heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> in varying aspect ratio two-pass rectangular smooth channels</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Siddique, Waseem; El-Gabry, Lamyaa; Shevchuk, Igor V.; Hushmandi, Narmin B.; Fransson, Torsten H.</p> <p>2012-05-01</p> <p>Two-pass channels are used for internal cooling in a number of engineering systems e.g., gas turbines. Fluid travelling through the curved path, experiences <span class="hlt">pressure</span> and centrifugal forces, that result in <span class="hlt">pressure</span> driven secondary motion. This motion helps in moving the cold high momentum fluid from the channel core to the side walls and plays a significant role in the heat transfer in the channel bend and outlet pass. The present study investigates using Computational Fluid Dynamics (CFD), the flow structure, heat transfer enhancement and <span class="hlt">pressure</span> <span class="hlt">drop</span> in a smooth channel with varying aspect ratio channel at different divider-to-tip wall distances. Numerical simulations are performed in two-pass smooth channel with aspect ratio Win/H = 1:3 at inlet pass and Wout/H = 1:1 at outlet pass for a variety of divider-to-tip wall distances. The results show that with a decrease in aspect ratio of inlet pass of the channel, <span class="hlt">pressure</span> loss decreases. The divider-to-tip wall distance (Wel) not only influences the <span class="hlt">pressure</span> <span class="hlt">drop</span>, but also the heat transfer enhancement at the bend and outlet pass. With an increase in the divider-to-tip wall distance, the areas of enhanced heat transfer shifts from side walls of outlet pass towards the inlet pass. To compromise between heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> in the channel, Wel/H = 0.88 is found to be optimum for the channel under study.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016E%26ES...49b2007R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016E%26ES...49b2007R"><span>Implementation of <span class="hlt">pressurized</span> <span class="hlt">air</span> injection system in a Kaplan prototype for the reduction of vibration caused by tip vortex cavitation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rivetti, A.; Angulo, M.; Lucino, C.; Hene, M.; Capezio, O.; Liscia, S.</p> <p>2016-11-01</p> <p>Blade tip cavitation is a well-known phenomenon that affects the performance of large-diameter Kaplan turbines and induces structural vibration. Injection of <span class="hlt">pressurized</span> <span class="hlt">air</span> has been found to yield promising results in reducing those damaging effects. In this work, the results of an experimental test of <span class="hlt">air</span> injection on a 9.5-m-diameter Kaplan turbine are reported. Experiments were performed for several load conditions and for two different net heads. Accelerations, <span class="hlt">pressure</span> pulsation and noise emission were monitored for every tested condition. Results show that, at the expense of a maximum efficiency <span class="hlt">drop</span> of 0.2%, <span class="hlt">air</span> injection induces a decrease on the level of vibration from 57% up to 84%, depending on the load condition. Such decrease is seen to be proportional to the <span class="hlt">air</span> flow rate, in the range from 0.06 to 0.8‰ (respect to the discharge at the best efficiency point).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1990AcAAS..11..157W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1990AcAAS..11..157W"><span>Study on atomization features of a plain injector in high speed transverse <span class="hlt">air</span> stream</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wan, Jian; Gu, Shanjian; Yang, Maolin; Xiao, Weihui</p> <p>1990-04-01</p> <p>The atomization features of a plain injector in high-speed transverse <span class="hlt">air</span> stream were investigated by Malvern. In this investigation, <span class="hlt">air</span> velocity ranged from 50-150m/s, <span class="hlt">pressure</span> <span class="hlt">drop</span> of fuel injector, (1.1 - 4.2) x 10 to the 6th Pa, diameter of orifice, 0.5 - 0.9 mm, axial distance between the injector and the survey plane, 50 - 250 mm. Aviation kerosene was used in all experiments. It was found that the atomization features in high <span class="hlt">pressure</span> <span class="hlt">drop</span> of fuel injector were greatly differed from the low <span class="hlt">pressure</span> <span class="hlt">drop</span> of fuel injector.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17376468','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17376468"><span>Generation and characterization of surface layers on acoustically levitated <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tuckermann, Rudolf; Bauerecker, Sigurd; Cammenga, Heiko K</p> <p>2007-06-15</p> <p>Surface layers of natural and technical amphiphiles, e.g., octadecanol, stearic acid and related compounds as well as perfluorinated fatty alcohols (PFA), have been investigated on the surface of acoustically levitated <span class="hlt">drops</span>. In contrast to Langmuir troughs, traditionally used in the research of surface layers at the <span class="hlt">air</span>-water interface, acoustic levitation offers the advantages of a minimized and contact-less technique. Although the film <span class="hlt">pressure</span> cannot be directly adjusted on acoustically levitated <span class="hlt">drops</span>, it runs through a wide <span class="hlt">pressure</span> range due to the shrinking surface of an evaporating <span class="hlt">drop</span>. During this process, different states of the generated surface layer have been identified, in particular the phase transition from the gaseous or liquid-expanded to the liquid-condensed state of surface layers of octadecanol and other related amphiphiles. Characteristic parameters, such as the relative permeation resistance and the area per molecule in a condensed surface layer, have been quantified and were found comparable to results obtained from surface layers generated on Langmuir troughs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26398125','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26398125"><span>Noncontact Monitoring of Respiration by Dynamic <span class="hlt">Air-Pressure</span> Sensor.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Takarada, Tohru; Asada, Tetsunosuke; Sumi, Yoshihisa; Higuchi, Yoshinori</p> <p>2015-01-01</p> <p>We have previously reported that a dynamic <span class="hlt">air-pressure</span> sensor system allows respiratory status to be visually monitored for patients in minimally clothed condition. The dynamic <span class="hlt">air-pressure</span> sensor measures vital information using changes in <span class="hlt">air</span> <span class="hlt">pressure</span>. To utilize this device in the field, we must clarify the influence of clothing conditions on measurement. The present study evaluated use of the dynamic <span class="hlt">air-pressure</span> sensor system as a respiratory monitor that can reliably detect change in breathing patterns irrespective of clothing. Twelve healthy volunteers reclined on a dental chair positioned horizontally with the sensor pad for measuring <span class="hlt">air-pressure</span> signals corresponding to respiration placed on the seat back of the dental chair in the central lumbar region. Respiratory measurements were taken under 2 conditions: (a) thinly clothed (subject lying directly on the sensor pad); and (b) thickly clothed (subject lying on the sensor pad covered with a <span class="hlt">pressure</span>-reducing sheet). <span class="hlt">Air-pressure</span> signals were recorded and time integration values for <span class="hlt">air</span> <span class="hlt">pressure</span> during each expiration were calculated. This information was compared with expiratory tidal volume measured simultaneously by a respirometer connected to the subject via face mask. The dynamic <span class="hlt">air-pressure</span> sensor was able to receive the signal corresponding to respiration regardless of clothing conditions. A strong correlation was identified between expiratory tidal volume and time integration values for <span class="hlt">air</span> <span class="hlt">pressure</span> during each expiration for all subjects under both clothing conditions (0.840-0.988 for the thinly clothed condition and 0.867-0.992 for the thickly clothed condition). These results show that the dynamic <span class="hlt">air-pressure</span> sensor is useful for monitoring respiratory physiology irrespective of clothing.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820015565','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820015565"><span>The production of <span class="hlt">drops</span> by the bursting of a bubble at an <span class="hlt">air</span> liquid interface</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Darrozes, J. S.; Ligneul, P.</p> <p>1982-01-01</p> <p>The fundamental mechanism arising during the bursting of a bubble at an <span class="hlt">air</span>-liquid interface is described. A single bubble was followed from an arbitrary depth in the liquid, up to the creation and motion of the film and jet <span class="hlt">drops</span>. Several phenomena were involved and their relative order of magnitude was compared in order to point out the dimensionless parameters which govern each step of the motion. High-speed cinematography is employed. The characteristic bubble radius which separates the creation of jet <span class="hlt">drops</span> from cap bursting without jet <span class="hlt">drops</span> is expressed mathematically. The corresponding numerical value for water is 3 mm and agrees with experimental observations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013Cryo...58...45C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013Cryo...58...45C"><span>Two-phase heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of LNG during saturated flow boiling in a horizontal tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Dongsheng; Shi, Yumei</p> <p>2013-12-01</p> <p>Two-phase heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of LNG (liquefied natural gas) have been measured in a horizontal smooth tube with an inner diameter of 8 mm. The experiments were conducted at inlet <span class="hlt">pressures</span> from 0.3 to 0.7 MPa with a heat flux of 8-36 kW m-2, and mass flux of 49.2-201.8 kg m-2 s-1. The effect of vapor quality, inlet <span class="hlt">pressure</span>, heat flux and mass flux on the heat transfer characteristic are discussed. The comparisons of the experimental data with the predicted value by existing correlations are analyzed. Zou et al. (2010) correlation shows the best accuracy with 24.1% RMS deviation among them. Moreover four frictional <span class="hlt">pressure</span> <span class="hlt">drop</span> methods are also chosen to compare with the experimental database.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19800000549&hterms=cooling+tower&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcooling%2Btower','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19800000549&hterms=cooling+tower&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dcooling%2Btower"><span><span class="hlt">Drop</span> tower with no aerodynamic drag</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kendall, J. M., Jr.</p> <p>1981-01-01</p> <p>Cooling <span class="hlt">air</span> accelerated to match velocity of falling object eliminates drag. 3 meter <span class="hlt">drop</span> tower with suction fan and specific geometry causes <span class="hlt">air</span> to accelerate downward at 1 g. Although cooling of molten material released from top is slow because surrounding <span class="hlt">air</span> moves with it, <span class="hlt">drop</span> remains nearly spherical.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013IJMPS..2460002Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013IJMPS..2460002Z"><span><span class="hlt">Air</span> <span class="hlt">Pressure</span> Controlled Mass Measurement System</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhong, Ruilin; Wang, Jian; Cai, Changqing; Yao, Hong; Ding, Jin'an; Zhang, Yue; Wang, Xiaolei</p> <p></p> <p>Mass measurement is influenced by <span class="hlt">air</span> <span class="hlt">pressure</span>, temperature, humidity and other facts. In order to reduce the influence, mass laboratory of National Institute of Metrology, China has developed an <span class="hlt">air</span> <span class="hlt">pressure</span> controlled mass measurement system. In this system, an automatic mass comparator is installed in an airtight chamber. The Chamber is equipped with a <span class="hlt">pressure</span> controller and associate valves, thus the <span class="hlt">air</span> <span class="hlt">pressure</span> can be changed and stabilized to the pre-set value, the preferred <span class="hlt">pressure</span> range is from 200 hPa to 1100 hPa. In order to keep the environment inside the chamber stable, the display and control part of the mass comparator are moved outside the chamber, and connected to the mass comparator by feed-throughs. Also a lifting device is designed for this system which can easily lift up the upper part of the chamber, thus weights can be easily put inside the mass comparator. The whole system is put on a marble platform, and the temperature and humidity of the laboratory is very stable. The temperature, humidity, and carbon dioxide content inside the chamber are measured in real time and can be used to get <span class="hlt">air</span> density. Mass measurement cycle from 1100 hPa to 200 hPa and back to 1100 hPa shows the effective of the system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19730004','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19730004"><span>The relationships between <span class="hlt">air</span> exposure, negative <span class="hlt">pressure</span>, and hemolysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pohlmann, Joshua R; Toomasian, John M; Hampton, Claire E; Cook, Keith E; Annich, Gail M; Bartlett, Robert H</p> <p>2009-01-01</p> <p>The purpose of this study was to describe the hemolytic effects of both negative <span class="hlt">pressure</span> and an <span class="hlt">air</span>-blood interface independently and in combination in an in vitro static blood model. Samples of fresh ovine or human blood (5 ml) were subjected to a bubbling <span class="hlt">air</span> interface (0-100 ml/min) or negative <span class="hlt">pressure</span> (0-600 mm Hg) separately, or in combination, for controlled periods of time and analyzed for hemolysis. Neither negative <span class="hlt">pressure</span> nor an <span class="hlt">air</span> interface alone increased hemolysis. However, when <span class="hlt">air</span> and negative <span class="hlt">pressure</span> were combined, hemolysis increased as a function of negative <span class="hlt">pressure</span>, the <span class="hlt">air</span> interface, and time. Moreover, when blood samples were exposed to <span class="hlt">air</span> before initiating the test, hemolysis was four to five times greater than samples not preexposed to <span class="hlt">air</span>. When these experiments were repeated using freshly drawn human blood, the same phenomena were observed, but the hemolysis was significantly higher than that observed in sheep blood. In this model, hemolysis is caused by combined <span class="hlt">air</span> and negative <span class="hlt">pressure</span> and is unrelated to either factor alone.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3662481','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3662481"><span>The Relationships between <span class="hlt">Air</span> Exposure, Negative <span class="hlt">Pressure</span> and Hemolysis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Pohlmann, Joshua R.; Toomasian, John M.; Hampton, Claire E.; Cook, Keith E.; Annich, Gail M.; Bartlett, Robert H.</p> <p>2013-01-01</p> <p>The purpose of this study was to describe the hemolytic effects of both negative <span class="hlt">pressure</span> and an <span class="hlt">air</span>-blood interface independently and in combination in an in-vitro static blood model. Samples of fresh ovine or human blood (5 mL) were subjected to a bubbling <span class="hlt">air</span> interface (0–100 mL/min) or negative <span class="hlt">pressure</span> (0–600 mmHg) separately, or in combination, for controlled periods of time, and analyzed for hemolysis. Neither negative <span class="hlt">pressure</span> nor an <span class="hlt">air</span> interface alone increased hemolysis. However, when <span class="hlt">air</span> and negative <span class="hlt">pressure</span> were combined, hemolysis increased as a function of negative <span class="hlt">pressure</span>, the <span class="hlt">air</span> interface, and time. Moreover, when blood samples were exposed to <span class="hlt">air</span> prior to initiating the test, hemolysis was 4–5 times greater than samples not pre-exposed to <span class="hlt">air</span>. When these experiments were repeated using freshly drawn human blood the same phenomena were observed, but the hemolysis was significantly higher than that observed in sheep blood. In this model, hemolysis is caused by combined <span class="hlt">air</span> and negative <span class="hlt">pressure</span> and is unrelated to either factor alone. PMID:19730004</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950017633','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950017633"><span>Airborne rotary <span class="hlt">air</span> separator study</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Acharya, A.; Gottzmann, C. F.; Nowobilski, J. J.</p> <p>1990-01-01</p> <p>Several <span class="hlt">air</span> breathing propulsion concepts for future earth-to-orbit transport vehicles utilize <span class="hlt">air</span> collection and enrichment, and subsequent storage of liquid oxygen for later use in the vehicle emission. Work performed during the 1960's established the feasibility of substantially reducing weight and volume of a distillation type <span class="hlt">air</span> separator system by operating the distillation elements in high 'g' fields obtained by rotating the separator assembly. This contract studied the capability test and hydraulic behavior of a novel structured or ordered distillation packing in a rotating device using <span class="hlt">air</span> and water. <span class="hlt">Pressure</span> <span class="hlt">drop</span> and flood points were measured for different <span class="hlt">air</span> and water flow rates in gravitational fields of up to 700 g. Behavior of the packing follows the correlations previously derived from tests at normal gravity. The novel ordered packing can take the place of trays in a rotating <span class="hlt">air</span> separation column with the promise of substantial reduction in <span class="hlt">pressure</span> <span class="hlt">drop</span>, volume, and system weight. The results obtained in the program are used to predict design and performance of rotary separators for <span class="hlt">air</span> collection and enrichment systems of interest for past and present concepts of <span class="hlt">air</span> breathing propulsion (single or two-stage to orbit) systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..326a2002B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..326a2002B"><span>Effect of Water Cut on <span class="hlt">Pressure</span> <span class="hlt">Drop</span> of Oil (D130) -Water Flow in 4″Horizontal Pipe</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Basha, Mehaboob; Shaahid, S. M.; Al-Hems, Luai M.</p> <p>2018-03-01</p> <p>The oil-water flow in pipes is a challenging subject that is rich in physics and practical applications. It is often encountered in many oil and chemical industries. The <span class="hlt">pressure</span> gradient of two phase flow is still subject of immense research. The present study reports <span class="hlt">pressure</span> measurements of oil (D130)-water flow in a horizontal 4″ diameter stainless steel pipe at different flow conditions. Experiments were carried out for different water cuts (WC); 0-100%. Inlet oil-water flow rates were varied from 4000 to 8000 barrels-per-day in steps of 2000. It has been found that the frictional <span class="hlt">pressure</span> <span class="hlt">drop</span> decreases for WC = 0 - 40 %. With further increase in WC, friction <span class="hlt">pressure</span> <span class="hlt">drop</span> increases, this could be due to phase inversion.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014APS..DFDL13002K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014APS..DFDL13002K"><span>Coalescence of <span class="hlt">Drops</span> of a Power-law Fluid</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kamat, Pritish; Thete, Sumeet; Basaran, Osman</p> <p>2014-11-01</p> <p><span class="hlt">Drop</span> coalescence is crucial in a host of industrial, household, and natural processes that involve dispersions. Coalescence is a rate-controlling process in breaking emulsions and strongly influences <span class="hlt">drop</span>-size-distributions in sprays. In a continuum approach, coalescence begins by the formation of a microscopic, non-slender bridge connecting the two <span class="hlt">drops</span>. Indefinitely large axial curvature at the neck results in local lowering of <span class="hlt">pressure</span> that drives fluid from the bulk of the <span class="hlt">drops</span> toward the neck, thereby causing the bridge radius r (t) and height z (t) to increase in time t. The coalescence of Newtonian <span class="hlt">drops</span> in <span class="hlt">air</span> has heretofore been thoroughly studied. Here, we extend these earlier studies by analyzing the coalescence of <span class="hlt">drops</span> of power-law fluids because many fluids encountered in real applications, including cosmetic creams, shampoos, grease, and paint, exhibit power-law (deformation-rate thinning) rheology. On account of the non-slender geometry of the liquid bridge connecting the two <span class="hlt">drops</span> (z << r) , we analyze the resulting free surface flow problem by numerical simulation. Among other results, we present and discuss the nature of flows and scaling behaviors for r and z as functions of the initial viscosity and power-law index (0 < n <= 1) .</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1255128','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1255128"><span>Testing of a 4 K to 2 K heat exchanger with an intermediate <span class="hlt">pressure</span> <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Knudsen, Peter N.; Ganni, Venkatarao</p> <p>2015-12-01</p> <p>Most large sub-atmospheric helium refrigeration systems incorporate a heat exchanger at the load, or in the distribution system, to counter-flow the sub-atmospheric return with the super-critical or liquid supply. A significant process improvement is theoretically obtainable by handling the exergy loss across the Joule-Thompson throttling valve supplying the flow to the load in a simple but different manner. As briefly outlined in previous publications, the exergy loss can be minimized by allowing the supply flow <span class="hlt">pressure</span> to decrease to a sub-atmospheric <span class="hlt">pressure</span> concurrent with heat exchange flow from the load. One practical implementation is to sub-divide the supply flow pressuremore » <span class="hlt">drop</span> between two heat exchanger sections, incorporating an intermediate <span class="hlt">pressure</span> <span class="hlt">drop</span>. Such a test is being performed at Jefferson Lab's Cryogenic Test Facility (CTF). This paper will briefly discuss the theory, practical implementation and test results and analysis obtained to date.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20179887','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20179887"><span>[Aerodynamics study on <span class="hlt">pressure</span> changes inside <span class="hlt">pressure</span>-type whole-body plethysmograph produced by flowing <span class="hlt">air</span>].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Wei-Hua; Shen, Hua-Hao</p> <p>2010-02-25</p> <p>When using <span class="hlt">pressure</span>-type plethysmography to test lung function of rodents, calculation of lung volume is always based on Boyle's law. The precondition of Boyle's law is that perfect <span class="hlt">air</span> is static. However, <span class="hlt">air</span> in the chamber is flowing continuously when a rodent breathes inside the chamber. Therefore, Boyle's law, a principle of <span class="hlt">air</span> statics, may not be appropriate for measuring <span class="hlt">pressure</span> changes of flowing <span class="hlt">air</span>. In this study, we deduced equations for <span class="hlt">pressure</span> changes inside <span class="hlt">pressure</span>-type plethysmograph and then designed three experiments to testify the theoretic deduction. The results of theoretic deduction indicated that increased <span class="hlt">pressure</span> was generated from two sources: one was based on Boyle's law, and the other was based on the law of conservation of momentum. In the first experiment, after injecting 0.1 mL, 0.2 mL, 0.4 mL of <span class="hlt">air</span> into the plethysmograph, the <span class="hlt">pressure</span> inside the chamber increased sharply to a peak value, then promptly decreased to horizontal <span class="hlt">pressure</span>. Peak values were significantly higher than the horizontal values (P<0.001). This observation revealed that flowing <span class="hlt">air</span> made an extra effect on <span class="hlt">air</span> <span class="hlt">pressure</span> in the plethysmograph. In the second experiment, the same volume of <span class="hlt">air</span> was injected into the plethysmograph at different frequencies (0, 0.5, 1, 2, 3 Hz) and <span class="hlt">pressure</span> changes inside were measured. The results showed that, with increasing frequencies, the <span class="hlt">pressure</span> changes in the chamber became significantly higher (P<0.001). In the third experiment, small animal ventilator and pipette were used to make two types of airflow with different functions of time. The <span class="hlt">pressure</span> changes produced by the ventilator were significantly greater than those produced by the pipette (P<0.001). Based on the data obtained, we draw the conclusion that, the flow of <span class="hlt">air</span> plays a role in <span class="hlt">pressure</span> changes inside the plethysmograph, and the faster the airflow is, the higher the <span class="hlt">pressure</span> changes reach. Furthermore, the type of airflow also influences the <span class="hlt">pressure</span> changes.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_7 --> <div id="page_8" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="141"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4936686','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4936686"><span>Sound Wave Energy Resulting from the Impact of Water <span class="hlt">Drops</span> on the Soil Surface</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Ryżak, Magdalena; Bieganowski, Andrzej; Korbiel, Tomasz</p> <p>2016-01-01</p> <p>The splashing of water <span class="hlt">drops</span> on a soil surface is the first step of water erosion. There have been many investigations into splashing–most are based on recording and analysing images taken with high-speed cameras, or measuring the mass of the soil moved by splashing. Here, we present a new aspect of the splash phenomenon’s characterization the measurement of the sound <span class="hlt">pressure</span> level and the sound energy of the wave that propagates in the <span class="hlt">air</span>. The measurements were carried out for 10 consecutive water <span class="hlt">drop</span> impacts on the soil surface. Three soils were tested (Endogleyic Umbrisol, Fluvic Endogleyic Cambisol and Haplic Chernozem) with four initial moisture levels (<span class="hlt">pressure</span> heads: 0.1 kPa, 1 kPa, 3.16 kPa and 16 kPa). We found that the values of the sound <span class="hlt">pressure</span> and sound wave energy were dependent on the particle size distribution of the soil, less dependent on the initial <span class="hlt">pressure</span> head, and practically the same for subsequent water <span class="hlt">drops</span> (from the first to the tenth <span class="hlt">drop</span>). The highest sound <span class="hlt">pressure</span> level (and the greatest variability) was for Endogleyic Umbrisol, which had the highest sand fraction content. The sound <span class="hlt">pressure</span> for this soil increased from 29 dB to 42 dB with the next incidence of <span class="hlt">drops</span> falling on the sample The smallest (and the lowest variability) was for Fluvic Endogleyic Cambisol which had the highest clay fraction. For all experiments the sound <span class="hlt">pressure</span> level ranged from ~27 to ~42 dB and the energy emitted in the form of sound waves was within the range of 0.14 μJ to 5.26 μJ. This was from 0.03 to 1.07% of the energy of the incident <span class="hlt">drops</span>. PMID:27388276</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27388276','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27388276"><span>Sound Wave Energy Resulting from the Impact of Water <span class="hlt">Drops</span> on the Soil Surface.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ryżak, Magdalena; Bieganowski, Andrzej; Korbiel, Tomasz</p> <p>2016-01-01</p> <p>The splashing of water <span class="hlt">drops</span> on a soil surface is the first step of water erosion. There have been many investigations into splashing-most are based on recording and analysing images taken with high-speed cameras, or measuring the mass of the soil moved by splashing. Here, we present a new aspect of the splash phenomenon's characterization the measurement of the sound <span class="hlt">pressure</span> level and the sound energy of the wave that propagates in the <span class="hlt">air</span>. The measurements were carried out for 10 consecutive water <span class="hlt">drop</span> impacts on the soil surface. Three soils were tested (Endogleyic Umbrisol, Fluvic Endogleyic Cambisol and Haplic Chernozem) with four initial moisture levels (<span class="hlt">pressure</span> heads: 0.1 kPa, 1 kPa, 3.16 kPa and 16 kPa). We found that the values of the sound <span class="hlt">pressure</span> and sound wave energy were dependent on the particle size distribution of the soil, less dependent on the initial <span class="hlt">pressure</span> head, and practically the same for subsequent water <span class="hlt">drops</span> (from the first to the tenth <span class="hlt">drop</span>). The highest sound <span class="hlt">pressure</span> level (and the greatest variability) was for Endogleyic Umbrisol, which had the highest sand fraction content. The sound <span class="hlt">pressure</span> for this soil increased from 29 dB to 42 dB with the next incidence of <span class="hlt">drops</span> falling on the sample The smallest (and the lowest variability) was for Fluvic Endogleyic Cambisol which had the highest clay fraction. For all experiments the sound <span class="hlt">pressure</span> level ranged from ~27 to ~42 dB and the energy emitted in the form of sound waves was within the range of 0.14 μJ to 5.26 μJ. This was from 0.03 to 1.07% of the energy of the incident <span class="hlt">drops</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5333141','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5333141"><span>The respective effect of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> of flow fields on the performance of PEM fuel cells</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Wang, Chao; Zhang, Qinglei; Shen, Shuiyun; Yan, Xiaohui; Zhu, Fengjuan; Cheng, Xiaojing; Zhang, Junliang</p> <p>2017-01-01</p> <p>The flow field configuration plays an important role on the performance of proton exchange membrane fuel cells (PEMFCs). For instance, channel/rib width and total channel cross-sectional area determine the under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> respectively, both of which directly influence the water removal, in turn affecting the oxygen supply and cathodic oxygen reduction reaction. In this study, effects of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> on cell performance are investigated experimentally and numerically by adjusting the channel/rib width and channel cross-sectional area of flow fields. The results show that the performance differences with various flow field configurations mainly derive from the oxygen transport resistance which is determined by the water accumulation degree, and the cell performance would benefit from the narrower channels and smaller cross sections. It reveals that at low current densities when water starts to accumulate in GDL at under-rib regions, the under-rib convection plays a more important role in water removal than <span class="hlt">pressure</span> <span class="hlt">drop</span> does; in contrast, at high current densities when water starts to accumulate in channels, the <span class="hlt">pressure</span> <span class="hlt">drop</span> dominates the water removal to facilitate the oxygen transport to the catalyst layer. PMID:28251983</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28251983','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28251983"><span>The respective effect of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> of flow fields on the performance of PEM fuel cells.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wang, Chao; Zhang, Qinglei; Shen, Shuiyun; Yan, Xiaohui; Zhu, Fengjuan; Cheng, Xiaojing; Zhang, Junliang</p> <p>2017-03-02</p> <p>The flow field configuration plays an important role on the performance of proton exchange membrane fuel cells (PEMFCs). For instance, channel/rib width and total channel cross-sectional area determine the under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> respectively, both of which directly influence the water removal, in turn affecting the oxygen supply and cathodic oxygen reduction reaction. In this study, effects of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> on cell performance are investigated experimentally and numerically by adjusting the channel/rib width and channel cross-sectional area of flow fields. The results show that the performance differences with various flow field configurations mainly derive from the oxygen transport resistance which is determined by the water accumulation degree, and the cell performance would benefit from the narrower channels and smaller cross sections. It reveals that at low current densities when water starts to accumulate in GDL at under-rib regions, the under-rib convection plays a more important role in water removal than <span class="hlt">pressure</span> <span class="hlt">drop</span> does; in contrast, at high current densities when water starts to accumulate in channels, the <span class="hlt">pressure</span> <span class="hlt">drop</span> dominates the water removal to facilitate the oxygen transport to the catalyst layer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NatSR...743447W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NatSR...743447W"><span>The respective effect of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> of flow fields on the performance of PEM fuel cells</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Chao; Zhang, Qinglei; Shen, Shuiyun; Yan, Xiaohui; Zhu, Fengjuan; Cheng, Xiaojing; Zhang, Junliang</p> <p>2017-03-01</p> <p>The flow field configuration plays an important role on the performance of proton exchange membrane fuel cells (PEMFCs). For instance, channel/rib width and total channel cross-sectional area determine the under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> respectively, both of which directly influence the water removal, in turn affecting the oxygen supply and cathodic oxygen reduction reaction. In this study, effects of under-rib convection and <span class="hlt">pressure</span> <span class="hlt">drop</span> on cell performance are investigated experimentally and numerically by adjusting the channel/rib width and channel cross-sectional area of flow fields. The results show that the performance differences with various flow field configurations mainly derive from the oxygen transport resistance which is determined by the water accumulation degree, and the cell performance would benefit from the narrower channels and smaller cross sections. It reveals that at low current densities when water starts to accumulate in GDL at under-rib regions, the under-rib convection plays a more important role in water removal than <span class="hlt">pressure</span> <span class="hlt">drop</span> does; in contrast, at high current densities when water starts to accumulate in channels, the <span class="hlt">pressure</span> <span class="hlt">drop</span> dominates the water removal to facilitate the oxygen transport to the catalyst layer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19810000242&hterms=air+bags&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bbags','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19810000242&hterms=air+bags&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bbags"><span><span class="hlt">Air</span> Bag Applies Uniform Bonding <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gillespie, C. A.</p> <p>1982-01-01</p> <p><span class="hlt">Air</span>-bag box applies constant uniform <span class="hlt">pressure</span> to tiles and other objects undergoing adhesive bonding. Box is basically a compliant clamp with adjustable force and position. Can be used on irregular surfaces as well as on flat ones. <span class="hlt">Pressurized</span> <span class="hlt">air</span> is fed to bag through a tube so that it expands, filling the box and pressing against work. Bag adopts a contour that accommodates surface under open side of box.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930081535','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930081535"><span>Aerodynamic heating and the deflection of <span class="hlt">drops</span> by an obstacle in an <span class="hlt">air</span> stream in relation to aircraft icing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kantrowitz, Arthur</p> <p>1940-01-01</p> <p>Two topics of interest to persons attempting to apply the heat method of preventing ice formation on aircraft are considered. Surfaces moving through <span class="hlt">air</span> at high speed are shown, both theoretically and experimentally, to be subject to important aerodynamic heating effects that will materially reduce the heat required to prevent ice. Numerical calculations of the path of water <span class="hlt">drops</span> in an <span class="hlt">air</span> stream around a circular cylinder are given. From these calculations, information is obtained on the percentage of the swept area cleared of <span class="hlt">drops</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDF24003Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDF24003Z"><span>Simultaneous velocity and <span class="hlt">pressure</span> quantification using <span class="hlt">pressure</span>-sensitive flow tracers in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Peng; Peterson, Sean; Porfiri, Maurizio</p> <p>2017-11-01</p> <p>Particle-based measurement techniques for assessing the velocity field of a fluid have advanced rapidly over the past two decades. Full-field <span class="hlt">pressure</span> measurement techniques have remained elusive, however. In this work, we aim to demonstrate the possibility of direct simultaneous planar velocity and <span class="hlt">pressure</span> measurement of a high speed aerodynamic flow by employing novel <span class="hlt">pressure</span>-sensitive tracer particles for particle image velocimetry (PIV). Specifically, the velocity and <span class="hlt">pressure</span> variations of an airflow through a converging-diverging channel are studied. Polystyrene microparticles embedded with a <span class="hlt">pressure</span>-sensitive phosphorescent dye-platinum octaethylporphyrin (PtOEP)-are used as seeding particles. Due to the oxygen quenching effect, the emission lifetime of PtOEP is highly sensitive to the oxygen concentration, that is, the partial <span class="hlt">pressure</span> of oxygen, in the <span class="hlt">air</span>. Since the partial <span class="hlt">pressure</span> of oxygen is linearly proportional to the <span class="hlt">air</span> <span class="hlt">pressure</span>, we can determine the <span class="hlt">air</span> <span class="hlt">pressure</span> through the phosphorescence emission lifetime of the dye. The velocity field is instead obtained using traditional PIV methods. The particles have a <span class="hlt">pressure</span> resolution on the order of 1 kPa, which may be improved by optimizing the particle size and dye concentration to suit specific flow scenarios. This work was supported by the National Science Foundation under Grant Number CBET-1332204.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EGUGA..1610314C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EGUGA..1610314C"><span>Extremely cold events and sudden <span class="hlt">air</span> temperature <span class="hlt">drops</span> during winter season in the Czech Republic</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Crhová, Lenka; Valeriánová, Anna; Holtanová, Eva; Müller, Miloslav; Kašpar, Marek; Stříž, Martin</p> <p>2014-05-01</p> <p>Today a great attention is turned to analysis of extreme weather events and frequency of their occurrence under changing climate. In most cases, these studies are focused on extremely warm events in summer season. However, extremely low values of <span class="hlt">air</span> temperature during winter can have serious impacts on many sectors as well (e.g. power engineering, transportation, industry, agriculture, human health). Therefore, in present contribution we focus on extremely and abnormally cold <span class="hlt">air</span> temperature events in winter season in the Czech Republic. Besides the seasonal extremes of minimum <span class="hlt">air</span> temperature determined from station data, the standardized data with removed annual cycle are used as well. Distribution of extremely cold events over the season and the temporal evolution of frequency of occurrence during the period 1961-2010 are analyzed. Furthermore, the connection of cold events with extreme sudden temperature <span class="hlt">drops</span> is studied. The extreme <span class="hlt">air</span> temperature events and events of extreme sudden temperature <span class="hlt">drop</span> are assessed using the Weather Extremity Index, which evaluates the extremity (based on return periods) and spatial extent of the meteorological extreme event of interest. The generalized extreme value distribution parameters are used to estimate return periods of daily temperature values. The work has been supported by the grant P209/11/1990 funded by the Czech Science Foundation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730008202','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730008202"><span>High-<span class="hlt">pressure</span> combustor exhaust emissions with improved <span class="hlt">air</span>-atomizing and conventional <span class="hlt">pressure</span>-atomizing fuel nozzles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ingebo, R. D.; Norgren, C. T.</p> <p>1973-01-01</p> <p>A high-<span class="hlt">pressure</span> combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by 0.305 meter (6 by 12 in.) was tested with specially designed <span class="hlt">air</span>-atomizing and conventional <span class="hlt">pressure</span>-atomizing fuel nozzles at inlet-<span class="hlt">air</span> temperatures of 340 to 755 k (610 deg to 1360 R), reference velocities of 12.4 to 26.1 meters per second (41 to 86 ft/sec), and fuel-<span class="hlt">air</span> ratios of 0.008 to 0.020. Increasing inlet-<span class="hlt">air</span> <span class="hlt">pressure</span> from 4 to 20 atmospheres generally increased smoke number and nitric oxide, but decreased carbon monoxide and unburned hydrocarbon concentrations with <span class="hlt">air</span>-atomizing and <span class="hlt">pressure</span>-atomizing nozzles. Emission indexes for carbon monoxide and unburned hydrocarbons were lower at 4, 10, and 20 atmospheres, and nitric oxide emission indexes were lower at 10 and 20 atmospheres with <span class="hlt">air</span>-atomizing than with <span class="hlt">pressure</span>-atomizing nozzles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JPhCS.656a2067D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JPhCS.656a2067D"><span>Numerical investigation of cavitation flow inside spool valve with large <span class="hlt">pressure</span> <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Deng, Jian; Pan, Dingyi; Xie, Fangfang; Shao, Xueming</p> <p>2015-12-01</p> <p>Spool valves play an important role in fluid power system. Cavitation phenomena happen frequently inside the spool valves, which cause structure damages, noise and lower down hydrodynamic performance. A numerical tools incorporating the cavitation model, are developed to predict the flow structure and cavitation pattern in the spool valve. Two major flow states in the spool valve chamber, i.e. flow-in and flow-out, are studies. The <span class="hlt">pressure</span> distributions along the spool wall are first investigated, and the results agree well with the experimental data. For the flow-in cases, the local <span class="hlt">pressure</span> at the throttling area <span class="hlt">drops</span> much deeper than the <span class="hlt">pressure</span> in flow-out cases. Meanwhile, the bubbles are more stable in flow-in cases than those in flow-out cases, which are ruptured and shed into the downstream.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999JGR...10422067W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999JGR...10422067W"><span><span class="hlt">Pressure</span> at the ground in a large tornado</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Winn, W. P.; Hunyady, S. J.; Aulich, G. D.</p> <p>1999-09-01</p> <p>A number of instruments were placed on the ground across the path of a large tornado that passed west of the town of Allison, Texas, on June 8, 1995. The center of the tornado came within 660 m of the closest instrument, which recorded a <span class="hlt">pressure</span> <span class="hlt">drop</span> of 55 mbar and a subsequent <span class="hlt">pressure</span> rise of 60 mbar. During the lowest recorded <span class="hlt">pressures</span> (near r = 660 m), there were large and rapid <span class="hlt">pressure</span> fluctuations; the largest fluctuation was a 10-mbar spike lasting 2 s. A second instrument on the opposite side of the tornado recorded a <span class="hlt">pressure</span> <span class="hlt">drop</span> of 26 mbar. From the <span class="hlt">pressure</span> variations with time P(t) at the two instruments, the variation of <span class="hlt">pressure</span> with distance p(r) from the center of the tornado has been deduced for r>660 m. As r decreases, the measured <span class="hlt">pressure</span> function p(r) <span class="hlt">drops</span> more abruptly than would be expected from conservation of angular momentum of <span class="hlt">air</span> spiraling inward near the ground level.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013PhDT.......143F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013PhDT.......143F"><span>Effect of aviation fuel type and fuel injection conditions on the spray characteristics of <span class="hlt">pressure</span> swirl and hybrid <span class="hlt">air</span> blast fuel injectors</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Feddema, Rick</p> <p></p> <p>Feddema, Rick T. M.S.M.E., Purdue University, December 2013. Effect of Aviation Fuel Type and Fuel Injection Conditions on the Spray Characteristics of <span class="hlt">Pressure</span> Swirl and Hybrid <span class="hlt">Air</span> Blast Fuel Injectors. Major Professor: Dr. Paul E. Sojka, School of Mechanical Engineering Spray performance of <span class="hlt">pressure</span> swirl and hybrid <span class="hlt">air</span> blast fuel injectors are central to combustion stability, combustor heat management, and pollutant formation in aviation gas turbine engines. Next generation aviation gas turbine engines will optimize spray atomization characteristics of the fuel injector in order to achieve engine efficiency and emissions requirements. Fuel injector spray atomization performance is affected by the type of fuel injector, fuel liquid properties, fuel injection <span class="hlt">pressure</span>, fuel injection temperature, and ambient <span class="hlt">pressure</span>. Performance of <span class="hlt">pressure</span> swirl atomizer and hybrid <span class="hlt">air</span> blast nozzle type fuel injectors are compared in this study. Aviation jet fuels, JP-8, Jet A, JP-5, and JP-10 and their effect on fuel injector performance is investigated. Fuel injector set conditions involving fuel injector <span class="hlt">pressure</span>, fuel temperature and ambient <span class="hlt">pressure</span> are varied in order to compare each fuel type. One objective of this thesis is to contribute spray patternation measurements to the body of existing <span class="hlt">drop</span> size data in the literature. Fuel droplet size tends to increase with decreasing fuel injection <span class="hlt">pressure</span>, decreasing fuel injection temperature and increasing ambient injection <span class="hlt">pressure</span>. The differences between fuel types at particular set conditions occur due to differences in liquid properties between fuels. Liquid viscosity and surface tension are identified to be fuel-specific properties that affect the <span class="hlt">drop</span> size of the fuel. An open aspect of current research that this paper addresses is how much the type of aviation jet fuel affects spray atomization characteristics. Conventional aviation fuel specifications are becoming more important with new interest in alternative</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840022154','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840022154"><span>Atomization of liquid sheets in high <span class="hlt">pressure</span> airflow</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ingebo, R. D.</p> <p>1984-01-01</p> <p>An investigation of liquid sheet atomization is made with combustor simulated inlet <span class="hlt">air</span> <span class="hlt">pressures</span> varied from 0.10 to 2.1 MPa. Mean <span class="hlt">drop</span> diameters are measured with an improved scanning radiometer and correlated with the liquid and <span class="hlt">air</span> stream Reynolds numbers, RE(1) and RE(A) and the airstream <span class="hlt">pressure</span> sensitive group GC(2). These data are used in the modeling of the combustion process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22552108','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22552108"><span><span class="hlt">Pressure</span> ulcer incidence and progression in critically ill subjects: influence of low <span class="hlt">air</span> loss mattress versus a powered <span class="hlt">air</span> <span class="hlt">pressure</span> redistribution mattress.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Black, Joyce; Berke, Christine; Urzendowski, Gail</p> <p>2012-01-01</p> <p>The primary objective of this study was to compare facility-acquired <span class="hlt">pressure</span> ulcer incidence and progression of <span class="hlt">pressure</span> ulcers present on admission in critically ill patients, using 2 different support surfaces. We completed a comparison cohort study in a surgical intensive care unit (ICU). The study setting was a 12-bed cardiovascular ICU in a university-based hospital in the Midwestern United States. The sample comprised 52 critically ill patients; 31 were placed on low <span class="hlt">air</span> loss weight-based <span class="hlt">pressure</span> redistribution-microclimate management system beds and 21 were placed on integrated powered <span class="hlt">air</span> <span class="hlt">pressure</span> redistribution beds. Prior to the start of the study, 5 low airloss beds were placed in open rooms in the cardiovascular surgical ICU. Inclusion criteria were anticipated ICU stay of 3 days, and patients did not receive a speciality bed for pulmonary or wound issues. Initial assessment of the patients included risk assessment and prior events that would increase risk for <span class="hlt">pressure</span> ulcer development such as extended time in operating room, along with skin assessment for existing <span class="hlt">pressure</span> ulcers. Subjects in both groups had ongoing skin assessment every 3 to 4 days and a subjective evaluation of heel elevation and turning or repositioning by the researcher. Data were collected until the subjects were dismissed from the ICU. Patients admitted to the unit were assigned to open rooms following the usual protocols. The mean length of stay was 7.0 days, with an 8.1-day length of stay for subjects on "low <span class="hlt">air</span> loss with microclimate management" beds (LAL-MCM) and 6.6 days on the integrated power <span class="hlt">pressure</span> <span class="hlt">air</span> redistribution (IP-AR) beds (P = NS). The incidence of <span class="hlt">pressure</span> ulcers on the buttocks, sacrum, or coccyx was 0% (0/31) on the low <span class="hlt">air</span> loss bed and 18% (4/21) on the IP-AR bed (P = .046). Five subjects had 6 <span class="hlt">pressure</span> ulcers on admission. Two <span class="hlt">pressure</span> ulcers on 2 patients worsened on the integrated power <span class="hlt">air</span> redistribution beds, which required specialty bed rental</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930089515','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930089515"><span>A Balanced-<span class="hlt">pressure</span> Sliding Seal for Transfer of <span class="hlt">Pressurized</span> <span class="hlt">Air</span> Between Stationary and Rotating Parts</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Curren, Arthur N; Cochran, Reeves P</p> <p>1957-01-01</p> <p>A combination sliding-ring and <span class="hlt">pressure</span>-balancing seal capable of transferring <span class="hlt">pressurize</span> <span class="hlt">air</span> from stationary to rotating parts was developed and experimentally investigated at sliding velocities and cooling-<span class="hlt">air</span> <span class="hlt">pressures</span> up to 10,000 feet per minute and 38.3 pounds per square inch absolute, respectively. Leakage of cooling <span class="hlt">air</span> was completely eliminated with an expenditure of balance <span class="hlt">air</span> less than one-fourth the leakage loss of <span class="hlt">air</span> from labyrinth seals under the same conditions. Additional cooling of the carbon-base seal rings was required, and the maximum wear rate on the rings was about 0.0005 inch per hour.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018Metro..55S..52S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018Metro..55S..52S"><span>Development of a primary standard for dynamic <span class="hlt">pressure</span> based on <span class="hlt">drop</span> weight method covering a range of 10 MPa-400 MPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Salminen, J.; Högström, R.; Saxholm, S.; Lakka, A.; Riski, K.; Heinonen, M.</p> <p>2018-04-01</p> <p>In this paper we present the development of a primary standard for dynamic <span class="hlt">pressures</span> that is based on the <span class="hlt">drop</span> weight method. At the moment dynamic <span class="hlt">pressure</span> transducers are typically calibrated using reference transducers, which are calibrated against static <span class="hlt">pressure</span> standards. Because dynamic and static characteristics of <span class="hlt">pressure</span> transducers may significantly differ from each other, it is important that these transducers are calibrated against dynamic <span class="hlt">pressure</span> standards. In a method developed in VTT Technical Research Centre of Finland Ltd, Centre for Metrology MIKES, a <span class="hlt">pressure</span> pulse is generated by impact between a <span class="hlt">dropping</span> weight and a piston of a liquid-filled piston-cylinder assembly. The traceability to SI-units is realized through interferometric measurement of the acceleration of the <span class="hlt">dropping</span> weight during impact, the effective area of the piston-cylinder assembly and the mass of the weight. Based on experimental validation and an uncertainty evaluation, the developed primary standard provides traceability for peak <span class="hlt">pressures</span> in the range from 10 MPa to 400 MPa with a few millisecond pulse width and a typical relative expanded uncertainty (k  =  2) of 1.5%. The performance of the primary standard is demonstrated by test calibrations of two dynamic <span class="hlt">pressure</span> transducers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23727922','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23727922"><span>Reduction of enhanced rabbit intraocular <span class="hlt">pressure</span> by instillation of pyroglutamic acid eye <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ito, Yoshimasa; Nagai, Noriaki; Okamoto, Norio; Shimomura, Yoshikazu; Nakanishi, Kunio; Tanaka, Ryuichiro</p> <p>2013-01-01</p> <p>L-Pyroglutamic acid (PGA) is an endogenous molecule derived from l-glutamate. We demonstrate the effects of PGA on intraocular <span class="hlt">pressure</span> (IOP) in experimentally induced ocular hypertension in rabbits. In the in vitro and in vivo transcorneal penetration studies, the PGA solution (PGA in saline) did not penetrate the rabbit cornea. On the other hand, the penetration of PGA was improved by the addition of zinc chloride and 2-hydroxypropyl-β-cyclodextrin (HPCD), and PGA penetration was enhanced with increasing HPCD concentration. Therefore, PGA solutions containing 0.5% zinc chloride and 5% or 10% HPCD (PGA/HPCD(5% or 10%) eye <span class="hlt">drops</span>) were used to investigate the effects for IOP in this study. An elevation in IOP was induced by the rapid infusion of 5% glucose solution (15 mL/kg of body weight) through the marginal ear vein or maintaining under dark phase for 5 h. In the both models, the induced elevation in IOP was prevented by the instillation of PGA/HPCD eye <span class="hlt">drops</span>, and the IOP-reducing effect enhanced with increasing HPCD concentration in the <span class="hlt">drops</span>. Nitric oxide (NO) levels elevated in the aqueous humor following the infusion of 5% glucose solution, and this increase was also suppressed by the instillation of PGA/HPCD eye <span class="hlt">drops</span>. In conclusion, the present study demonstrates that the instillation of PGA/HPCD eye <span class="hlt">drops</span> has an IOP-reducing effect in rabbits with experimentally induced ocular hypertension, probably as a result of the suppression of NO production.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940019170','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940019170"><span>Prediction of <span class="hlt">pressure</span> <span class="hlt">drop</span> in fluid tuned mounts using analytical and computational techniques</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lasher, William C.; Khalilollahi, Amir; Mischler, John; Uhric, Tom</p> <p>1993-01-01</p> <p>A simplified model for predicting <span class="hlt">pressure</span> <span class="hlt">drop</span> in fluid tuned isolator mounts was developed. The model is based on an exact solution to the Navier-Stokes equations and was made more general through the use of empirical coefficients. The values of these coefficients were determined by numerical simulation of the flow using the commercial computational fluid dynamics (CFD) package FIDAP.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhyE...97..155H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhyE...97..155H"><span>Convective heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of aqua based TiO2 nanofluids at different diameters of nanoparticles: Data analysis and modeling with artificial neural network</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hemmat Esfe, Mohammad; Nadooshan, Afshin Ahmadi; Arshi, Ali; Alirezaie, Ali</p> <p>2018-03-01</p> <p>In this study, experimental data related to the Nusselt number and <span class="hlt">pressure</span> <span class="hlt">drop</span> of aqueous nanofluids of Titania is modeled and estimated by using ANN with 2 hidden layers and 8 neurons in each layer. Also in this study the effect of various effective variables in the Nusselt number and <span class="hlt">pressure</span> <span class="hlt">drop</span> is surveyed. This study indicated that the neural network modeling has been able to model experimental data with great accuracy. The modeling regression coefficient for the data of Nusselt number and relative <span class="hlt">pressure</span> <span class="hlt">drop</span> is 99.94% and 99.97% respectively. Besides, it represented that the increment of the Reynolds number and concentration made the increment of Nusselt number and <span class="hlt">pressure</span> <span class="hlt">drop</span> of aqueous nanofluid.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_8 --> <div id="page_9" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="161"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24398394','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24398394"><span>In vitro estimation of <span class="hlt">pressure</span> <span class="hlt">drop</span> across tracheal tubes during high-frequency percussive ventilation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ajčević, M; Lucangelo, U; Ferluga, M; Zin, W A; Accardo, A</p> <p>2014-02-01</p> <p>Tracheal tubes (TT) are used in clinical practice to connect an artificial ventilator to the patient's airways. It is important to know the <span class="hlt">pressure</span> used to overcome tube impedance to avoid lung injury. Although high-frequency percussive ventilation (HFPV) has been increasingly used, the mechanical behavior of TT under HFPV has not yet been described. Thus, we aimed at characterizing in vitro the <span class="hlt">pressure</span> <span class="hlt">drop</span> across TT (ΔPTT) by identifying the model that best fits the measured <span class="hlt">pressure</span>-flow (P-V̇) relationships during HFPV under different working <span class="hlt">pressures</span> (PWork), percussive frequencies and mechanical loads. Three simple models relating ΔPTT and flow (V̇) were tested. Model 1 is characterized by linear resistive [Rtube ⋅ V̇(t)] and inertial [I · V̈(t)] terms. Model 2 takes into consideration Rohrer's approach [K1· V̇(t) + K2 ⋅V̇(t)] and inertance [I ·V̈(t)]. In model 3 the <span class="hlt">pressure</span> <span class="hlt">drop</span> caused by friction is represented by the non-linear Blasius component [Kb· V̇(1.75)(t)] and the inertial term [I· V̈(t)]. Model 1 presented a significantly higher root mean square error of approximation than models 2 and 3, which were similar. Thus, model 1 was not as accurate as the latter, possibly due to turbulence. Model 3 presented the most robust resistance-related coefficient. Estimated inertances did not vary among the models using the same tube. In conclusion, in HFPV ΔPTT can be easily calculated by the physician using model 3.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPA....7h5017Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPA....7h5017Z"><span>Investigating performance of microchannel evaporators for automobile <span class="hlt">air</span> conditioning with different port structures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhou, Guoliang; Su, Lin; Cheng, Qia; Wu, Longbing</p> <p>2017-08-01</p> <p>Microchannel evaporator has been widely applied in automobile <span class="hlt">air</span> conditioning, while it faces the problem of refrigerant maldistribution which deteriorates the thermal performance of evaporator. In this study, the performances of microchannel evaporators with different port structures are experimentally investigated for purpose of reducing evaporator <span class="hlt">pressure</span> <span class="hlt">drop</span>. Four evaporator samples with different port number and hydraulic diameter are made for this study. The performances of the evaporator samples are tested on a psychometric calorimeter test bench with the refrigerant R-134A at a real automobile <span class="hlt">air</span> conditioning. The results on the variations of the evaporator <span class="hlt">pressure</span> <span class="hlt">drop</span> and evaporator surface temperature distribution are presented and analyzed. By studying the performance of an evaporator, seeking proper port structure is an approach to reduce refrigerant <span class="hlt">pressure</span> <span class="hlt">drop</span> as well as improve refrigerant distribution.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3913518','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3913518"><span>Experimental Study on the Flow Regimes and <span class="hlt">Pressure</span> Gradients of <span class="hlt">Air</span>-Oil-Water Three-Phase Flow in Horizontal Pipes</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Al-Hadhrami, Luai M.; Shaahid, S. M.; Tunde, Lukman O.; Al-Sarkhi, A.</p> <p>2014-01-01</p> <p>An experimental investigation has been carried out to study the flow regimes and <span class="hlt">pressure</span> gradients of <span class="hlt">air</span>-oil-water three-phase flows in 2.25 ID horizontal pipe at different flow conditions. The effects of water cuts, liquid and gas velocities on flow patterns and <span class="hlt">pressure</span> gradients have been studied. The experiments have been conducted at 20°C using low viscosity Safrasol D80 oil, tap water and <span class="hlt">air</span>. Superficial water and oil velocities were varied from 0.3 m/s to 3 m/s and <span class="hlt">air</span> velocity varied from 0.29 m/s to 52.5 m/s to cover wide range of flow patterns. The experiments were performed for 10% to 90% water cuts. The flow patterns were observed and recorded using high speed video camera while the <span class="hlt">pressure</span> <span class="hlt">drops</span> were measured using <span class="hlt">pressure</span> transducers and U-tube manometers. The flow patterns show strong dependence on water fraction, gas velocities, and liquid velocities. The observed flow patterns are stratified (smooth and wavy), elongated bubble, slug, dispersed bubble, and annular flow patterns. The <span class="hlt">pressure</span> gradients have been found to increase with the increase in gas flow rates. Also, for a given superficial gas velocity, the <span class="hlt">pressure</span> gradients increased with the increase in the superficial liquid velocity. The <span class="hlt">pressure</span> gradient first increases and then decreases with increasing water cut. In general, phase inversion was observed with increase in the water cut. The experimental results have been compared with the existing unified Model and a good agreement has been noticed. PMID:24523645</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24523645','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24523645"><span>Experimental study on the flow regimes and <span class="hlt">pressure</span> gradients of <span class="hlt">air</span>-oil-water three-phase flow in horizontal pipes.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Al-Hadhrami, Luai M; Shaahid, S M; Tunde, Lukman O; Al-Sarkhi, A</p> <p>2014-01-01</p> <p>An experimental investigation has been carried out to study the flow regimes and <span class="hlt">pressure</span> gradients of <span class="hlt">air</span>-oil-water three-phase flows in 2.25 ID horizontal pipe at different flow conditions. The effects of water cuts, liquid and gas velocities on flow patterns and <span class="hlt">pressure</span> gradients have been studied. The experiments have been conducted at 20 °C using low viscosity Safrasol D80 oil, tap water and <span class="hlt">air</span>. Superficial water and oil velocities were varied from 0.3 m/s to 3 m/s and <span class="hlt">air</span> velocity varied from 0.29 m/s to 52.5 m/s to cover wide range of flow patterns. The experiments were performed for 10% to 90% water cuts. The flow patterns were observed and recorded using high speed video camera while the <span class="hlt">pressure</span> <span class="hlt">drops</span> were measured using <span class="hlt">pressure</span> transducers and U-tube manometers. The flow patterns show strong dependence on water fraction, gas velocities, and liquid velocities. The observed flow patterns are stratified (smooth and wavy), elongated bubble, slug, dispersed bubble, and annular flow patterns. The <span class="hlt">pressure</span> gradients have been found to increase with the increase in gas flow rates. Also, for a given superficial gas velocity, the <span class="hlt">pressure</span> gradients increased with the increase in the superficial liquid velocity. The <span class="hlt">pressure</span> gradient first increases and then decreases with increasing water cut. In general, phase inversion was observed with increase in the water cut. The experimental results have been compared with the existing unified Model and a good agreement has been noticed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19162923','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19162923"><span>The impact of wall shear stress and <span class="hlt">pressure</span> <span class="hlt">drop</span> on the stability of the atherosclerotic plaque.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Li, Zhi-Yong; Taviani, Valentina; Gillard, Jonathan H</p> <p>2008-01-01</p> <p>Rupture of vulnerable atheromatous plaque in the carotid and coronary arteries often leads to stroke and heart attack respectively. The mechanism of blood flow and plaque rupture in stenotic arteries is still not fully understood. A three dimensional rigid wall model was solved under steady state conditions and unsteady conditions by assuming a time-varying inlet velocity profile to investigate the relative importance of axial forces and <span class="hlt">pressure</span> <span class="hlt">drops</span> in arteries with asymmetric stenosis. Flow-structure interactions were investigated for the same geometry and the results were compared with those retrieved with the corresponding 2D cross-section structural models. The Navier-Stokes equations were used as the governing equations for the fluid. The tube wall was assumed hyperelastic, homogeneous, isotropic and incompressible. The analysis showed that the three dimensional behavior of velocity, <span class="hlt">pressure</span> and wall shear stress is in general very different from that predicted by cross-section models. <span class="hlt">Pressure</span> <span class="hlt">drop</span> across the stenosis was found to be much higher than shear stress. Therefore, <span class="hlt">pressure</span> may be the more important mechanical trigger for plaque rupture other than shear stress, although shear stress is closely related to plaque formation and progression.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1915734M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1915734M"><span>Investigation of the spatial variability and possible origins of wind-induced <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations responsible for <span class="hlt">pressure</span> pumping</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mohr, Manuel; Laemmel, Thomas; Maier, Martin; Zeeman, Matthias; Longdoz, Bernard; Schindler, Dirk</p> <p>2017-04-01</p> <p>The exchange of greenhouse gases between the soil and the atmosphere is highly relevant for the climate of the Earth. Recent research suggests that wind-induced <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations can alter the soil gas transport and therefore soil gas efflux significantly. Using a newly developed method, we measured soil gas transport in situ in a well aerated forest soil. Results from these measurements showed that the commonly used soil gas diffusion coefficient is enhanced up to 30% during periods of strong wind-induced <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations. The <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations above the forest floor are only induced at high above-canopy wind speeds (> 5 m s-1) and lie in the frequency range 0.01-0.1 Hz. Moreover, the amplitudes of <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations in this frequency range show a clear quadratic dependence on mean above-canopy wind speed. However, the origin of these wind-induced <span class="hlt">pressure</span> fluctuations is still unclear. Airflow measurements and high-precision <span class="hlt">air</span> <span class="hlt">pressure</span> measurements were conducted at three different vegetation-covered sites (conifer forest, deciduous forest, grassland) to investigate the spatial variability of dominant <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations, their origin and vegetation-dependent characteristics. At the conifer forest site, a vertical profile of <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations was measured and an array consisting of five <span class="hlt">pressure</span> sensors were installed at the forest floor. At the grassland site, the <span class="hlt">air</span> <span class="hlt">pressure</span> measurements were compared with wind observations made by ground-based LIDAR and spatial temperature observations from a fibre-optic sensing network (ScaleX Campaign 2016). Preliminary results show that at all sites the amplitudes of relevant <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations increase with increasing wind speed. Data from the array measurements reveal that there are no time lags between the <span class="hlt">air</span> <span class="hlt">pressure</span> signals of different heights, but a time lag existed between the <span class="hlt">air</span> <span class="hlt">pressure</span> signals of the sensors distributed laterally on the forest floor</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title21-vol8/pdf/CFR-2013-title21-vol8-sec880-5550.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title21-vol8/pdf/CFR-2013-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2013-04-01 2013-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title21-vol8/pdf/CFR-2010-title21-vol8-sec880-5550.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title21-vol8/pdf/CFR-2010-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2010-04-01 2010-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title21-vol8/pdf/CFR-2014-title21-vol8-sec880-5550.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title21-vol8/pdf/CFR-2014-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2014-04-01 2014-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title21-vol8/pdf/CFR-2011-title21-vol8-sec880-5550.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title21-vol8/pdf/CFR-2011-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2011-04-01 2011-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title21-vol8/pdf/CFR-2012-title21-vol8-sec880-5550.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title21-vol8/pdf/CFR-2012-title21-vol8-sec880-5550.pdf"><span>21 CFR 880.5550 - Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-04-01</p> <p>... body <span class="hlt">pressure</span>. The device is used to prevent and treat decubitus ulcers (bed sores). (b) Classification... 21 Food and Drugs 8 2012-04-01 2012-04-01 false Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. 880... Personal Use Therapeutic Devices § 880.5550 Alternating <span class="hlt">pressure</span> <span class="hlt">air</span> flotation mattress. (a) Identification...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27706831','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27706831"><span>Evaluation of browning ratio in an image analysis of apple slices at different stages of instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span>-assisted hot-<span class="hlt">air</span> drying (AD-DIC).</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Gao, Kun; Zhou, Linyan; Bi, Jinfeng; Yi, Jianyong; Wu, Xinye; Zhou, Mo; Wang, Xueyuan; Liu, Xuan</p> <p>2017-06-01</p> <p>Computer vision-based image analysis systems are widely used in food processing to evaluate quality changes. They are able to objectively measure the surface colour of various products since, providing some obvious advantages with their objectivity and quantitative capabilities. In this study, a computer vision-based image analysis system was used to investigate the colour changes of apple slices dried by instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span>-assisted hot <span class="hlt">air</span> drying (AD-DIC). The CIE L* value and polyphenol oxidase activity in apple slices decreased during the entire drying process, whereas other colour indexes, including CIE a*, b*, ΔE and C* values, increased. The browning ratio calculated by image analysis increased during the drying process, and a sharp increment was observed for the DIC process. The change in 5-hydroxymethylfurfural (5-HMF) and fluorescent compounds (FIC) showed the same trend with browning ratio due to Maillard reaction. Moreover, the concentrations of 5-HMF and FIC both had a good quadratic correlation (R 2  > 0.998) with the browning ratio. Browning ratio was a reliable indicator of 5-HMF and FIC changes in apple slices during drying. The image analysis system could be used to monitor colour changes, 5-HMF and FIC in dehydrated apple slices during the AD-DIC process. © 2016 Society of Chemical Industry. © 2016 Society of Chemical Industry.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860004208','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860004208"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> performance of a finned-tube heat exchanger proposed for use in the NASA Lewis Altitude Wind Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Vanfossen, G. J.</p> <p>1985-01-01</p> <p>A segment of the heat exchanger proposed for use in the NASA Lewis Altitude Wind Tunnel (AWT) facility has been tested under dry and icing conditions. The heat exchanger has the largest <span class="hlt">pressure</span> <span class="hlt">drop</span> of any component in the AWT loop. It is therefore critical that its performance be known at all conditions before the final design of the AWT is complete. The heat exchanger segment is tested in the NASA Lewis Icing Research Tunnel (IRT) in order to provide an icing cloud environment similar to what will be encountered in the AWT. Dry heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> data are obtained and compared to correlations available in the literature. The effects of icing sprays on heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> are also investigated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25945543','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25945543"><span>Bioinspired <span class="hlt">air</span>-retaining nanofur for drag reduction.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kavalenka, Maryna N; Vüllers, Felix; Lischker, Simone; Zeiger, Claudia; Hopf, Andreas; Röhrig, Michael; Rapp, Bastian E; Worgull, Matthias; Hölscher, Hendrik</p> <p>2015-05-27</p> <p>Bioinspired nanofur, covered by a dense layer of randomly distributed high aspect ratio nano- and microhairs, possesses superhydrophobic and <span class="hlt">air</span>-retaining properties. Nanofur is fabricated using a highly scalable hot pulling method in which softened polymer is elongated with a heated sandblasted plate. Here we investigate the stability of the underwater <span class="hlt">air</span> layer retained by the irregular nanofur topography by applying hydraulic <span class="hlt">pressure</span> to the nanofur kept underwater, and evaluate the gradual changes in the <span class="hlt">air</span>-covered area. Furthermore, the drag reduction resulting from the nanofur <span class="hlt">air</span> retention is characterized by measuring the <span class="hlt">pressure</span> <span class="hlt">drop</span> across channels with and without nanofur.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007ApPhL..90t4104X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007ApPhL..90t4104X"><span>Sound field inside acoustically levitated spherical <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xie, W. J.; Wei, B.</p> <p>2007-05-01</p> <p>The sound field inside an acoustically levitated small spherical water <span class="hlt">drop</span> (radius of 1mm) is studied under different incident sound <span class="hlt">pressures</span> (amplitude p0=2735-5643Pa). The transmitted <span class="hlt">pressure</span> ptr in the <span class="hlt">drop</span> 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 <span class="hlt">drop</span>. Whereas the secondary maximum appears at the uppermost point if the incident <span class="hlt">pressure</span> amplitude p0 is higher than an intermediate value (3044Pa), in which there exists a <span class="hlt">pressure</span> nodal surface in the <span class="hlt">drop</span> 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 <span class="hlt">pressures</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air&pg=4&id=EJ920071','ERIC'); return false;" href="https://eric.ed.gov/?q=air&pg=4&id=EJ920071"><span>One-Component <span class="hlt">Pressure</span>-Temperature Phase Diagrams in the Presence of <span class="hlt">Air</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Andrade-Gamboa, Julio; Martire, Daniel O.; Donati, Edgardo R.</p> <p>2010-01-01</p> <p>One-component phase diagrams are good approximations to predict <span class="hlt">pressure</span>-temperature ("P-T") behavior of a substance in the presence of <span class="hlt">air</span>, provided <span class="hlt">air</span> <span class="hlt">pressure</span> is not much higher than the vapor <span class="hlt">pressure</span>. However, at any <span class="hlt">air</span> <span class="hlt">pressure</span>, and from the conceptual point of view, the use of a traditional "P-T" phase diagram is not strictly correct. In…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1027616','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1027616"><span>Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span> and Saline Filled Cuffs</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2017-01-31</p> <p>AFRL-SA-WP-SR-2017-0004 Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span>- and Saline -Filled...Correlation Between Endotracheal Tube Cuff <span class="hlt">Pressure</span> and Tracheal Wall <span class="hlt">Pressure</span> Using <span class="hlt">Air</span>- and Saline -Filled Cuffs 5a. CONTRACT NUMBER FA8650-14...descending from altitude. When using saline in the ETT cuff, TW <span class="hlt">pressure</span> differences with the 7.5 high-volume, low-<span class="hlt">pressure</span> cuff and 8.0 TaperGuard</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28054663','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28054663"><span>Thermal separation of soil particles from thermal conductivity measurement under various <span class="hlt">air</span> <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lu, Sen; Ren, Tusheng; Lu, Yili; Meng, Ping; Zhang, Jinsong</p> <p>2017-01-05</p> <p>The thermal conductivity of dry soils is related closely to <span class="hlt">air</span> <span class="hlt">pressure</span> and the contact areas between solid particles. In this study, the thermal conductivity of two-phase soil systems was determined under reduced and increased <span class="hlt">air</span> <span class="hlt">pressures</span>. The thermal separation of soil particles, i.e., the characteristic dimension of the pore space (d), was then estimated based on the relationship between soil thermal conductivity and <span class="hlt">air</span> <span class="hlt">pressure</span>. Results showed that under both reduced and increased <span class="hlt">air</span> <span class="hlt">pressures</span>, d estimations were significantly larger than the geometrical mean separation of solid particles (D), which suggested that conductive heat transfer through solid particles dominated heat transfer in dry soils. The increased <span class="hlt">air</span> <span class="hlt">pressure</span> approach gave d values lower than that of the reduced <span class="hlt">air</span> <span class="hlt">pressure</span> method. With increasing <span class="hlt">air</span> <span class="hlt">pressure</span>, more collisions between gas molecules and solid surface occurred in micro-pores and intra-aggregate pores due to the reduction of mean free path of <span class="hlt">air</span> molecules. Compared to the reduced <span class="hlt">air</span> <span class="hlt">pressure</span> approach, the increased <span class="hlt">air</span> <span class="hlt">pressure</span> approach expressed more micro-pore structure attributes in heat transfer. We concluded that measuring thermal conductivity under increased <span class="hlt">air</span> <span class="hlt">pressure</span> procedures gave better-quality d values, and improved soil micro-pore structure estimation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1174722','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/1174722"><span><span class="hlt">Pressurized</span> solid oxide fuel cell integral <span class="hlt">air</span> accumular containment</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Gillett, James E.; Zafred, Paolo R.; Basel, Richard A.</p> <p>2004-02-10</p> <p>A fuel cell generator apparatus contains at least one fuel cell subassembly module in a module housing, where the housing is surrounded by a <span class="hlt">pressure</span> vessel such that there is an <span class="hlt">air</span> accumulator space, where the apparatus is associated with an <span class="hlt">air</span> compressor of a turbine/generator/<span class="hlt">air</span> compressor system, where <span class="hlt">pressurized</span> <span class="hlt">air</span> from the compressor passes into the space and occupies the space and then flows to the fuel cells in the subassembly module, where the <span class="hlt">air</span> accumulation space provides an accumulator to control any unreacted fuel gas that might flow from the module.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19750047374&hterms=oil+drilling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Doil%2Bdrilling','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19750047374&hterms=oil+drilling&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Doil%2Bdrilling"><span>Underground storage systems for high-<span class="hlt">pressure</span> <span class="hlt">air</span> and gases</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Beam, B. H.; Giovannetti, A.</p> <p>1975-01-01</p> <p>This paper is a discussion of the safety and cost of underground high-<span class="hlt">pressure</span> <span class="hlt">air</span> and gas storage systems based on recent experience with a high-<span class="hlt">pressure</span> <span class="hlt">air</span> system installed at Moffett Field, California. The system described used threaded and coupled oil well casings installed vertically to a depth of 1200 ft. Maximum <span class="hlt">pressure</span> was 3000 psi and capacity was 500,000 lb of <span class="hlt">air</span>. A failure mode analysis is presented, and it is shown that underground storage offers advantages in avoiding catastrophic consequences from <span class="hlt">pressure</span> vessel failure. Certain problems such as corrosion, fatigue, and electrolysis are discussed in terms of the economic life of such vessels. A cost analysis shows that where favorable drilling conditions exist, the cost of underground high-<span class="hlt">pressure</span> storage is approximately one-quarter that of equivalent aboveground storage.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_9 --> <div id="page_10" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="181"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/865745','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/865745"><span><span class="hlt">Air</span> separation with temperature and <span class="hlt">pressure</span> swing</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Cassano, Anthony A.</p> <p>1986-01-01</p> <p>A chemical absorbent <span class="hlt">air</span> separation process is set forth which uses a temperature swing absorption-desorption cycle in combination with a <span class="hlt">pressure</span> swing wherein the <span class="hlt">pressure</span> is elevated in the desorption stage of the process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19818553','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19818553"><span>Temperature and <span class="hlt">pressure</span> influence on explosion <span class="hlt">pressures</span> of closed vessel propane-<span class="hlt">air</span> deflagrations.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razus, Domnina; Brinzea, Venera; Mitu, Maria; Oancea, Dumitru</p> <p>2010-02-15</p> <p>An experimental study on <span class="hlt">pressure</span> evolution during closed vessel explosions of propane-<span class="hlt">air</span> mixtures was performed, for systems with various initial concentrations and <span class="hlt">pressures</span> ([C(3)H(8)]=2.50-6.20 vol.%, p(0)=0.3-1.2 bar). The explosion <span class="hlt">pressures</span> and explosion times were measured in a spherical vessel (Phi=10 cm), at various initial temperatures (T(0)=298-423 K) and in a cylindrical vessel (Phi=10 cm; h=15 cm), at ambient initial temperature. The experimental values of explosion <span class="hlt">pressures</span> are examined against literature values and compared to adiabatic explosion <span class="hlt">pressures</span>, computed by assuming chemical equilibrium within the flame front. The influence of initial <span class="hlt">pressure</span>, initial temperature and fuel concentration on explosion <span class="hlt">pressures</span> and explosion times are discussed. At constant temperature and fuel/oxygen ratio, the explosion <span class="hlt">pressures</span> are linear functions of total initial <span class="hlt">pressure</span>, as reported for other fuel-<span class="hlt">air</span> mixtures. At constant initial <span class="hlt">pressure</span> and composition, both the measured and calculated (adiabatic) explosion <span class="hlt">pressures</span> are linear functions of reciprocal value of initial temperature. Such correlations are extremely useful for predicting the explosion <span class="hlt">pressures</span> of flammable mixtures at elevated temperatures and/or <span class="hlt">pressures</span>, when direct measurements are not available.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JPS...332..447H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JPS...332..447H"><span><span class="hlt">Pressurized</span> <span class="hlt">air</span> cathodes for enhanced stability and power generation by microbial fuel cells</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>He, Weihua; Yang, Wulin; Tian, Yushi; Zhu, Xiuping; Liu, Jia; Feng, Yujie; Logan, Bruce E.</p> <p>2016-11-01</p> <p>Large differences between the water and <span class="hlt">air</span> <span class="hlt">pressure</span> in microbial fuel cells (MFCs) can deform and damage cathodes. To avoid deformation, the cathode <span class="hlt">air</span> <span class="hlt">pressure</span> was controlled to balance <span class="hlt">pressure</span> differences between the <span class="hlt">air</span> and water. Raising the <span class="hlt">air</span> <span class="hlt">pressures</span> from 0 to 10 kPa at a set cathode potential of -0.3 V (versus Ag/AgCl) enhanced cathode performance by 17%, but <span class="hlt">pressures</span> ≥25 kPa decreased current and resulted in <span class="hlt">air</span> leakage into the solution. Matching the <span class="hlt">air</span> <span class="hlt">pressure</span> with the water <span class="hlt">pressure</span> avoided cathode deformation and improved performance. The maximum power density increased by 15%, from 1070 ± 20 to 1230 ± 70 mW m-2, with balanced <span class="hlt">air</span> and water <span class="hlt">pressures</span> of 10-25 kPa. Oxygen partial <span class="hlt">pressures</span> ≥12.5 kPa in the cathode compartment maintained the oxygen reduction rate to be within 92 ± 1% of that in ambient <span class="hlt">air</span>. The use of <span class="hlt">pressurized</span> <span class="hlt">air</span> flow through the cathode compartments can enable closer spacing of the cathodes compared to passive gas transfer systems, which could make the reactor design more compact. The energy cost of <span class="hlt">pressurizing</span> the cathodes was estimated to be smaller than the increase in power that resulted from the use of <span class="hlt">pressurized</span> cathodes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999JFM...380..297S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999JFM...380..297S"><span>Levitation of a <span class="hlt">drop</span> over a film flow</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sreenivas, K. R.; de, P. K.; Arakeri, Jaywant H.</p> <p>1999-02-01</p> <p>A vertical jet of water impinging on a horizontal surface produces a radial film flow followed by a circular hydraulic jump. We report a phenomenon where fairly large (1 ml) <span class="hlt">drops</span> of liquid levitate just upstream of the jump on a thin <span class="hlt">air</span> layer between the <span class="hlt">drop</span> and the film flow. We explain the phenomenon using lubrication theory. Bearing action both in the <span class="hlt">air</span> film and the water film seems to be necessary to support large <span class="hlt">drops</span>. Horizontal support is given to the <span class="hlt">drop</span> by the hydraulic jump. A variety of <span class="hlt">drop</span> shapes is observed depending on the volume of the <span class="hlt">drop</span> and liquid properties. We show that interaction of the forces due to gravity, surface tension, viscosity and inertia produces these various shapes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPS...364..280K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPS...364..280K"><span>Effects of oxygen partial <span class="hlt">pressure</span> on Li-<span class="hlt">air</span> battery performance</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwon, Hyuk Jae; Lee, Heung Chan; Ko, Jeongsik; Jung, In Sun; Lee, Hyun Chul; Lee, Hyunpyo; Kim, Mokwon; Lee, Dong Joon; Kim, Hyunjin; Kim, Tae Young; Im, Dongmin</p> <p>2017-10-01</p> <p>For application in electric vehicles (EVs), the Li-<span class="hlt">air</span> battery system needs an <span class="hlt">air</span> intake system to supply dry oxygen at controlled concentration and feeding rate as the cathode active material. To facilitate the design of such <span class="hlt">air</span> intake systems, we have investigated the effects of oxygen partial <span class="hlt">pressure</span> (≤1 atm) on the performance of the Li-<span class="hlt">air</span> cell, which has not been systematically examined. The amounts of consumed O2 and evolved CO2 from the Li-<span class="hlt">air</span> cell are measured with a custom in situ differential electrochemical gas chromatography-mass spectrometry (DEGC-MS). The amounts of consumed O2 suggest that the oxygen partial <span class="hlt">pressure</span> does not affect the reaction mechanism during discharge, and the two-electron reaction occurs under all test conditions. On the other hand, the charging behavior varies by the oxygen partial <span class="hlt">pressure</span>. The highest O2 evolution ratio is attained under 70% O2, along with the lowest CO2 evolution. The cell cycle life also peaks at 70% O2 condition. Overall, an oxygen partial <span class="hlt">pressure</span> of about 0.5-0.7 atm maximizes the Li-<span class="hlt">air</span> cell capacity and stability at 1 atm condition. The findings here indicate that the appropriate oxygen partial <span class="hlt">pressure</span> can be a key factor when developing practical Li-<span class="hlt">air</span> battery systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19750005995','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19750005995"><span><span class="hlt">Pressure</span> <span class="hlt">Drop</span> Across Woven Screens Under Uniform and Nonuniform Flow Conditions. [flow characteristics of water through Dutch twill and square weave fabrics</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ludewig, M.; Omori, S.; Rao, G. L.</p> <p>1974-01-01</p> <p>Tests were conducted to determine the experimental <span class="hlt">pressure</span> <span class="hlt">drop</span> and velocity data for water flowing through woven screens. The types of materials used are dutch twill and square weave fabrics. <span class="hlt">Pressure</span> <span class="hlt">drop</span> measures were made at four locations in a rectangular channel. The data are presented as change in <span class="hlt">pressure</span> compared with the average entry velocity and the numerical relationship is determined by dividing the volumetric flow rate by the screen area open to flow. The equations of continuity and momentum are presented. A computer program listing an extension of a theoretical model and data from that computer program are included.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DFDG33002P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DFDG33002P"><span><span class="hlt">Drop</span> impact on thin liquid films using TIRM</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pack, Min; Ying Sun Team</p> <p>2015-11-01</p> <p><span class="hlt">Drop</span> impact on thin liquid films is relevant to a number of industrial processes such as pesticide spraying and repellent surface research such as self-cleaning applications. In this study, we systematically investigate the <span class="hlt">drop</span> impact dynamics on thin liquid films on plain glass substrates by varying the film thickness, viscosity and impact velocity. High speed imaging is used to track the droplet morphology and trajectory over time as well as observing instability developments at high Weber number impacts. Moreover, the <span class="hlt">air</span> layer between the <span class="hlt">drop</span> and thin film upon <span class="hlt">drop</span> impact is probed by total internal reflection microscopy (TIRM) where the grayscale intensity is used to measure the <span class="hlt">air</span> layer thickness and spreading radius over time. For low We impact on thick films (We ~ 10), the effect of the <span class="hlt">air</span> entrainment is pronounced where the adhesion of the droplet to the wall is delayed by the <span class="hlt">air</span> depletion and liquid film drainage, whereas for high We impact (We >100) the <span class="hlt">air</span> layer is no longer formed and instead, the <span class="hlt">drop</span> contact with the wall is limited only to the film drainage for all film thicknesses. In addition, the maximum spreading radius of the droplet is analyzed for varying thin film thickness and viscosity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/5950','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/5950"><span><span class="hlt">Air</span> <span class="hlt">pressures</span> in wood frame walls</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Anton TenWolde; Charles G. Carll; Vyto Malinauskas</p> <p>1998-01-01</p> <p>Wind <span class="hlt">pressures</span> can play an important role in the wetting of exterior walls (driving rain). In response, the rain screen concept, including compartmentalization and <span class="hlt">air</span> spaces, has been developed to provide <span class="hlt">pressure</span> equalization and limit water entry into the wall. However, conventional construction such as wood lap siding has not been evaluated as to its ability to...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDM13009H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDM13009H"><span>Levitation and locomotion on an <span class="hlt">air</span>-table of plates with herringbone grooves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hinch, John; de Maleprade, Helene</p> <p>2017-11-01</p> <p>Recent experiments in ESPCI in Paris and numerical simulations in Nano- and Microfluidics in Darmstadt have shown that plates with herringbone grooves in their base are accelerated on an <span class="hlt">air</span>-table in the direction that the chevron grooves point. A simple two-dimensional model is constructed of the <span class="hlt">air</span> flow down a channel with <span class="hlt">pressure</span> controlled influx across the lower boundary. Limiting cases are considered of low and high Reynolds numbers, and of small and large <span class="hlt">pressure</span> <span class="hlt">drop</span> down the channel compared with the <span class="hlt">pressure</span> <span class="hlt">drop</span> across the porous plate. The levitation and locomotion forces are calculated. A prediction is made for the locomotive acceleration which avoids the complications of the shorter grooves which exit the front and back edges.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22488643-surface-treatment-polypropylene-pp-film-dielectric-barrier-discharge-produced-air-argon-air-mixture-atmospheric-pressure','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22488643-surface-treatment-polypropylene-pp-film-dielectric-barrier-discharge-produced-air-argon-air-mixture-atmospheric-pressure"><span>Surface treatment of polypropylene (PP) film by 50 Hz dielectric barrier discharge produced in <span class="hlt">air</span> and argon/<span class="hlt">air</span> mixture at atmospheric <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Joshi, Ujjwal Man, E-mail: umjoshi@gmail.com; Subedi, Deepak Prasad, E-mail: deepaksubedi2001@yahoo.com</p> <p></p> <p>Thin films of polypropylene (PP) are treated for improving hydrophilicity using non-thermal plasma generated by 50 Hz line frequency dielectric barrier discharge produced in <span class="hlt">air</span> and argon/<span class="hlt">air</span> mixture at atmospheric <span class="hlt">pressure</span>. PP samples before and after the treatments are studied using contact angle measurements, surface free energy calculations and scanning electron microscopy (SEM). Distilled water (H{sub 2}O), glycerol (C{sub 3}H{sub 8}O{sub 3}) and diiodomethane (CH{sub 2}I{sub 2}) are used as test liquids. The contact angle measurements between test liquids and PP samples are used to determine total surface free energy using sessile <span class="hlt">drop</span> technique. PP films show a remarkable increase inmore » surface free energy after plasma treatment. SEM analysis of the plasma-treated PP films shows that plasma treatment introduces greater roughness on the surface leading to the increased surface free energy. Furthermore, it is found that introducing a small quantity of argon can enhance the surface treatment remarkably.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920030717&hterms=sponge&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dsponge','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920030717&hterms=sponge&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dsponge"><span><span class="hlt">Pressure</span> <span class="hlt">drop</span> of He II flow through a porous media</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Maddocks, J. R.; Van Sciver, S. W.</p> <p>1990-01-01</p> <p>The paper reports on measurements of He II <span class="hlt">pressure</span> <span class="hlt">drop</span> across two porous SiO2 ceramic filter materials. These materials vary only in porosity, having values of 0.94 and 0.96. The average fiber diameter in both cases is approximately 5 microns. The experiment consists of a glass tube containing a piece of this sponge in one end. The tube is rapidly displaced downward in a bath of helium and the liquid levels are allowed to equilibrate over time producing variable velocities up to 10 cm/sec. The results are compared with those previously obtained using fine mesh screens. Good qualitative agreement is observed for turbulent flow; however, the behavior in the laminar flow regime is not fully understood.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3893195','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3893195"><span>Inverse Association between <span class="hlt">Air</span> <span class="hlt">Pressure</span> and Rheumatoid Arthritis Synovitis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Furu, Moritoshi; Nakabo, Shuichiro; Ohmura, Koichiro; Nakashima, Ran; Imura, Yoshitaka; Yukawa, Naoichiro; Yoshifuji, Hajime; Matsuda, Fumihiko; Ito, Hiromu; Fujii, Takao; Mimori, Tsuneyo</p> <p>2014-01-01</p> <p>Rheumatoid arthritis (RA) is a bone destructive autoimmune disease. Many patients with RA recognize fluctuations of their joint synovitis according to changes of <span class="hlt">air</span> <span class="hlt">pressure</span>, but the correlations between them have never been addressed in large-scale association studies. To address this point we recruited large-scale assessments of RA activity in a Japanese population, and performed an association analysis. Here, a total of 23,064 assessments of RA activity from 2,131 patients were obtained from the KURAMA (Kyoto University Rheumatoid Arthritis Management Alliance) database. Detailed correlations between <span class="hlt">air</span> <span class="hlt">pressure</span> and joint swelling or tenderness were analyzed separately for each of the 326 patients with more than 20 assessments to regulate intra-patient correlations. Association studies were also performed for seven consecutive days to identify the strongest correlations. Standardized multiple linear regression analysis was performed to evaluate independent influences from other meteorological factors. As a result, components of composite measures for RA disease activity revealed suggestive negative associations with <span class="hlt">air</span> <span class="hlt">pressure</span>. The 326 patients displayed significant negative mean correlations between <span class="hlt">air</span> <span class="hlt">pressure</span> and swellings or the sum of swellings and tenderness (p = 0.00068 and 0.00011, respectively). Among the seven consecutive days, the most significant mean negative correlations were observed for <span class="hlt">air</span> <span class="hlt">pressure</span> three days before evaluations of RA synovitis (p = 1.7×10−7, 0.00027, and 8.3×10−8, for swellings, tenderness and the sum of them, respectively). Standardized multiple linear regression analysis revealed these associations were independent from humidity and temperature. Our findings suggest that <span class="hlt">air</span> <span class="hlt">pressure</span> is inversely associated with synovitis in patients with RA. PMID:24454853</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5483033','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5483033"><span>Sensitivity Analysis and Accuracy of a CFD-TFM Approach to Bubbling Bed Using <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Fluctuations</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Tricomi, Leonardo; Melchiori, Tommaso; Chiaramonti, David; Boulet, Micaël; Lavoie, Jean Michel</p> <p>2017-01-01</p> <p>Based upon the two fluid model (TFM) theory, a CFD model was implemented to investigate a cold multiphase-fluidized bubbling bed reactor. The key variable used to characterize the fluid dynamic of the experimental system, and compare it to model predictions, was the time-<span class="hlt">pressure</span> <span class="hlt">drop</span> induced by the bubble motion across the bed. This time signal was then processed to obtain the power spectral density (PSD) distribution of <span class="hlt">pressure</span> fluctuations. As an important aspect of this work, the effect of the sampling time scale on the empirical power spectral density (PSD) was investigated. A time scale of 40 s was found to be a good compromise ensuring both simulation performance and numerical validation consistency. The CFD model was first numerically verified by mesh refinement process, after what it was used to investigate the sensitivity with regards to minimum fluidization velocity (as a calibration point for drag law), restitution coefficient, and solid <span class="hlt">pressure</span> term while assessing his accuracy in matching the empirical PSD. The 2D model provided a fair match with the empirical time-averaged <span class="hlt">pressure</span> <span class="hlt">drop</span>, the relating fluctuations amplitude, and the signal’s energy computed as integral of the PSD. A 3D version of the TFM was also used and it improved the match with the empirical PSD in the very first part of the frequency spectrum. PMID:28695119</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28695119','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28695119"><span>Sensitivity Analysis and Accuracy of a CFD-TFM Approach to Bubbling Bed Using <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Fluctuations.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tricomi, Leonardo; Melchiori, Tommaso; Chiaramonti, David; Boulet, Micaël; Lavoie, Jean Michel</p> <p>2017-01-01</p> <p>Based upon the two fluid model (TFM) theory, a CFD model was implemented to investigate a cold multiphase-fluidized bubbling bed reactor. The key variable used to characterize the fluid dynamic of the experimental system, and compare it to model predictions, was the time-<span class="hlt">pressure</span> <span class="hlt">drop</span> induced by the bubble motion across the bed. This time signal was then processed to obtain the power spectral density (PSD) distribution of <span class="hlt">pressure</span> fluctuations. As an important aspect of this work, the effect of the sampling time scale on the empirical power spectral density (PSD) was investigated. A time scale of 40 s was found to be a good compromise ensuring both simulation performance and numerical validation consistency. The CFD model was first numerically verified by mesh refinement process, after what it was used to investigate the sensitivity with regards to minimum fluidization velocity (as a calibration point for drag law), restitution coefficient, and solid <span class="hlt">pressure</span> term while assessing his accuracy in matching the empirical PSD. The 2D model provided a fair match with the empirical time-averaged <span class="hlt">pressure</span> <span class="hlt">drop</span>, the relating fluctuations amplitude, and the signal's energy computed as integral of the PSD. A 3D version of the TFM was also used and it improved the match with the empirical PSD in the very first part of the frequency spectrum.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1914443B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1914443B"><span>Sound wave energy emitted by water <span class="hlt">drop</span> during the splash on the soil surface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bieganowski, Andrzej; Ryżak, Magdalena; Korbiel, Tomasz</p> <p>2017-04-01</p> <p>A <span class="hlt">drop</span> of rain falling on the surface of bare soil not only moisturizes but also can cause splash or compaction, depending on the energy of incident <span class="hlt">drops</span> and the condition of the surface on which it falls. The splash phenomenon can be characterized by the weight of detached soil material (using splash cups) as well as the number and trajectory of splashed particles (using high-speed cameras). The study presents a new aspect of the analysis of the splash phenomenon by measurement of the sound <span class="hlt">pressure</span> level and the sound energy of the wave that propagates in the <span class="hlt">air</span>. The measurements were carried out in an anechoic chamber. Three soils (Endogleyic Umbrisol, Fluvic Endogleyic Cambisol, and Haplic Chernozem) with four initial moisture levels (<span class="hlt">pressure</span> heads: 0.1 kPa, 1 kPa, 3.16 kPa, and 16 kPa) were tested. <span class="hlt">Drops</span> of 4.2 mm diameter were falling from a height of 1.5m. The sound <span class="hlt">pressure</span> level was recorded after 10 consecutive water <span class="hlt">drop</span> impacts using a special set of microphones. In all measuring conditions with 1m distance, the sound <span class="hlt">pressure</span> level ranged from 27 to 42dB. The impact of water <span class="hlt">drops</span> on the ground created sound pulses, which were recalculated to the energy emitted in the form of sound waves. For all soil samples, the sound wave energy was within the range of 0.14 μJ to 5.26 μJ, which corresponds to 0.03-1.07% of the energy of the incident <span class="hlt">drops</span> (Ryżak et al., 2016). This work was partly financed from the National Science Centre, Poland; project no. 2014/14/E/ST10/00851. References Ryżak M., Bieganowski A., Korbiel T.: Sound wave Energy resulting from the impact of water <span class="hlt">drops</span> on the soil surface. PLoS One 11(7):e0158472. doi:10.1371/journal.pone.0158472, 2016</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150003353','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150003353"><span>Method and Apparatus for Measuring Surface <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lin, Bing (Inventor); Hu, Yongxiang (Inventor)</p> <p>2014-01-01</p> <p>The present invention is directed to an apparatus and method for remotely measuring surface <span class="hlt">air</span> <span class="hlt">pressure</span>. In one embodiment, the method of the present invention utilizes the steps of transmitting a signal having multiple frequencies into the atmosphere, measuring the transmitted/reflected signal to determine the relative received power level of each frequency and then determining the surface <span class="hlt">air</span> <span class="hlt">pressure</span> based upon the attenuation of the transmitted frequencies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4680856','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4680856"><span>Dysfunctional vestibular system causes a blood <span class="hlt">pressure</span> <span class="hlt">drop</span> in astronauts returning from space</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Hallgren, Emma; Migeotte, Pierre-François; Kornilova, Ludmila; Delière, Quentin; Fransen, Erik; Glukhikh, Dmitrii; Moore, Steven T.; Clément, Gilles; Diedrich, André; MacDougall, Hamish; Wuyts, Floris L.</p> <p>2015-01-01</p> <p>It is a challenge for the human body to maintain stable blood <span class="hlt">pressure</span> while standing. The body’s failure to do so can lead to dizziness or even fainting. For decades it has been postulated that the vestibular organ can prevent a <span class="hlt">drop</span> in <span class="hlt">pressure</span> during a position change – supposedly mediated by reflexes to the cardiovascular system. We show – for the first time – a significant correlation between decreased functionality of the vestibular otolith system and a decrease in the mean arterial <span class="hlt">pressure</span> when a person stands up. Until now, no experiments on Earth could selectively suppress both otolith systems; astronauts returning from space are a unique group of subjects in this regard. Their otolith systems are being temporarily disturbed and at the same time they often suffer from blood <span class="hlt">pressure</span> instability. In our study, we observed the functioning of both the otolith and the cardiovascular system of the astronauts before and after spaceflight. Our finding indicates that an intact otolith system plays an important role in preventing blood <span class="hlt">pressure</span> instability during orthostatic challenges. Our finding not only has important implications for human space exploration; they may also improve the treatment of unstable blood <span class="hlt">pressure</span> here on Earth. PMID:26671177</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23473519','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23473519"><span>[Effect of subglottic <span class="hlt">air</span> insufflation on subglottic <span class="hlt">pressure</span> during swallowing].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Clarett, M; Andreu, M F; Salvati, I G; Donnianni, M C; Montes, G S; Rodríguez, M G</p> <p>2014-04-01</p> <p>To determine whether there are differences between subglottic <span class="hlt">pressure</span> during swallowing with and without <span class="hlt">air</span> insufflation via a subglottic catheter in tracheostomized patients. A prospective, randomized cross-over study was made. Adult Intensive Care Units. Patients requiring mechanical ventilation and tracheostomy with a subglottic catheter, and with tolerance to deflation of the balloon and a speaking valve placed over the opening of the tracheostomy tube. Subglottic <span class="hlt">pressure</span> was measured during swallowing of a thickened solution with and without the delivery of airflow through the subglottic catheter. Subglottic <span class="hlt">pressure</span> during swallowing. Twelve out of 14 patients showed higher subglottic <span class="hlt">pressure</span> values during swallowing with <span class="hlt">air</span> insufflation. Two patients showed no differences between both conditions. Median (Med) values of subglottic <span class="hlt">pressure</span> for the first, second and third swallow were 5, 4 and 4.5 cmH2O (Med 4.5 cmH2O) without <span class="hlt">air</span> insufflation, and 8, 5.5 and 7.5 cmH2O (Med 5.5 cmH2O) with <span class="hlt">air</span> insufflation, respectively (Wilcoxon, Z=-3.078; p=.002). In a group of tracheostomized patients, <span class="hlt">air</span> insufflation via a subglottic catheter increased subglottic <span class="hlt">pressure</span> levels measured during swallowing. Copyright © 2012 Elsevier España, S.L. and SEMICYUC. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..19.6998W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..19.6998W"><span>Operational design and <span class="hlt">pressure</span> response of large-scale compressed <span class="hlt">air</span> energy storage in porous formations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Bo; Bauer, Sebastian</p> <p>2017-04-01</p> <p> day. The average bottom hole <span class="hlt">pressure</span> is 87 bars at the beginning of cyclic operation and reduces to 79 bars after 10 years. This <span class="hlt">pressure</span> <span class="hlt">drop</span> over time is caused by the open boundary conditions defined at the model edges and is not influenced by the cyclic operation. In the storage formation, the <span class="hlt">pressure</span> response induced by the initial filling can be observed in the whole model domain, and a maximum <span class="hlt">pressure</span> built-up of about 31 bars and 3 bars are observed near the wells and at a distance of 10 km from the wells, respectively. During the cyclic operation, however, <span class="hlt">pressure</span> fluctuations of more than 1 bar can only be observed within the gas phase. Assuming formations with different permeabilities, a sensitivity analysis is carried out to find the number of wells required. Results show that the number of wells required does not linearly decrease with increasing permeability of the storage formation due to well interference during <span class="hlt">air</span> extraction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19790016829','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19790016829"><span>Performance of a multiple venturi fuel-<span class="hlt">air</span> preparation system. [fuel injection for gas turbines</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Tacina, R. R.</p> <p>1979-01-01</p> <p>Spatial fuel-<span class="hlt">air</span> distributions, degree of vaporization, and <span class="hlt">pressure</span> <span class="hlt">drop</span> were measured 16.5 cm downstream of the fuel injection plane of a multiple Venturi tube fuel injector. Tests were performed in a 12 cm tubular duct. Test conditions were: a <span class="hlt">pressure</span> of 0.3 MPa, inlet <span class="hlt">air</span> temperature from 400 to 800K, <span class="hlt">air</span> velocities of 10 and 20 m/s, and fuel-<span class="hlt">air</span> ratios of 0.010 and 0.020. The fuel was Diesel #2. Spatial fuel-<span class="hlt">air</span> distributions were within + or - 20 percent of the mean at inlet <span class="hlt">air</span> temperatures above 450K. At an inlet <span class="hlt">air</span> temperature of 400K, the fuel-<span class="hlt">air</span> distribution was measured when a 50 percent blockage plate was placed 9.2 cm upstream of the fuel injection plane to distort the inlet <span class="hlt">air</span> velocity fuel injection plane to distort the inlet <span class="hlt">air</span> velocity profile. Vaporization of the fuel was 50 percent complete at an inlet <span class="hlt">air</span> temperature of 400K and the percentage increased linearly with temperature to complete vaporization at 600K. The <span class="hlt">pressure</span> <span class="hlt">drop</span> was 3 percent at the design point which was three times greater than the designed value and the single tube experiment value. No autoignition or flashback was observed at the conditions tested.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_10 --> <div id="page_11" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="201"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21233664','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21233664"><span>Hospital-acquired <span class="hlt">pressure</span> ulcer prevalence--evaluating low-<span class="hlt">air</span>-loss beds.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Johnson, Jane; Peterson, Darcie; Campbell, Betty; Richardson, Regina; Rutledge, Dana</p> <p>2011-01-01</p> <p>Higher-category <span class="hlt">pressure</span> redistribution mattresses are considered a critical component of a <span class="hlt">pressure</span> ulcer prevention program, but few studies have quantified the impact of specific preventive measures on the incidence or prevalence of hospital-acquired <span class="hlt">pressure</span> ulcers (HAPUs). Therefore, this study was undertaken to determine the impact of low-<span class="hlt">air</span>-loss beds on HAPU prevalence. This prospective, comparative cohort study monitored the prevalence of HAPU at our hospital and compared rates of matched medical-surgical units with and without low-<span class="hlt">air</span>-loss beds. Units without low-<span class="hlt">air</span>-loss beds used a variety of alternative <span class="hlt">pressure</span> redistribution devices for patients deemed at risk for <span class="hlt">pressure</span> ulceration. The prevalence of HAPU was operationally defined as the number of patients with HAPUs divided by numbers of patients observed. The prevalence of HAPU over 3 quarters in 2008 ranged from 1.0% to 3.3% (overall rate 2.4%). Eighty-three percent of patients with HAPUs were cared for on low-<span class="hlt">air</span>-loss beds. Of 12 patients with 16 HAPUs during this time, 75% were aged 70 years or older and 25% were managed in critical care units. Over half of patients who developed HAPUs had been hospitalized for 20 days or more. Half of the patients with HAPUs were scored as no-low risk on the Braden Scale.On the paired medical-surgical units, no statistically significant differences were found when patients with low-<span class="hlt">air</span>-loss beds were compared to standard hospital mattresses supplemented by a variety of <span class="hlt">pressure</span> redistribution devices. Seven of 11 HAPUs (63%) occurred in patients placed on low-<span class="hlt">air</span>-loss beds. The prevalence of HAPU in patients placed on low-<span class="hlt">air</span>-loss beds was no different from patients placed on standard hospital mattresses supplemented by a variety of <span class="hlt">pressure</span> redistribution devices. Further research is needed to determine the impact of specific strategies on prevention of HAPU.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3656658','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3656658"><span>Ambient <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> changes during pregnancy</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lee, Pei-Chen; Talbott, Evelyn O.; Roberts, James M.; Catov, Janet M.; Bilonick, Richard A.; Stone, Roslyn A.; Sharma, Ravi K.; Ritz, Beate</p> <p>2013-01-01</p> <p>Background Maternal exposure to ambient <span class="hlt">air</span> pollution has been associated with adverse birth outcomes such as preterm delivery. However, only one study to date has linked <span class="hlt">air</span> pollution to blood <span class="hlt">pressure</span> changes during pregnancy, a period of dramatic cardiovascular function changes. Objectives We examined whether maternal exposures to criteria <span class="hlt">air</span> pollutants, including particles of less than 10 µm (PM10) or 2.5 µm diameter (PM2.5), carbon monoxide (CO), nitrogen dioxide (NO2), sulfur dioxide (SO2), and ozone (O3), in each trimester of pregnancy are associated with magnitude of rise of blood <span class="hlt">pressure</span> between the first 20 weeks of gestation and late pregnancy in a prospectively followed cohort of 1684 pregnant women in Allegheny County, PA. Methods <span class="hlt">Air</span> pollution measures for maternal ZIP code areas were derived using Kriging interpolation. Using logistic regression analysis, we evaluated the associations between <span class="hlt">air</span> pollution exposures and blood <span class="hlt">pressure</span> changes between the first 20 weeks of gestation and late pregnancy. Results First trimester PM10 and ozone exposures were associated with blood <span class="hlt">pressure</span> changes between the first 20 weeks of gestation and late pregnancy, most strongly in non-smokers. Per interquartile increases in first trimester PM10 and O3 concentrations were associated with mean increases in systolic blood <span class="hlt">pressure</span> of 1.88 mmHg (95% CI = 0.84 to 2.93) and 1.84 (95% CI = 1.05 to 4.63), respectively, and in diastolic blood <span class="hlt">pressure</span> of 0.63 mmHg (95% CI= −0.50 to 1.76) and 1.13 (95% CI= −0.46 to 2.71) in non-smokers. Conclusions Our novel finding suggests that first trimester PM10 and O3 <span class="hlt">air</span> pollution exposures increase blood <span class="hlt">pressure</span> in the later stages of pregnancy. These changes may play a role in mediating the relationships between <span class="hlt">air</span> pollution and adverse birth outcomes. PMID:22835955</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPS...360..548K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPS...360..548K"><span>Effect of electrode intrusion on <span class="hlt">pressure</span> <span class="hlt">drop</span> and electrochemical performance of an all-vanadium redox flow battery</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kumar, S.; Jayanti, S.</p> <p>2017-08-01</p> <p>In this paper, we present a study of the effect of electrode intrusion into the flow channel in an all-vanadium redox flow battery. Permeability, <span class="hlt">pressure</span> <span class="hlt">drop</span> and electrochemical performance have been measured in a cell with active area 100 cm2and 414 cm2 fitted with a carbon felt electrode of thickness of 3, 6 or 9 mm compressed to 1.5, 2.5 or 4 mm, respectively, during assembly. Results show that the <span class="hlt">pressure</span> <span class="hlt">drop</span> is significantly higher than what can be expected in the thick electrode case while its electrochemical performance is lower. Detailed flow analysis using computational fluid dynamics simulations in two different flow fields shows that both these results can be attributed to electrode intrusion into the flow channel leading to increased resistance to electrolyte flow through the electrode. A correlation is proposed to evaluate electrode intrusion depth as a function of compression.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20060008906','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20060008906"><span>Two Phase Flow Modeling: Summary of Flow Regimes and <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Correlations in Reduced and Partial Gravity</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Balasubramaniam, R.; Rame, E.; Kizito, J.; Kassemi, M.</p> <p>2006-01-01</p> <p>The purpose of this report is to provide a summary of state-of-the-art predictions for two-phase flows relevant to Advanced Life Support. We strive to pick out the most used and accepted models for <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow regime predictions. The main focus is to identify gaps in predictive capabilities in partial gravity for Lunar and Martian applications. Following a summary of flow regimes and <span class="hlt">pressure</span> <span class="hlt">drop</span> correlations for terrestrial and zero gravity, we analyze the fully developed annular gas-liquid flow in a straight cylindrical tube. This flow is amenable to analytical closed form solutions for the flow field and heat transfer. These solutions, valid for partial gravity as well, may be used as baselines and guides to compare experimental measurements. The flow regimes likely to be encountered in the water recovery equipment currently under consideration for space applications are provided in an appendix.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014PhFl...26g2103K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014PhFl...26g2103K"><span>Bag breakup of low viscosity <span class="hlt">drops</span> in the presence of a continuous <span class="hlt">air</span> jet</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kulkarni, V.; Sojka, P. E.</p> <p>2014-07-01</p> <p>This work examines the breakup of a single <span class="hlt">drop</span> of various low viscosity fluids as it deforms in the presence of continuous horizontal <span class="hlt">air</span> jet. Such a fragmentation typically occurs after the bulk liquid has disintegrated upon exiting the atomizer and is in the form of an ensemble of <span class="hlt">drops</span> which undergo further breakup. The <span class="hlt">drop</span> deformation and its eventual disintegration is important in evaluating the efficacy of a particular industrial process, be it combustion in automobile engines or pesticide spraying in agricultural applications. The interplay between competing influences of surface tension and aerodynamic disruptive forces is represented by the Weber number, We, and Ohnesorge number, Oh, and used to describe the breakup morphology. The breakup pattern considered in our study corresponds to that of a bag attached to a toroidal ring which occurs from ˜12 < We < ˜16. We aim to address several issues connected with this breakup process and their dependence on We and Oh which have been hitherto unexplored. The We boundary at which breakup begins is theoretically determined and the expression obtained, We = 12( {1 + 2/3 Oh^2 } ), is found to match well with experimental data {[L.-P. Hsiang and G. M. Faeth, Int. J. Multiphase Flow 21(4), 545-560 (1995)] and [R. S. Brodkey, "Formation of <span class="hlt">drops</span> and bubbles," in The Phenomena of Fluid Motions (Addison-Wesley, Reading, 1967)]}. An exponential growth in the radial extent of the deformed <span class="hlt">drop</span> and the streamline dimension of the bag is predicted by a theoretical model and confirmed by experimental findings. These quantities are observed to strongly depend on We. However, their dependence on Oh is weak.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..307a2057C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..307a2057C"><span>The Influence of Shaping <span class="hlt">Air</span> <span class="hlt">Pressure</span> of Pneumatic Spray Gun</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Wenzhuo; Chen, Yan; Pan, Haiwei; Zhang, Weiming; Li, Bo</p> <p>2018-02-01</p> <p>The shaping <span class="hlt">air</span> <span class="hlt">pressure</span> is a very important parameter in the application of pneumatic spray gun, and studying its influence on spray flow field and film thickness distribution has practical values. In this paper, Euler-Lagrangian method is adopted to describe the two-phase spray flow of pneumatic painting process, and the <span class="hlt">air</span> flow fields, spray patterns and dynamic film thickness distributions were obtained with the help of the computational fluid dynamics code—ANSYS Fluent. Results show that with the increase of the shaping <span class="hlt">air</span> <span class="hlt">pressure</span>, the <span class="hlt">air</span> phase flow field spreads in the plane perpendicular to the shaping <span class="hlt">air</span> hole plane, the spray pattern becomes narrower and flatter, and the width of the dynamic film increases with the reduced maximum value of the film thickness. But the film thickness distribution seems to change little with the shaping <span class="hlt">air</span> <span class="hlt">pressure</span> decreasing from 0.6bar to 0.9bar.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4428615','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4428615"><span>Ultrasonic atomization of liquids in <span class="hlt">drop</span>-chain acoustic fountains</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Simon, Julianna C.; Sapozhnikov, Oleg A.; Khokhlova, Vera A.; Crum, Lawrence A.; Bailey, Michael R.</p> <p>2015-01-01</p> <p>When focused ultrasound waves of moderate intensity in liquid encounter an <span class="hlt">air</span> interface, a chain of <span class="hlt">drops</span> emerges from the liquid surface to form what is known as a <span class="hlt">drop</span>-chain fountain. Atomization, or the emission of micro-droplets, occurs when the acoustic intensity exceeds a liquid-dependent threshold. While the cavitation-wave hypothesis, which states that atomization arises from a combination of capillary-wave instabilities and cavitation bubble oscillations, is currently the most accepted theory of atomization, more data on the roles of cavitation, capillary waves, and even heat deposition or boiling would be valuable. In this paper, we experimentally test whether bubbles are a significant mechanism of atomization in <span class="hlt">drop</span>-chain fountains. High-speed photography was used to observe the formation and atomization of <span class="hlt">drop</span>-chain fountains composed of water and other liquids. For a range of ultrasonic frequencies and liquid sound speeds, it was found that the <span class="hlt">drop</span> diameters approximately equalled the ultrasonic wavelengths. When water was exchanged for other liquids, it was observed that the atomization threshold increased with shear viscosity. Upon heating water, it was found that the time to commence atomization decreased with increasing temperature. Finally, water was atomized in an overpressure chamber where it was found that atomization was significantly diminished when the static <span class="hlt">pressure</span> was increased. These results indicate that bubbles, generated by either acoustic cavitation or boiling, contribute significantly to atomization in the <span class="hlt">drop</span>-chain fountain. PMID:25977591</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19820009205&hterms=FAC&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DFAC','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19820009205&hterms=FAC&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DFAC"><span>Heat loss and drag of spherical <span class="hlt">drop</span> tube samples</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wallace, D. B.</p> <p>1982-01-01</p> <p>Analysis techniques for three aspects of the performance of the NASA/MSFC 32 meter <span class="hlt">drop</span> tube are considered. Heat loss through the support wire in a pendant <span class="hlt">drop</span> sample, temperature history of a <span class="hlt">drop</span> falling through the <span class="hlt">drop</span> tube when the tube is filled with helium gas at various <span class="hlt">pressures</span>, and drag and resulting g-levels experienced by a <span class="hlt">drop</span> falling through the tube when the tube is filled with helium gas at various <span class="hlt">pressures</span> are addressed. The developed methods apply to systems with sufficiently small Knudsen numbers for which continuum theory may be applied. Sample results are presented, using niobium <span class="hlt">drops</span>, to indicate the magnitudes of the effects. Helium gas at one atmosphere <span class="hlt">pressure</span> can approximately double the amount of possible undercooling but it results in an apparent gravity levels of up to 0.1 g.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016HMT....52.2833K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016HMT....52.2833K"><span>Condensation heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of R-410A in a 7.0 mm O.D. microfin tube at low mass fluxes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Nae-Hyun</p> <p>2016-12-01</p> <p>R-410A condensation heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> data are provided for a 7.0 mm O.D. microfin tube at low mass fluxes (50-250 kg/m2 s). The heat transfer coefficient of the microfin tube shows a minimum behavior with the mass flux. At a low mass flux, where flow pattern is stratified, condensation induced by surface tension by microfins overwhelms condensation induced by shear, and the heat transfer coefficient decreases as mass flux increases. At a high mass flux, where flow pattern is annular, condensation induced by shear governs the heat transfer, and the heat transfer coefficient increases as mass flux increases. The <span class="hlt">pressure</span> <span class="hlt">drop</span> of the microfin tube is larger than that of the smooth tube at the annular flow regime. On the contrary, the <span class="hlt">pressure</span> <span class="hlt">drop</span> of the smooth tube is larger than that of the microfin tube at the stratified flow regime.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014IJBm...58.1327P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014IJBm...58.1327P"><span>Effects of sudden <span class="hlt">air</span> <span class="hlt">pressure</span> changes on hospital admissions for cardiovascular diseases in Prague, 1994-2009</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Plavcová, Eva; Kyselý, Jan</p> <p>2014-08-01</p> <p>Sudden weather changes have long been thought to be associated with negative impacts on human health, but relatively few studies have attempted to quantify these relationships. We use large 6-h changes in atmospheric <span class="hlt">pressure</span> as a proxy for sudden weather changes and evaluate their association with hospital admissions for cardiovascular diseases (CVD). Winter and summer seasons and positive and negative <span class="hlt">pressure</span> changes are analysed separately, using data for the city of Prague (population 1.2 million) over a 16-year period (1994-2009). We found that sudden <span class="hlt">pressure</span> <span class="hlt">drops</span> in winter are associated with significant rise in hospital admissions. Increased CVD morbidity was observed neither for <span class="hlt">pressure</span> <span class="hlt">drops</span> in summer nor <span class="hlt">pressure</span> increases in any season. Analysis of synoptic weather maps shows that large <span class="hlt">pressure</span> <span class="hlt">drops</span> in winter are associated with strong zonal flow and rapidly moving low-<span class="hlt">pressure</span> systems with centres over northern Europe and atmospheric fronts affecting western and central Europe. Analysis of links between passages of strong atmospheric fronts and hospital admissions, however, shows that the links disappear if weather changes are characterised by frontal passages. Sudden <span class="hlt">pressure</span> <span class="hlt">drops</span> in winter are associated also with significant excess CVD mortality. As climate models project strengthening of zonal circulation in winter and increased frequency of windstorms, the negative effects of such weather phenomena and their possible changes in a warmer climate of the twenty-first century need to be better understood, particularly as their importance in inducing excess morbidity and mortality in winter may increase compared to cold spells.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17079636','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17079636"><span>Compressed <span class="hlt">air</span> injection technique to standardize block injection <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tsui, Ban C H; Li, Lisa X Y; Pillay, Jennifer J</p> <p>2006-11-01</p> <p>Presently, no standardized technique exists to monitor injection <span class="hlt">pressures</span> during peripheral nerve blocks. Our objective was to determine if a compressed <span class="hlt">air</span> injection technique, using an in vitro model based on Boyle's law and typical regional anesthesia equipment, could consistently maintain injection <span class="hlt">pressures</span> below a 1293 mmHg level associated with clinically significant nerve injury. Injection <span class="hlt">pressures</span> for 20 and 30 mL syringes with various needle sizes (18G, 20G, 21G, 22G, and 24G) were measured in a closed system. A set volume of <span class="hlt">air</span> was aspirated into a saline-filled syringe and then compressed and maintained at various percentages while <span class="hlt">pressure</span> was measured. The needle was inserted into the injection port of a <span class="hlt">pressure</span> sensor, which had attached extension tubing with an injection plug clamped "off". Using linear regression with all data points, the <span class="hlt">pressure</span> value and 99% confidence interval (CI) at 50% <span class="hlt">air</span> compression was estimated. The linearity of Boyle's law was demonstrated with a high correlation, r = 0.99, and a slope of 0.984 (99% CI: 0.967-1.001). The net <span class="hlt">pressure</span> generated at 50% compression was estimated as 744.8 mmHg, with the 99% CI between 729.6 and 760.0 mmHg. The various syringe/needle combinations had similar results. By creating and maintaining syringe <span class="hlt">air</span> compression at 50% or less, injection <span class="hlt">pressures</span> will be substantially below the 1293 mmHg threshold considered to be an associated risk factor for clinically significant nerve injury. This technique may allow simple, real-time and objective monitoring during local anesthetic injections while inherently reducing injection speed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhFl...30e7101R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhFl...30e7101R"><span>Magnetohydrodynamic <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow balancing of liquid metal flow in a prototypic fusion blanket manifold</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rhodes, Tyler J.; Smolentsev, Sergey; Abdou, Mohamed</p> <p>2018-05-01</p> <p>Understanding magnetohydrodynamic (MHD) phenomena associated with the flow of electrically conducting fluids in complex geometry ducts subject to a strong magnetic field is required to effectively design liquid metal (LM) blankets for fusion reactors. Particularly, accurately predicting the 3D MHD <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow distribution is important. To investigate these topics, we simulate a LM MHD flow through an electrically non-conducting prototypic manifold for a wide range of flow and geometry parameters using a 3D MHD solver, HyPerComp incompressible MHD solver for arbitrary geometry. The reference manifold geometry consists of a rectangular feeding duct which suddenly expands such that the duct thickness in the magnetic field direction abruptly increases by a factor rexp. Downstream of the sudden expansion, the LM is distributed into several parallel channels. As a first step in qualifying the flow, a magnitude of the curl of the induced Lorentz force was used to distinguish between inviscid, irrotational core flows and boundary and internal shear layers where inertia and/or viscous forces are important. Scaling laws have been obtained which characterize the 3D MHD <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow balancing as a function of the flow parameters and the manifold geometry. Associated Hartmann and Reynolds numbers in the computations were ˜103 and ˜101-103, respectively, while rexp was varied from 4 to 12. An accurate model for the <span class="hlt">pressure</span> <span class="hlt">drop</span> was developed for the first time for inertial-electromagnetic and viscous-electromagnetic regimes based on 96 computed cases. Analysis shows that flow balance can be improved by lengthening the distance between the manifold inlet and the entrances of the parallel channels by utilizing the effect of flow transitioning to a quasi-two-dimensional state in the expansion region of the manifold.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=human+AND+body+AND+ratios&pg=2&id=EJ1015638','ERIC'); return false;" href="https://eric.ed.gov/?q=human+AND+body+AND+ratios&pg=2&id=EJ1015638"><span>Tongue-Palate Contact <span class="hlt">Pressure</span>, Oral <span class="hlt">Air</span> <span class="hlt">Pressure</span>, and Acoustics of Clear Speech</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Searl, Jeff; Evitts, Paul M.</p> <p>2013-01-01</p> <p>Purpose: The authors compared articulatory contact <span class="hlt">pressure</span> (ACP), oral <span class="hlt">air</span> <span class="hlt">pressure</span> (Po), and speech acoustics for conversational versus clear speech. They also assessed the relationship of these measures to listener perception. Method: Twelve adults with normal speech produced monosyllables in a phrase using conversational and clear speech.…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25570740','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25570740"><span>An alternating <span class="hlt">pressure</span> sequence proposal for an <span class="hlt">air</span>-cell cushion for preventing <span class="hlt">pressure</span> ulcers.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Arias, Sandra; Cardiel, Eladio; Rogeli, Pablo; Mori, Taketoshi; Nakagami, Gojiro; Noguchi, Hiroshi; Sanada, Hiromi</p> <p>2014-01-01</p> <p>The distribution and release of <span class="hlt">pressure</span> on ischial regions are two important parameters for evaluating the effectiveness of a cushion; especially the release of <span class="hlt">pressure</span> over time on ischial tuberosities, which is significant for preventing <span class="hlt">pressure</span> ulcers. The aim of this work is to evaluate the effect on interface <span class="hlt">pressure</span> through the application of a proposed alternating <span class="hlt">pressure</span> sequence for an <span class="hlt">air</span>-cell cushion. Six healthy volunteers were asked to sit on the <span class="hlt">air</span> cell cushion, in static and alternating modes, as well as on a typical foam cushion for 12 minutes. Interface <span class="hlt">pressure</span> was monitored with a matrix sensor system. Interface <span class="hlt">pressure</span> values on ischial tuberosities, user contact area and <span class="hlt">pressure</span> distribution were analyzed. Results showed that IP on IT tends to increase in both foam and static cushions, while in alternating cushion IP on IT tends to decrease. User contact area was significantly larger in alternating cushion than in static or foam cushions. Moreover, there is a better <span class="hlt">pressure</span> re-distribution with alternating cushion than with the other cushions. The goal of the alternating sequence is to redistribute <span class="hlt">pressure</span> and stimulate the ischial regions in order to promote blood flow and prevent <span class="hlt">pressure</span> occurring in wheelchair users.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920011167','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920011167"><span>Acoustic forcing of a liquid <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lyell, M. J.</p> <p>1992-01-01</p> <p>The development of systems such as acoustic levitation chambers will allow for the positioning and manipulation of material samples (<span class="hlt">drops</span>) in a microgravity environment. This provides the capability for fundamental studies in droplet dynamics as well as containerless processing work. Such systems use acoustic radiation <span class="hlt">pressure</span> forces to position or to further manipulate (e.g., oscillate) the sample. The primary objective was to determine the effect of a viscous acoustic field/tangential radiation <span class="hlt">pressure</span> forcing on <span class="hlt">drop</span> oscillations. To this end, the viscous acoustic field is determined. Modified (forced) hydrodynamic field equations which result from a consistent perturbation expansion scheme are solved. This is done in the separate cases of an unmodulated and a modulated acoustic field. The effect of the tangential radiation stress on the hydrodynamic field (<span class="hlt">drop</span> oscillations) is found to manifest as a correction to the velocity field in a sublayer region near the <span class="hlt">drop</span>/host interface. Moreover, the forcing due to the radiation <span class="hlt">pressure</span> vector at the interface is modified by inclusion of tangential stresses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014ApPhL.105h3703S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014ApPhL.105h3703S"><span>Automated single cell sorting and deposition in submicroliter <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Salánki, Rita; Gerecsei, Tamás; Orgovan, Norbert; Sándor, Noémi; Péter, Beatrix; Bajtay, Zsuzsa; Erdei, Anna; Horvath, Robert; Szabó, Bálint</p> <p>2014-08-01</p> <p>Automated manipulation and sorting of single cells are challenging, when intact cells are needed for further investigations, e.g., RNA or DNA sequencing. We applied a computer controlled micropipette on a microscope admitting 80 PCR (Polymerase Chain Reaction) tubes to be filled with single cells in a cycle. Due to the Laplace <span class="hlt">pressure</span>, fluid starts to flow out from the micropipette only above a critical <span class="hlt">pressure</span> preventing the precise control of <span class="hlt">drop</span> volume in the submicroliter range. We found an anomalous <span class="hlt">pressure</span> additive to the Laplace <span class="hlt">pressure</span> that we attribute to the evaporation of the <span class="hlt">drop</span>. We have overcome the problem of the critical <span class="hlt">dropping</span> <span class="hlt">pressure</span> with sequentially operated fast fluidic valves timed with a millisecond precision. Minimum <span class="hlt">drop</span> volume was 0.4-0.7 μl with a sorting speed of 15-20 s per cell. After picking NE-4C neuroectodermal mouse stem cells and human primary monocytes from a standard plastic Petri dish we could gently deposit single cells inside tiny <span class="hlt">drops</span>. 94 ± 3% and 54 ± 7% of the deposited <span class="hlt">drops</span> contained single cells for NE-4C and monocytes, respectively. 7.5 ± 4% of the <span class="hlt">drops</span> contained multiple cells in case of monocytes. Remaining <span class="hlt">drops</span> were empty. Number of cells deposited in a <span class="hlt">drop</span> could be documented by imaging the Petri dish before and after sorting. We tuned the adhesion force of cells to make the manipulation successful without the application of microstructures for trapping cells on the surface. We propose that our straightforward and flexible setup opens an avenue for single cell isolation, critically needed for the rapidly growing field of single cell biology.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24320194','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24320194"><span>Development and evaluation of a self-regulating alternating <span class="hlt">pressure</span> <span class="hlt">air</span> cushion.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nakagami, Gojiro; Sanada, Hiromi; Sugama, Junko</p> <p>2015-03-01</p> <p>To investigate the effect of alternating <span class="hlt">air</span> cells of a newly developed dynamic cushion on interface <span class="hlt">pressure</span> and tissue oxygenation levels. This cross-over experimental study included 19 healthy volunteers. The dynamic cushion used has an automatic self-regulating alternating <span class="hlt">pressure</span> <span class="hlt">air</span>-cell system with 35 small and four large <span class="hlt">air</span> cells for maintaining posture while seated. This cushion also has 17 bottoming-out detectors that automatically inflate the <span class="hlt">air</span> cells to release a high interface <span class="hlt">pressure</span>. To assess the effect of this alternating system, participants sat on the new cushion with an alternating system or static system for 30 min and then performed push-ups. The interface <span class="hlt">pressure</span> was monitored by <span class="hlt">pressure</span>-sensitive and conductive ink film sensors and tissue oxygenation levels were monitored by near-infrared spectroscopy. A reactive hyperaemia indicator was calculated using tissue oxygenation levels as an outcome measure. The peak interface <span class="hlt">pressure</span> was not significantly different between the groups. The reactive hyperaemia indicator was significantly higher in the static group than in the alternating group. An alternating system has beneficial effects on blood oxygenation levels without increasing interface <span class="hlt">pressure</span>. Therefore, our new cushion is promising for preventing <span class="hlt">pressure</span> ulcers with patients with limited ability to perform push-ups. Implications for Rehabilitation A dynamic cushion was developed, which consists of a uniquely-designed <span class="hlt">air</span>-cell layout, detectors for bottoming out, and an alternating system with multiple <span class="hlt">air</span>-cell lines. The alternating system did not increase interface <span class="hlt">pressure</span> and it significantly reduced reactive hyperaemia after 30 min of sitting in healthy volunteers. This cushion is a new option for individuals who require stable posture but have limitations in performing scheduled push-ups for prevention of <span class="hlt">pressure</span> ulcers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010PhDT.......228K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010PhDT.......228K"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements in prototypic heat exchanges for the supercritical carbon dioxide Brayton power cycles</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kruizenga, Alan Michael</p> <p></p> <p>An experimental facility was built to perform heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements in supercritical carbon dioxide. Inlet temperatures ranged from 30--125 °C with mass velocities ranging from 118--1050 kg/m2s and system <span class="hlt">pressures</span> of 7.5--10.2 MPa. Tests were performed in horizontal, upward, and downward flow conditions to test the influence of buoyancy forces on the heat transfer. Horizontal tests showed that for system <span class="hlt">pressures</span> of 8.1 MPa and up standard Nusselt correlations predicted the heat transfer behavior with good agreement. Tests performed at 7.5 MPa were not well predicted by existing correlations, due to large property variations. The data collected in this work can be used to better understand heat transfer near the critical point. The CFD package FLUENT was found to yield adequate prediction for the heat transfer behavior for low <span class="hlt">pressure</span> cases, where standard correlations were inaccurate, however it was necessary to have fine mesh spacing (y+˜1) in order to capture the observed behavior. Vertical tests found, under the test conditions considered, that flow orientation had little or no effect on the heat transfer behavior, even in flow regions where buoyancy forces should result in a difference between up and down flow heat transfer. CFD results found that for a given set of boundary conditions a large increase in the gravitational acceleration could cause noticeable heat transfer deterioration. Studies performed with CFD further led to the hypothesis that typical buoyancy induced heat transfer deterioration exhibited in supercritical flows were mitigated through a complex interaction with the inertial force, which is caused by bulk cooling of the flow. This hypothesis to explain the observed data requires further investigation. Prototypic heat exchangers channels (i.e. zig-zag) proved that the heat transfer coefficient was consistently three to four times higher as compared to straight channel geometry. However, the form <span class="hlt">pressure</span> loss due</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22311233-bag-breakup-low-viscosity-drops-presence-continuous-air-jet','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22311233-bag-breakup-low-viscosity-drops-presence-continuous-air-jet"><span>Bag breakup of low viscosity <span class="hlt">drops</span> in the presence of a continuous <span class="hlt">air</span> jet</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kulkarni, V., E-mail: vkulkarn@purdue.edu; Sojka, P. E.</p> <p></p> <p>This work examines the breakup of a single <span class="hlt">drop</span> of various low viscosity fluids as it deforms in the presence of continuous horizontal <span class="hlt">air</span> jet. Such a fragmentation typically occurs after the bulk liquid has disintegrated upon exiting the atomizer and is in the form of an ensemble of <span class="hlt">drops</span> which undergo further breakup. The <span class="hlt">drop</span> deformation and its eventual disintegration is important in evaluating the efficacy of a particular industrial process, be it combustion in automobile engines or pesticide spraying in agricultural applications. The interplay between competing influences of surface tension and aerodynamic disruptive forces is represented by themore » Weber number, We, and Ohnesorge number, Oh, and used to describe the breakup morphology. The breakup pattern considered in our study corresponds to that of a bag attached to a toroidal ring which occurs from ∼12 < We < ∼16. We aim to address several issues connected with this breakup process and their dependence on We and Oh which have been hitherto unexplored. The We boundary at which breakup begins is theoretically determined and the expression obtained, We=12(1+2/3Oh{sup 2}), is found to match well with experimental data ([L.-P. Hsiang and G. M. Faeth, Int. J. Multiphase Flow 21(4), 545–560 (1995)] and [R. S. Brodkey, “Formation of <span class="hlt">drops</span> and bubbles,” in The Phenomena of Fluid Motions (Addison-Wesley, Reading, 1967)]). An exponential growth in the radial extent of the deformed <span class="hlt">drop</span> and the streamline dimension of the bag is predicted by a theoretical model and confirmed by experimental findings. These quantities are observed to strongly depend on We. However, their dependence on Oh is weak.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title29-vol7/pdf/CFR-2012-title29-vol7-sec1915-172.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title29-vol7/pdf/CFR-2012-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... 29 Labor 7 2012-07-01 2012-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_11 --> <div id="page_12" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="221"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title29-vol7/pdf/CFR-2013-title29-vol7-sec1915-172.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title29-vol7/pdf/CFR-2013-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... 29 Labor 7 2013-07-01 2013-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title29-vol7/pdf/CFR-2014-title29-vol7-sec1915-172.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title29-vol7/pdf/CFR-2014-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... 29 Labor 7 2014-07-01 2014-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span> Vessels, Drums and Containers, Other Than Ship's Equipment § 1915.172 Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Portable, unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100014092','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100014092"><span>Fuel Cells Utilizing Oxygen From <span class="hlt">Air</span> at Low <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cisar, Alan; Boyer, Chris; Greenwald, Charles</p> <p>2006-01-01</p> <p>A fuel cell stack has been developed to supply power for a high-altitude aircraft with a minimum of <span class="hlt">air</span> handling. The fuel cell is capable of utilizing oxygen from ambient <span class="hlt">air</span> at low <span class="hlt">pressure</span> with no need for compression. For such an application, it is advantageous to take oxygen from the <span class="hlt">air</span> (in contradistinction to carrying a supply of oxygen onboard), but it is a challenging problem to design a fuel-cell stack of reasonable weight that can generate sufficient power while operating at reduced <span class="hlt">pressures</span>. The present fuel-cell design is a response to this challenge. The design features a novel bipolar plate structure in combination with a gas-diffusion structure based on a conductive metal core and a carbon gas-diffusion matrix. This combination makes it possible for the flow fields in the stack to have a large open fraction (ratio between open volume and total volume) to permit large volumes of <span class="hlt">air</span> to flow through with exceptionally low backpressure. Operations at reduced <span class="hlt">pressure</span> require a corresponding increase in the volume of <span class="hlt">air</span> that must be handled to deliver the same number of moles of oxygen to the anodes. Moreover, the increase in the open fraction, relative to that of a comparable prior fuel-cell design, reduces the mass of the stack. The fuel cell has been demonstrated to operate at a power density as high as 105 W/cm2 at an <span class="hlt">air</span> <span class="hlt">pressure</span> as low as 2 psia (absolute <span class="hlt">pressure</span> 14 kPa), which is the atmospheric <span class="hlt">pressure</span> at an altitude of about 50,000 ft ( 15.2 km). The improvements in the design of this fuel cell could be incorporated into designs of other fuel cells to make them lighter in weight and effective at altitudes higher than those of prior designs. Potential commercial applications for these improvements include most applications now under consideration for fuel cells.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..DFDL34008S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..DFDL34008S"><span><span class="hlt">Drops</span> moving along and across a filament</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sahu, Rakesh P.; Sinha-Ray, Suman; Yarin, Alexander; Pourdeyhimi, Behnam</p> <p>2013-11-01</p> <p>The present work is devoted to the experimental study of oil <span class="hlt">drop</span> motion both along and across a filament due to the <span class="hlt">air</span> jet blowing. In case of <span class="hlt">drop</span> moving along the filament, phenomena such as <span class="hlt">drop</span> stick-slip motion, shape oscillations, shedding of a tail along the filament, the tail capillary instability and <span class="hlt">drop</span> recoil motion were observed which were rationalized in the framework of simplified models. Experiments with cross-flow of the surrounding gas relative to the filament with an oil <span class="hlt">drop</span> on it were conducted, with <span class="hlt">air</span> velocity in the range of 7.23 to 22.7 m s-1. The Weber number varied from 2 to 40 and the Ohnesorge number varied from 0.07 to 0.8. The lower and upper critical Weber numbers were introduced to distinguish between the beginning of the <span class="hlt">drop</span> blowing off the filament and the onset of the bag-stamen breakup. The range of the Weber number between these two critical values is filled with three types of vibrational breakup: V1 (a balloon-like <span class="hlt">drop</span> being blown off), V2 (a <span class="hlt">drop</span> on a single stamen being blown off), and V3 (a <span class="hlt">drop</span> on a double stamen being blown off). The Weber number/Ohnesorge number plane was delineated into domains of different breakup regimes. The work is supported by the Nonwovens Cooperative Research Center (NCRC).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009SPIE.7362E..14W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009SPIE.7362E..14W"><span>A method for improving the <span class="hlt">drop</span> test performance of a MEMS microphone</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Winter, Matthias; Ben Aoun, Seifeddine; Feiertag, Gregor; Leidl, Anton; Scheele, Patrick; Seidel, Helmut</p> <p>2009-05-01</p> <p>Most micro electro mechanical system (MEMS) microphones are designed as capacitive microphones where a thin conductive membrane is located in front of a rigid counter electrode. The membrane is exposed to the environment to convert sound into vibrations of the membrane. The movement of the membrane causes a change in the capacitance between the membrane and the counter electrode. The resonance frequency of the membrane is designed to occur above the acoustic spectrum to achieve a linear frequency response. To obtain a good sensitivity the thickness of the membrane must be as small as possible, typically below 0.5 μm. These fragile membranes may be damaged by rapid <span class="hlt">pressure</span> changes. For cell phones, <span class="hlt">drop</span> tests are among the most relevant reliability tests. The extremely high acceleration during the <span class="hlt">drop</span> impact leads to fast <span class="hlt">pressure</span> changes in the microphone which could result in a rupture of the membrane. To overcome this problem a stable protection layer can be placed at a small distance to the membrane. The protective layer has small holes to form a low pass filter for <span class="hlt">air</span> <span class="hlt">pressure</span>. The low pass filter reduces <span class="hlt">pressure</span> changes at high frequencies so that damage to the membrane by excitation in resonance will be prevented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005ApPhL..87r4107L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005ApPhL..87r4107L"><span>Observation of ice nucleation in acoustically levitated water <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lü, Y. J.; Xie, W. J.; Wei, B.</p> <p>2005-10-01</p> <p>The supercooling and nucleation of acoustically levitated water <span class="hlt">drops</span> were investigated at two different sound <span class="hlt">pressure</span> levels (SPL). These water <span class="hlt">drops</span> were supercooled by 13to16K at the low SPL of 160.6dB, whereas their supercoolings varied from 5to11K at the high SPL of 164.4dB. The maximum supercooling obtained in the experiments is 32K. Statistical analyses based on the classical nucleation theory reveal that the occurrence of ice nucleation in water <span class="hlt">drops</span> is mainly confined to the surface region under acoustic levitation conditions and the enlargement of <span class="hlt">drop</span> surface area caused by the acoustic radiation <span class="hlt">pressure</span> reduces water supercoolability remarkably. A comparison of the nucleation rates at the two SPLs indicates that the sound <span class="hlt">pressure</span> can strengthen the surface-dominated nucleation of water <span class="hlt">drops</span>. The acoustic stream around levitated water <span class="hlt">drops</span> and the cavitation effect associated with ultrasonic field are the main factors that induce surface-dominated nucleation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AGUFM.V14B..03C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AGUFM.V14B..03C"><span>The Impact of a Laki-style Eruption on Cloud <span class="hlt">Drops</span>, Indirect Radiative Forcing and <span class="hlt">Air</span> Quality</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Carslaw, K.; Schmidt, A.; Mann, G.; Pringle, K. J.; Forster, P.; Wilson, M.; Thordarson, T.</p> <p>2010-12-01</p> <p>We assess the impact of 1783-1784 Laki eruption on changes in cloud <span class="hlt">drop</span> number concentrations and the aerosol indirect (cloud) radiative forcing using an advanced global aerosol microphysics model. We further extend these simulations to quantify the impact of a modern-day Laki on <span class="hlt">air</span> quality. Our results suggest that the first aerosol indirect effect is of similar magnitude as the direct forcing calculated in previous assessments of the Laki eruption, but has a different spatial pattern. We estimate that northern hemisphere mean cloud <span class="hlt">drop</span> concentrations in low-level clouds increased by a factor 2.7 in the 3 months after the onset of the eruption, with peak changes exceeding a factor 10. The calculated northern hemisphere mean aerosol indirect effect peaks at -5.2 W/m2 in the month after the eruption and remains larger than -2 W/m2 for 6 months. From our understanding of anthropogenic aerosol effects on modern-day clouds, the calculated changes in cloud <span class="hlt">drop</span> concentrations after Laki are likely to have caused substantial changes in pecipitation and cloud dynamics. Our results also show that a modern-day Laki-style volcanic <span class="hlt">air</span> pollution event would be a severe health hazard, increasing excess mortality in Europe on a scale that is at least comparable with excess mortality due to seasonal flu. Investigating the potential impact of such an eruption is crucial in order to inform policy makers and society about the potential impact of such an event so that precautionary measures can be taken.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AIPC.1770c0005S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AIPC.1770c0005S"><span>Multi-hole <span class="hlt">pressure</span> probes to <span class="hlt">air</span> data system for subsonic small-scale <span class="hlt">air</span> vehicles</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shevchenko, A. M.; Berezin, D. R.; Puzirev, L. N.; Tarasov, A. Z.; Kharitonov, A. M.; Shmakov, A. S.</p> <p>2016-10-01</p> <p>A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static <span class="hlt">pressure</span> of a flying vehicle. The basis of these works is the application a well-known classical multi-hole <span class="hlt">pressure</span> probe technique of measuring of a 3D flow to use in the <span class="hlt">air</span> data system. Two multi-hole <span class="hlt">pressure</span> probes with spherical and hemispherical head to <span class="hlt">air</span>-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. The probes were calibrated in the wind tunnel, one of them is in-flight tested.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013EGUGA..15.2025K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013EGUGA..15.2025K"><span>Effects of sudden <span class="hlt">air</span> <span class="hlt">pressure</span> changes on hospital admissions for cardiovascular diseases in Prague</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kysely, Jan; Plavcova, Eva</p> <p>2013-04-01</p> <p>Sudden weather changes have long been supposed to be associated with negative impacts on human health. However, relatively few studies attempted to quantify these relationships. In this study, we use large 6-hour changes of atmospheric sea level <span class="hlt">pressure</span> as proxy for sudden weather changes, and evaluate their association with hospital admissions for cardiovascular diseases. Winter and summer seasons and positive and negative <span class="hlt">pressure</span> changes are analyzed separately, using data for the city of Prague (population of 1.2 million) over 16-year period (1994-2009). We find that sudden <span class="hlt">pressure</span> <span class="hlt">drops</span> in winter are associated with significant increases in the number of hospital admissions. Increases in morbidity are not observed for <span class="hlt">pressure</span> <span class="hlt">drops</span> in summer, nor <span class="hlt">pressure</span> increases in any season. Analysis of synoptic weather maps shows that the large <span class="hlt">pressure</span> <span class="hlt">drops</span> in winter are associated with strong zonal (westerly) flow and rapidly moving low <span class="hlt">pressure</span> systems with centres over Northern Europe and atmospheric fronts affecting the area of Western and Central Europe. Several of the largest <span class="hlt">pressure</span> decreases were associated with infamous winter storms (such as Lothar on December 25, 1999 and Kyrill on January 18, 2007). Analysis of links between passages of strong atmospheric fronts and hospital admissions shows that the links are much weaker if weather changes are characterized by frontal passages. Since climate models project strengthening of the zonal circulation in winter and increased frequency of winter storms, the negative effects of such weather phenomena and their possible changes in a warmer climate of the 21st century need to be better understood, particularly as their importance in inducing excess morbidity and mortality in winter may increase compared to cold spells.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28478681','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28478681"><span>Sensitive Determination of Cd in Small-Volume Samples by Miniaturized Liquid <span class="hlt">Drop</span> Anode Atmospheric <span class="hlt">Pressure</span> Glow Discharge Optical Emission Spectrometry.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Jamroz, Piotr; Greda, Krzysztof; Dzimitrowicz, Anna; Swiderski, Krzysztof; Pohl, Pawel</p> <p>2017-06-06</p> <p>A novel liquid <span class="hlt">drop</span> anode (LDA) direct current atmospheric <span class="hlt">pressure</span> glow discharge (dc-APGD) system was applied for direct determination of Cd in liquid microsamples (50 μL) by optical emission spectrometry (OES). The microdischarge was generated in open-to-<span class="hlt">air</span> atmosphere between a solid pin type tungsten cathode and a liquid <span class="hlt">drop</span> placed on a graphite disk anode. The arrangement of the graphite disk placed on a PTFE chip platform as well as the solid pin type cathode was simple and robust. The limit of detection (LOD) of Cd for the developed LDA-APGD-OES method was 0.20-0.40 μg L -1 , while precision (as the relative standard deviation for the repeated measurements) was within 2-5%. By using the liquid <span class="hlt">drop</span> of 50 μL, the linearity range of 1-1000 μg L -1 was achieved. The effect of addition of the low-molecular weight (LMW) organic compounds, easily ionized elements (EIEs), i.e., Ca, K, Mg, and Na, as well as the foreign ions (Al, Cu, Fe, Mn, Zn) to the solution on the in situ atomization and excitation processes occurred during operation of the LDA-APGD system, and the response of Cd was studied. Validation of the proposed method was demonstrated by analysis of Lobster hepatopancreas (TORT-2), pig kidney (ERM-BB186), and groundwater (ERM-CA615) certified reference materials (CRMs) and recoveries of Cd from water samples spiked with 25 μg L -1 of Cd. Very good agreement between the found and certified values of Cd in the CRMs (the recoveries were within the range of 96.3-99.6%) indicated trueness of the method and its reliability for determination of traces of Cd. In the case of the spiked water samples, the recoveries obtained were in the range from 95.2 to 99.5%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15244616','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15244616"><span>Soft Listeria: actin-based propulsion of liquid <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Boukellal, Hakim; Campás, Otger; Joanny, Jean-François; Prost, Jacques; Sykes, Cécile</p> <p>2004-06-01</p> <p>We study the motion of oil <span class="hlt">drops</span> propelled by actin polymerization in cell extracts. <span class="hlt">Drops</span> deform and acquire a pearlike shape under the action of the elastic stresses exerted by the actin comet, a tail of cross-linked actin filaments. We solve this free boundary problem and calculate the <span class="hlt">drop</span> shape taking into account the elasticity of the actin gel and the variation of the polymerization velocity with normal stress. The <span class="hlt">pressure</span> balance on the liquid <span class="hlt">drop</span> imposes a zero propulsive force if gradients in surface tension or internal <span class="hlt">pressure</span> are not taken into account. Quantitative parameters of actin polymerization are obtained by fitting theory to experiment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2004ASAJ..115R2419M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2004ASAJ..115R2419M"><span>Shape oscillations of acoustically levitated <span class="hlt">drops</span> in water: Early research with Bob Apfel on modulated radiation <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Marston, Philip L.</p> <p>2004-05-01</p> <p>In 1976, research in collaboration with Bob Apfel demonstrated that low-frequency shape oscillations of hydrocarbon <span class="hlt">drops</span> levitated in water could be driven using modulated radiation <span class="hlt">pressure</span>. While that response to modulated ultrasound was subsequently extended to a range of systems, the emphasis here is to recall the initial stages of development in Bob Apfel's laboratory leading to some publications [P. L. Marston and R. E. Apfel, J. Colloid Interface Sci. 68, 280-286 (1979); J. Acoust. Soc. Am. 67, 27-37 (1980)]. The levitation technology used at that time was such that it was helpful to develop a sensitive method for detecting weak oscillations using the interference pattern in laser light scattered by levitated <span class="hlt">drops</span>. The initial experiments to verify this scattering method used shape oscillations induced by modulated electric fields within the acoustic levitator. Light scattering was subsequently used to detect shape oscillations induced by amplitude modulating a carrier having a high frequency (around 680 kHz) at a resonance of the transducer. Methods were also developed for quantitative measurements of the <span class="hlt">drop</span>'s response and with improved acoustic coupling <span class="hlt">drop</span> fission was observed. The connection with research currently supported by NASA will also be noted.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS.995a2051A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS.995a2051A"><span>Preliminary Investigation on the Behavior of Pore <span class="hlt">Air</span> <span class="hlt">Pressure</span> During Rainfall Infiltration</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ashraf Mohamad Ismail, Mohd; Min, Ng Soon; Hasliza Hamzah, Nur; Hazreek Zainal Abidin, Mohd; Madun, Aziman; Tajudin, Saiful Azhar Ahmad</p> <p>2018-04-01</p> <p>This paper focused on the preliminary investigation of pore <span class="hlt">air</span> <span class="hlt">pressure</span> behaviour during rainfall infiltration in order to substantiate the mechanism of rainfall induced slope failure. The actual behaviour or pore <span class="hlt">air</span> <span class="hlt">pressure</span> during infiltration is yet to be clearly understood as it is regularly assumed as atmospheric. Numerical modelling of one dimensional (1D) soil column was utilized in this study to provide a preliminary insight of this highlighted uncertainty. Parametric study was performed by using rainfall intensities of 1.85 x 10-3m/s and 1.16 x 10-4m/s applied on glass beads to simulate intense and modest rainfall conditions. Analysis results show that the high rainfall intensity causes more development of pore <span class="hlt">air</span> <span class="hlt">pressure</span> compared to low rainfall intensity. This is because at high rainfall intensity, the rainwater cannot replace the pore <span class="hlt">air</span> smoothly thus confining the pore <span class="hlt">air</span>. Therefore, the effect of pore <span class="hlt">air</span> <span class="hlt">pressure</span> has to be taken into consideration particularly during heavy rainfall.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25553669','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25553669"><span>In vitro comparison of Günther Tulip and Celect filters: testing filtering efficiency and <span class="hlt">pressure</span> <span class="hlt">drop</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nicolas, M; Malvé, M; Peña, E; Martínez, M A; Leask, R</p> <p>2015-02-05</p> <p>In this study, the trapping ability of the Günther Tulip and Celect inferior vena cava filters was evaluated. Thrombus capture rates of the filters were tested in vitro in horizontal position with thrombus diameters of 3 and 6mm and tube diameter of 19mm. The filters were tested in centered and tilted positions. Sets of 30 clots were injected into the model and the same process was repeated 20 times for each different condition simulated. <span class="hlt">Pressure</span> <span class="hlt">drop</span> experienced along the system was also measured and the percentage of clots captured was recorded. The Günther Tulip filter showed superiority in all cases, trapping almost 100% of 6mm clots both in an eccentric and tilted position and trapping 81.7% of the 3mm clots in a centered position and 69.3% in a maximum tilted position. The efficiency of all filters tested decreased as the size of the embolus decreased and as the filter was tilted. The injection of 6 clots raised the <span class="hlt">pressure</span> <span class="hlt">drop</span> to 4.1mmHg, which is a reasonable value that does not cause the obstruction of blood flow through the system. Copyright © 2014 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26223846','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26223846"><span>Feasibility of granular bed filtration of an aerosol of ultrafine metallic particles including a <span class="hlt">pressure</span> <span class="hlt">drop</span> regeneration system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bémer, D; Wingert, L; Morele, Y; Subra, I</p> <p>2015-09-01</p> <p>A process for filtering an aerosol of ultrafine metallic particles (UFP) has been designed and tested, based on the principle of a multistage granular bed. The filtration system comprised a succession of granular beds of varying thickness composed of glass beads of different diameters. This system allows the <span class="hlt">pressure</span> <span class="hlt">drop</span> to be regenerated during filtration ("on-line" mode) using a vibrating probe. Tests monitoring the <span class="hlt">pressure</span> <span class="hlt">drop</span> were conducted on a "10-L/min" low airflow rate device and on a "100-m(3)/hr" prototype. Granular bed unclogging is automated on the latter. The cyclic operation and filtration performances are similar to that of filter medium-based industrial dust collectors. Filtration of ultrafine metallic particles generated by different industrial processes such as arc welding, metal cutting, or spraying constitutes a difficult problem due to the high filter clogging properties of these particles and to the high temperatures generally encountered. Granular beds represent an advantageous means of filtering these aerosols with difficult properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22300638','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22300638"><span>Bed mixing and leachate recycling strategies to overcome <span class="hlt">pressure</span> <span class="hlt">drop</span> buildup in the biofiltration of hydrogen sulfide.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Roshani, Babak; Torkian, Ayoob; Aslani, Hasan; Dehghanzadeh, Reza</p> <p>2012-04-01</p> <p>The effects of leachate recycling and bed mixing on the removal rate of H(2)S from waste gas stream were investigated. The experimental setup consisted of an epoxy-coated three-section biofilter with an ID of 8 cm and effective bed height of 120 cm. Bed material consisted of municipal solid waste compost and PVC bits with an overall porosity of 54% and dry bulk density of 0.456 g cm(-3). Leachate recycling had a positive effect of increasing elimination capacity (EC) up to 21 g S m(-3) bed h(-1) at recycling rates of 75 ml d(-1), but in the bed mixing period EC declined to 8 g S m(-3) bed h(-1). <span class="hlt">Pressure</span> <span class="hlt">drop</span> had a range of zero to 18 mm H(2)O m(-1) in the course of leachate recycling. Accumulation of sulfur reduced removal efficiency and increased <span class="hlt">pressure</span> <span class="hlt">drop</span> up to 110 mm H(2)O m(-1) filter during the bed mixing stage. Copyright © 2012 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1995PhFl....7.1545S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1995PhFl....7.1545S"><span>Oscillations of a deformed liquid <span class="hlt">drop</span> in an acoustic field</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shi, Tao; Apfel, Robert E.</p> <p>1995-07-01</p> <p>The oscillations of an axially symmetric liquid <span class="hlt">drop</span> in an acoustic standing wave field in <span class="hlt">air</span> have been studied using the boundary integral method. The interaction between the <span class="hlt">drop</span> oscillation and sound field has been included in this analysis. Our computations focus on the frequency shift of small-amplitude oscillations of an acoustically deformed <span class="hlt">drop</span> typical of a <span class="hlt">drop</span> levitated in <span class="hlt">air</span>. In the presence or absence of gravity, the trend and the magnitude of the frequency shift have been given in terms of <span class="hlt">drop</span> size, <span class="hlt">drop</span> deformation, and the strength of the sound field. Our calculations are compared with experiments performed on the United States Microgravity Laboratory (USML-1) and with ground-based measurements, and are found to be in good agreement within the accuracy of the experimental data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26282384','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26282384"><span>The influence of intraocular <span class="hlt">pressure</span> and <span class="hlt">air</span> jet <span class="hlt">pressure</span> on corneal contactless tonometry tests.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Simonini, Irene; Pandolfi, Anna</p> <p>2016-05-01</p> <p>The <span class="hlt">air</span> puff is a dynamic contactless tonometer test used in ophthalmology clinical practice to assess the biomechanical properties of the human cornea and the intraocular <span class="hlt">pressure</span> due to the filling fluids of the eye. The test is controversial, since the dynamic response of the cornea is governed by the interaction of several factors which cannot be discerned within a single measurement. In this study we describe a numerical model of the <span class="hlt">air</span> puff tests, and perform a parametric analysis on the major action parameters (jet <span class="hlt">pressure</span> and intraocular <span class="hlt">pressure</span>) to assess their relevance on the mechanical response of a patient-specific cornea. The particular cornea considered here has been treated with laser reprofiling to correct myopia, and the parametric study has been conducted on both the preoperative and postoperative geometries. The material properties of the cornea have been obtained by means of an identification procedure that compares the static biomechanical response of preoperative and postoperative corneas under the physiological IOP. The parametric study on the intraocular <span class="hlt">pressure</span> suggests that the displacement of the cornea׳s apex can be a reliable indicator for tonometry, and the one on the <span class="hlt">air</span> jet <span class="hlt">pressure</span> predicts the outcomes of two or more distinct measurements on the same cornea, which can be used in inverse procedures to estimate the material properties of the tissue. Copyright © 2015 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080008680','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080008680"><span>Method and apparatus for monitoring oxygen partial <span class="hlt">pressure</span> in <span class="hlt">air</span> masks</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kelly, Mark E. (Inventor); Pettit, Donald R. (Inventor)</p> <p>2006-01-01</p> <p>Method and apparatus are disclosed for monitoring an oxygen partial <span class="hlt">pressure</span> in an <span class="hlt">air</span> mask and providing a tactile warning to the user. The oxygen partial <span class="hlt">pressure</span> in the <span class="hlt">air</span> mask is detected using an electrochemical sensor, the output signal from which is provided to a comparator. The comparator compares the output signal with a preset reference value or range of values representing acceptable oxygen partial <span class="hlt">pressures</span>. If the output signal is different than the reference value or outside the range of values, the <span class="hlt">air</span> mask is vibrated by a vibrating motor to alert the user to a potentially hypoxic condition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25085005','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25085005"><span>Prosthetics socket that incorporates an <span class="hlt">air</span> splint system focusing on dynamic interface <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razak, Nasrul Anuar Abd; Osman, Noor Azuan Abu; Gholizadeh, Hossein; Ali, Sadeeq</p> <p>2014-08-01</p> <p>The interface <span class="hlt">pressure</span> between the residual limb and prosthetic socket has a significant effect on an amputee's satisfaction and comfort. This paper presents the design and performance of a new prosthetic socket that uses an <span class="hlt">air</span> splint system. The <span class="hlt">air</span> splint prosthetic socket system was implemented by combining the <span class="hlt">air</span> splint with a <span class="hlt">pressure</span> sensor that the transhumeral user controls through the use of a microcontroller. The modular construction of the system developed allows the FSR <span class="hlt">pressure</span> sensors that are placed inside the <span class="hlt">air</span> splint socket to determine the required size and fitting for the socket used. Fifteen transhumeral amputees participated in the study. The subject's dynamic <span class="hlt">pressure</span> on the socket that's applied while wearing the <span class="hlt">air</span> splint systems was recorded using F-socket transducers and microcontroller analysis. The values collected by the F-socket sensor for the <span class="hlt">air</span> splint prosthetic socket system were determined accordingly by comparing the dynamic <span class="hlt">pressure</span> applied using statically socket. The <span class="hlt">pressure</span> volume of the <span class="hlt">air</span> splint fluctuated and was recorded at an average of 38 kPa (2.5) to 41 kPa (1.3) over three hours. The <span class="hlt">air</span> splint socket might reduce the <span class="hlt">pressure</span> within the interface of residual limb. This is particularly important during the daily life activities and may reduce the pain and discomfort at the residual limb in comparison to the static socket. The potential development of an auto-adjusted socket that uses an <span class="hlt">air</span> splint system as the prosthetic socket will be of interest to researchers involved in rehabilitation engineering, prosthetics and orthotics.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_12 --> <div id="page_13" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="241"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22036812-correlation-current-drop-filling-gas-pressure-ion-beam-emission-low-energy-mather-type-plasma-focus-device','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22036812-correlation-current-drop-filling-gas-pressure-ion-beam-emission-low-energy-mather-type-plasma-focus-device"><span>Correlation of current <span class="hlt">drop</span>, filling gas <span class="hlt">pressure</span>, and ion beam emission in a low energy Mather-type plasma focus device</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Behbahani, R. A.; Aghamir, F. M.</p> <p></p> <p>The behavior of current <span class="hlt">drop</span> and its correlation with ion beam emission during the radial phase of a high inductance low energy Mather type plasma focus device have been studied. The study includes two ranges of filling gas <span class="hlt">pressure</span>, namely the low range of 0.2-0.8 mbar and the high range of 0.8-1.5 mbar. Two different current simulation processes were performed to aid the interpretation of the experimental results. Within the low range of operating <span class="hlt">pressure</span>, an acceptable match between the computed and experimental current signals was achieved when the effects of anomalous resistances were contemplated. While in the high rangemore » of <span class="hlt">pressure</span>, the computed and experimental current traces were in line even without considering the effects of anomalous resistances. The analysis shows that by decreasing the filling gas <span class="hlt">pressure</span> the effects of instabilities are intensified. The computed and experimental current traces, along with ion beam signals gathered from a faraday cup, show that there is a strong correlation between the intensity of ion beam and its duration with the current <span class="hlt">drop</span> during the radial phase.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920034807&hterms=momentum+bernoulli&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dmomentum%2Bbernoulli','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920034807&hterms=momentum+bernoulli&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dmomentum%2Bbernoulli"><span>Nonlinear oscillations of inviscid free <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Patzek, T. W.; Benner, R. E., Jr.; Basaran, O. A.; Scriven, L. E.</p> <p>1991-01-01</p> <p>The present analysis of free liquid <span class="hlt">drops</span>' inviscid oscillations proceeds through solution of Bernoulli's equation to obtain the free surface shape and of Laplace's equation for the velocity potential field. Results thus obtained encompass <span class="hlt">drop</span>-shape sequences, <span class="hlt">pressure</span> distributions, particle paths, and the temporal evolution of kinetic and surface energies; accuracy is verified by the near-constant <span class="hlt">drop</span> volume and total energy, as well as the diminutiveness of mass and momentum fluxes across <span class="hlt">drop</span> surfaces. Further insight into the nature of oscillations is provided by Fourier power spectrum analyses of mode interactions and frequency shifts.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990019812','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990019812"><span>Bubble and <span class="hlt">Drop</span> Nonlinear Dynamics (BDND)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Trinh, E. H.; Leal, L. Gary; Thomas, D. A.; Crouch, R. K.</p> <p>1998-01-01</p> <p>Free <span class="hlt">drops</span> and bubbles are weakly nonlinear mechanical systems that are relatively simple to characterize experimentally in 1-G as well as in microgravity. The understanding of the details of their motion contributes to the fundamental study of nonlinear phenomena and to the measurement of the thermophysical properties of freely levitated melts. The goal of this Glovebox-based experimental investigation is the low-gravity assessment of the capabilities of a modular apparatus based on ultrasonic resonators and on the pseudo- extinction optical method. The required experimental task is the accurate measurements of the large-amplitude dynamics of free <span class="hlt">drops</span> and bubbles in the absence of large biasing influences such as gravity and levitation fields. A single-axis levitator used for the positioning of <span class="hlt">drops</span> in <span class="hlt">air</span>, and an ultrasonic water-filled resonator for the trapping of <span class="hlt">air</span> bubbles have been evaluated in low-gravity and in 1-G. The basic feasibility of <span class="hlt">drop</span> positioning and shape oscillations measurements has been verified by using a laptop-interfaced automated data acquisition and the optical extinction technique. The major purpose of the investigation was to identify the salient technical issues associated with the development of a full-scale Microgravity experiment on single <span class="hlt">drop</span> and bubble dynamics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4120006','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4120006"><span>Prosthetics socket that incorporates an <span class="hlt">air</span> splint system focusing on dynamic interface <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2014-01-01</p> <p>Background The interface <span class="hlt">pressure</span> between the residual limb and prosthetic socket has a significant effect on an amputee’s satisfaction and comfort. This paper presents the design and performance of a new prosthetic socket that uses an <span class="hlt">air</span> splint system. Methods The <span class="hlt">air</span> splint prosthetic socket system was implemented by combining the <span class="hlt">air</span> splint with a <span class="hlt">pressure</span> sensor that the transhumeral user controls through the use of a microcontroller. The modular construction of the system developed allows the FSR <span class="hlt">pressure</span> sensors that are placed inside the <span class="hlt">air</span> splint socket to determine the required size and fitting for the socket used. Fifteen transhumeral amputees participated in the study. Results The subject’s dynamic <span class="hlt">pressure</span> on the socket that’s applied while wearing the <span class="hlt">air</span> splint systems was recorded using F-socket transducers and microcontroller analysis. The values collected by the F-socket sensor for the <span class="hlt">air</span> splint prosthetic socket system were determined accordingly by comparing the dynamic <span class="hlt">pressure</span> applied using statically socket. The <span class="hlt">pressure</span> volume of the <span class="hlt">air</span> splint fluctuated and was recorded at an average of 38 kPa (2.5) to 41 kPa (1.3) over three hours. Conclusion The <span class="hlt">air</span> splint socket might reduce the <span class="hlt">pressure</span> within the interface of residual limb. This is particularly important during the daily life activities and may reduce the pain and discomfort at the residual limb in comparison to the static socket. The potential development of an auto-adjusted socket that uses an <span class="hlt">air</span> splint system as the prosthetic socket will be of interest to researchers involved in rehabilitation engineering, prosthetics and orthotics. PMID:25085005</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title49-vol5/pdf/CFR-2011-title49-vol5-sec393-51.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title49-vol5/pdf/CFR-2011-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-10-01</p> <p>... 49 Transportation 5 2011-10-01 2011-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraphs (b), (c), (d) or (e) of this section. (b) Hydraulic brakes. Vehicles manufactured on or after...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol5/pdf/CFR-2014-title49-vol5-sec393-51.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title49-vol5/pdf/CFR-2014-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... 49 Transportation 5 2014-10-01 2014-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraphs (b), (c), (d) or (e) of this section. (b) Hydraulic brakes. Vehicles manufactured on or after...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083221','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083221"><span>Simple Experiments for Teaching <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Shamsipour, Gholamreza</p> <p>2006-01-01</p> <p>Everyone who teaches physics knows very well that sometimes a simple device or experiment can help to make a concept clear. In this paper, inspired by "The Jumping Pencil" by Martin Gardner, I will discuss a simple demonstration device that can be used to start the study of <span class="hlt">air</span> <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://files.eric.ed.gov/fulltext/EJ1138838.pdf','ERIC'); return false;" href="http://files.eric.ed.gov/fulltext/EJ1138838.pdf"><span>Influence of Peer <span class="hlt">Pressure</span> on Secondary School Students <span class="hlt">Drop</span> out in Rongo Sub-County, Migori County, Kenya</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Omollo, Atieno Evaline; Yambo, Onyango J. M.</p> <p>2017-01-01</p> <p>The purpose of this study was to establish the influence of peer <span class="hlt">pressure</span> on secondary school students' <span class="hlt">drop</span> out in Rongo Sub-County, Migori County, Kenya. The statement of the problem showed that the sub-county had a dropout rate of 43 percent as compared to the neighboring sub counties like Uriri, Awendo, Nyatike, Kuria and Migori which had 25,…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol5/pdf/CFR-2013-title49-vol5-sec393-51.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title49-vol5/pdf/CFR-2013-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... 49 Transportation 5 2013-10-01 2013-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraph (f), must be equipped with a signal that provides a warning to the driver when a failure occurs in...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol5/pdf/CFR-2012-title49-vol5-sec393-51.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title49-vol5/pdf/CFR-2012-title49-vol5-sec393-51.pdf"><span>49 CFR 393.51 - Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... 49 Transportation 5 2012-10-01 2012-10-01 false Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span> and vacuum gauges... REGULATIONS PARTS AND ACCESSORIES NECESSARY FOR SAFE OPERATION Brakes § 393.51 Warning signals, <span class="hlt">air</span> <span class="hlt">pressure</span>... paragraph (f), must be equipped with a signal that provides a warning to the driver when a failure occurs in...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDL12008K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDL12008K"><span>Spread of pathogens through rain <span class="hlt">drop</span> impact</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Seungho; Gruszewski, Hope; Gidley, Todd; Schmale, David G., III; Jung, Sunghwan</p> <p>2017-11-01</p> <p>Rain <span class="hlt">drop</span> impact can disperse micron-sized pathogenic particles over long distances. In this study, we aim to elucidate mechanisms for disease dispersal when a rain <span class="hlt">drop</span> impacts a particle-laden solid surface. Three different dispersal types were observed depending on whether the dispersed glass particles were dry or wet. For a dry particle dispersal, the movement of contact line made the particles initially jump off the surface with relatively high velocity. Then, <span class="hlt">air</span> vortex was formed due to the <span class="hlt">air</span> current entrained along with the falling <span class="hlt">drop</span>, and advected the particles with relatively low velocity. For a wet particle dispersal, the contact line of a spreading liquid became unstable due to the presence of the particles on the substrate. This caused splashing at the contact line and ejected liquid droplets carrying the particles. Finally, we released a <span class="hlt">drop</span> onto wheat plants infected with the rust fungus, Puccinia triticina, and found that nearly all of the satellite droplets from a single <span class="hlt">drop</span> contained at least one rust spore. Also, we visualized such novel dispersal dynamics with a high-speed camera and characterized their features by scaling models. This research was partially supported by National Science Foundation Grant CBET-1604424.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..274a2046S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..274a2046S"><span>Simulation and Experiment Research on Fatigue Life of High <span class="hlt">Pressure</span> <span class="hlt">Air</span> Pipeline Joint</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shang, Jin; Xie, Jianghui; Yu, Jian; Zhang, Deman</p> <p>2017-12-01</p> <p>High <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint is important part of high <span class="hlt">pressure</span> <span class="hlt">air</span> system, whose reliability is related to the safety and stability of the system. This thesis developed a new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint, carried out dynamics research on CB316-1995 and new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint with finite element method, deeply analysed the join forms of different design schemes and effect of materials on stress, tightening torque and fatigue life of joint. Research team set up vibration/pulse test bench, carried out joint fatigue life contrast test. The result shows: the maximum stress of the joint is inverted in the inner side of the outer sleeve nut, which is consistent with the failure mode of the crack on the outer sleeve nut in practice. Simulation and experiment of fatigue life and tightening torque of new type-high <span class="hlt">pressure</span> <span class="hlt">air</span> pipeline joint are better than CB316-1995 joint.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19821629','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19821629"><span><span class="hlt">Drop</span> impact upon micro- and nanostructured superhydrophobic surfaces.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tsai, Peichun; Pacheco, Sergio; Pirat, Christophe; Lefferts, Leon; Lohse, Detlef</p> <p>2009-10-20</p> <p>We experimentally investigate <span class="hlt">drop</span> impact dynamics onto different superhydrophobic surfaces, consisting of regular polymeric micropatterns and rough carbon nanofibers, with similar static contact angles. The main control parameters are the Weber number We and the roughness of the surface. At small We, i.e., small impact velocity, the impact evolutions are similar for both types of substrates, exhibiting Fakir state, complete bouncing, partial rebouncing, trapping of an <span class="hlt">air</span> bubble, jetting, and sticky vibrating water balls. At large We, splashing impacts emerge forming several satellite droplets, which are more pronounced for the multiscale rough carbon nanofiber jungles. The results imply that the multiscale surface roughness at nanoscale plays a minor role in the impact events for small We less than or approximately equal 120 but an important one for large We greater than or approximately equal 120. Finally, we find the effect of ambient <span class="hlt">air</span> <span class="hlt">pressure</span> to be negligible in the explored parameter regime We less than or approximately equal 150.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930081405','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930081405"><span>Compression-ignition Engine Performance at Altitudes and at Various <span class="hlt">Air</span> <span class="hlt">Pressures</span> and Temperatures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moore, Charles S; Collins, John H</p> <p>1937-01-01</p> <p>Engine test results are presented for simulated altitude conditions. A displaced-piston combustion chamber on a 5- by 7-inch single cylinder compression-ignition engine operating at 2,000 r.p.m. was used. Inlet <span class="hlt">air</span> temperature equivalent to standard altitudes up to 14,000 feet were obtained. Comparison between performance at altitude of the unsupercharged compression-ignition engine compared favorably with the carburetor engine. Analysis of the results for which the inlet <span class="hlt">air</span> temperature, inlet <span class="hlt">air</span> <span class="hlt">pressure</span>, and inlet and exhaust <span class="hlt">pressure</span> were varied indicates that engine performance cannot be reliably corrected on the basis of inlet <span class="hlt">air</span> density or weight of <span class="hlt">air</span> charge. Engine power increases with inlet <span class="hlt">air</span> <span class="hlt">pressure</span> and decreases with inlet <span class="hlt">air</span> temperatures very nearly as straight line relations over a wide range of <span class="hlt">air</span>-fuel ratios. Correction factors are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21889152','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21889152"><span><span class="hlt">Drop</span> shape visualization and contact angle measurement on curved surfaces.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Guilizzoni, Manfredo</p> <p>2011-12-01</p> <p>The shape and contact angles of <span class="hlt">drops</span> on curved surfaces is experimentally investigated. Image processing, spline fitting and numerical integration are used to extract the <span class="hlt">drop</span> contour in a number of cross-sections. The three-dimensional surfaces which describe the surface-<span class="hlt">air</span> and <span class="hlt">drop-air</span> interfaces can be visualized and a simple procedure to determine the equilibrium contact angle starting from measurements on curved surfaces is proposed. Contact angles on flat surfaces serve as a reference term and a procedure to measure them is proposed. Such procedure is not as accurate as the axisymmetric <span class="hlt">drop</span> shape analysis algorithms, but it has the advantage of requiring only a side view of the <span class="hlt">drop</span>-surface couple and no further information. It can therefore be used also for fluids with unknown surface tension and there is no need to measure the <span class="hlt">drop</span> volume. Examples of application of the proposed techniques for distilled water <span class="hlt">drops</span> on gemstones confirm that they can be useful for <span class="hlt">drop</span> shape analysis and contact angle measurement on three-dimensional sculptured surfaces. Copyright © 2011 Elsevier Inc. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993PhDT.......155W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993PhDT.......155W"><span>O the Electrohydrodynamics of <span class="hlt">Drop</span> Extraction from a Conductive Liquid Meniscus</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wright, Graham Scott</p> <p></p> <p>This thesis is concerned with the use of an electric field in the extraction of liquid <span class="hlt">drops</span> from a capillary orifice or nozzle. The motivating application is ink jet printing. Current <span class="hlt">drop</span>-on-demand ink jets use <span class="hlt">pressure</span> pulses to eject <span class="hlt">drops</span>. Literature on electrostatic spraying suggests that by using an electric field, <span class="hlt">drops</span> could be produced with a wider range of sizes and speeds than is possible with <span class="hlt">pressure</span> ejection. Previous efforts to apply electric spraying to printing or similar selective coating tasks have taken an experimental approach based on steady or periodic spraying phenomena, without attempting cycle -by-cycle <span class="hlt">drop</span> control. The centerpiece of this thesis is a simulation tool developed to explore such possibilities. A simplified analytic model is developed as a preliminary step, yielding formulas for force and time scales that provide an appropriate basis for nondimensionalization of the governing differential equations; important dimensionless parameters are identified. The complete self-consistent model permits simulation of meniscus behavior under time -varying applied voltage or <span class="hlt">pressure</span>, with the electric field solution continually updated as the surface changes shape. The model uses a quasi-one-dimensional hydrodynamic formulation and a two-dimensional axisymmetric boundary element solution for the electric field. The simulation is checked against experimental results for meniscus stability, resonant modes, and <span class="hlt">drop</span> emission under electric field. The simulation faithfully captures important qualitative aspects of meniscus behavior and gives reasonable quantitative agreement within the limitations of the model. Insights gained in simulation point the way to a successful laboratory demonstration of <span class="hlt">drop</span> extraction using a shaped voltage pulse. <span class="hlt">Drop</span> size control is pursued in simulation using <span class="hlt">pressure</span> and voltage pulses both alone and in combination, for both light and viscous liquids. Combining <span class="hlt">pressure</span> and field pulses is shown to be</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20737925','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20737925"><span>Compressed-<span class="hlt">air</span> work is entering the field of high <span class="hlt">pressures</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Le Péchon, J Cl; Gourdon, G</p> <p>2010-01-01</p> <p>Since 1850, compressed-<span class="hlt">air</span> work has been used to prevent shafts or tunnels under construction from flooding. Until the 1980s, workers were digging in compressed-<span class="hlt">air</span> environments. Since the introduction of tunnel boring machines (TBMs), very little digging under <span class="hlt">pressure</span> is needed. However, the wearing out of cutter-head tools requires inspection and repair. Compressed-<span class="hlt">air</span> workers enter the <span class="hlt">pressurized</span> working chamber only occasionally to perform such repairs. <span class="hlt">Pressures</span> between 3.5 and 4.5 bar, that stand outside a reasonable range for <span class="hlt">air</span> breathing, were reached by 2002. Offshore deep diving technology had to be adapted to TBM work. Several sites have used mixed gases: in Japan for deep shaft sinking (4.8 bar), in The Netherlands at Western Scheldt Tunnels (6.9 bar), in Russia for St. Petersburg Metro (5.8 bar) and in the United States at Seattle (5.8 bar). Several tunnel projects are in progress that may involve higher <span class="hlt">pressures</span>: Hallandsås (Sweden) interventions in heliox saturation up to 13 bar, and Lake Mead (U.S.) interventions to about 12 bar (2010). Research on TBMs and grouting technologies tries to reduce the requirements for hyperbaric works. Adapted international rules, expertise and services for saturation work, shuttles and trained personnel matching industrial requirements are the challenges.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5936785','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5936785"><span>Left Ventricular Trabeculations Decrease the Wall Shear Stress and Increase the Intra-Ventricular <span class="hlt">Pressure</span> <span class="hlt">Drop</span> in CFD Simulations</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Sacco, Federica; Paun, Bruno; Lehmkuhl, Oriol; Iles, Tinen L.; Iaizzo, Paul A.; Houzeaux, Guillaume; Vázquez, Mariano; Butakoff, Constantine; Aguado-Sierra, Jazmin</p> <p>2018-01-01</p> <p>The aim of the present study is to characterize the hemodynamics of left ventricular (LV) geometries to examine the impact of trabeculae and papillary muscles (PMs) on blood flow using high performance computing (HPC). Five pairs of detailed and smoothed LV endocardium models were reconstructed from high-resolution magnetic resonance images (MRI) of ex-vivo human hearts. The detailed model of one LV pair is characterized only by the PMs and few big trabeculae, to represent state of art level of endocardial detail. The other four detailed models obtained include instead endocardial structures measuring ≥1 mm2 in cross-sectional area. The geometrical characterizations were done using computational fluid dynamics (CFD) simulations with rigid walls and both constant and transient flow inputs on the detailed and smoothed models for comparison. These simulations do not represent a clinical or physiological scenario, but a characterization of the interaction of endocardial structures with blood flow. Steady flow simulations were employed to quantify the <span class="hlt">pressure</span> <span class="hlt">drop</span> between the inlet and the outlet of the LVs and the wall shear stress (WSS). Coherent structures were analyzed using the Q-criterion for both constant and transient flow inputs. Our results show that trabeculae and PMs increase the intra-ventricular <span class="hlt">pressure</span> <span class="hlt">drop</span>, reduce the WSS and disrupt the dominant single vortex, usually present in the smoothed-endocardium models, generating secondary small vortices. Given that obtaining high resolution anatomical detail is challenging in-vivo, we propose that the effect of trabeculations can be incorporated into smoothed ventricular geometries by adding a porous layer along the LV endocardial wall. Results show that a porous layer of a thickness of 1.2·10−2 m with a porosity of 20 kg/m2 on the smoothed-endocardium ventricle models approximates the <span class="hlt">pressure</span> <span class="hlt">drops</span>, vorticities and WSS observed in the detailed models. PMID:29760665</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5228218','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5228218"><span>Impacts of Changes of Indoor <span class="hlt">Air</span> <span class="hlt">Pressure</span> and <span class="hlt">Air</span> Exchange Rate in Vapor Intrusion Scenarios</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Shen, Rui; Suuberg, Eric M.</p> <p>2016-01-01</p> <p>There has, in recent years, been increasing interest in understanding the transport processes of relevance in vapor intrusion of volatile organic compounds (VOCs) into buildings on contaminated sites. These studies have included fate and transport modeling. Most such models have simplified the prediction of indoor <span class="hlt">air</span> contaminant vapor concentrations by employing a steady state assumption, which often results in difficulties in reconciling these results with field measurements. This paper focuses on two major factors that may be subject to significant transients in vapor intrusion situations, including the indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and the <span class="hlt">air</span> exchange rate in the subject building. A three-dimensional finite element model was employed with consideration of daily and seasonal variations in these factors. From the results, the variations of indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and <span class="hlt">air</span> exchange rate are seen to contribute to significant variations in indoor <span class="hlt">air</span> contaminant vapor concentrations. Depending upon the assumptions regarding the variations in these parameters, the results are only sometimes consistent with the reports of several orders of magnitude in indoor <span class="hlt">air</span> concentration variations from field studies. The results point to the need to examine more carefully the interplay of these factors in order to quantitatively understand the variations in potential indoor <span class="hlt">air</span> exposures. PMID:28090133</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28090133','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28090133"><span>Impacts of Changes of Indoor <span class="hlt">Air</span> <span class="hlt">Pressure</span> and <span class="hlt">Air</span> Exchange Rate in Vapor Intrusion Scenarios.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shen, Rui; Suuberg, Eric M</p> <p>2016-02-01</p> <p>There has, in recent years, been increasing interest in understanding the transport processes of relevance in vapor intrusion of volatile organic compounds (VOCs) into buildings on contaminated sites. These studies have included fate and transport modeling. Most such models have simplified the prediction of indoor <span class="hlt">air</span> contaminant vapor concentrations by employing a steady state assumption, which often results in difficulties in reconciling these results with field measurements. This paper focuses on two major factors that may be subject to significant transients in vapor intrusion situations, including the indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and the <span class="hlt">air</span> exchange rate in the subject building. A three-dimensional finite element model was employed with consideration of daily and seasonal variations in these factors. From the results, the variations of indoor <span class="hlt">air</span> <span class="hlt">pressure</span> and <span class="hlt">air</span> exchange rate are seen to contribute to significant variations in indoor <span class="hlt">air</span> contaminant vapor concentrations. Depending upon the assumptions regarding the variations in these parameters, the results are only sometimes consistent with the reports of several orders of magnitude in indoor <span class="hlt">air</span> concentration variations from field studies. The results point to the need to examine more carefully the interplay of these factors in order to quantitatively understand the variations in potential indoor <span class="hlt">air</span> exposures.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_13 --> <div id="page_14" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="261"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012JPhCS.395a2038J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012JPhCS.395a2038J"><span>Measurement and modelling of forced convective heat transfer coefficient and <span class="hlt">pressure</span> <span class="hlt">drop</span> of Al2O3- and SiO2-water nanofluids</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Julia, J. E.; Hernández, L.; Martínez-Cuenca, R.; Hibiki, T.; Mondragón, R.; Segarra, C.; Jarque, J. C.</p> <p>2012-11-01</p> <p>Forced convective heat transfer coefficient and <span class="hlt">pressure</span> <span class="hlt">drop</span> of SiO2- and Al2O3-water nanofluids were characterized. The experimental facility was composed of thermal-hydraulic loop with a tank with an immersed heater, a centrifugal pump, a bypass with a globe valve, an electromagnetic flow-meter, a 18 kW in-line pre-heater, a test section with band heaters, a differential <span class="hlt">pressure</span> transducer and a heat exchanger. The test section consists of a 1000 mm long aluminium pipe with an inner diameter of 31.2 mm. Eighteen band heaters were placed all along the test section in order to provide a uniform heat flux. Heat transfer coefficient was calculated measuring fluid temperature using immersed thermocouples (Pt100) placed at both ends of the test section and surface thermocouples in 10 axial locations along the test section (Pt1000). The measurements have been performed for different nanoparticles (Al2O3 and SiO2 with primary size of 11 nm and 12 nm, respectively), volume concentrations (1% v., 5% v.), and flow rates (3 103Re<105). Maximum heat transfer coefficient enhancement (300%) and <span class="hlt">pressure</span> <span class="hlt">drop</span> penalty (1000%) is obtained with 5% v. SiO2 nanofluid. Existing correlations can predict, at least in a first approximation, the heat transfer coefficient and <span class="hlt">pressure</span> <span class="hlt">drop</span> of nanofluids if thermal conductivity, viscosity and specific heat were properly modelled.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016E%26ES...49b2006A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016E%26ES...49b2006A"><span><span class="hlt">Air</span> injection test on a Kaplan turbine: prototype - model comparison</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Angulo, M.; Rivetti, A.; Díaz, L.; Liscia, S.</p> <p>2016-11-01</p> <p><span class="hlt">Air</span> injection is a very well-known resource to reduce <span class="hlt">pressure</span> pulsation magnitude in turbines, especially on Francis type. In the case of large Kaplan designs, even when not so usual, it could be a solution to mitigate vibrations arising when tip vortex cavitation phenomenon becomes erosive and induces structural vibrations. In order to study this alternative, aeration tests were performed on a Kaplan turbine at model and prototype scales. The research was focused on efficiency of different <span class="hlt">air</span> flow rates injected in reducing vibrations, especially at the draft tube and the discharge ring and also in the efficiency <span class="hlt">drop</span> magnitude. It was found that results on both scales presents the same trend in particular for vibration levels at the discharge ring. The efficiency <span class="hlt">drop</span> was overestimated on model tests while on prototype were less than 0.2 % for all power output. On prototype, <span class="hlt">air</span> has a beneficial effect in reducing <span class="hlt">pressure</span> fluctuations up to 0.2 ‰ of <span class="hlt">air</span> flow rate. On model high speed image computing helped to quantify the volume of tip vortex cavitation that is strongly correlated with the vibration level. The hydrophone measurements did not capture the cavitation intensity when <span class="hlt">air</span> is injected, however on prototype, it was detected by a sonometer installed at the draft tube access gallery.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec57-13015.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>... 30 Mineral Resources 1 2010-07-01 2010-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and...-UNDERGROUND METAL AND NONMETAL MINES Compressed <span class="hlt">Air</span> and Boilers § 57.13015 Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec56-13015.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title30-vol1/pdf/CFR-2010-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>... 30 Mineral Resources 1 2010-07-01 2010-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and... METAL AND NONMETAL MINES Compressed <span class="hlt">Air</span> and Boilers § 56.13015 Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19770005057','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19770005057"><span>Cold-<span class="hlt">air</span> performance of a tip turbine designed to drive a lift fan. 1: Baseline performance</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Haas, J. E.; Kofskey, M. G.; Hotz, G. M.; Futral, S. M., Jr.</p> <p>1976-01-01</p> <p>Full admission baseline performance was obtained for a 0.4 linear scale of the LF460 lift fan turbine over a range of speeds and <span class="hlt">pressure</span> ratios without leakage <span class="hlt">air</span>. These cold-<span class="hlt">air</span> tests covered a range of speeds from 40 to 140 percent of design equivalent speed and a range of scroll inlet to diffuser exit static <span class="hlt">pressure</span> ratios from 2.0 to 4.2. Results are presented in terms of specific work, torque, mass flow, efficiency, and total <span class="hlt">pressure</span> <span class="hlt">drop</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091386','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091386"><span>Tables for <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zahm, A F; Louden, F A</p> <p>1930-01-01</p> <p>In Technical Report no. 247 of the National Advisory Committee for Aeronautics theoretical formulas are given from which was computed a table for the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds, such as those of aircraft and propeller blades. In that report, the table gave incompressible and adiabatic stop <span class="hlt">pressures</span> of <span class="hlt">air</span> for even-speed intervals in miles per hour and for some even-speed intervals in knots per hour. Table II of the present report extends the above-mentioned table by including the stop <span class="hlt">pressures</span> of <span class="hlt">air</span> for even-speed intervals in miles per hour, feet per-second, knots per hour, kilometers per hour, and meters per second. The <span class="hlt">pressure</span> values in table II are also more exact than values given in the previous table. To furnish the aeronautical engineer with ready numerical formulas for finding the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest, table I has been derived for the standard values specified below it. This table first presents the theoretical <span class="hlt">pressure</span>-speed formulas and their working forms in C. G. S. Units as given in NACA Technical Report No. 247, then furnishes additional working formulas for several special units of speed. (author)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010cosp...38.3367R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010cosp...38.3367R"><span><span class="hlt">Air</span> Circulation and Heat Exchange under Reduced <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rygalov, Vadim; Wheeler, Raymond; Dixon, Mike; Hillhouse, Len; Fowler, Philip</p> <p></p> <p>Low <span class="hlt">pressure</span> atmospheres were suggested for Space Greenhouses (SG) design to minimize sys-tem construction and re-supply materials, as well as system manufacturing and deployment costs. But rarified atmospheres modify heat exchange mechanisms what finally leads to alter-ations in thermal control for low <span class="hlt">pressure</span> closed environments. Under low atmospheric <span class="hlt">pressures</span> (e.g., lower than 25 kPa compare to 101.3 kPa for normal Earth atmosphere), convection is becoming replaced by diffusion and rate of heat exchange reduces significantly. During a period from 2001 to 2009, a series of hypobaric experiments were conducted at Space Life Sciences Lab (SLSLab) NASA's Kennedy Space Center and the Department of Space Studies, University of North Dakota. Findings from these experiments showed: -<span class="hlt">air</span> circulation rate decreases non-linearly with lowering of total atmospheric <span class="hlt">pressure</span>; -heat exchange slows down with <span class="hlt">pressure</span> decrease creating risk of thermal stress (elevated leaf tem-peratures) for plants in closed environments; -low <span class="hlt">pressure</span>-induced thermal stress could be reduced by either lowering system temperature set point or increasing forced convection rates (circulation fan power) within certain limits; <span class="hlt">Air</span> circulation is an important constituent of controlled environments and plays crucial role in material and heat exchange. Theoretical schematics and mathematical models are developed from a series of observations. These models can be used to establish optimal control algorithms for low <span class="hlt">pressure</span> environments, such as a space greenhouse, as well as assist in fundamental design concept developments for these or similar habitable structures.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDG12005R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDG12005R"><span>The Role of Drag Force in Shedding of Multiple Sessile <span class="hlt">Drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Razzaghi, Aysan; Banitabaei, Sayyed Hossein; Amirfazli, Alidad; -Team</p> <p>2017-11-01</p> <p>A sessile <span class="hlt">drop</span> placed on a solid surface can shed, if the drag force due to a shearing airflow overcomes the <span class="hlt">drop</span> adhesion to the surface. Sessile <span class="hlt">drop</span> shedding is of importance due to its applications in condensation, fuel cells, icing, etc. Majority of the studies so far have considered the shedding of a single sessile droplet; however, in the applications above, multiple sessile droplets appear on a surface. Shedding of sessile <span class="hlt">drops</span> in different arrangements, i.e. tandem, side by side, triangle, and rectangle have been investigated both experimentally and through VOF simulations. The minimum <span class="hlt">air</span> velocity (Ucr) at which the <span class="hlt">drop(s</span>) at the upstream dislodge from the surface was measured. <span class="hlt">Drops</span> were placed in a wind tunnel with increasing <span class="hlt">air</span> velocity at a rate of 1m/s2. It has been found that Ucr, deviates from its value for a single <span class="hlt">drop</span> due to presence of the neighboring <span class="hlt">drops</span>. The amount of the deviation is closely related to the flow pattern and interaction of <span class="hlt">drop</span> wakes which are elucidated numerically. The interacting wakes change the drag force on the <span class="hlt">drops</span>. Generally, the adhesion force is not affected by presence of other <span class="hlt">drops</span>. As such, when the <span class="hlt">drops</span>' wakes are interacting strongly, Ucr can increase by 45%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvF...2c1602M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvF...2c1602M"><span>Star-shaped oscillations of Leidenfrost <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ma, Xiaolei; Liétor-Santos, Juan-José; Burton, Justin C.</p> <p>2017-03-01</p> <p>We experimentally investigate the self-sustained, star-shaped oscillations of Leidenfrost <span class="hlt">drops</span>. The <span class="hlt">drops</span> levitate on a cushion of evaporated vapor over a heated, curved surface. We observe modes with n =2 -13 lobes around the <span class="hlt">drop</span> periphery. We find that the wavelength of the oscillations depends only on the capillary length of the liquid and is independent of the <span class="hlt">drop</span> radius and substrate temperature. However, the number of observed modes depends sensitively on the liquid viscosity. The dominant frequency of <span class="hlt">pressure</span> variations in the vapor layer is approximately twice the <span class="hlt">drop</span> oscillation frequency, consistent with a parametric forcing mechanism. Our results show that the star-shaped oscillations are driven by capillary waves of a characteristic wavelength beneath the <span class="hlt">drop</span> and that the waves are generated by a large shear stress at the liquid-vapor interface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFD.D5004P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFD.D5004P"><span>Impacts of coronary artery eccentricity on macro-recirculation and <span class="hlt">pressure</span> <span class="hlt">drops</span> using computational fluid dynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Poon, Eric; Thondapu, Vikas; Barlis, Peter; Ooi, Andrew</p> <p>2017-11-01</p> <p>Coronary artery disease remains a major cause of mortality in developed countries, and is most often due to a localized flow-limiting stenosis, or narrowing, of coronary arteries. Patients often undergo invasive procedures such as X-ray angiography and fractional flow reserve to diagnose flow-limiting lesions. Even though such diagnostic techniques are well-developed, the effects of diseased coronary segments on local flow are still poorly understood. Therefore, this study investigated the effect of irregular geometries of diseased coronary segments on the macro-recirculation and local <span class="hlt">pressure</span> minimum regions. We employed an idealized coronary artery model with a diameter of stenosis of 75%. By systematically adjusting the eccentricity and the asymmetry of the coronary stenosis, we uncovered an increase in macro-recirculation size. Most importantly, the presence of this macro-recirculation signifies a local <span class="hlt">pressure</span> minimum (identified by λ2 vortex identification method). This local <span class="hlt">pressure</span> minimum has a profound effect on the <span class="hlt">pressure</span> <span class="hlt">drops</span> in both longitudinal and planar directions, which has implications for diagnosis and treatment of coronary artery disease. Supported by Australian Research Council LP150100233 and National Computational Infrastructure m45.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810017608','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810017608"><span>Subsonic tests of an all-flush-<span class="hlt">pressure</span>-orifice <span class="hlt">air</span> data system</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Larson, T. J.; Siemers, P. M., III</p> <p>1981-01-01</p> <p>The use of an all-flush-<span class="hlt">pressure</span>-orifice array as a subsonic <span class="hlt">air</span> data system was evaluated in flight and wind tunnel tests. Two orifice configurations were investigated. Both used orifices arranged in a cruciform pattern on the airplane nose. One configuration also used orifices on the sides of the fuselage for a source of static <span class="hlt">pressure</span>. The all-nose-orifice configuration was similar to the shuttle entry <span class="hlt">air</span> data system (SEADS). The flight data were obtained with a KC-135A airplane. The wind tunnel data were acquired with a 0.035-scale model of the KC-135A airplane. With proper calibration, several orifices on the vertical centerline of the vehicle's nose were found to be satisfactory for the determination of total <span class="hlt">pressure</span> and angle of attack. Angle of sideslip could be accurately determined from <span class="hlt">pressure</span> measurements made on the horizontal centerline of the aircraft. Orifice pairs were also found that provided <span class="hlt">pressure</span> ratio relationships suitable for the determination of Mach number. The accuracy that can be expected for the <span class="hlt">air</span> data determined with SEADS during subsonic orbiter flight is indicated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23100258','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23100258"><span>Three types of cavitation caused by <span class="hlt">air</span> seeding.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shen, Fanyi; Wang, Yuansheng; Cheng, Yanxia; Zhang, Li</p> <p>2012-11-01</p> <p>There are different opinions of the dynamics of an <span class="hlt">air</span> bubble entering a xylem conduit. In this paper, we present a thorough mechanical analysis and conclude that there are three types of cavitation caused by <span class="hlt">air</span> seeding. After an <span class="hlt">air</span> seed enters a conduit at high xylem <span class="hlt">pressure</span> P'(1), along with the <span class="hlt">drop</span> of the water potential, it will expand gradually to a long-shaped bubble and extend continually. This is the first type of <span class="hlt">air</span> seeding, or the type of expanding gradually. When the xylem <span class="hlt">pressure</span> is moderate, right after an <span class="hlt">air</span> seed enters a conduit, it will expand first. Then, as soon as the <span class="hlt">pressure</span> reaches a threshold the bubble will blow up to form a bubble in long shape, accompanied by acoustic (or ultra-acoustic) emission. It will extend further as xylem <span class="hlt">pressure</span> decreases continually. This is the second type of <span class="hlt">air</span> seeding, or the type of expanding-exploding, becoming a long-shaped bubble-lengthening by degrees. In the range of P'(1) ≤ - 3P(o) (P(o) is atmospheric <span class="hlt">pressure</span>), soon after an <span class="hlt">air</span> seed is sucked into a conduit it will explode immediately and the conduit will be full of the gas of the bubble instantly. This is the third type of <span class="hlt">air</span> seeding, or the type of sudden exploding and filling conduit instantly. The third type is the frequent event in daily life of plant.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940009274','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940009274"><span><span class="hlt">Drop</span> dynamics in space and interference with acoustic field (M-15)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yamanaka, Tatsuo</p> <p>1993-01-01</p> <p>The objective of the experiment is to study contactless positioning of liquid <span class="hlt">drops</span>, excitation of capillary waves on the surface of acoustically levitated liquid <span class="hlt">drops</span>, and deformation of liquid <span class="hlt">drops</span> by means of acoustic radiation <span class="hlt">pressure</span>. Contactless positioning technologies are very important in space materials processing because the melt is processed without contacting the wall of a crucible which can easily contaminate the melt specifically for high melting temperatures and chemically reactive materials. Among the contactless positioning technologies, an acoustic technology is especially important for materials unsusceptible to electromagnetic fields such as glasses and ceramics. The shape of a levitated liquid <span class="hlt">drop</span> in the weightless condition is determined by its surface tension and the internal and external <span class="hlt">pressure</span> distribution. If the surface temperature is constant and there exist neither internal nor external <span class="hlt">pressure</span> perturbations, the levitated liquid <span class="hlt">drop</span> forms a shape of perfect sphere. If temperature gradients on the surface and internal or external <span class="hlt">pressure</span> perturbations exist, the liquid <span class="hlt">drop</span> forms various modes of shapes with proper vibrations. A rotating liquid <span class="hlt">drop</span> was specifically studied not only as a classical problem of theoretical mechanics to describe the shapes of the planets of the solar system, as well as their arrangement, but it is also more a contemporary problem of modern non-linear mechanics. In the experiment, we are expecting to observe various shapes of a liquid <span class="hlt">drop</span> such as cocoon, tri-lobed, tetropod, multi-lobed, and doughnut.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080009526','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080009526"><span>Hanging <span class="hlt">drop</span> crystal growth apparatus and method</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Carter, Daniel C. (Inventor); Smith, Robbie E. (Inventor)</p> <p>1989-01-01</p> <p>An apparatus (10) is constructed having a cylindrical enclosure (16) within which a disc-shaped wicking element (18) is positioned. A well or recess (22) is cut into an upper side (24) of this wicking element, and a glass cover plate or slip (28) having a protein <span class="hlt">drop</span> disposed thereon is sealably positioned on the wicking element (18), with <span class="hlt">drop</span> (12) being positioned over well or recess (22). A flow of control fluid is generated by a programmable gradient former (16), with this control fluid having a vapor <span class="hlt">pressure</span> that is selectively variable. This flow of control fluid is coupled to the wicking element (18) where control fluid vapor diffusing from walls (26) of the recess (22) is exposed to the <span class="hlt">drop</span> (12), forming a vapor <span class="hlt">pressure</span> gradient between the <span class="hlt">drop</span> (12) and the control fluid vapor. Initially, this gradient is adjusted to draw solvent from the <span class="hlt">drop</span> (12) at a relatively high rate, and as the critical supersaturation point is approached (the point at which crystal nucleation occurs), the gradient is reduced to more slowly draw solvent from the <span class="hlt">drop</span> (12). This allows discrete protein molecules more time to orient themselves into an ordered crystalline lattice, producing protein crystals which, when processed by X-ray crystallography, possess a high degree of resolution.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21514044','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21514044"><span>Temperature and <span class="hlt">pressure</span> influence on maximum rates of <span class="hlt">pressure</span> rise during explosions of propane-<span class="hlt">air</span> mixtures in a spherical vessel.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Razus, D; Brinzea, V; Mitu, M; Movileanu, C; Oancea, D</p> <p>2011-06-15</p> <p>The maximum rates of <span class="hlt">pressure</span> rise during closed vessel explosions of propane-<span class="hlt">air</span> mixtures are reported, for systems with various initial concentrations, <span class="hlt">pressures</span> and temperatures ([C(3)H(8)]=2.50-6.20 vol.%, p(0)=0.3-1.3 bar; T(0)=298-423 K). Experiments were performed in a spherical vessel (Φ=10 cm) with central ignition. The deflagration (severity) index K(G), calculated from experimental values of maximum rates of <span class="hlt">pressure</span> rise is examined against the adiabatic deflagration index, K(G, ad), computed from normal burning velocities and peak explosion <span class="hlt">pressures</span>. At constant temperature and fuel/oxygen ratio, both the maximum rates of <span class="hlt">pressure</span> rise and the deflagration indices are linear functions of total initial <span class="hlt">pressure</span>, as reported for other fuel-<span class="hlt">air</span> mixtures. At constant initial <span class="hlt">pressure</span> and composition, the maximum rates of <span class="hlt">pressure</span> rise and deflagration indices are slightly influenced by the initial temperature; some influence of the initial temperature on maximum rates of <span class="hlt">pressure</span> rise is observed only for propane-<span class="hlt">air</span> mixtures far from stoichiometric composition. The differentiated temperature influence on the normal burning velocities and the peak explosion <span class="hlt">pressures</span> might explain this behaviour. Copyright © 2011 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790042653&hterms=aerodynamics+parachutes&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Daerodynamics%2Bparachutes','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790042653&hterms=aerodynamics+parachutes&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Daerodynamics%2Bparachutes"><span>Performance evaluation of Space Shuttle SRB parachutes from <span class="hlt">air</span> <span class="hlt">drop</span> and scaled model wind tunnel tests. [Solid Rocket Booster recovery system</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Moog, R. D.; Bacchus, D. L.; Utreja, L. R.</p> <p>1979-01-01</p> <p>The aerodynamic performance characteristics have been determined for the Space Shuttle Solid Rocket Booster drogue, main, and pilot parachutes. The performance evaluation on the 20-degree conical ribbon parachutes is based primarily on <span class="hlt">air</span> <span class="hlt">drop</span> tests of full scale prototype parachutes. In addition, parametric wind tunnel tests were performed and used in parachute configuration development and preliminary performance assessments. The wind tunnel test data are compared to the <span class="hlt">drop</span> test results and both sets of data are used to determine the predicted performance of the Solid Rocket Booster flight parachutes. Data from other <span class="hlt">drop</span> tests of large ribbon parachutes are also compared with the Solid Rocket Booster parachute performance characteristics. Parameters assessed include full open terminal drag coefficients, reefed drag area, opening characteristics, clustering effects, and forebody interference.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29157605','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29157605"><span>Extraction of essential oil from Bunium Persicum (Boiss.) by instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span> (DIC).</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Feyzi, Elnaz; Eikani, Mohammad H; Golmohammad, Fereshteh; Tafaghodinia, Bahram</p> <p>2017-12-29</p> <p>Essential oils extraction from Bunium Persicum (Boiss) was performed using instant controlled <span class="hlt">pressure</span> <span class="hlt">drop</span> (in French: Détente Instantanée Contrôlée or DIC) thechnology and optimum extraction conditions were obtained. Response surface methodology (RSM) was used to determine the optimal conditions and the results were 20s heating time, 3.5bar <span class="hlt">pressure</span>, 0.44mm particle diameter and 9 cycles. Essential oils extraction was also compared with Hydrodistillation (HD), ultrasound-assisted extraction (UAE) and Soxhlet (SOX) extraction. Results show higher efficiency of the DIC than other methods and more oxygenated components were observed. Impact of DIC, HD, UAE and SOX on the morphological structure of the plant was studied by SEM. Antioxidant activity and total phenolic content (TPC) of the extract were determined and comapred by HD. Results show that DIC facilitates achieving to higher TPC and more antioxidant activity. Copyright © 2017 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800024952','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800024952"><span>Orbiter thermal <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristics for shuttle orbiter thermal protection system components: High density tile, low density tile, densified low density tile, and strain isolation pad</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lawing, P. L.; Nystrom, D. M.</p> <p>1980-01-01</p> <p><span class="hlt">Pressure</span> <span class="hlt">drop</span> tests were conducted on available samples of low and high density tile, densified low density tile, and strain isolation pads. The results are presented in terms of <span class="hlt">pressure</span> <span class="hlt">drop</span>, material thickness and volume flow rate. Although the test apparatus was only capable of a small part of the range of conditions to be encountered in a Shuttle Orbiter flight, the data serve to determine the type of flow characteristics to be expected for each material type tested; the measured quantities also should serve as input for initial venting and flow through analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014SPIE.9234E..0DO','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014SPIE.9234E..0DO"><span>Influence of water depth on the sound generated by <span class="hlt">air</span>-bubble vibration in the water musical instrument</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ohuchi, Yoshito; Nakazono, Yoichi</p> <p>2014-06-01</p> <p>We have developed a water musical instrument that generates sound by the falling of water <span class="hlt">drops</span> within resonance tubes. The instrument can give people who hear it the healing effect inherent in the sound of water. The sound produced by falling water <span class="hlt">drops</span> arises from <span class="hlt">air</span>- bubble vibrations. To investigate the impact of water depth on the <span class="hlt">air</span>-bubble vibrations, we conducted experiments at varying values of water <span class="hlt">pressure</span> and nozzle shape. We found that <span class="hlt">air</span>-bubble vibration frequency does not change at a water depth of 50 mm or greater. Between 35 and 40 mm, however, the frequency decreases. At water depths of 30 mm or below, the <span class="hlt">air</span>-bubble vibration frequency increases. In our tests, we varied the nozzle diameter from 2 to 4 mm. In addition, we discovered that the time taken for <span class="hlt">air</span>-bubble vibration to start after the water <span class="hlt">drops</span> start falling is constant at water depths of 40 mm or greater, but slower at depths below 40 mm.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013EGUGA..15.7634C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013EGUGA..15.7634C"><span>Combining spray nozzle simulators with meshes: characterization of rainfall intensity and <span class="hlt">drop</span> properties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Carvalho, Sílvia C. P.; de Lima, João L. M. P.; de Lima, M. Isabel P.</p> <p>2013-04-01</p> <p>Rainfall simulators can be a powerful tool to increase our understanding of hydrological and geomorphological processes. Nevertheless, rainfall simulators' design and operation might be rather demanding, for achieving specific rainfall intensity distributions and <span class="hlt">drop</span> characteristics. The <span class="hlt">pressurized</span> simulators have some advantages over the non-<span class="hlt">pressurized</span> simulators: <span class="hlt">drops</span> do not rely on gravity to reach terminal velocity, but are sprayed out under <span class="hlt">pressure</span>; <span class="hlt">pressurized</span> simulators also yield a broad range of <span class="hlt">drop</span> sizes in comparison with <span class="hlt">drop</span>-formers simulators. The main purpose of this study was to explore in the laboratory the potential of combining spray nozzle simulators with meshes in order to change rainfall characteristics (rainfall intensity and diameters and fall speed of <span class="hlt">drops</span>). Different types of spray nozzles were tested, such as single full-cone and multiple full-cone nozzles. The impact of the meshes on the simulated rain was studied by testing different materials (i.e. plastic and steel meshes), square apertures and wire thicknesses, and different vertical distances between the nozzle and the meshes underneath. The diameter and fall speed of the rain <span class="hlt">drops</span> were measured using a Laser Precipitation Monitor (Thies Clima). The rainfall intensity range and coefficients of uniformity of the sprays and the <span class="hlt">drop</span> size distribution, fall speed and kinetic energy were analysed. Results show that when meshes intercept <span class="hlt">drop</span> trajectories the spatial distribution of rainfall intensity and the <span class="hlt">drop</span> size distribution are affected. As the spray nozzles generate typically small <span class="hlt">drop</span> sizes and narrow <span class="hlt">drop</span> size distributions, meshes can be used to promote the formation of bigger <span class="hlt">drops</span> and random their landing positions.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_14 --> <div id="page_15" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="281"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=aerodynamics&pg=5&id=EJ823335','ERIC'); return false;" href="https://eric.ed.gov/?q=aerodynamics&pg=5&id=EJ823335"><span>Respiratory and Laryngeal Responses to an Oral <span class="hlt">Air</span> <span class="hlt">Pressure</span> Bleed during Speech</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Huber, Jessica E.; Stathopoulos, Elaine T.</p> <p>2003-01-01</p> <p>Researchers have hypothesized that the respiratory and laryngeal speech subsystems would respond to an <span class="hlt">air</span> <span class="hlt">pressure</span> bleed, but these responses have not been empirically studied. The present study examined the nature of the responses of the respiratory and laryngeal subsystems to an <span class="hlt">air</span> <span class="hlt">pressure</span> bleed in order to provide information relevant to the…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec56-13015.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2011-07-01 2011-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec56-13015.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2012-07-01 2012-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec57-13015.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2014-07-01 2014-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec56-13015.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title30-vol1/pdf/CFR-2014-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2014-07-01 2014-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec56-13015.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec56-13015.pdf"><span>30 CFR 56.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels... 30 Mineral Resources 1 2013-07-01 2013-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 56.13015 Section 56.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec57-13015.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title30-vol1/pdf/CFR-2012-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2012-07-01 2012-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec57-13015.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title30-vol1/pdf/CFR-2013-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2013-07-01 2013-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec57-13015.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title30-vol1/pdf/CFR-2011-title30-vol1-sec57-13015.pdf"><span>30 CFR 57.13015 - Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... receivers and other unfired <span class="hlt">pressure</span> vessels. (a) Compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span>... 30 Mineral Resources 1 2011-07-01 2011-07-01 false Inspection of compressed-<span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 57.13015 Section 57.13015 Mineral Resources MINE SAFETY AND HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/11071051','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/11071051"><span><span class="hlt">Air</span>-braked cycle ergometers: validity of the correction factor for barometric <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Finn, J P; Maxwell, B F; Withers, R T</p> <p>2000-10-01</p> <p>Barometric <span class="hlt">pressure</span> exerts by far the greatest influence of the three environmental factors (barometric <span class="hlt">pressure</span>, temperature and humidity) on power outputs from <span class="hlt">air</span>-braked ergometers. The barometric <span class="hlt">pressure</span> correction factor for power outputs from <span class="hlt">air</span>-braked ergometers is in widespread use but apparently has never been empirically validated. Our experiment validated this correction factor by calibrating two <span class="hlt">air</span>-braked cycle ergometers in a hypobaric chamber using a dynamic calibration rig. The results showed that if the power output correction for changes in <span class="hlt">air</span> resistance at barometric <span class="hlt">pressures</span> corresponding to altitudes of 38, 600, 1,200 and 1,800 m above mean sea level were applied, then the coefficients of variation were 0.8-1.9% over the range of 160-1,597 W. The overall mean error was 3.0 % but this included up to 0.73 % for the propagated error that was associated with errors in the measurement of: a) temperature b) relative humidity c) barometric <span class="hlt">pressure</span> d) force, distance and angular velocity by the dynamic calibration rig. The overall mean error therefore approximated the +/- 2.0% of true load that was specified by the Laboratory Standards Assistance Scheme of the Australian Sports Commission. The validity of the correction factor for barometric <span class="hlt">pressure</span> on power output was therefore demonstrated over the altitude range of 38-1,800 m.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22056165','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22056165"><span>Multi-stage versus single-stage inflation and deflation cycle for alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattresses to prevent <span class="hlt">pressure</span> ulcers in hospitalised patients: a randomised-controlled clinical trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Demarré, L; Beeckman, D; Vanderwee, K; Defloor, T; Grypdonck, M; Verhaeghe, S</p> <p>2012-04-01</p> <p>The duration and the amount of <span class="hlt">pressure</span> and shear must be reduced in order to minimize the risk of <span class="hlt">pressure</span> ulcer development. Alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattresses with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells have been developed to relieve <span class="hlt">pressure</span> by sequentially inflating and deflating the <span class="hlt">air</span> cells. Evidence about the effectiveness of this type of mattress in clinical practice is lacking. This study aimed to compare the effectiveness of an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress that has a standard single-stage inflation and deflation cycle of the <span class="hlt">air</span> cells with an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. A randomised controlled trial was performed in a convenience sample of 25 wards in five hospitals in Belgium. In total, 610 patients were included and randomly assigned to the experimental group (n=298) or the control group (n=312). In the experimental group, patients were allocated to an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. In the control group, patients were allocated to an alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with a standard single-stage inflation and deflation cycle of the <span class="hlt">air</span> cells. The outcome was defined as cumulative <span class="hlt">pressure</span> ulcer incidence (Grade II-IV). An intention-to-treat analysis was performed. There was no significant difference in cumulative <span class="hlt">pressure</span> ulcer incidence (Grade II-IV) between both groups (Exp.=5.7%, Contr.=5.8%, p=0.97). When patients developed a <span class="hlt">pressure</span> ulcer, the median time was 5.0 days in the experimental group (IQR=3.0-8.5) and 8.0 days in the control group (IQR=3.0-8.5) (Mann-Whitney U-test=113, p=0.182). The probability to remain <span class="hlt">pressure</span> ulcer free during the observation period in this trial did not differ significantly between the experimental group and the control group (log-rank χ(2)=0.013, df=1, p=0.911). An alternating low <span class="hlt">pressure</span> <span class="hlt">air</span> mattress with multi-stage inflation</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PlST...20c5401W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PlST...20c5401W"><span>Exploration to generate atmospheric <span class="hlt">pressure</span> glow discharge plasma in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wenzheng, LIU; Chuanlong, MA; Shuai, ZHAO; Xiaozhong, CHEN; Tahan, WANG; Luxiang, ZHAO; Zhiyi, LI; Jiangqi, NIU; Liying, ZHU; Maolin, CHAI</p> <p>2018-03-01</p> <p>Atmospheric <span class="hlt">pressure</span> glow discharge (APGD) plasma in <span class="hlt">air</span> has high application value. In this paper, the methods of generating APGD plasma in <span class="hlt">air</span> are discussed, and the characteristics of dielectric barrier discharge (DBD) in non-uniform electric field are studied. It makes sure that APGD in <span class="hlt">air</span> is formed by DBD in alternating current electric field with using the absorbing electron capacity of electret materials to provide initial electrons and to end the discharge progress. Through designing electric field to form two-dimensional space varying electric field and three-dimensional space varying electric field, the development of electron avalanches in <span class="hlt">air</span>-gap is suppressed effectively and a large space of APGD plasma in <span class="hlt">air</span> is generated. Further, through combining electrode structures, a large area of APGD plasma in <span class="hlt">air</span> is generated. On the other hand, by using the method of increasing the density of initial electrons, millimeter-gap glow discharge in atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> is formed, and a maximum gap distance between electrodes is 8 mm. By using the APGD plasma surface treatment device composed of contact electrodes, the surface modification of high polymer materials such as aramid fiber and polyester are studied and good effect of modifications is obtained. The present paper provides references for the researchers of industrial applications of plasma.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25030238','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25030238"><span>Can we trust intraocular <span class="hlt">pressure</span> measurements in eyes with intracameral <span class="hlt">air</span>?</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Jóhannesson, Gauti; Lindén, Christina; Eklund, Anders; Behndig, Anders; Hallberg, Per</p> <p>2014-10-01</p> <p>To evaluate the effect of intracameral <span class="hlt">air</span> on intraocular <span class="hlt">pressure</span> (IOP) measurements using Goldmann applanation tonometry (GAT) and applanation resonance tonometry (ART) in an in-vitro porcine eye model. IOP was measured on thirteen freshly enucleated eyes at three reference <span class="hlt">pressures</span>: 20, 30, and 40 mmHg. Six measurements/method were performed in a standardized order with GAT and ART respectively. <span class="hlt">Air</span> was injected intracamerally in the same manner as during Descemet's stripping endothelial keratoplasty (DSEK) and Descemet's membrane endothelial keratoplasty (DMEK), and the measurements were repeated. Measured IOP increased significantly for both tonometry methods after <span class="hlt">air</span> injection: 0.7 ± 2.1 mmHg for GAT and 10.6 ± 4.9 mmHg for ART. This difference was significant at each reference <span class="hlt">pressure</span> for ART but not for GAT. Although slightly affected, this study suggests that we can trust GAT IOP-measurements in eyes with intracameral <span class="hlt">air</span>, such as after DSEK/DMEK operations. Ultrasound-based methods such as ART should not be used.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18686821','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18686821"><span>[<span class="hlt">Air</span> travel during pregnancy].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Rabinerson, David; Ninio, Avraham; Glezerman, Marek</p> <p>2008-04-01</p> <p>Nowadays, millions of people travel by <span class="hlt">air</span> every day and it is common to find pregnant women among the passengers. Travelling during pregnancy raises the question of the woman's safety during the flight. This is due to the risk of exposure to cosmic radiation, the <span class="hlt">drop</span> in <span class="hlt">air</span> <span class="hlt">pressure</span>, and the possibility of thromboembolism due to seating conditions and flight duration. Other risks include obstetric emergencies, such as hemorrhage, premature contractions and actual labor. Further issues associated with <span class="hlt">air</span> travel during pregnancy have to do with the safety of pregnant aircrew, if emergency evacuation becomes necessary and the airline's view regarding the admittance of pregnant women on flights. We discuss these issues extensively in our review. We conclude that for a healthy woman whose pregnancy involves no risk factors, <span class="hlt">air</span> travel is safe up to the 36th gestational week.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006AcAau..59..278V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006AcAau..59..278V"><span>The new <span class="hlt">Drop</span> Tower catapult system</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>von Kampen, Peter; Kaczmarczik, Ulrich; Rath, Hans J.</p> <p>2006-07-01</p> <p>The Center of Applied Space Technology and Microgravity (ZARM) was founded in 1985 as an institute of the University Bremen, which focuses on research on gravitational and space-related phenomena. In 1988, the construction of the "<span class="hlt">Drop</span> Tower" began. Since then, the eye-catching tower with a height of 146 m and its characteristic glass roof has become the emblem of the technology centre in Bremen. The <span class="hlt">Drop</span> Tower Bremen provides a facility for experiments under conditions of weightlessness. Items are considered weightless, when they are in "free fall", i.e. moving without propulsion within the gravity field of the earth. The height of the tower limits the simple "free fall" experiment period to max. 4.74 s. With the inauguration of the catapult system in December 2004, the ZARM is entering a new dimension. This world novelty will meet scientists' demands of extending the experiment period up to 9.5 s. Since turning the first sod on May 3rd, 1988, the later installation of the catapult system has been taken into account by building the necessary chamber under the tower. The catapult system is located in a chamber 10 m below the base of the tower. This chamber is almost completely occupied by 12 huge <span class="hlt">pressure</span> tanks. These tanks are placed around the elongation of the vacuum chamber of the <span class="hlt">drop</span> tube. In its centre there is the pneumatic piston that accelerates the <span class="hlt">drop</span> capsule by the <span class="hlt">pressure</span> difference between the vacuum inside the <span class="hlt">drop</span> tube and the <span class="hlt">pressure</span> inside the tanks. The acceleration level is adjusted by means of a servo hydraulic breaking system controlling the piston velocity. After only a quarter of a second the <span class="hlt">drop</span> capsule achieves its lift-off speed of 175 km/h. With this exact speed, the capsule will rise up to the top of the tower and afterwards fall down again into the deceleration unit which has been moved under the <span class="hlt">drop</span> tube in the meantime. The scientific advantages of the doubled experiment time are obvious: during almost 10 s of high</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19910035061&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19910035061&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure"><span><span class="hlt">Pressure</span> Distribution and <span class="hlt">Air</span> Data System for the Aeroassist Flight Experiment</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gibson, Lorelei S.; Siemers, Paul M., III; Kern, Frederick A.</p> <p>1989-01-01</p> <p>The Aeroassist Flight Experiment (AFE) is designed to provide critical flight data necessary for the design of future Aeroassist Space Transfer Vehicles (ASTV). This flight experiment will provide aerodynamic, aerothermodynamic, and environmental data for verification of experimental and computational flow field techniques. The <span class="hlt">Pressure</span> Distribution and <span class="hlt">Air</span> Data System (PD/ADS), one of the measurement systems incorporated into the AFE spacecraft, is designed to provide accurate <span class="hlt">pressure</span> measurements on the windward surface of the vehicle. These measurements will be used to determine the <span class="hlt">pressure</span> distribution and <span class="hlt">air</span> data parameters (angle of attack, angle of sideslip, and free-stream dynamic <span class="hlt">pressure</span>) encountered by the blunt-bodied vehicle over an altitude range of 76.2 km to 94.5 km. Design and development data are presented and include: measurement requirements, measurement heritage, theoretical studies to define the vehicle environment, flush-mounted orifice configuration, <span class="hlt">pressure</span> transducer selection and performance evaluation data, and <span class="hlt">pressure</span> tubing response analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=36744&Lab=ORD&keyword=Battery+AND+efficiency&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50','EPA-EIMS'); return false;" href="https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=36744&Lab=ORD&keyword=Battery+AND+efficiency&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50"><span>AMERICAN <span class="hlt">AIR</span> FILTER KINPACTOR 10 X 56 VENTURI SCRUBBER EVALUATION</span></a></p> <p><a target="_blank" href="http://oaspub.epa.gov/eims/query.page">EPA Science Inventory</a></p> <p></p> <p></p> <p>The report gives results of an evaluation of an American <span class="hlt">Air</span> Filter Kinpactor 10 x 56 venturi scrubber, operating on emissions from a large borax fusing furnace. Average total efficiency was 97.5% during the test period. The venturi was operated at a <span class="hlt">pressure</span> <span class="hlt">drop</span> of 110 cm W. C....</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4288121','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4288121"><span>Acute <span class="hlt">Air</span> Pollution Exposure and Blood <span class="hlt">Pressure</span> at Delivery Among Women With and Without Hypertension</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Männistö, Tuija; Liu, Danping; Leishear, Kira; Sherman, Seth; Laughon, S. Katherine</p> <p>2015-01-01</p> <p>BACKGROUND Chronic <span class="hlt">air</span> pollution exposure increases risk for hypertensive disorders of pregnancy, but the effect of acute <span class="hlt">air</span> pollution exposure on blood <span class="hlt">pressure</span> during pregnancy is less well known. METHODS We studied 151,276 singleton term deliveries from the Consortium on Safe Labor (2002–2008) with clinical blood <span class="hlt">pressure</span> measured at admission to labor/delivery and diagnoses of hypertensive disorders collected from electronic medical records and hospital discharge summaries. <span class="hlt">Air</span> pollution exposures were estimated for the admission hour and the 4 hours preceding admission using a modified version of the Community Multiscale <span class="hlt">Air</span> Quality models and observed <span class="hlt">air</span> monitoring data. Blood <span class="hlt">pressure</span> was categorized as normal; high normal; and mild, moderate, or severe hypertension based on pregnancy cut points. Adjusted ordinal logistic regression estimated the odds of women having a higher admission blood <span class="hlt">pressure</span> category as a function of <span class="hlt">air</span> pollutant, hypertensive disorders, and their interaction effect. RESULTS Odds of high blood <span class="hlt">pressure</span> at admission to labor/delivery were increased in normotensive women after exposure to nitrogen oxides (by 0.2%/5 units), sulfur dioxide (by 0.3%/1 unit), carbon monoxide and several <span class="hlt">air</span> toxics (by 3%–4%/high exposure). The effects were often similar or stronger among women with gestational hypertension and preeclampsia. Exposure to particulate matter <10 μm increased odds of high blood <span class="hlt">pressure</span> in women with preeclampsia by 3%/5 units. CONCLUSIONS <span class="hlt">Air</span> pollution can influence admission blood <span class="hlt">pressure</span> in term deliveries and may increase likelihood of preeclampsia screening at delivery admission. PMID:24795401</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23455767','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23455767"><span>Torricelli and the ocean of <span class="hlt">air</span>: the first measurement of barometric <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>West, John B</p> <p>2013-03-01</p> <p>The recognition of barometric <span class="hlt">pressure</span> was a critical step in the development of environmental physiology. In 1644, Evangelista Torricelli described the first mercury barometer in a remarkable letter that contained the phrase, "We live submerged at the bottom of an ocean of the element <span class="hlt">air</span>, which by unquestioned experiments is known to have weight." This extraordinary insight seems to have come right out of the blue. Less than 10 years before, the great Galileo had given an erroneous explanation for the related problem of pumping water from a deep well. Previously, Gasparo Berti had filled a very long lead vertical tube with water and showed that a vacuum formed at the top. However, Torricelli was the first to make a mercury barometer and understand that the mercury was supported by the <span class="hlt">pressure</span> of the <span class="hlt">air</span>. Aristotle stated that the <span class="hlt">air</span> has weight, although this was controversial for some time. Galileo described a method of measuring the weight of the <span class="hlt">air</span> in detail, but for reasons that are not clear his result was in error by a factor of about two. Torricelli surmised that the <span class="hlt">pressure</span> of the <span class="hlt">air</span> might be less on mountains, but the first demonstration of this was by Blaise Pascal. The first <span class="hlt">air</span> pump was built by Otto von Guericke, and this influenced Robert Boyle to carry out his classical experiments of the physiological effects of reduced barometric <span class="hlt">pressure</span>. These were turning points in the early history of high-altitude physiology.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21827644','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21827644"><span>Performance evaluation on an <span class="hlt">air</span>-cooled heat exchanger for alumina nanofluid under laminar flow.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Teng, Tun-Ping; Hung, Yi-Hsuan; Teng, Tun-Chien; Chen, Jyun-Hong</p> <p>2011-08-09</p> <p>This study analyzes the characteristics of alumina (Al2O3)/water nanofluid to determine the feasibility of its application in an <span class="hlt">air</span>-cooled heat exchanger for heat dissipation for PEMFC or electronic chip cooling. The experimental sample was Al2O3/water nanofluid produced by the direct synthesis method at three different concentrations (0.5, 1.0, and 1.5 wt.%). The experiments in this study measured the thermal conductivity and viscosity of nanofluid with weight fractions and sample temperatures (20-60°C), and then used the nanofluid in an actual <span class="hlt">air</span>-cooled heat exchanger to assess its heat exchange capacity and <span class="hlt">pressure</span> <span class="hlt">drop</span> under laminar flow. Experimental results show that the nanofluid has a higher heat exchange capacity than water, and a higher concentration of nanoparticles provides an even better ratio of the heat exchange. The maximum enhanced ratio of heat exchange and <span class="hlt">pressure</span> <span class="hlt">drop</span> for all the experimental parameters in this study was about 39% and 5.6%, respectively. In addition to nanoparticle concentration, the temperature and mass flow rates of the working fluid can affect the enhanced ratio of heat exchange and <span class="hlt">pressure</span> <span class="hlt">drop</span> of nanofluid. The cross-section aspect ratio of tube in the heat exchanger is another important factor to be taken into consideration.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_15 --> <div id="page_16" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="301"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3212002','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3212002"><span>Performance evaluation on an <span class="hlt">air</span>-cooled heat exchanger for alumina nanofluid under laminar flow</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2011-01-01</p> <p>This study analyzes the characteristics of alumina (Al2O3)/water nanofluid to determine the feasibility of its application in an <span class="hlt">air</span>-cooled heat exchanger for heat dissipation for PEMFC or electronic chip cooling. The experimental sample was Al2O3/water nanofluid produced by the direct synthesis method at three different concentrations (0.5, 1.0, and 1.5 wt.%). The experiments in this study measured the thermal conductivity and viscosity of nanofluid with weight fractions and sample temperatures (20-60°C), and then used the nanofluid in an actual <span class="hlt">air</span>-cooled heat exchanger to assess its heat exchange capacity and <span class="hlt">pressure</span> <span class="hlt">drop</span> under laminar flow. Experimental results show that the nanofluid has a higher heat exchange capacity than water, and a higher concentration of nanoparticles provides an even better ratio of the heat exchange. The maximum enhanced ratio of heat exchange and <span class="hlt">pressure</span> <span class="hlt">drop</span> for all the experimental parameters in this study was about 39% and 5.6%, respectively. In addition to nanoparticle concentration, the temperature and mass flow rates of the working fluid can affect the enhanced ratio of heat exchange and <span class="hlt">pressure</span> <span class="hlt">drop</span> of nanofluid. The cross-section aspect ratio of tube in the heat exchanger is another important factor to be taken into consideration. PMID:21827644</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21305591','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21305591"><span>Comparison of <span class="hlt">air</span>-charged and water-filled urodynamic <span class="hlt">pressure</span> measurement catheters.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cooper, M A; Fletter, P C; Zaszczurynski, P J; Damaser, M S</p> <p>2011-03-01</p> <p>Catheter systems are utilized to measure <span class="hlt">pressure</span> for diagnosis of voiding dysfunction. In a clinical setting, patient movement and urodynamic pumps introduce hydrostatic and motion artifacts into measurements. Therefore, complete characterization of a catheter system includes its response to artifacts as well its frequency response. The objective of this study was to compare the response of two disposable clinical catheter systems: water-filled and <span class="hlt">air</span>-charged, to controlled <span class="hlt">pressure</span> signals to assess their similarities and differences in <span class="hlt">pressure</span> transduction. We characterized frequency response using a transient step test, which exposed the catheters to a sudden change in <span class="hlt">pressure</span>; and a sinusoidal frequency sweep test, which exposed the catheters to a sinusoidal <span class="hlt">pressure</span> wave from 1 to 30 Hz. The response of the catheters to motion artifacts was tested using a vortex and the response to hydrostatic <span class="hlt">pressure</span> changes was tested by moving the catheter tips to calibrated heights. Water-filled catheters acted as an underdamped system, resonating at 10.13 ± 1.03 Hz and attenuating signals at frequencies higher than 19 Hz. They demonstrated significant motion and hydrostatic artifacts. <span class="hlt">Air</span>-charged catheters acted as an overdamped system and attenuated signals at frequencies higher than 3.02 ± 0.13 Hz. They demonstrated significantly less motion and hydrostatic artifacts than water-filled catheters. The transient step and frequency sweep tests gave comparable results. <span class="hlt">Air</span>-charged and water-filled catheters respond to <span class="hlt">pressure</span> changes in dramatically different ways. Knowledge of the characteristics of the <span class="hlt">pressure</span>-measuring system is essential to finding the best match for a specific application. Copyright © 2011 Wiley-Liss, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMNH51D1931E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMNH51D1931E"><span>An experimental study of geyser-like flows induced by a <span class="hlt">pressurized</span> <span class="hlt">air</span> pocket</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Elayeb, I. S.; Leon, A.; Choi, Y.; Alnahit, A. O.</p> <p>2015-12-01</p> <p>Previous studies argues that the entrapment of <span class="hlt">pressurized</span> <span class="hlt">air</span> pockets within combined sewer systems can produce geyser flows, which is an oscillating jetting of a mixture of gas-liquid flows. To verify that <span class="hlt">pressurized</span> <span class="hlt">air</span> pockets can effectively produce geysers, laboratory experiments were conducted. However, past experiments were conducted in relatively small-scale apparatus (i.e. maximum φ2" vertical shaft). This study conducted a set of experiments in a larger apparatus. The experimental setup consists of an upstream head tank, a downstream head tank, a horizontal pipe (46.5ft long, φ6") and a vertical pipe (10ft long, φ6"). The initial condition for the experiments is constant flow discharge through the horizontal pipe. The experiments are initiated by injecting an <span class="hlt">air</span> pocket with pre-determined volume and <span class="hlt">pressure</span> at the upstream end of the horizontal pipe. The <span class="hlt">air</span> pocket propagates through the horizontal pipe until it arrives to the vertical shaft, where it is released producing a geyser-like flow. Three flow rates in the horizontal pipe and three injected <span class="hlt">air</span> <span class="hlt">pressures</span> were tested. The variables measured were <span class="hlt">pressure</span> at two locations in the horizontal pipe and two locations in the vertical pipe. High resolution videos at two regions in the vertical shaft were also recorded. To gain further insights in the physics of <span class="hlt">air</span>-water interaction, the laboratory experiments were complemented with numerical simulations conducted using a commercial 3D CFD model, previously validated with experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017HMT....53.3013L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017HMT....53.3013L"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristics of the tube bank fin heat exchanger with fin punched with flow redistributors and curved triangular vortex generators</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Song; Jin, Hua; Song, KeWei; Wang, LiangChen; Wu, Xiang; Wang, LiangBi</p> <p>2017-10-01</p> <p>The heat transfer performance of the tube bank fin heat exchanger is limited by the <span class="hlt">air</span>-side thermal resistance. Thus, enhancing the <span class="hlt">air</span>-side heat transfer is an effective method to improve the performance of the heat exchanger. A new fin pattern with flow redistributors and curved triangular vortex generators is experimentally studied in this paper. The effects of the flow redistributors located in front of the tube stagnation point and the curved vortex generators located around the tube on the characteristics of heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> are discussed in detail. A performance comparison is also carried out between the fins with and without flow redistributors. The experimental results show that the flow redistributors stamped out from the fin in front of the tube stagnation points can decrease the friction factor at the cost of decreasing the heat transfer performance. Whether the combination of the flow redistributors and the curved vortex generators will present a better heat transfer performance depends on the size of the curved vortex generators. As for the studied two sizes of vortex generators, the heat transfer performance is promoted by the flow redistributors for the fin with larger size of vortex generators and the performance is suppressed by the flow redistributors for the fin with smaller vortex generators.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008IJTPE.128.1439Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008IJTPE.128.1439Y"><span>Insulation Technology in Dry <span class="hlt">Air</span> and Vacuum for a 72kV Low <span class="hlt">Pressured</span> Dry <span class="hlt">Air</span> Insulated Switchgear</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yoshida, Tadahiro; Koga, Hiromi; Harada, Takakazu; Miki, Shinichi; Arioka, Masahiro; Sato, Shinji; Yoshida, Satoru; Inoue, Naoaki; Maruyama, Akihiko; Takeuchi, Toshie</p> <p></p> <p>A new 72kV rated low <span class="hlt">pressured</span> dry <span class="hlt">air</span> insulated switchgear applying electromagnetic actuation and function that supports CBM has been developed. First, dielectric characteristics in dry <span class="hlt">air</span> under lightning impulse application has been investigated at bare and insulator covered electrodes. Dependence of the breakdown electric field strength on the effective area has been clarified to apply the configuration design of the insulation mold for the vacuum interrupter. In addition, moisture volume dependence on surface resistance has been clarified to decide moisture volume in gas <span class="hlt">pressure</span> tank. Next, a new vacuum circuit breaker (VCB) has been designed. To keep dimensions from former 72kV SF6 gas insulated switchgear, distance between contacts in vacuum interrupter is needed to be shorter than that of former switchgear. Voltage withstand capability between electrodes practically designed for vacuum interrupter has been investigated under dc voltage application simulated the small capacitive current breaking test. Gap configuration including contacts and slits has been optimized and distance has been shortened 11% from former switchgear. As a result, the new low <span class="hlt">pressured</span> dry <span class="hlt">air</span> insulated switchgear has been designed comparably in outer size to former SF6 gas insulated switchgear. Using dry <span class="hlt">air</span> as an insulation medium with low <span class="hlt">pressure</span> has been able to reduce the environmental burden.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091314','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091314"><span><span class="hlt">Pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Zahm, A F</p> <p>1927-01-01</p> <p>The text gives theoretical formulas from which is computed a table for the <span class="hlt">pressure</span> of <span class="hlt">air</span> on coming to rest from various speeds, such as those of aircraft and propeller blades. <span class="hlt">Pressure</span> graphs are given for speeds from 1 cm. Sec. up to those of swift projectiles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19770020261','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19770020261"><span>High <span class="hlt">pressure</span> flame system for pollution studies with results for methane-<span class="hlt">air</span> diffusion flames</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Miller, I. M.; Maahs, H. G.</p> <p>1977-01-01</p> <p>A high <span class="hlt">pressure</span> flame system was designed and constructed for studying nitrogen oxide formation in fuel <span class="hlt">air</span> combustion. Its advantages and limitations were demonstrated by tests with a confined laminar methane <span class="hlt">air</span> diffusion flame over the <span class="hlt">pressure</span> range from 1 to 50 atm. The methane issued from a 3.06 mm diameter port concentrically into a stream of <span class="hlt">air</span> contained within a 20.5 mm diameter chimney. As the combustion <span class="hlt">pressure</span> is increased, the flame changes in shape from wide and convex to slender and concave, and there is a marked increase in the amount of luminous carbon. The height of the flame changes only moderately with <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28562393','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28562393"><span>Association between lower <span class="hlt">air</span> <span class="hlt">pressure</span> and the onset of ischemic colitis: a case-control study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kimura, Takefumi; Shinji, Akihiro; Tanaka, Naoki; Koinuma, Masayoshi; Yamaura, Maki; Nagaya, Tadanobu; Joshita, Satoru; Komatsu, Michiharu; Umemura, Takeji; Horiuchi, Akira; Wada, Shuichi; Tanaka, Eiji</p> <p>2017-09-01</p> <p>Ischemic colitis (IC) often affects the elderly. Proarteriosclerotic factors, such as hypertension and smoking, and cardiovascular disease are considered major contributors to IC. Although a possible link between certain cerebrocardiovascular disorders and meteorological phenomena has been reported, the relationship between IC onset and weather changes remains uninvestigated. This study examined whether specific meteorological factors were associated with the occurrence of IC. We retrospectively enrolled 303 patients who had been diagnosed with IC between January 2003 and June 2010 at Suwa Red Cross Hospital in Nagano Prefecture, Japan. The meteorological data of the days on which IC patients visited the hospital (IC+ days) were compared with those of the days on which IC patients did not (IC- days). Univariate analysis indicated that IC+ days had significantly lower <span class="hlt">air</span> <span class="hlt">pressure</span> (P<0.001), depressed <span class="hlt">air</span> <span class="hlt">pressure</span> from the previous day (P<0.001), and fewer daylight hours (P<0.001), as well as higher <span class="hlt">air</span> temperature (P=0.017), <span class="hlt">air</span> humidity (P=0.004), wind velocity (P<0.001), and rainfall (P=0.012) compared with IC- days. Multivariate logistic regression analysis of the meteorological data showed that <span class="hlt">air</span> <span class="hlt">pressure</span> (odds ratio: 0.935, P<0.001) and change in <span class="hlt">air</span> <span class="hlt">pressure</span> from the previous day (odds ratio: 0.934, P<0.001) were related to onset of IC. Lower <span class="hlt">air</span> <span class="hlt">pressure</span> and decrease in <span class="hlt">air</span> <span class="hlt">pressure</span> from the previous day are possible novel factors associated with the development of IC.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24795401','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24795401"><span>Acute <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> at delivery among women with and without hypertension.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Männistö, Tuija; Mendola, Pauline; Liu, Danping; Leishear, Kira; Sherman, Seth; Laughon, S Katherine</p> <p>2015-01-01</p> <p>Chronic <span class="hlt">air</span> pollution exposure increases risk for hypertensive disorders of pregnancy, but the effect of acute <span class="hlt">air</span> pollution exposure on blood <span class="hlt">pressure</span> during pregnancy is less well known. We studied 151,276 singleton term deliveries from the Consortium on Safe Labor (2002-2008) with clinical blood <span class="hlt">pressure</span> measured at admission to labor/delivery and diagnoses of hypertensive disorders collected from electronic medical records and hospital discharge summaries. <span class="hlt">Air</span> pollution exposures were estimated for the admission hour and the 4 hours preceding admission using a modified version of the Community Multiscale <span class="hlt">Air</span> Quality models and observed <span class="hlt">air</span> monitoring data. Blood <span class="hlt">pressure</span> was categorized as normal; high normal; and mild, moderate, or severe hypertension based on pregnancy cut points. Adjusted ordinal logistic regression estimated the odds of women having a higher admission blood <span class="hlt">pressure</span> category as a function of <span class="hlt">air</span> pollutant, hypertensive disorders, and their interaction effect. Odds of high blood <span class="hlt">pressure</span> at admission to labor/delivery were increased in normotensive women after exposure to nitrogen oxides (by 0.2%/5 units), sulfur dioxide (by 0.3%/1 unit), carbon monoxide and several <span class="hlt">air</span> toxics (by 3%-4%/high exposure). The effects were often similar or stronger among women with gestational hypertension and preeclampsia. Exposure to particulate matter <10 μm increased odds of high blood <span class="hlt">pressure</span> in women with preeclampsia by 3%/5 units. <span class="hlt">Air</span> pollution can influence admission blood <span class="hlt">pressure</span> in term deliveries and may increase likelihood of preeclampsia screening at delivery admission. © Published by Oxford University Press on behalf of American Journal of Hypertension Ltd 2014. This work is written by (a) US Government employees(s) and is in the public domain in the US.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFM.A22A..03L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFM.A22A..03L"><span>Active Sensing <span class="hlt">Air</span> <span class="hlt">Pressure</span> Using Differential Absorption Barometric Radar</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lin, B.</p> <p>2016-12-01</p> <p>Tropical storms and other severe weathers cause huge life losses and property damages and have major impacts on public safety and national security. Their observations and predictions need to be significantly improved. This effort tries to develop a feasible active microwave approach that measures surface <span class="hlt">air</span> <span class="hlt">pressure</span>, especially over open seas, from space using a Differential-absorption BArometric Radar (DiBAR) operating at 50-55 GHz O2 absorption band in order to constrain assimilated dynamic fields of numerical weather Prediction (NWP) models close to actual conditions. <span class="hlt">Air</span> <span class="hlt">pressure</span> is the most important variable that drives atmospheric dynamics, and currently can only be measured by limited in-situ observations over oceans. Even over land there is no uniform coverage of surface <span class="hlt">air</span> <span class="hlt">pressure</span> measurements. Analyses show that with the proposed space radar the errors in instantaneous (averaged) <span class="hlt">pressure</span> estimates can be as low as 4mb ( 1mb) under all weather conditions. NASA Langley research team has made substantial progresses in advancing the DiBAR concept. The feasibility assessment clearly shows the potential of surface barometry using existing radar technologies. The team has also developed a DiBAR system design, fabricated a Prototype-DiBAR (P-DiBAR) for proof-of-concept, conducted laboratory, ground and airborne P-DiBAR tests. The flight test results are consistent with the instrumentation goals. The precision and accuracy of radar surface <span class="hlt">pressure</span> measurements are within the range of the theoretical analysis of the DiBAR concept. Observational system simulation experiments for space DiBAR performance based on the existing DiBAR technology and capability show substantial improvements in tropical storm predictions, not only for the hurricane track and position but also for the hurricane intensity. DiBAR measurements will provide us an unprecedented level of the prediction and knowledge on global extreme weather and climate conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970000447','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970000447"><span>Nonlinear Bubble Interactions in Acoustic <span class="hlt">Pressure</span> Fields</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Barbat, Tiberiu; Ashgriz, Nasser; Liu, Ching-Shi</p> <p>1996-01-01</p> <p>The systems consisting of a two-phase mixture, as clouds of bubbles or <span class="hlt">drops</span>, have shown many common features in their responses to different external force fields. One of particular interest is the effect of an unsteady <span class="hlt">pressure</span> field applied to these systems, case in which the coupling of the vibrations induced in two neighboring components (two <span class="hlt">drops</span> or two bubbles) may result in an interaction force between them. This behavior was explained by Bjerknes by postulating that every body that is moving in an accelerating fluid is subjected to a 'kinetic buoyancy' equal with the product of the acceleration of the fluid multiplied by the mass of the fluid displaced by the body. The external sound wave applied to a system of <span class="hlt">drops</span>/bubbles triggers secondary sound waves from each component of the system. These secondary <span class="hlt">pressure</span> fields integrated over the surface of the neighboring <span class="hlt">drop</span>/bubble may result in a force additional to the effect of the primary sound wave on each component of the system. In certain conditions, the magnitude of these secondary forces may result in significant changes in the dynamics of each component, thus in the behavior of the entire system. In a system containing bubbles, the sound wave radiated by one bubble at the location of a neighboring one is dominated by the volume oscillation mode and its effects can be important for a large range of frequencies. The interaction forces in a system consisting of <span class="hlt">drops</span> are much smaller than those consisting of bubbles. Therefore, as a first step towards the understanding of the <span class="hlt">drop-drop</span> interaction subject to external <span class="hlt">pressure</span> fluctuations, it is more convenient to study the bubble interactions. This paper presents experimental results and theoretical predictions concerning the interaction and the motion of two levitated <span class="hlt">air</span> bubbles in water in the presence of an acoustic field at high frequencies (22-23 KHz).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740022383','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740022383"><span>Improved fireman's compressed <span class="hlt">air</span> breathing system <span class="hlt">pressure</span> vessel development program</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>King, H. A.; Morris, E. E.</p> <p>1973-01-01</p> <p>Prototype high <span class="hlt">pressure</span> glass filament-wound, aluminum-lined <span class="hlt">pressurant</span> vessels suitable for use in a fireman's compressed <span class="hlt">air</span> breathing system were designed, fabricated, and acceptance tested in order to demonstrate the feasibility of producing such high performance, lightweight units. The 4000 psi tanks have a 60 standard cubic foot (SCF) <span class="hlt">air</span> capacity, and have a 6.5 inch diamter, 19 inch length, 415 inch volume, weigh 13 pounds when empty, and contain 33 percent more <span class="hlt">air</span> than the current 45 SCF (2250 psi) steel units. The current steel 60 SCF (3000 psi) tanks weigh approximately twice as much as the prototype when empty, and are 2 inches, or 10 percent shorter. The prototype units also have non-rusting aluminum interiors, which removes the hazard of corrosion, the need for internal coatings, and the possibility of rust particles clogging the breathing system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768090','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768090"><span>Torricelli and the Ocean of <span class="hlt">Air</span>: The First Measurement of Barometric <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2013-01-01</p> <p>The recognition of barometric <span class="hlt">pressure</span> was a critical step in the development of environmental physiology. In 1644, Evangelista Torricelli described the first mercury barometer in a remarkable letter that contained the phrase, “We live submerged at the bottom of an ocean of the element <span class="hlt">air</span>, which by unquestioned experiments is known to have weight.” This extraordinary insight seems to have come right out of the blue. Less than 10 years before, the great Galileo had given an erroneous explanation for the related problem of pumping water from a deep well. Previously, Gasparo Berti had filled a very long lead vertical tube with water and showed that a vacuum formed at the top. However, Torricelli was the first to make a mercury barometer and understand that the mercury was supported by the <span class="hlt">pressure</span> of the <span class="hlt">air</span>. Aristotle stated that the <span class="hlt">air</span> has weight, although this was controversial for some time. Galileo described a method of measuring the weight of the <span class="hlt">air</span> in detail, but for reasons that are not clear his result was in error by a factor of about two. Torricelli surmised that the <span class="hlt">pressure</span> of the <span class="hlt">air</span> might be less on mountains, but the first demonstration of this was by Blaise Pascal. The first <span class="hlt">air</span> pump was built by Otto von Guericke, and this influenced Robert Boyle to carry out his classical experiments of the physiological effects of reduced barometric <span class="hlt">pressure</span>. These were turning points in the early history of high-altitude physiology. PMID:23455767</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=EM-0034-01&hterms=air+company&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dair%2Bcompany','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=EM-0034-01&hterms=air+company&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dair%2Bcompany"><span>X-24B launch - <span class="hlt">air</span> <span class="hlt">drop</span> from mothership</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>1974-01-01</p> <p> powered mission November 15, 1973. Among the final flights with the X-24B were two precise landings on the main concrete runway at Edwards, California, which showed that accurate unpowered reentry vehicle landings were operationally feasible. These missions were flown by Manke and <span class="hlt">Air</span> Force Maj. Mike Love and represented the final milestone in a program that helped write the flight plan for the Space Shuttle program of today. After launch from the B-52 'mothership' at an altitude of about 45,000 feet, the XLR-11 rocket engine was ignited and the vehicle accelerated to speeds of more than 1,100 miles per hour and to altitudes of 60,000 to 70,000 feet. After the rocket engine was shut down, the pilots began steep glides towards the Edwards runway. As the pilots entered the final leg of their approach, they increased their rate of descent to build up speed and used this energy to perform a 'flare out' maneuver, which slowed their landing speed to about 200 miles per hour--the same basic approach pattern and landing speed of the Space Shuttles today. The final powered flight with the X-24B aircraft was on September 23, l975. The pilot was Bill Dana, and it was also the last rocket-powered flight flown at Dryden. It was also Dana who flew the last X-15 mission about seven years earlier. Top speed reached with the X-24B was 1,164 miles per hour (Mach 1.76) by Love on October 25, 1974. The highest altitude reached was 74,100 feet, by Manke on May 22, 1975. The X-24B is on public display at the <span class="hlt">Air</span> Force Museum, Wright-Patterson AFB, Ohio. This roughly 20-second video clip shows the X-24B <span class="hlt">dropping</span> from the B-52 mothership, after which the rocket engine ignites.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170006617','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170006617"><span>Filter Efficiency and <span class="hlt">Pressure</span> Testing of Returned ISS Bacterial Filter Elements (BFEs)</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Green, Robert D.; Agui, Juan H.; Berger, Gordon M.; Vijayakumar, R.; Perry, Jay L.</p> <p>2017-01-01</p> <p>The <span class="hlt">air</span> quality control equipment aboard the International Space Station (ISS) and future deep space exploration vehicles provide the vital function of maintaining a clean cabin environment for the crew and the hardware. This becomes a serious challenge in <span class="hlt">pressurized</span> space compartments since no outside <span class="hlt">air</span> ventilation is possible, and a larger particulate load is imposed on the filtration system due to lack of sedimentation. The ISS Environmental Control and Life Support (ECLS) system architecture in the U.S. Segment uses a distributed particulate filtration approach consisting of traditional High-Efficiency Particulate <span class="hlt">Air</span> (HEPA) filters deployed at multiple locations in each U.S. Seg-ment module; these filters are referred to as Bacterial Filter Elements, or BFEs. In our previous work, we presented results of efficiency and <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements for a sample set of two returned BFEs with a service life of 2.5 years. In this follow-on work, we present similar efficiency, <span class="hlt">pressure</span> <span class="hlt">drop</span>, and leak tests results for a larger sample set of six returned BFEs. The results of this work can aid the ISS Program in managing BFE logistics inventory through the stations planned lifetime as well as provide insight for managing filter element logistics for future exploration missions. These results also can provide meaningful guidance for particulate filter designs under consideration for future deep space exploration missions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AIPC.1703f0004S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AIPC.1703f0004S"><span><span class="hlt">Pressures</span> in the human cochlea during bone conduction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Stieger, Christof; Farahmand, Rosemary B.; Page, Brent F.; Roushan, Kourosh; Merchant, Julie P.; Abur, Defne; Rosowski, John J.; Nakajima, Hideko Heidi</p> <p>2015-12-01</p> <p>The mechanisms of bone conduction (BC) hearing, which is important in diagnosis and treatment of hearing loss, are poorly understood, thus limiting use of BC. Recently, information gained by intracochlear <span class="hlt">pressure</span> measurements has revealed that the mechanisms of sound transmission that drive <span class="hlt">pressure</span> differences across the cochlear partition are different for <span class="hlt">air</span> conduction (AC) than for round-window stimulation. Presently we are utilizing these <span class="hlt">pressure</span> measurement techniques in fresh human cadaveric preparations to improve our understanding of sound transmission during BC. We have modified our technique of intracochlear <span class="hlt">pressure</span> measurements for the special requirements of studying BC, as bone vibration poses challenges for making these measurements. Fiberoptic <span class="hlt">pressure</span> sensors were inserted through cochleostomies in both scalae at the base of the cochlea. The cochleostomies were then tightly sealed with the sensors in place to prevent <span class="hlt">air</span> and fluid leaks, and the sensors were firmly secured to ensure uniform vibrations of the sensors and surrounding bone of the cochlea. The velocity of the stapes, round window and cochlear promontory were each measured with laser Doppler vibrometry simultaneous to the intracochlear <span class="hlt">pressure</span> measurements. To understand the contribution of middle-ear inertia, the incudo-stapedial joint was severed. Subsequently, the stapes footplate was fixed (similar to the consequence of otosclerosis) to determine the effect of removing the mobility of the oval window. BC stimulation resulted in <span class="hlt">pressure</span> in scala vestibuli that was significantly higher than in scala tympani, such that the differential <span class="hlt">pressure</span> across the partition - the cochlear drive input - was similar to scala vestibuli <span class="hlt">pressure</span> (and overall, similar to the relationship found during AC but different than during round-window stimulation). After removing the inertial mass of the middle ear, with only the stapes attached to the flexible oval window, all <span class="hlt">pressures</span> <span class="hlt">dropped</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26712286','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26712286"><span>Adding a custom made <span class="hlt">pressure</span> release valve during <span class="hlt">air</span> enema for intussusception: A new technique.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ahmed, Hosni Morsi; Ahmed, Osama; Ahmed, Refaat Khodary</p> <p>2015-01-01</p> <p>Non-surgical reduction remains the first line treatment of choice for intussusception. The major complication of <span class="hlt">air</span> enema reduction is bowel perforation. The authors developed a custom made <span class="hlt">pressure</span> release valve to be added to portable insufflation devices, delivering <span class="hlt">air</span> at <span class="hlt">pressures</span> accepted as safe for effective reduction of intussusception in children under fluoroscopic guidance. The aim of this study was to develop a custom made <span class="hlt">pressure</span> release valve that is suitable for the insufflation devices used for <span class="hlt">air</span> enema reduction of intussusception and to put this valve into regular clinical practice. An adjustable, custom made <span class="hlt">pressure</span> release valve was assembled by the authors using readily available components. The valve was coupled to a simple <span class="hlt">air</span> enema insufflation device. The device was used for the trial of reduction of intussusception in a prospective study that included 132 patients. The success rate for <span class="hlt">air</span> enema reduction with the new device was 88.2%. The mean <span class="hlt">pressure</span> required to achieve complete reduction was 100 mmHg. The insufflation <span class="hlt">pressure</span> never exceeded the preset value (120 mmHg). Of the successful cases, 58.3% were reduced from the first attempt while 36.1% required a second insufflation. Only 5.55% required a third insufflation to complete the reduction. In cases with unsuccessful pneumatic reduction attempt (18.1%), surgical treatment was required. Surgery ranged from simple reduction to resection with a primary end to end anastomosis. No complications from <span class="hlt">air</span> enema were recorded. The authors recommend adding <span class="hlt">pressure</span> release valves to ensure safety by avoiding <span class="hlt">pressure</span> overshoot during the procedure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017HMT....53..343K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017HMT....53..343K"><span>A critical review of forced convection heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of Al2O3, TiO2 and CuO nanofluids</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Khurana, Deepak; Choudhary, Rajesh; Subudhi, Sudhakar</p> <p>2017-01-01</p> <p>Nanofluid is the colloidal suspension of nanosized solid particles like metals or metal oxides in some conventional fluids like water and ethylene glycol. Due to its unique characteristics of enhanced heat transfer compared to conventional fluid, it has attracted the attention of research community. The forced convection heat transfer of nanofluid is investigated by numerous researchers. This paper critically reviews the papers published on experimental studies of forced convection heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> of Al2O3, TiO2 and CuO based nanofluids dispersed in water, ethylene glycol and water-ethylene glycol mixture. Most of the researchers have shown a little rise in <span class="hlt">pressure</span> <span class="hlt">drop</span> with the use of nanofluids in plain tube. Literature has reported that the pumping power is appreciably high, only at very high particle concentration i.e. more than 5 %. As nanofluids are able to enhance the heat transfer at low particle concentrations so most of the researchers have used less than 3 % volume concentration in their studies. Almost no disagreement is observed on <span class="hlt">pressure</span> <span class="hlt">drop</span> results of different researchers. But there is not a common agreement in magnitude and mechanism of heat transfer enhancement. Few studies have shown an anomalous enhancement in heat transfer even at low particle concentration. On the contrary, some researchers have shown little heat transfer enhancement at the same particle concentration. A large variation (2-3 times) in Nusselt number was observed for few studies under similar conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28594862','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28594862"><span>Application of acoustic agglomeration to enhance <span class="hlt">air</span> filtration efficiency in <span class="hlt">air</span>-conditioning and mechanical ventilation (ACMV) systems.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ng, Bing Feng; Xiong, Jin Wen; Wan, Man Pun</p> <p>2017-01-01</p> <p>The recent episodes of haze in Southeast Asia have caused some of the worst regional atmospheric pollution ever recorded in history. In order to control the levels of airborne fine particulate matters (PM) indoors, filtration systems providing high PM capturing efficiency are often sought, which inadvertently also results in high airflow resistance (or <span class="hlt">pressure</span> <span class="hlt">drop</span>) that increases the energy consumption for <span class="hlt">air</span> distribution. A pre-conditioning mechanism promoting the formation of particle clusters to enhance PM capturing efficiency without adding flow resistance in the <span class="hlt">air</span> distribution ductwork could provide an energy-efficient solution. This pre-conditioning mechanism can be fulfilled by acoustic agglomeration, which is a phenomenon that promotes the coagulation of suspended particles by acoustic waves propagating in the fluid medium. This paper discusses the basic mechanisms of acoustic agglomeration along with influencing factors that could affect the agglomeration efficiency. The feasibility to apply acoustic agglomeration to improve filtration in <span class="hlt">air</span>-conditioning and mechanical ventilation (ACMV) systems is investigated experimentally in a small-scale wind tunnel. Experimental results indicate that this novel application of acoustic pre-conditioning improves the PM2.5 filtration efficiency of the test filters by up to 10% without introducing additional <span class="hlt">pressure</span> <span class="hlt">drop</span>. The fan energy savings from not having to switch to a high capturing efficiency filter largely outstrip the additional energy consumed by the acoustics system. This, as a whole, demonstrates potential energy savings from the combined acoustic-enhanced filtration system without compromising on PM capturing efficiency.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5464643','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5464643"><span>Application of acoustic agglomeration to enhance <span class="hlt">air</span> filtration efficiency in <span class="hlt">air</span>-conditioning and mechanical ventilation (ACMV) systems</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Xiong, Jin Wen; Wan, Man Pun</p> <p>2017-01-01</p> <p>The recent episodes of haze in Southeast Asia have caused some of the worst regional atmospheric pollution ever recorded in history. In order to control the levels of airborne fine particulate matters (PM) indoors, filtration systems providing high PM capturing efficiency are often sought, which inadvertently also results in high airflow resistance (or <span class="hlt">pressure</span> <span class="hlt">drop</span>) that increases the energy consumption for <span class="hlt">air</span> distribution. A pre-conditioning mechanism promoting the formation of particle clusters to enhance PM capturing efficiency without adding flow resistance in the <span class="hlt">air</span> distribution ductwork could provide an energy-efficient solution. This pre-conditioning mechanism can be fulfilled by acoustic agglomeration, which is a phenomenon that promotes the coagulation of suspended particles by acoustic waves propagating in the fluid medium. This paper discusses the basic mechanisms of acoustic agglomeration along with influencing factors that could affect the agglomeration efficiency. The feasibility to apply acoustic agglomeration to improve filtration in <span class="hlt">air</span>-conditioning and mechanical ventilation (ACMV) systems is investigated experimentally in a small-scale wind tunnel. Experimental results indicate that this novel application of acoustic pre-conditioning improves the PM2.5 filtration efficiency of the test filters by up to 10% without introducing additional <span class="hlt">pressure</span> <span class="hlt">drop</span>. The fan energy savings from not having to switch to a high capturing efficiency filter largely outstrip the additional energy consumed by the acoustics system. This, as a whole, demonstrates potential energy savings from the combined acoustic-enhanced filtration system without compromising on PM capturing efficiency. PMID:28594862</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_16 --> <div id="page_17" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="321"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24925548','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24925548"><span>Layers of <span class="hlt">air</span> in the water beneath the floating fern Salvinia are exposed to fluctuations in <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mayser, Matthias J; Barthlott, Wilhelm</p> <p>2014-12-01</p> <p>Superhydrophobic, hierarchically structured, technical surfaces (Lotus-effect) are of high scientific and economic interest because of their remarkable properties. Recently, the immense potential of <span class="hlt">air</span>-retaining superhydrophobic surfaces, for example, for low-friction transport of fluids and drag-reducing coatings of ships has begun to be explored. A major problem of superhydrophobic surfaces mimicking the Lotus-effect is the limited persistence of the <span class="hlt">air</span> retained, especially under rough conditions of flow. However, there are a variety of floating or diving plant and animal species that possess <span class="hlt">air</span>-retaining surfaces optimized for durable water-repellency (Salvinia-effect). Especially floating ferns of the genus Salvinia have evolved superhydrophobic surfaces capable of maintaining layers of <span class="hlt">air</span> for months. Apart from maintaining stability under water, the layer of <span class="hlt">air</span> has to withstand the stresses of water <span class="hlt">pressure</span> (up to 2.5 bars). Both of these aspects have an application to create permanent <span class="hlt">air</span> layers on ships' hulls. We investigated the effect of <span class="hlt">pressure</span> on <span class="hlt">air</span> layers in a <span class="hlt">pressure</span> cell and exposed the <span class="hlt">air</span> layer to <span class="hlt">pressures</span> of up to 6 bars. We investigated the suppression of the <span class="hlt">air</span> layer at increasing <span class="hlt">pressures</span> as well as its restoration during decreases in <span class="hlt">pressure</span>. Three of the four examined Salvinia species are capable of maintaining <span class="hlt">air</span> layers at <span class="hlt">pressures</span> relevant to the conditions applying to ships' hulls. High volumes of <span class="hlt">air</span> per surface area are advantageous for retaining at least a partial Cassie-Baxter-state under <span class="hlt">pressure</span>, which also helps in restoring the <span class="hlt">air</span> layer after depressurization. Closed-loop structures such as the baskets at the top of the "egg-beater hairs" (see main text) also help return the <span class="hlt">air</span> layer to its original level at the tip of the hairs by trapping <span class="hlt">air</span> bubbles. © The Author 2014. Published by Oxford University Press on behalf of the Society for Integrative and Comparative Biology. All rights reserved. For permissions</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21890395','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21890395"><span>An analysis of contact stiffness between a finger and an object when wearing an <span class="hlt">air</span>-cushioned glove: the effects of the <span class="hlt">air</span> <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wu, John Z; Wimer, Bryan M; Welcome, Daniel E; Dong, Ren G</p> <p>2012-04-01</p> <p><span class="hlt">Air</span>-cushioned gloves have the advantages of lighter weight, lower cost, and unique mechanical performance, compared to gloves made of conventional engineering materials. The goal of this study is to analyze the contact interaction between fingers and object when wearing an <span class="hlt">air</span>-cushioned glove. The contact interactions between the the fingertip and <span class="hlt">air</span> bubbles, which is considered as a cell of a typical <span class="hlt">air</span>-cushioned glove, has been analyzed theoretically. Two-dimensional finite element models were developed for the analysis. The fingertip model was assumed to be composed of skin layers, subcutaneous tissue, bone, and nail. The <span class="hlt">air</span> bubbles were modeled as <span class="hlt">air</span> sealed in the container of nonelastic membrane. We simulated two common scenarios: a fingertip in contact with one single <span class="hlt">air</span> bubble and with two <span class="hlt">air</span> cushion bubbles simultaneously. Our simulation results indicated that the internal <span class="hlt">air</span> <span class="hlt">pressure</span> can modulate the fingertip-object contact characteristics. The contact stiffness reaches a minimum when the initial <span class="hlt">air</span> <span class="hlt">pressure</span> is equal to 1.3 and 1.05 times of the atmosphere <span class="hlt">pressure</span> for the single <span class="hlt">air</span> bubble and the double <span class="hlt">air</span> bubble contact, respectively. Furthermore, the simulation results indicate that the double <span class="hlt">air</span> bubble contact will result in smaller volumetric tissue strain than the single <span class="hlt">air</span> bubble contact for the same force. Published by Elsevier Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007JPhCS..90a2026P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007JPhCS..90a2026P"><span>Microcontrolled <span class="hlt">air</span>-mattress for ulcer by <span class="hlt">pressure</span> prevention</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pasluosta, Cristian F.; Fontana, Juan M.; Beltramone, Diego A.; Taborda, Ricardo A. M.</p> <p>2007-11-01</p> <p>An ulcer by <span class="hlt">pressure</span> is produced when a constant <span class="hlt">pressure</span> is exerted over the skin. This generates the collapse of the blood vessels and, therefore, a lack in the contribution of the necessary nutrients for the affected zone. As a consequence, the skin deteriorates, eventually causing an ulcer. In order to prevent it, a protocol must be applied to the patient, which is reflected on time and cost of treatment. There are some <span class="hlt">air</span> mattresses available for this purpose, but whose performance does not fulfill all requirements. The prototype designed in our laboratory is based on the principle of the <span class="hlt">air</span> mattress. Its objective is to improve on existing technologies and, due to an increased automation, reduce time dedication for personnel in charge of the patient. A clinical experience was made in the local Emergencies Hospital and also in an institution dedicated to aged patients care. In both cases, the results obtained and the comments from the personnel involved were favorable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA243535','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA243535"><span>Evaluation of BAUER High <span class="hlt">Pressure</span> Breathing <span class="hlt">Air</span> P-2 Purification System</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1991-08-01</p> <p>and is a coalescing type separator that removes oil and water vapors suspended in the compressed <span class="hlt">air</span> . The molecular sieve is made to adsorb oil and...filtering, moisture separation, and prevents compressed <span class="hlt">air</span> return from the charged <span class="hlt">air</span> storage flasks to the compressor during unit shutdown. A manual...1111111111111 1111 IE IH fil91i C NAVY EXPERIMENTAL DIVING UNIT REPORT NO. 10-91 EVALUATION OF BAUER HIGH <span class="hlt">PRESSURE</span> BREATHING <span class="hlt">AIR</span> P-2 PURIFICATION SYSTEM GEORGE D</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/874070','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/874070"><span>Combustor <span class="hlt">air</span> flow control method for fuel cell apparatus</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Clingerman, Bruce J.; Mowery, Kenneth D.; Ripley, Eugene V.</p> <p>2001-01-01</p> <p>A method for controlling the heat output of a combustor in a fuel cell apparatus to a fuel processor where the combustor has dual <span class="hlt">air</span> inlet streams including atmospheric <span class="hlt">air</span> and fuel cell cathode effluent containing oxygen depleted <span class="hlt">air</span>. In all operating modes, an enthalpy balance is provided by regulating the quantity of the <span class="hlt">air</span> flow stream to the combustor to support fuel cell processor heat requirements. A control provides a quick fast forward change in an <span class="hlt">air</span> valve orifice cross section in response to a calculated predetermined <span class="hlt">air</span> flow, the molar constituents of the <span class="hlt">air</span> stream to the combustor, the <span class="hlt">pressure</span> <span class="hlt">drop</span> across the <span class="hlt">air</span> valve, and a look up table of the orifice cross sectional area and valve steps. A feedback loop fine tunes any error between the measured <span class="hlt">air</span> flow to the combustor and the predetermined <span class="hlt">air</span> flow.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPCM...30i4002Q','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPCM...30i4002Q"><span>Hydrodynamic shrinkage of liquid CO2 Taylor <span class="hlt">drops</span> in a straight microchannel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Qin, Ning; Wen, John Z.; Ren, Carolyn L.</p> <p>2018-03-01</p> <p>Hydrodynamic shrinkage of liquid CO2 <span class="hlt">drops</span> in water under a Taylor flow regime is studied using a straight microchannel (length/width ~100). A general form of a mathematical model of the solvent-side mass transfer coefficient (k s) is developed first. Based on formulations of the surface area (A) and the volume (V) of a general Taylor <span class="hlt">drop</span> in a rectangular microchannel, a specific form of k s is derived. <span class="hlt">Drop</span> length and speed are experimentally measured at three specified positions of the straight channel, namely, immediately after <span class="hlt">drop</span> generation (position 1), the midpoint of the channel (position 2) and the end of the channel (position 3). The reductions of <span class="hlt">drop</span> length (L x , x  =  1, 2, 3) from position 1 to 2 and down to 3 are used to quantify the <span class="hlt">drop</span> shrinkage. Using the specific model, k s is calculated mainly based on L x and <span class="hlt">drop</span> flowing time (t). Results show that smaller CO2 <span class="hlt">drops</span> produced by lower flow rate ratios ({{Q}LC{{O2}}}/{{Q}{{H2}O}} ) are generally characterized by higher (nearly three times) k s and Sherwood numbers than those produced by higher {{Q}LC{{O2}}}/{{Q}{{H2}O}} , which is essentially attributed to the larger effective portion of the smaller <span class="hlt">drop</span> contributing in the mass transfer under same levels of the flowing time and the surface-to-volume ratio (~104 m-1) of all <span class="hlt">drops</span>. Based on calculated <span class="hlt">pressure</span> <span class="hlt">drops</span> of the segmented flow in microchannel, the Peng-Robinson equation of state and initial <span class="hlt">pressures</span> of <span class="hlt">drops</span> at the T-junction in experiments, overall <span class="hlt">pressure</span> <span class="hlt">drop</span> (ΔP t) in the straight channel as well as the resulted <span class="hlt">drop</span> volume change are quantified. ΔP t from position 1-3 is by average 3.175 kPa with a ~1.6% standard error, which only leads to relative <span class="hlt">drop</span> volume changes of 0.3‰ to 0.52‰.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16790065','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16790065"><span>Transient integral boundary layer method to calculate the translesional <span class="hlt">pressure</span> <span class="hlt">drop</span> and the fractional flow reserve in myocardial bridges.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bernhard, Stefan; Möhlenkamp, Stefan; Tilgner, Andreas</p> <p>2006-06-21</p> <p>The <span class="hlt">pressure</span> <span class="hlt">drop</span>-flow relations in myocardial bridges and the assessment of vascular heart disease via fractional flow reserve (FFR) have motivated many researchers the last decades. The aim of this study is to simulate several clinical conditions present in myocardial bridges to determine the flow reserve and consequently the clinical relevance of the disease. From a fluid mechanical point of view the pathophysiological situation in myocardial bridges involves fluid flow in a time dependent flow geometry, caused by contracting cardiac muscles overlying an intramural segment of the coronary artery. These flows mostly involve flow separation and secondary motions, which are difficult to calculate and analyse. Because a three dimensional simulation of the haemodynamic conditions in myocardial bridges in a network of coronary arteries is time-consuming, we present a boundary layer model for the calculation of the <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow separation. The approach is based on the assumption that the flow can be sufficiently well described by the interaction of an inviscid core and a viscous boundary layer. Under the assumption that the idealised flow through a constriction is given by near-equilibrium velocity profiles of the Falkner-Skan-Cooke (FSC) family, the evolution of the boundary layer is obtained by the simultaneous solution of the Falkner-Skan equation and the transient von-Kármán integral momentum equation. The model was used to investigate the relative importance of several physical parameters present in myocardial bridges. Results have been obtained for steady and unsteady flow through vessels with 0 - 85% diameter stenosis. We compare two clinical relevant cases of a myocardial bridge in the middle segment of the left anterior descending coronary artery (LAD). The <span class="hlt">pressure</span> derived FFR of fixed and dynamic lesions has shown that the flow is less affected in the dynamic case, because the distal <span class="hlt">pressure</span> partially recovers during re-opening of the vessel in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=1564397','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=1564397"><span>Transient integral boundary layer method to calculate the translesional <span class="hlt">pressure</span> <span class="hlt">drop</span> and the fractional flow reserve in myocardial bridges</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Bernhard, Stefan; Möhlenkamp, Stefan; Tilgner, Andreas</p> <p>2006-01-01</p> <p>Background The <span class="hlt">pressure</span> <span class="hlt">drop</span> – flow relations in myocardial bridges and the assessment of vascular heart disease via fractional flow reserve (FFR) have motivated many researchers the last decades. The aim of this study is to simulate several clinical conditions present in myocardial bridges to determine the flow reserve and consequently the clinical relevance of the disease. From a fluid mechanical point of view the pathophysiological situation in myocardial bridges involves fluid flow in a time dependent flow geometry, caused by contracting cardiac muscles overlying an intramural segment of the coronary artery. These flows mostly involve flow separation and secondary motions, which are difficult to calculate and analyse. Methods Because a three dimensional simulation of the haemodynamic conditions in myocardial bridges in a network of coronary arteries is time-consuming, we present a boundary layer model for the calculation of the <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow separation. The approach is based on the assumption that the flow can be sufficiently well described by the interaction of an inviscid core and a viscous boundary layer. Under the assumption that the idealised flow through a constriction is given by near-equilibrium velocity profiles of the Falkner-Skan-Cooke (FSC) family, the evolution of the boundary layer is obtained by the simultaneous solution of the Falkner-Skan equation and the transient von-Kármán integral momentum equation. Results The model was used to investigate the relative importance of several physical parameters present in myocardial bridges. Results have been obtained for steady and unsteady flow through vessels with 0 – 85% diameter stenosis. We compare two clinical relevant cases of a myocardial bridge in the middle segment of the left anterior descending coronary artery (LAD). The <span class="hlt">pressure</span> derived FFR of fixed and dynamic lesions has shown that the flow is less affected in the dynamic case, because the distal <span class="hlt">pressure</span> partially recovers</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..DFDL33007K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..DFDL33007K"><span>Propelling a water <span class="hlt">drop</span> with the vapor-mediated Marangoni effect</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Seungho; Kim, Ho-Young</p> <p>2013-11-01</p> <p>We show that a water <span class="hlt">drop</span> on solid surfaces can be propelled just by placing a volatile alcohol <span class="hlt">drop</span> nearby. It is found to be because the water-<span class="hlt">air</span> interface near the alcohol <span class="hlt">drop</span> mixes with alcohol vapor, thereby locally lowering the surface tension. The surface-tension-gradient induces the motion of the water <span class="hlt">drop</span>, enabling the trajectory control of water <span class="hlt">drops</span> through the motion of remote alcohol <span class="hlt">drops</span>. This vapor-mediated Marangoni effect also gives rise to other interesting interfacial flow phenomena, such as nucleation of holes on a water film and ballooning of a water <span class="hlt">drop</span> hanging from a syringe needle with the approach of an alcohol <span class="hlt">drop</span>. We visualize such interfacial dynamics with a high-speed camera and rationalize their salient features by scaling analysis. This work was supported by the National Research Foundation of Korea (grant no. 2012-008023).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016MMTB...47.1409H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016MMTB...47.1409H"><span>Heat Transfer and Observation of Droplet-Surface Interactions During <span class="hlt">Air</span>-Mist Cooling at CSP Secondary System Temperatures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huerta L., Mario E.; Mejía G., M. Esther; Castillejos E., A. Humberto</p> <p>2016-04-01</p> <p><span class="hlt">Air</span>-mists are key elements in the secondary cooling of modern thin steel slab continuous casters. The selection of water, W, and <span class="hlt">air</span>, A, flow rates, and <span class="hlt">pressures</span> in pneumatic nozzles open up a wide spectrum of cooling possibilities by their influence on droplet diameter, d, droplet velocity, v, and water impact flux, w. Nonetheless, due to the harsh environment resulting from the high temperatures and dense mists involved, there is very little information about the correlation between heat flux extracted, - q, and mist characteristics, and none about the dynamics of <span class="hlt">drop</span>-wall interactions. For obtaining both kinds of information, this work combines a steady-state heat flux measuring method with a visualization technique based on a high-speed camera and a laser illumination system. For wall temperatures, T w, between ~723 K and ~1453 K (~450 °C and ~1180 °C), which correspond to film boiling regime, it was confirmed that - q increases with increase in v, w, and T w and with decrease in d. It should be noticed, however, that the increase in w generally decreases the spray cooling effectiveness because striking <span class="hlt">drops</span> do not evaporate efficiently due to the interference by liquid remains from previous <span class="hlt">drops</span>. Visualization of the events happening close to the surface also reveals that the contact time of the liquid with the surface is very brief and that rebounding, splashing, sliding, and levitation of <span class="hlt">drops</span> lead to ineffective contact with the surface. At the center of the mist footprint, where <span class="hlt">drops</span> impinge nearly normal to the surface those with enough momentum establish intimate contact with it before forming a vapor layer that pushes away the remaining liquid. Also, some <span class="hlt">drops</span> are observed sliding upon the surface or levitating close to it; these are <span class="hlt">drops</span> with low momentum which are influenced by the deflecting <span class="hlt">air</span> stream. At footprint positions where oblique impingement occurs, frequently <span class="hlt">drops</span> are spotted sliding or levitating and liquid films flowing in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ApPhL.109j1602Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ApPhL.109j1602Z"><span>Vertical vibration dynamics of acoustically levitated <span class="hlt">drop</span> containing two immiscible liquids</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zang, Duyang; Zhai, Zhicong; Li, Lin; Lin, Kejun; Li, Xiaoguang; Geng, Xingguo</p> <p>2016-09-01</p> <p>We have studied the levitation and oscillation dynamics of complex <span class="hlt">drops</span> containing two immiscible liquids. Two types of <span class="hlt">drops</span>, core-shell <span class="hlt">drop</span> and abnormal-shaped <span class="hlt">drop</span>, have been obtained depending on the levitation procedures. The oscillation dynamics of the <span class="hlt">drops</span> have been studied using a high speed camera. It has been found that the oscillation of the abnormal-shaped <span class="hlt">drop</span> has a longer oscillation period and decays much faster than that of the core-shell <span class="hlt">drop</span>, which cannot be accounted for by the <span class="hlt">air</span> resistance itself. The acoustic streaming induced by ultrasound may bring an additional force against the motion of the <span class="hlt">drop</span> due to the Bernoulli effect. This is responsible for the enhanced damping during the oscillation in acoustic levitation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970000446','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970000446"><span>Studies of the Stability and Dynamics of Levitated <span class="hlt">Drops</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anikumar, A.; Lee, Chun Ping; Wang, T. G.</p> <p>1996-01-01</p> <p>This is a review of our experimental and theoretical studies relating to equilibrium and stability of liquid <span class="hlt">drops</span>, typically of low viscosity, levitated in <span class="hlt">air</span> by a sound field. The major emphasis here is on the physical principles and understanding behind the stability of levitated <span class="hlt">drops</span>. A comparison with experimental data is also given, along with some fascinating pictures from high-speed photography. One of the aspects we shall deal with is how a <span class="hlt">drop</span> can suddenly burst in an intense sound field; a phenomenon which can find applications in atomization technology. Also, we are currently investigating the phenomenon of suppression of coalescence between <span class="hlt">drops</span> levitated in intense acoustic fields.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.891a2017S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.891a2017S"><span>Evaporation of oil-water emulsion <span class="hlt">drops</span> when heated at high temperature</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Strizhak, P. A.; Piskunov, M. V.; Kuznetsov, G. V.; Voytkov, I. S.</p> <p>2017-10-01</p> <p>An experimental study on conditions and main characteristics for high-temperature (more than 700 K) evaporation of oil-water <span class="hlt">drops</span> is presented. The high-temperature water purification from impurities can be the main practical application of research results. Thus, the heating of <span class="hlt">drops</span> is implemented by the two typical schemes: on a massive substrate (the heating conditions are similar to those achieved in a heating chamber) and in a flow of the heated <span class="hlt">air</span>. In the latter case, the heating conditions correspond to those attained while moving water <span class="hlt">drops</span> with impurities in a counter high-temperature gaseous flow in the process of water purification. Evaporation time as function of heating temperature is presented. The influence of oil product concentration in an emulsion <span class="hlt">drop</span> on evaporation characteristics is discussed. The conditions for intensive flash boiling of an emulsion <span class="hlt">drop</span> and its explosive breakup with formation of the fine droplets cloud are pointed out. Heat fluxes required for intensive flash boiling and explosive breakup of a <span class="hlt">drop</span> with further formation of the fine aerosol are determined in the boundary layer of a <span class="hlt">drop</span>. The fundamental differences between flash boiling and explosive breakup of an emulsion <span class="hlt">drop</span> when heated on a substrate and in a flow of the heated <span class="hlt">air</span> are described. The main prospects for the development of the high-temperature water purification technology are detailed taking into account the fast emulsion <span class="hlt">drop</span> breakup investigated in the paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24787565','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24787565"><span>Analysis of the intraocular jet flows and <span class="hlt">pressure</span> gradients induced by <span class="hlt">air</span> and fluid infusion: mechanism of focal chorioretinal damage.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kim, Yong Joon; Jo, Sungkil; Moon, Daruchi; Joo, Youngcheol; Choi, Kyung Seek</p> <p>2014-05-01</p> <p>To comprehend the mechanism of focal chorioretinal damage by analysis of the <span class="hlt">pressure</span> distribution and dynamic <span class="hlt">pressure</span> induced by infused <span class="hlt">air</span> during fluid-<span class="hlt">air</span> exchange. A precise simulation featuring a model eye and a fluid circuit was designed to analyze fluid-<span class="hlt">air</span> exchange. The <span class="hlt">pressure</span> distribution, flow velocity, and dynamic <span class="hlt">pressure</span> induced by infusion of <span class="hlt">air</span> into an <span class="hlt">air</span>-filled eye were analyzed using an approach based on fluid dynamics. The size of the port and the infusion <span class="hlt">pressure</span> were varied during simulated iterations. We simulated infusion of an <span class="hlt">air</span>-filled eye with balanced salt solution (BSS) to better understand the mechanism of chorioretinal damage induced by infused <span class="hlt">air</span>. Infused <span class="hlt">air</span> was projected straight toward a point on the retina contralateral to the infusion port (the "vulnerable point"). The highest <span class="hlt">pressure</span> was evident at the vulnerable point, and the lowest <span class="hlt">pressure</span> was recorded on most retinal areas. Simulations using greater infusion <span class="hlt">pressure</span> and a port of larger size were associated with elevations in dynamic <span class="hlt">pressure</span> and the <span class="hlt">pressure</span> gradient. The <span class="hlt">pressure</span> gradients were 2.8 and 5.1 mm Hg, respectively, when infusion <span class="hlt">pressures</span> of 30 and 50 mm Hg were delivered through a 20-gauge port. The <span class="hlt">pressure</span> gradient associated with BSS infusion was greater than that created by <span class="hlt">air</span>, but lasted for only a moment. Our simulation explains the mechanism of focal chorioretinal damage in numerical terms. Infused <span class="hlt">air</span> induces a prolonged increase in focal <span class="hlt">pressure</span> on the vulnerable point, and this may be responsible for visual field defects arising after fluid-<span class="hlt">air</span> exchange. Copyright 2014 The Association for Research in Vision and Ophthalmology, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4590742','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4590742"><span>Long-Term <span class="hlt">Air</span> Pollution Exposure and Blood <span class="hlt">Pressure</span> in the Sister Study</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chan, Stephanie H.; Van Hee, Victor C.; Bergen, Silas; Szpiro, Adam A.; DeRoo, Lisa A.; London, Stephanie J.; Marshall, Julian D.; Sandler, Dale P.</p> <p>2015-01-01</p> <p>Background Exposure to <span class="hlt">air</span> pollution has been consistently associated with cardiovascular morbidity and mortality, but mechanisms remain uncertain. Associations with blood <span class="hlt">pressure</span> (BP) may help to explain the cardiovascular effects of <span class="hlt">air</span> pollution. Objective We examined the cross-sectional relationship between long-term (annual average) residential <span class="hlt">air</span> pollution exposure and BP in the National Institute of Environmental Health Sciences’ Sister Study, a large U.S. cohort study investigating risk factors for breast cancer and other outcomes. Methods This analysis included 43,629 women 35–76 years of age, enrolled 2003–2009, who had a sister with breast cancer. Geographic information systems contributed to satellite-based nitrogen dioxide (NO2) and fine particulate matter (≤ 2.5 μm; PM2.5) predictions at participant residences at study entry. Generalized additive models were used to examine the relationship between pollutants and measured BP at study entry, adjusting for cardiovascular disease risk factors and including thin plate splines for potential spatial confounding. Results A 10-μg/m3 increase in PM2.5 was associated with 1.4-mmHg higher systolic BP (95% CI: 0.6, 2.3; p < 0.001), 1.0-mmHg higher pulse <span class="hlt">pressure</span> (95% CI: 0.4, 1.7; p = 0.001), 0.8-mmHg higher mean arterial <span class="hlt">pressure</span> (95% CI: 0.2, 1.4; p = 0.01), and no significant association with diastolic BP. A 10-ppb increase in NO2 was associated with a 0.4-mmHg (95% CI: 0.2, 0.6; p < 0.001) higher pulse <span class="hlt">pressure</span>. Conclusions Long-term PM2.5 and NO2 exposures were associated with higher blood <span class="hlt">pressure</span>. On a population scale, such <span class="hlt">air</span> pollution–related increases in blood <span class="hlt">pressure</span> could, in part, account for the increases in cardiovascular disease morbidity and mortality seen in prior studies. Citation Chan SH, Van Hee VC, Bergen S, Szpiro AA, DeRoo LA, London SJ, Marshall JD, Kaufman JD, Sandler DP. 2015. Long-term <span class="hlt">air</span> pollution exposure and blood <span class="hlt">pressure</span> in the Sister Study. Environ Health</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970008136','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970008136"><span>Study of Critical Heat Flux and Two-Phase <span class="hlt">Pressure</span> <span class="hlt">Drop</span> Under Reduced Gravity</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Abdollahian, Davood; Quintal, Joseph; Barez, Fred; Zahm, Jennifer; Lohr, Victor</p> <p>1996-01-01</p> <p>The design of the two-phase flow systems which are anticipated to be utilized in future spacecraft thermal management systems requires a knowledge of two-phase flow and heat transfer phenomena in reduced gravities. This program was funded by NASA headquarters in response to NRA-91-OSSA-17 and was managed by Lewis Research Center. The main objective of this program was to design and construct a two-phase test loop, and perform a series of normal gravity and aircraft trajectory experiments to study the effect of gravity on the Critical Heat Flux (CHF) and onset of instability. The test loop was packaged on two aircraft racks and was also instrumented to generate data for two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span>. The normal gravity tests were performed with vertical up and downflow configurations to bound the effect of gravity on the test parameters. One set of aircraft trajectory tests was performed aboard the NASA DC-9 aircraft. These tests were mainly intended to evaluate the test loop and its operational performance under actual reduced gravity conditions, and to produce preliminary data for the test parameters. The test results were used to demonstrate the applicability of the normal gravity models for prediction of the two-phase friction <span class="hlt">pressure</span> <span class="hlt">drop</span>. It was shown that the two-phase friction multipliers for vertical upflow and reduced gravity conditions can be successfully predicted by the appropriate normal gravity models. Limited critical heat flux data showed that the measured CHF under reduced gravities are of the same order of magnitude as the test results with vertical upflow configuration. A simplified correlation was only successful in predicting the measured CHF for low flow rates. Instability tests with vertical upflow showed that flow becomes unstable and critical heat flux occurs at smaller powers when a parallel flow path exists. However, downflow tests and a single reduced gravity instability experiment indicated that the system actually became more stable with a</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17315914','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17315914"><span>Interfacial behavior of N-nitrosodiethylamine/bovine serum albumin complexes at the <span class="hlt">air</span>-water and the chloroform-water interfaces by axisymmetric <span class="hlt">drop</span> tensiometry.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Juárez, J; Galaz, J G; Machi, L; Burboa, M; Gutiérrez-Millán, L E; Goycoolea, F M; Valdez, M A</p> <p>2007-03-15</p> <p>Interfacial properties of N-nitrosodiethylamine/bovine serum albumin (NDA/BSA) complexes were investigated at the <span class="hlt">air</span>-water interface. The interfacial behavior at the chloroform-water interface of the interaction product of phospholipid 1,2-dipalmitoyl-sn-glycero-3-phosphocholine (DPPC), dissolved in the chloroform phase, and NDA/BSA complex, in the aqueous phase, were also analyzed by using a <span class="hlt">drop</span> tensiometer. The secondary structure changes of BSA with different NDA concentrations were monitored by circular dichroism spectroscopy at different pH and the NDA/BSA interaction was probed by fluorescence spectroscopy. Different NDA/BSA mixtures were prepared from 0, 7.5 x 10(-5), 2.2 x 10(-4), 3.7 x 10(-4), 5 x 10(-4), 1.6 x 10(-3), and 3.1 x 10(-3) M NDA solutions in order to afford 0, 300/1, 900/1, 1 500/1, 2 000/1, 6 000/1, and 12 500/1 NDA/BSA molar ratios, respectively, in the aqueous solutions. Increments of BSA alpha-helix contents were obtained up to the 2 000/1 NDA/BSA molar ratio, but at ratios beyond this value, the alpha-helix content practically disappeared. These BSA structure changes produced an increment of the surface <span class="hlt">pressure</span> at the <span class="hlt">air</span>-water interface, as the alpha-helix content increased with the concentration of NDA. On the contrary, when alpha-helix content decreased, the surface <span class="hlt">pressure</span> also appeared lower than the one obtained with pure BSA solutions. The interaction of DPPC with NDA/BSA molecules at the chloroform-water interface produced also a small, but measurable, <span class="hlt">pressure</span> increment with the addition of NDA molecules. Dynamic light scattering measurements of the molecular sizes of NDA/BSA complex at pH 4.6, 7.1, and 8.4 indicated that the size of extended BSA molecules at pH 4.6 increased in a greater proportion with the increment in NDA concentration than at the other studied pH values. Diffusion coefficients calculated from dynamic surface tension values, using a short-term solution of the general adsorption model of Ward and Tordai</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24047569','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24047569"><span>Traffic-related <span class="hlt">air</span> pollution and noise and children's blood <span class="hlt">pressure</span>: results from the PIAMA birth cohort study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bilenko, Natalya; van Rossem, Lenie; Brunekreef, Bert; Beelen, Rob; Eeftens, Marloes; Hoek, Gerard; Houthuijs, Danny; de Jongste, Johan C; van Kempen, Elise; Koppelman, Gerard H; Meliefste, Kees; Oldenwening, Marieke; Smit, Henriette A; Wijga, Alet H; Gehring, Ulrike</p> <p>2015-01-01</p> <p>Elevation of a child's blood <span class="hlt">pressure</span> may cause possible health risks in later life. There is evidence for adverse effects of exposure to <span class="hlt">air</span> pollution and noise on blood <span class="hlt">pressure</span> in adults. Little is known about these associations in children. We investigated the associations of <span class="hlt">air</span> pollution and noise exposure with blood <span class="hlt">pressure</span> in 12-year-olds. Blood <span class="hlt">pressure</span> was measured at age 12 years in 1432 participants of the PIAMA birth cohort study. Annual average exposure to traffic-related <span class="hlt">air</span> pollution [NO2, mass concentrations of particulate matter with diameters of less than 2.5 µm (PM2.5) and less than 10 µm (PM10), and PM2.5 absorbance] at the participants' home and school addresses at the time of blood <span class="hlt">pressure</span> measurements was estimated by land-use regression models. <span class="hlt">Air</span> pollution exposure on the days preceding blood <span class="hlt">pressure</span> measurements was estimated from routine <span class="hlt">air</span> monitoring data. Long-term noise exposure was assessed by linking addresses to modelled equivalent road traffic noise levels. Associations of exposures with blood <span class="hlt">pressure</span> were analysed by linear regression. Effects are presented for an interquartile range increase in exposure. Long-term exposure to NO2 and PM2.5 absorbance were associated with increased diastolic blood <span class="hlt">pressure</span>, in children who lived at the same address since birth [adjusted mean difference (95% confidence interval) [mmHg] 0.83 (0.06 to 1.61) and 0.75 (-0.08 to 1.58), respectively], but not with systolic blood <span class="hlt">pressure</span>. We found no association of blood <span class="hlt">pressure</span> with short-term <span class="hlt">air</span> pollution or noise exposure. Long-term exposure to traffic-related <span class="hlt">air</span> pollution may increase diastolic blood <span class="hlt">pressure</span> in children. © The European Society of Cardiology 2013 Reprints and permissions: sagepub.co.uk/journalsPermissions.nav.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29524199','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29524199"><span>Self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q® intubating laryngeal airway versus the LMA® Classic™: a randomized clinical trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ha, Sang Hee; Kim, Min-Soo; Suh, Jiwoo; Lee, Jong Seok</p> <p>2018-05-01</p> <p>The self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q® (<span class="hlt">air</span>-Q SP) intubating laryngeal airway is a relatively new supraglottic airway (SGA) device. The intracuff <span class="hlt">pressure</span> of <span class="hlt">air</span>-Q dynamically equilibrates with the airway <span class="hlt">pressure</span> and adjusts to the patient's pharyngeal and periglottic anatomy, potentially providing improved airway fit and seal. The aim of this prospective randomized study was to compare the clinical performance of <span class="hlt">air</span>-Q to the LMA® Classic™ SGA. Adult patients requiring general anesthesia for elective surgery were prospectively enrolled and randomly assigned to either <span class="hlt">air</span>-Q SP or the LMA Classic SGA. Oropharyngeal leak <span class="hlt">pressure</span> (primary endpoint), success rate, insertion features (insertion time, ease of insertion, requirement for device manipulation), sealing function, gastric insufflation, bronchoscopic view, and oropharyngeal complications at device insertion and following its removal (sore throat, dysphagia, dysphonia) were compared. The mean (standard deviation [SD]) oropharyngeal leak <span class="hlt">pressure</span> just after insertion was similar in the <span class="hlt">air</span>-Q SP and LMA [16.8 (4.9) vs 18.6 (5.5) cm H 2 O, respectively; mean difference, 1.8 cm H 2 O; 95% CI, -0.5 to 4.2; P = 0.13] and did not differ at ten minutes following device insertion. Median [interquartile range (IQR)] peak inspiratory <span class="hlt">pressure</span> just after insertion was lower in the <span class="hlt">air</span>-Q SP (11.0 [10.0-13.0] vs 13.0 [11.0-14.0] cmH 2 O, median difference, 1.0 cm H 2 O; 95% CI, 0.0 to 2.0; P = 0.03) but no difference was observed at ten minutes. The median [IQR] insertion time was faster with the <span class="hlt">air</span>-Q SP (15.9 [13.6-20.3] sec vs 24 [21.2-27.1] sec; median difference, 8.1 sec; 95% CI, 5.6 to 9.9; P < 0.001) and improved bronchoscopic viewing grade were seen with the <span class="hlt">air</span>-Q SP immediately after insertion (P < 0.001). No differences between the groups were observed with respect to the rate of successful insertion at first attempt, overall insertion success rate, ease of insertion, and complications. The <span class="hlt">air</span>-Q SP had similar leak</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title29-vol7/pdf/CFR-2010-title29-vol7-sec1915-172.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title29-vol7/pdf/CFR-2010-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-07-01</p> <p>..., 1963. They shall be subjected to a hydrostatic <span class="hlt">pressure</span> test of one and one-half times the working... quarterly by a competent person. They shall be subjected yearly to a hydrostatic <span class="hlt">pressure</span> test of one and... 29 Labor 7 2010-07-01 2010-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels...</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_17 --> <div id="page_18" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="341"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26121822','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26121822"><span>[Nitrous Oxide Exposure-mediated Increases in Cuff <span class="hlt">Pressure</span>: A Comparison of Disposable Type and Re-use Type <span class="hlt">air</span>-Q Devices].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Miyazaki, Yu; Komasawa, Nobuyasu; Fujiawara, Shunsuke; Majima, Nozomi; Tatsumi, Shinichi; Minami, Toshiaki</p> <p>2015-02-01</p> <p>BaCKGROUND: The present study aimed to compare nitrous oxide-mediated increases in cuff <span class="hlt">pressure</span> between the disposable type <span class="hlt">air</span>-Q (<span class="hlt">air</span>-Q-DT) and re-use type <span class="hlt">air</span>-Q (<span class="hlt">air</span>-Q-RU) in a simulated adult airway model. Automated cuff <span class="hlt">pressure</span> was adjusted to 10, 20, and 30 cmH2O. The <span class="hlt">air</span>-Q-DT and <span class="hlt">air</span>-Q-RU were exposed to 80% nitrous oxide and cuff <span class="hlt">pressure</span> was measured 15 and 30 minutes later. Cuff <span class="hlt">pressure</span> of the <span class="hlt">air</span>-Q-DT was significantly lower than that of the <span class="hlt">air</span>-Q-RU after 15 and 30 minutes, regardless of the initial <span class="hlt">pressure</span>. The polyvinyl chloride-based <span class="hlt">air</span>-Q-DT may be more effective than the silicon-based <span class="hlt">air</span>-Q-RU in preventing hyperinflation of the tracheal tube cuff in response to nitrous oxide exposure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28906592','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28906592"><span>Influence of bronchial diameter change on the airflow dynamics based on a <span class="hlt">pressure</span>-controlled ventilation system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ren, Shuai; Cai, Maolin; Shi, Yan; Xu, Weiqing; Zhang, Xiaohua Douglas</p> <p>2018-03-01</p> <p>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 <span class="hlt">pressure</span>-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 <span class="hlt">air</span> <span class="hlt">pressure</span> (maximum <span class="hlt">air</span> <span class="hlt">pressure</span> in lungs) decreases by nearly 16%, the maximum flow decreases by nearly 30%, and the total airway <span class="hlt">pressure</span> loss (sum of each generation <span class="hlt">pressure</span> <span class="hlt">drop</span>) is more than 5 times the original value. Moreover, in airway generations 8 to 16, with increasing diameter, the maximum <span class="hlt">air</span> <span class="hlt">pressure</span>, maximum flow, and total airway <span class="hlt">pressure</span> loss remain almost constant. When the diameter is reduced to half of the original value, the maximum <span class="hlt">air</span> <span class="hlt">pressure</span> decreases by 3%, the maximum flow decreases by nearly 5%, and the total airway <span class="hlt">pressure</span> loss increases by 200%. The study creates a foundation for improvement in respiratory disease diagnosis and treatment. Copyright © 2017 John Wiley & Sons, Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDF27002F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDF27002F"><span>Static structure of a pointed charged <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fernandez de La Mora, Juan</p> <p>2017-11-01</p> <p>The static equilibrium structure of an equipotential <span class="hlt">drop</span> with two symmetric Taylor cones is computed by assigning a charge distribution along the z axis q (z) = ∑Bn (L2 -z2)n + 1 / 2 . Taylor's local equilibrium at the poles z = L , - L fixes two of the Bn coefficients as a function of the other, determined by minimizing stress imbalance. Just two optimally chosen terms in the Bn expansion yield imperceptible errors. Prior work has argued that an exploding <span class="hlt">drop</span> initially carrying Rayleigh's charge qR is quasi static. Paradoxically, quasi-static predictions on the size of the progeny <span class="hlt">drops</span> emitted during a Coulombic explosion disagree with observations. The static <span class="hlt">drop</span> structure found here also models poorly a Coulomb explosion having an equatorial over polar length ratio (0.42) and the a <span class="hlt">drop</span> charge exceeding those observed (0.28-0.36 and qR / 2). Our explanation for this paradox is that, while the duration tc of a Coulomb explosion is much larger than the charge relaxation time, the dynamic time scale for <span class="hlt">drop</span> elongation is typically far longer than tc. Therefore, the <span class="hlt">pressure</span> distribution within the exploding <span class="hlt">drop</span> is not uniform. A similar analysis for a <span class="hlt">drop</span> in an external field fits well the experimental shape.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930094692','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930094692"><span>Development of <span class="hlt">Air</span>-cooled Engines with Blower Cooling</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lohner, Kurt</p> <p>1933-01-01</p> <p>With the aid of a heating device, the heat transfer to cylinders with conical fins of various forms is determined both for shrouded and exposed cylinders. Simultaneously the <span class="hlt">pressure</span> <span class="hlt">drop</span> for overcoming the resistance to the motion of <span class="hlt">air</span> between the fins of the enclosed cylinder is measured. Thus the relations between the heat transfer and the energy required for cooling are discovered. The investigations show that the heat transfer in a conducted <span class="hlt">air</span> flow is much greater than in a free current and that further improvement, as compared with free exposure, is possible through narrower spaces between the fins.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014ApPhL.104o4107W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014ApPhL.104o4107W"><span>Modeling of <span class="hlt">drop</span> breakup in the bag breakup regime</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, C.; Chang, S.; Wu, H.; Xu, J.</p> <p>2014-04-01</p> <p>Several analytic models for predicting the <span class="hlt">drop</span> deformation and breakup have been developed over the last three decades, but modeling <span class="hlt">drop</span> breakup in the bag-type regime is less reported. In this Letter, a breakup model has been proposed to predict the <span class="hlt">drop</span> deformation length and breakup time in the bag-type breakup regime in a more accurate manner. In the present model, the <span class="hlt">drop</span> deformation which is approximately as the displacement of the centre of mass (c. m.) along the axis located at the centre of the <span class="hlt">drop</span>, and the movement of c. m. is obtained by solving the <span class="hlt">pressure</span> balance equation. The effects of the <span class="hlt">drop</span> deformation on the <span class="hlt">drop</span> external aerodynamic force are considered in this model. <span class="hlt">Drop</span> breakup occurs when the deformation length reaches the maximum value and the maximum deformation length is a function of Weber number. The performance and applicability of the proposed breakup model are tested against the published experimental data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014HMT....50..341A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014HMT....50..341A"><span>Coalescence of viscous <span class="hlt">drops</span> translating through a capillary tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>AlMatroushi, Eisa; Borhan, Ali</p> <p>2014-03-01</p> <p>An experimental study of the interaction and coalescence of viscous <span class="hlt">drops</span> moving through a cylindrical capillary tube under low Reynolds number conditions is presented. The combined <span class="hlt">pressure</span>- and buoyancy-driven motion of <span class="hlt">drops</span> in a Newtonian continuous phase is examined. The interaction between two <span class="hlt">drops</span> is quantified using image analysis, and measurements of the coalescence time are reported for various <span class="hlt">drop</span> size ratios, Bond numbers, and viscosity ratios. The time scale for coalescence in the non-axisymmetric configuration is found to be substantially larger than that for coalescence in the axisymmetric configuration. Measurements of the radius of the liquid film formed between the two <span class="hlt">drops</span> at the instant of apparent contact are used in conjunction with a planar film drainage model to predict the dependence of the coalescence time on <span class="hlt">drop</span> size ratio for coalescence of low viscosity-ratio <span class="hlt">drops</span> in the axisymmetric configuration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA455690','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA455690"><span>Basic Studies on High <span class="hlt">Pressure</span> <span class="hlt">Air</span> Plasmas</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2006-08-30</p> <p>which must be added a 1.5 month salary to A. Bugayev for assistance in laser and optic techniques. 2 Part II Technical report Plasma-induced phase shift...two-wavelength heterodyne interferometry applied to atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> plasma 11.1 .A. Plasma-induced phase shift - Electron density...a driver, since the error on the frequency leads to an error on the phase shift. (c) Optical elements Mirrors Protected mirrors must be used to stand</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016SPIE.9701E..0SC','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016SPIE.9701E..0SC"><span>Advancing a smart <span class="hlt">air</span> cushion system for preventing <span class="hlt">pressure</span> ulcers using projection Moiré for large deformation measurements</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cheng, Sheng-Lin; Tsai, Tsung-Heng; Lee, Carina Jean-Tien; Hsu, Yu-Hsiang; Lee, Chih-Kung</p> <p>2016-03-01</p> <p>A <span class="hlt">pressure</span> ulcer is one of the most important concerns for wheelchair bound patients with spinal cord injuries. A <span class="hlt">pressure</span> ulcer is a localized injury near the buttocks that bear ischial tuberosity oppression over a long period of time. Due to elevated compression to blood vessels, the surrounding tissues suffer from a lack of oxygen and nutrition. The ulcers eventually lead to skin damage followed by tissue necrosis. The current medical strategy is to minimize the occurrence of <span class="hlt">pressure</span> ulcers by regularly helping patients change their posture. However, these methods do not always work effectively or well. As a solution to fundamentally prevent <span class="hlt">pressure</span> ulcers, a smart <span class="hlt">air</span> cushion system was developed to detect and control <span class="hlt">pressure</span> actively. The <span class="hlt">air</span> cushion works by automatically adjusting a patient's sitting posture to effectively relieve the buttock <span class="hlt">pressure</span>. To analyze the correlation between the dynamic <span class="hlt">pressure</span> profiles of an <span class="hlt">air</span> cell with a patient's weight, a projection Moiré system was adopted to measure the deformation of an <span class="hlt">air</span> cell and its associated stress distribution. Combining a full-field deformation imaging with <span class="hlt">air</span> <span class="hlt">pressure</span> measured within an <span class="hlt">air</span> cell, the patient's weight and the stress distribution can be simultaneously obtained. By integrating a full-field optical metrology with a time varying <span class="hlt">pressure</span> sensor output coupled with different active <span class="hlt">air</span> control algorithms for various designs, we can tailor the ratio of the <span class="hlt">air</span> cells. Our preliminary data suggests that this newly developed smart <span class="hlt">air</span> cushion has the potential to selectively reduce localized compression on the tissues at the buttocks. Furthermore, it can take a patient's weight which is an additional benefit so that medical personnel can reference it to prescribe the correct drug dosages.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title42-vol1/pdf/CFR-2010-title42-vol1-sec84-149.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title42-vol1/pdf/CFR-2010-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title42-vol1/pdf/CFR-2011-title42-vol1-sec84-149.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title42-vol1/pdf/CFR-2011-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-149.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-149.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-149.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-149.pdf"><span>42 CFR 84.149 - Type C supplied-<span class="hlt">air</span> respirator, demand and <span class="hlt">pressure</span> demand class; minimum requirements.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... per square inch) with from 6 to 76 m. (15 to 250 feet) of <span class="hlt">air</span>-supply hose. (c) The specified <span class="hlt">air</span>... pounds per square inch gage). (d)(1) Where the <span class="hlt">pressure</span> in the <span class="hlt">air</span>-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a <span class="hlt">pressure</span>-release mechanism that...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27300985','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27300985"><span>Electrohydrodynamics of a viscous <span class="hlt">drop</span> with inertia.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nganguia, H; Young, Y-N; Layton, A T; Lai, M-C; Hu, W-F</p> <p>2016-05-01</p> <p>Most of the existing numerical and theoretical investigations on the electrohydrodynamics of a viscous <span class="hlt">drop</span> have focused on the creeping Stokes flow regime, where nonlinear inertia effects are neglected. In this work we study the inertia effects on the electrodeformation of a viscous <span class="hlt">drop</span> under a DC electric field using a novel second-order immersed interface method. The inertia effects are quantified by the Ohnesorge number Oh, and the electric field is characterized by an electric capillary number Ca_{E}. Below the critical Ca_{E}, small to moderate electric field strength gives rise to steady equilibrium <span class="hlt">drop</span> shapes. We found that, at a fixed Ca_{E}, inertia effects induce larger deformation for an oblate <span class="hlt">drop</span> than a prolate <span class="hlt">drop</span>, consistent with previous results in the literature. Moreover, our simulations results indicate that inertia effects on the equilibrium <span class="hlt">drop</span> deformation are dictated by the direction of normal electric stress on the <span class="hlt">drop</span> interface: Larger <span class="hlt">drop</span> deformation is found when the normal electric stress points outward, and smaller <span class="hlt">drop</span> deformation is found otherwise. To our knowledge, such inertia effects on the equilibrium <span class="hlt">drop</span> deformation has not been reported in the literature. Above the critical Ca_{E}, no steady equilibrium <span class="hlt">drop</span> deformation can be found, and often the <span class="hlt">drop</span> breaks up into a number of daughter droplets. In particular, our Navier-Stokes simulations show that, for the parameters we use, (1) daughter droplets are larger in the presence of inertia, (2) the <span class="hlt">drop</span> deformation evolves more rapidly compared to creeping flow, and (3) complex distribution of electric stresses for <span class="hlt">drops</span> with inertia effects. Our results suggest that normal electric <span class="hlt">pressure</span> may be a useful tool in predicting <span class="hlt">drop</span> pinch-off in oblate deformations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4384198','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4384198"><span>Prenatal <span class="hlt">Air</span> Pollution Exposure and Newborn Blood <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Rifas-Shiman, Sheryl L.; Melly, Steven J.; Kloog, Itai; Luttmann-Gibson, Heike; Zanobetti, Antonella; Coull, Brent A.; Schwartz, Joel D.; Mittleman, Murray A.; Oken, Emily; Gillman, Matthew W.; Koutrakis, Petros; Gold, Diane R.</p> <p>2015-01-01</p> <p>Background <span class="hlt">Air</span> pollution exposure has been associated with increased blood <span class="hlt">pressure</span> in adults. Objective: We examined associations of antenatal exposure to ambient <span class="hlt">air</span> pollution with newborn systolic blood <span class="hlt">pressure</span> (SBP). Methods: We studied 1,131 mother–infant pairs in a Boston, Massachusetts, area pre-birth cohort. We calculated average exposures by trimester and during the 2 to 90 days before birth for temporally resolved fine particulate matter (≤ 2.5 μm; PM2.5), black carbon (BC), nitrogen oxides, nitrogen dioxide, ozone (O3), and carbon monoxide measured at stationary monitoring sites, and for spatiotemporally resolved estimates of PM2.5 and BC at the residence level. We measured SBP at a mean age of 30 ± 18 hr with an automated device. We used mixed-effects models to examine associations between <span class="hlt">air</span> pollutant exposures and SBP, taking into account measurement circumstances; child’s birth weight; mother’s age, race/ethnicity, socioeconomic position, and third-trimester BP; and time trend. Estimates represent differences in SBP associated with an interquartile range (IQR) increase in each pollutant. Results: Higher mean PM2.5 and BC exposures during the third trimester were associated with higher SBP (e.g., 1.0 mmHg; 95% CI: 0.1, 1.8 for a 0.32-μg/m3 increase in mean 90-day residential BC). In contrast, O3 was negatively associated with SBP (e.g., –2.3 mmHg; 95% CI: –4.4, –0.2 for a 13.5-ppb increase during the 90 days before birth). Conclusions: Exposures to PM2.5 and BC in late pregnancy were positively associated with newborn SBP, whereas O3 was negatively associated with SBP. Longitudinal follow-up will enable us to assess the implications of these findings for health during later childhood and adulthood. Citation: van Rossem L, Rifas-Shiman SL, Melly SJ, Kloog I, Luttmann-Gibson H, Zanobetti A, Coull BA, Schwartz JD, Mittleman MA, Oken E, Gillman MW, Koutrakis P, Gold DR. 2015. Prenatal <span class="hlt">air</span> pollution exposure and newborn blood <span class="hlt">pressure</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1916285M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1916285M"><span>Influence of wind-induced <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations on topsoil gas concentrations within a Scots pine forest</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mohr, Manuel; Laemmel, Thomas; Maier, Martin; Schindler, Dirk</p> <p>2017-04-01</p> <p>Commonly it is assumed that soil gas transport is dominated by molecular diffusion. Few recent studies indicate that the atmosphere above the soil triggers non-diffusive gas transport processes in the soil, which can enhance soil gas transport and therefore soil gas efflux significantly. During high wind speed conditions, the so called <span class="hlt">pressure</span> pumping effect has been observed: the enhancement of soil gas transport through dynamic changes in the <span class="hlt">air</span> <span class="hlt">pressure</span> field above the soil. However, the amplitudes and frequencies of the <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations responsible for <span class="hlt">pressure</span> pumping are still uncertain. Moreover, an in situ observation of the <span class="hlt">pressure</span> pumping effect is still missing. To investigate the <span class="hlt">pressure</span> pumping effect, airflow measurements above and below the canopy of a Scots pine forest and high-precision relative <span class="hlt">air</span> <span class="hlt">pressure</span> measurements were conducted in the below-canopy space and in the soil over a measurement period of 16 weeks. To monitor the soil gas transport, a newly developed gas measurement system was used. The gas measurement system continuously injects helium as a tracer gas into the soil until a diffusive steady state is reached. With the steady state concentration profile of the tracer gas, it is possible to inversely model the gas diffusion coefficient profile of the soil. If the gas diffusion coefficient profile differed from steady state, we deduced that the soil gas transport is not only diffusive, but also influenced by non-diffusive processes. Results show that the occurrence of small <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations is strongly dependent on the mean above-canopy wind speed. The wind-induced <span class="hlt">air</span> <span class="hlt">pressure</span> fluctuations have mean amplitudes up to 10 Pa and lie in the frequency range 0.01-0.1 Hz. To describe the pumping motion of the <span class="hlt">air</span> <span class="hlt">pressure</span> field, the <span class="hlt">pressure</span> pumping coefficient (PPC) was defined as the mean change in <span class="hlt">pressure</span> per second. The PPC shows a clear quadratic dependence on mean above-canopy wind speed. Empirical modelling of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA281061','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA281061"><span>Evaluation of Bauer K-20 Diesel Drive High <span class="hlt">Pressure</span> Breathing <span class="hlt">Air</span> Compressor</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1993-12-01</p> <p>was to: A. Determine if the compressor and Purification System provides compressed <span class="hlt">air</span> at the required <span class="hlt">pressures</span>, flow rates, quality and cleanliness... compressed <span class="hlt">air</span> return from the <span class="hlt">air</span> storage flasks to the compressor during unit shut down. All four stages of the compressor are protected by safety...1993. 6. Naval Ships Technical Manual, S9086-SY-STM-0O0, Chapeter 551 1st Rev. I November 1987. Compressed <span class="hlt">Air</span> Plants and Systems, para 551-4.2.21. 7</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21742627','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21742627"><span>Comparison of <span class="hlt">pressure</span> <span class="hlt">drop</span> and filtration efficiency of particulate respirators using welding fumes and sodium chloride.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cho, Hyun-Woo; Yoon, Chung-Sik; Lee, Jin-Ho; Lee, Seung-Joo; Viner, Andrew; Johnson, Erik W</p> <p>2011-07-01</p> <p>Respirators are used to help reduce exposure to a variety of contaminants in workplaces. Test aerosols used for certification of particulate respirators (PRs) include sodium chloride (NaCl), dioctyl phthalate, and paraffin oil. These aerosols are generally assumed to be worst case surrogates for aerosols found in the workplace. No data have been published to date on the performance of PRs with welding fumes, a hazardous aerosol that exists in real workplace settings. The aim of this study was to compare the performance of respirators and filters against a NaCl aerosol and a welding fume aerosol and determine whether or not a correlation between the two could be made. Fifteen commercial PRs and filters (seven filtering facepiece, two replaceable single-type filters, and six replaceable dual-type filters) were chosen for investigation. Four of the filtering facepiece respirators, one of the single-type filters, and all of the dual-type filters contained carbon to help reduce exposure to ozone and other vapors generated during the welding process. For the NaCl test, a modified National Institute for Occupational Safety and Health protocol was adopted for use with the TSI Model 8130 automated filter tester. For the welding fume test, welding fumes from mild steel flux-cored arcs were generated and measured with a SIBATA filter tester (AP-634A, Japan) and a manometer in the upstream and downstream sections of the test chamber. Size distributions of the two aerosols were measured using a scanning mobility particle sizer. Penetration and <span class="hlt">pressure</span> <span class="hlt">drop</span> were measured over a period of aerosol loading onto the respirator or filter. Photos and scanning electron microscope images of clean and exposed respirators were taken. The count median diameter (CMD) and mass median diameter (MMD) for the NaCl aerosol were smaller than the welding fumes (CMD: 74 versus 216 nm; MMD: 198 versus 528 nm, respectively). Initial penetration and peak penetration were higher with the NaCl aerosol</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29504266','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29504266"><span>Prevention of <span class="hlt">pressure</span> ulcers with a static <span class="hlt">air</span> support surface: A systematic review.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Serraes, Brecht; van Leen, Martin; Schols, Jos; Van Hecke, Ann; Verhaeghe, Sofie; Beeckman, Dimitri</p> <p>2018-06-01</p> <p>The aims of this study were to identify, assess, and summarise available evidence about the effectiveness of static <span class="hlt">air</span> mattress overlays to prevent <span class="hlt">pressure</span> ulcers. The primary outcome was the incidence of <span class="hlt">pressure</span> ulcers. Secondary outcomes included costs and patient comfort. This study was a systematic review. Six electronic databases were consulted: Cochrane Library, EMBASE, PubMed (Medline), CINAHL (EBSCOhost interface), Science direct, and Web of Science. In addition, a hand search through reviews, conference proceedings, and the reference lists of the included studies was performed to identify additional studies. Potential studies were reviewed and assessed by 2 independent authors based on the title and abstract. Decisions regarding inclusion or exclusion of the studies were based on a consensus between the authors. Studies were included if the following criteria were met: reporting an original study; the outcome was the incidence of <span class="hlt">pressure</span> ulcer categories I to IV when using a static <span class="hlt">air</span> mattress overlay and/or in comparison with other <span class="hlt">pressure</span>-redistribution device(s); and studies published in English, French, and Dutch. No limitation was set on study setting, design, and date of publication. The methodological quality assessment was evaluated using the Critical Appraisal Skills Program Tool. Results were reported in a descriptive way to reflect the exploratory nature of the review. The searches included 13 studies: randomised controlled trials (n = 11) and cohort studies (n = 2). The mean <span class="hlt">pressure</span> ulcer incidence figures found in the different settings were, respectively, 7.8% <span class="hlt">pressure</span> ulcers of categories II to IV in nursing homes, 9.06% <span class="hlt">pressure</span> ulcers of categories I to IV in intensive care settings, and 12% <span class="hlt">pressure</span> ulcers of categories I to IV in orthopaedic wards. Seven comparative studies reported a lower incidence in the groups of patients on a static <span class="hlt">air</span> mattress overlay. Three studies reported a statistical (P < .1) lower incidence compared</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010004374','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010004374"><span>Thermocapillary Migration and Interactions of Bubbles and <span class="hlt">Drops</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Subramaniam, R. Shankar; Balasubramaniam, R.; Wozniak, G.; Hadland, P. H.</p> <p>1999-01-01</p> <p>Experiments were performed aboard the LMS mission of the Space Shuttle in summer 1996 in the BDPU on isolated <span class="hlt">air</span> bubbles and Fluorinert FC-75 <span class="hlt">drops</span> as well as on interacting bubbles/<span class="hlt">drops</span> migrating in a temperature gradient in a Dow-Corning DC-200 series silicone oil of nominal viscosity 10 centistokes. The data, recorded in the form of videotape images as well as cine images in selected runs, have been analyzed. The behavior of the isolated objects is consistent with earlier observations made aboard the IML-2 mission while the range of Reynolds and Marangoni numbers has been extended substantially over that in the IML-2 experiments. Large bubbles were found to be slightly deformed to an oblate shape while no deformation could be detected in the case of similarly large <span class="hlt">drops</span>. Results on interacting <span class="hlt">drops</span> and bubbles display interesting and unanticipated features. In some experiments, <span class="hlt">drops</span> are found to follow a three-dimensional trajectory. In others, trailing <span class="hlt">drops</span> and bubbles are found to move off the axis of the cell when migrating behind a leading <span class="hlt">drop</span> or bubble which moves along the axis. In this type of run, if the trailing <span class="hlt">drop</span> is sufficiently large, it is found to pass the leading <span class="hlt">drop</span>. Finally, behavior similar to that observed in IML-2, namely that a small leading <span class="hlt">drop</span> slows the movement of a larger trailing <span class="hlt">drop</span> moving along the cell axis, was observed as well.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_18 --> <div id="page_19" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="361"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26860399','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26860399"><span>Tracheostomy Tube Type and Inner Cannula Selection Impact <span class="hlt">Pressure</span> and Resistance to <span class="hlt">Air</span> Flow.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pryor, Lee N; Baldwin, Claire E; Ward, Elizabeth C; Cornwell, Petrea L; O'Connor, Stephanie N; Chapman, Marianne J; Bersten, Andrew D</p> <p>2016-05-01</p> <p>Advancements in tracheostomy tube design now provide clinicians with a range of options to facilitate communication for individuals receiving ventilator assistance through a cuffed tube. Little is known about the impact of these modern design features on resistance to <span class="hlt">air</span> flow. We undertook a bench model test to measure <span class="hlt">pressure</span>-flow characteristics and resistance of a range of tubes of similar outer diameter, including those enabling subglottic suction and speech. A constant inspiratory ± expiratory <span class="hlt">air</span> flow was generated at increasing flows up to 150 L/min through each tube (with or without optional, mandatory, or interchangeable inner cannula). Driving <span class="hlt">pressures</span> were measured, and resistance was calculated (cm H2O/L/s). <span class="hlt">Pressures</span> changed with increasing flow (P < .001) and tube type (P < .001), with differing patterns of <span class="hlt">pressure</span> change according to the type of tube (P < .001) and direction of <span class="hlt">air</span> flow. The single-lumen reference tube encountered the lowest inspiratory and expiratory <span class="hlt">pressures</span> compared with all double-lumen tubes (P < .001); placement of an optional inner cannula increased bidirectional tube resistance by a factor of 3. For a tube with interchangeable inner cannulas, the type of cannula altered <span class="hlt">pressure</span> and resistance differently (P < .001); the speech cannula in particular amplified <span class="hlt">pressure</span>-flow changes and increased tube resistance by more than a factor of 4. Tracheostomy tube type and inner cannula selection imposed differing <span class="hlt">pressures</span> and resistance to <span class="hlt">air</span> flow during inspiration and expiration. These differences may be important when selecting airway equipment or when setting parameters for monitoring, particularly for patients receiving supported ventilation or during the weaning process. Copyright © 2016 by Daedalus Enterprises.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22121605','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22121605"><span>Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristics of nanofluids in a plate heat exchanger.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kwon, Y H; Kim, D; Li, C G; Lee, J K; Hong, D S; Lee, J G; Lee, S H; Cho, Y H; Kim, S H</p> <p>2011-07-01</p> <p>In this paper, the heat transfer characteristics and <span class="hlt">pressure</span> <span class="hlt">drop</span> of the ZnO and Al2O3 nanofluids in a plate heat exchanger were studied. The experimental conditions were 100-500 Reynolds number and the respective volumetric flow rates. The working temperature of the heat exchanger was within 20-40 degrees C. The measured thermophysical properties, such as thermal conductivity and kinematic viscosity, were applied to the calculation of the convective heat transfer coefficient of the plate heat exchanger employing the ZnO and Al2O3 nanofluids made through a two-step method. According to the Reynolds number, the overall heat transfer coefficient for 6 vol% Al2O3 increased to 30% because at the given viscosity and density of the nanofluids, they did not have the same flow rates. At a given volumetric flow rate, however, the performance did not improve. After the nanofluids were placed in the plate heat exchanger, the experimental results pertaining to nanofluid efficiency seemed inauspicious.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/az0246.photos.009708p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/az0246.photos.009708p/"><span>27. EXTENSION OF SURGE CHAMBER AND <span class="hlt">AIR</span> PIPES TO <span class="hlt">PRESSURE</span> ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>27. EXTENSION OF SURGE CHAMBER AND <span class="hlt">AIR</span> PIPES TO <span class="hlt">PRESSURE</span> LINE, HIGHLINE PUMPING PLANT. December 11, 1920 - Highline Canal & Pumping Station, South side of Salt River between Tempe, Phoenix & Mesa, Tempe, Maricopa County, AZ</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EPJWC..9202015D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EPJWC..9202015D"><span><span class="hlt">Pressure</span> Regulators as Valves for Saving Compressed <span class="hlt">Air</span> and their Influence on System Dynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dvořák, Lukáš; Fojtášek, Kamil</p> <p>2015-05-01</p> <p><span class="hlt">Pressure</span> regulators in the field of pneumatic mechanisms can be used as valves for saving compressed <span class="hlt">air</span>. For example it can be used to reduce the <span class="hlt">pressure</span> when the piston rod is retracting unloaded and thus it is possible to save some energy. However the problem is that saving valve can significantly affect the dynamics of the pneumatic system. The lower <span class="hlt">pressure</span> in the piston rod chamber causes extension of time for retraction of the piston rod. This article compare the <span class="hlt">air</span> consumption experimentally determined and calculated, measured curves of <span class="hlt">pressure</span> in cylinder chambers and piston speed when saving valve is set up differently.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880028849&hterms=disruption&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Ddisruption','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880028849&hterms=disruption&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Ddisruption"><span>Sooting and disruption in spherically symmetrical combustion of decane droplets in <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dryer, F. L.; Williams, F. A.; Haggard, J. B., Jr.; Shaw, B. D.</p> <p>1987-01-01</p> <p>The paper presents the results of experiments on the burning of individual 1-2 mm decane droplets in <span class="hlt">air</span> at room temperature and atmospheric <span class="hlt">pressure</span>. The NASA Lewis 2.2 s <span class="hlt">drop</span> tower was used as well as a newly designed droplet-combustion apparatus that promotes nearly spherically symmetrical combustion. Unanticipated disruptions related to sooting behavior were encountered.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930081170','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930081170"><span>Some Characteristics of Fuel Sprays at Low-injection <span class="hlt">Pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rothrock, A M; Waldron, C D</p> <p>1931-01-01</p> <p>This report presents the results of tests conducted at the Langley Memorial Aeronautical Laboratory, Langley Field, Va., to determine some of the characteristics of the fuel sprays obtained from an 0.008-inch and a 0.020-inch open nozzle when injection <span class="hlt">pressures</span> from 100 to 500 pounds per square inch were used. Fuel oil and gasoline were injected into <span class="hlt">air</span> at densities of atmospheric land 0.325 pound per cubic foot. It was found that the penetration rate at these low <span class="hlt">pressures</span> was about the same as the rate obtained with higher <span class="hlt">pressures</span>. Spray cone-angles were small and individual oil <span class="hlt">drops</span> were visible in all the sprays. Gasoline and fuel oil sprays had similar characteristics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25831297','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25831297"><span>Fiber in-line Mach-Zehnder interferometer based on an inner <span class="hlt">air</span>-cavity for high-<span class="hlt">pressure</span> sensing.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Talataisong, W; Wang, D N; Chitaree, R; Liao, C R; Wang, C</p> <p>2015-04-01</p> <p>We demonstrate a fiber in-line Mach-Zehnder interferometer based on an inner <span class="hlt">air</span>-cavity with open micro-channel for high-<span class="hlt">pressure</span> sensing applications. The inner <span class="hlt">air</span>-cavity is fabricated by combining femtosecond laser micromachining and the fusion splicing technique. The micro-channel is drilled on the top of the inner <span class="hlt">air</span>-cavity to allow the high-<span class="hlt">pressure</span> gas to flow in. The fiber in-line device is miniature, robust, and stable in operation and exhibits a high <span class="hlt">pressure</span> sensitivity of ∼8,239  pm/MPa.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21288438','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21288438"><span>Effect of impeded medial longitudinal arch <span class="hlt">drop</span> on vertical ground reaction force and center of <span class="hlt">pressure</span> during static loading.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Shing-Jye; Gielo-Perczak, Krystyna</p> <p>2011-01-01</p> <p>Arch supports commonly used to alleviate foot pain can impede the normal <span class="hlt">drop</span> of medial longitudinal arch (MLA) thereby altering its function. The purpose of the study was to examine the effect of using arch supports on vertical ground reaction force (GRF) and center of <span class="hlt">pressure</span> (COP) during simulated midstance while the foot was statically loaded. Ten healthy young subjects were recruited. Two dimensional (2D) analysis of the MLA was captured for both barefoot (BF) and arch support conditions before and after loading via a custom made weight loading apparatus. The foot was loaded and positioned to simulate the midstance phase of walking. Two-dimensional reflective markers demarcated the MLA and captured with the loaded foot on a force platform. The impeded MLA <span class="hlt">drop</span> was compared between the unloaded BF, loaded BF and loaded arch support conditions. The vertical GRF, the anterior-posterior and the medial-lateral COP displacements were also measured in response to the impeded MLA by the arch supports. The arch supports impeded the MLA <span class="hlt">drop</span> (p<0.05) and shifted the COP toward the medial side (p<0.05), specifically for the rearfoot (calcaneal segment region), but no changes were determined for the vertical GRF (p>0.05). The impedance of MLA <span class="hlt">drop</span> by the arch support altered the pattern of the ML COP shift in the rearfoot region. The use of arch supports may not relieve painful foot conditions that are associated with excessive calcaneal eversion indicated by altering COP shifts in localized foot regions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29363824','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29363824"><span>Comparison of water and <span class="hlt">air</span> charged transducer catheter <span class="hlt">pressures</span> in the evaluation of cystometrogram and voiding <span class="hlt">pressure</span> studies.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>McKinney, Timothy B; Babin, Elizabeth A; Ciolfi, Veronica; McKinney, Cynthia R; Shah, Nima</p> <p>2018-04-01</p> <p><span class="hlt">Air</span>-charged (AC) and water-perfused (WP) catheters have been evaluated for differences in measuring <span class="hlt">pressures</span> for voiding dysfunction. Typically, a two-catheter system was used. We believe that simultaneous <span class="hlt">pressure</span> measurements with AC and WP in a single catheter will provide analogous <span class="hlt">pressures</span> for coughs, Valsalvas, and maximum <span class="hlt">pressures</span> in voiding <span class="hlt">pressure</span> studies (VPS). This IRB approved prospective study included 50 women over age 21. AC dual TDOC catheters were utilized. The water-filling channel served as the bladder filler and the water <span class="hlt">pressure</span> readings. Patients were evaluated with empty bladders and at volumes of 50-100 mL, 200 mL, and maximum capacity with cough and Valsalva maneuvers. Comparative analysis was performed on maximum stress peak <span class="hlt">pressures</span>. At maximum bladder capacity, VPS was done and maximum voiding <span class="hlt">pressure</span> was recorded. Comparing coughs and Valsalva maneuvers <span class="hlt">pressures</span>, there was significant increase in variability between AC and WP measurements with less than 50 mL volume (P < 0.001). Significant correlations were observed between AC and WP measurements for coughs and Valsalvas with bladder volume over 50 mL. Visual impression showed virtually identical tracings. Cough measurements had an average difference of 0.25 cmH 2 O (±8.81) and Valsalva measurements had an average difference of 3.15 cmH 2 O (±4.72). Thirty-eight women had usable maximum voiding <span class="hlt">pressure</span> measurements and had a strong correlation. Cystometrogram and maximum voiding <span class="hlt">pressure</span> measurements done with either water or <span class="hlt">air</span> charged catheters will yield similarly accurate results and are comparable. Results suggest more variability at low bladder volumes <50 mL. © 2018 Wiley Periodicals, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015ExFl...56...84D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015ExFl...56...84D"><span>Picosecond ballistic imaging of diesel injection in high-temperature and high-<span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Duran, Sean P.; Porter, Jason M.; Parker, Terence E.</p> <p>2015-04-01</p> <p>The first successful demonstration of picosecond ballistic imaging using a 15-ps-pulse-duration laser in diesel sprays at temperature and <span class="hlt">pressure</span> is reported. This technique uses an optical Kerr effect shutter constructed from a CS2 liquid cell and a 15-ps pulse at 532 nm. The optical shutter can be adjusted to produce effective imaging pulses between 7 and 16 ps. This technique is used to image the near-orifice region (first 3 mm) of diesel sprays from a high-<span class="hlt">pressure</span> single-hole fuel injector. Ballistic imaging of dodecane and methyl oleate sprays injected into ambient <span class="hlt">air</span> and diesel injection at preignition engine-like conditions are reported. Dodecane was injected into <span class="hlt">air</span> heated to 600 °C and <span class="hlt">pressurized</span> to 20 atm. The resulting images of the near-orifice region at these conditions reveal dramatic shedding of the liquid near the nozzle, an effect that has been predicted, but to our knowledge never before imaged. These shedding structures have an approximate spatial frequency of 10 mm-1 with lengths from 50 to 200 μm. Several parameters are explored including injection <span class="hlt">pressure</span>, liquid fuel temperature, <span class="hlt">air</span> temperature and <span class="hlt">pressure</span>, and fuel type. Resulting trends are summarized with accompanying images.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://rosap.ntl.bts.gov/view/dot/35042','DOTNTL'); return false;" href="https://rosap.ntl.bts.gov/view/dot/35042"><span>Post-Tensioning Duct <span class="hlt">Air</span> <span class="hlt">Pressure</span> Testing Effects on Web Cracking</span></a></p> <p><a target="_blank" href="http://ntlsearch.bts.gov/tris/index.do">DOT National Transportation Integrated Search</a></p> <p></p> <p>2015-01-01</p> <p>Nevada Department of Transportation (NDOT) post-tensioned concrete bridges have experienced web cracking near the post-tensioning ducts during the construction process. The ducts were <span class="hlt">air</span> <span class="hlt">pressure</span> tested to ensure the duct can successfully be grouted...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29606673','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29606673"><span><span class="hlt">Pressure</span> Injury Development in Patients Treated by Critical Care <span class="hlt">Air</span> Transport Teams: A Case-Control Study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dukes, Susan F; Maupin, Genny M; Thomas, Marilyn E; Mortimer, Darcy L</p> <p>2018-04-01</p> <p>The US <span class="hlt">Air</span> Force transports critically ill patients from all over the world, with transport times commonly ranging from 6 to 11 hours. Few outcome measures have been tracked for these patients. Traditional methods to prevent <span class="hlt">pressure</span> injuries in civilian hospitals are often not feasible in the military transport environment. The incidence rate and risk factors are described of en route-related <span class="hlt">pressure</span> injuries for patients overseen by the Critical Care <span class="hlt">Air</span> Transport Team. This retrospective, case-control, medical records review investigated risk factors for <span class="hlt">pressure</span> injury in patients who developed a <span class="hlt">pressure</span> injury after their transport flight compared with those with no documented <span class="hlt">pressure</span> injuries. The <span class="hlt">pressure</span> injury rate was 4.9%. Between 2008 and 2012, 141 patients in whom <span class="hlt">pressure</span> injuries developed and who had received care by the team were matched with 141 patients cared for by the team but did not have <span class="hlt">pressure</span> injury. According to regression analysis, body mass index and 2 or more Critical Care <span class="hlt">Air</span> Transport Team transports per patient were associated with <span class="hlt">pressure</span> injury development. Although the <span class="hlt">pressure</span> injury rate of 4.9% in this cohort of patients is consistent with that reported by civilian critical care units, the rate must be interpreted with caution, because civilian study data frequently represent the entire intensive care unit length of stay. Targeted interventions for patients with increased body mass index and 2 or more critical care <span class="hlt">air</span> transports per patient may help decrease the development of <span class="hlt">pressure</span> injury in these patients. ©2018 American Association of Critical-Care Nurses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/911582','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/911582"><span>Improving Vortex Generators to Enhance the Performance of <span class="hlt">Air</span>-Cooled Condensers in a Geothermal Power Plant</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Manohar S. Sohal</p> <p>2005-09-01</p> <p>This report summarizes work at the Idaho National Laboratory to develop strategies to enhance <span class="hlt">air</span>-side heat transfer in geothermal <span class="hlt">air</span>-cooled condensers such that it should not significantly increase <span class="hlt">pressure</span> <span class="hlt">drop</span> and parasitic fan pumping power. The work was sponsored by the U.S. Department of Energy, NEDO (New Energy and Industrial Technology Development Organization) of Japan, Yokohama National University, and the Indian Institute of Technology, Kanpur, India. A combined experimental and numerical investigation was performed to investigate heat transfer enhancement techniques that may be applicable to largescale <span class="hlt">air</span>-cooled condensers such as those used in geothermal power applications. A transient heat transfermore » visualization and measurement technique was employed in order to obtain detailed distributions of local heat transfer coefficients on model fin surfaces. <span class="hlt">Pressure</span> <span class="hlt">drop</span> measurements were obtained for a variety of tube and winglet configurations using a single-channel flow apparatus that included four tube rows in a staggered array. Heat transfer and <span class="hlt">pressure</span> <span class="hlt">drop</span> measurements were also acquired in a separate multiple-tube row apparatus in the Single Blow Test Facility. In addition, a numerical modeling technique was developed to predict local and average heat transfer for these low-Reynolds number flows, with and without winglets. Representative experimental and numerical results were obtained that reveal quantitative details of local finsurface heat transfer in the vicinity of a circular tube with a single delta winglet pair downstream of the cylinder. Heat transfer and <span class="hlt">pressure-drop</span> results were obtained for flow Reynolds numbers based on channel height and mean flow velocity ranging from 700 to 6500. The winglets were of triangular (delta) shape with a 1:2 or 1:3 height/length aspect ratio and a height equal to 90% of the channel height. Overall mean fin-surface heat transfer results indicate a significant level of heat transfer enhancement (in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title29-vol7/pdf/CFR-2011-title29-vol7-sec1915-172.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title29-vol7/pdf/CFR-2011-title29-vol7-sec1915-172.pdf"><span>29 CFR 1915.172 - Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-07-01</p> <p>... 29 Labor 7 2011-07-01 2011-07-01 false Portable <span class="hlt">air</span> receivers and other unfired <span class="hlt">pressure</span> vessels. 1915.172 Section 1915.172 Labor Regulations Relating to Labor (Continued) OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR (CONTINUED) OCCUPATIONAL SAFETY AND HEALTH STANDARDS FOR SHIPYARD EMPLOYMENT Portable, Unfired <span class="hlt">Pressure</span>...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880041359&hterms=Acoustic+levitation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DAcoustic%2Blevitation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880041359&hterms=Acoustic+levitation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3DAcoustic%2Blevitation"><span>Charged <span class="hlt">drop</span> dynamics experiment using an electrostatic-acoustic hybrid system</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rhim, W. K.; Chung, S. K.; Trinh, E. H.; Elleman, D. D.</p> <p>1987-01-01</p> <p>The design and the performance of an electrostatic-acoustic hybrid system and its application to a charge <span class="hlt">drop</span> rotation experiment are presented. This system can levitate a charged <span class="hlt">drop</span> electrostatically and induce <span class="hlt">drop</span> rotation or oscillation by imposing an acoustic torque or an oscillating acoustic <span class="hlt">pressure</span>. Using this system, the equilibrium shapes and stability of a rotating charged <span class="hlt">drop</span> were experimentally investigated. A 3 mm size water <span class="hlt">drop</span> was rotated as a rigid body and its gyrostatic equilibrium shapes were observed. Families of axisymmetric shapes, two-lobed shapes, and eventual fissioning have been observed. With the assumption of 'effective surface tension' in which the surface charge simply modified the surface tension of neutral liquid, the results agree exceptionally well with the Brown and Scriven's (1980) prediction for uncharged <span class="hlt">drops</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28361867','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28361867"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-03-31</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ∼3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NatCo...814950S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NatCo...814950S"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-03-01</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ~3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381006','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5381006"><span>Integrated arrays of <span class="hlt">air</span>-dielectric graphene transistors as transparent active-matrix <span class="hlt">pressure</span> sensors for wide <span class="hlt">pressure</span> ranges</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Shin, Sung-Ho; Ji, Sangyoon; Choi, Seiho; Pyo, Kyoung-Hee; Wan An, Byeong; Park, Jihun; Kim, Joohee; Kim, Ju-Young; Lee, Ki-Suk; Kwon, Soon-Yong; Heo, Jaeyeong; Park, Byong-Guk; Park, Jang-Ung</p> <p>2017-01-01</p> <p>Integrated electronic circuitries with <span class="hlt">pressure</span> sensors have been extensively researched as a key component for emerging electronics applications such as electronic skins and health-monitoring devices. Although existing <span class="hlt">pressure</span> sensors display high sensitivities, they can only be used for specific purposes due to the narrow range of detectable <span class="hlt">pressure</span> (under tens of kPa) and the difficulty of forming highly integrated arrays. However, it is essential to develop tactile <span class="hlt">pressure</span> sensors with a wide <span class="hlt">pressure</span> range in order to use them for diverse application areas including medical diagnosis, robotics or automotive electronics. Here we report an unconventional approach for fabricating fully integrated active-matrix arrays of <span class="hlt">pressure</span>-sensitive graphene transistors with <span class="hlt">air</span>-dielectric layers simply formed by folding two opposing panels. Furthermore, this realizes a wide tactile <span class="hlt">pressure</span> sensing range from 250 Pa to ∼3 MPa. Additionally, fabrication of <span class="hlt">pressure</span> sensor arrays and transparent <span class="hlt">pressure</span> sensors are demonstrated, suggesting their substantial promise as next-generation electronics. PMID:28361867</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5089803','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5089803"><span>A preliminary investigation of the <span class="hlt">air</span>-bone gap: Changes in intracochlear sound <span class="hlt">pressure</span> with <span class="hlt">air</span>- and bone-conducted stimuli after cochlear implantation</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Banakis Hartl, Renee M.; Mattingly, Jameson K.; Greene, Nathaniel T.; Jenkins, Herman A.; Cass, Stephen P.; Tollin, Daniel J.</p> <p>2016-01-01</p> <p>Hypothesis A cochlear implant electrode within the cochlea contributes to the <span class="hlt">air</span>-bone gap (ABG) component of postoperative changes in residual hearing after electrode insertion. Background Preservation of residual hearing after cochlear implantation has gained importance as simultaneous electric-acoustic stimulation allows for improved speech outcomes. Postoperative loss of residual hearing has previously been attributed to sensorineural changes; however, presence of increased postoperative <span class="hlt">air</span>-bone gap remains unexplained and could result in part from altered cochlear mechanics. Here, we sought to investigate changes to these mechanics via intracochlear <span class="hlt">pressure</span> measurements before and after electrode implantation to quantify the contribution to postoperative <span class="hlt">air</span>-bone gap. Methods Human cadaveric heads were implanted with titanium fixtures for bone conduction transducers. Velocities of stapes capitulum and cochlear promontory between the two windows were measured using single-axis laser Doppler vibrometry and fiber-optic sensors measured intracochlear <span class="hlt">pressures</span> in scala vestibuli and tympani for <span class="hlt">air</span>- and bone-conducted stimuli before and after cochlear implant electrode insertion through the round window. Results Intracochlear <span class="hlt">pressures</span> revealed only slightly reduced responses to <span class="hlt">air</span>-conducted stimuli consistent with prior literature. No significant changes were noted to bone-conducted stimuli after implantation. Velocities of the stapes capitulum and the cochlear promontory to both stimuli were stable following electrode placement. Conclusion Presence of a cochlear implant electrode causes alterations in intracochlear sound <span class="hlt">pressure</span> levels to <span class="hlt">air</span>, but not bone, conducted stimuli and helps to explain changes in residual hearing noted clinically. These results suggest the possibility of a cochlear conductive component to postoperative changes in hearing sensitivity. PMID:27579835</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008JPhCS.114a2067P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008JPhCS.114a2067P"><span>Quantitative study of sniffer leak rate and <span class="hlt">pressure</span> <span class="hlt">drop</span> leak rate of liquid nitrogen panels of SST-1 tokamak</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pathan, F. S.; Khan, Z.; Semwal, P.; Raval, D. C.; Joshi, K. S.; Thankey, P. L.; Dhanani, K. R.</p> <p>2008-05-01</p> <p>Steady State Super-conducting (SST-1) Tokamak is in commissioning stage at Institute for Plasma Research. Vacuum chamber of SST-1 Tokamak consists of 1) Vacuum vessel, an ultra high vacuum (UHV) chamber, 2) Cryostat, a high vacuum (HV) chamber. Cryostat encloses the liquid helium cooled super-conducting magnets (TF and PF), which require the thermal radiation protection against room temperature. Liquid nitrogen (LN2) cooled panels are used to provide thermal shield around super-conducting magnets. During operation, LN2 panels will be under <span class="hlt">pressurized</span> condition and its surrounding (cryostat) will be at high vacuum. Hence, LN2 panels must have very low leak rate. This paper describes an experiment to study the behaviour of the leaks in LN2 panels during sniffer test and <span class="hlt">pressure</span> <span class="hlt">drop</span> test using helium gas.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_19 --> <div id="page_20" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="381"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110023904','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110023904"><span>Monitoring Volcanoes by Use of <span class="hlt">Air-Dropped</span> Sensor Packages</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kedar, Sharon; Rivellini, Tommaso; Webb, Frank; Blaes, Brent; Bracho, Caroline; Lockhart, Andrew; McGee, Ken</p> <p>2003-01-01</p> <p>Sensor packages that would be <span class="hlt">dropped</span> from airplanes have been proposed for pre-eruption monitoring of physical conditions on the flanks of awakening volcanoes. The purpose of such monitoring is to gather data that could contribute to understanding and prediction of the evolution of volcanic systems. Each sensor package, denoted a volcano monitoring system (VMS), would include a housing with a parachute attached at its upper end and a crushable foam impact absorber at its lower end (see figure). The housing would contain survivable low-power instrumentation that would include a Global Positioning System (GPS) receiver, an inclinometer, a seismometer, a barometer, a thermometer, and CO2 and SO2 analyzers. The housing would also contain battery power, control, data-logging, and telecommunication subsystems. The proposal for the development of the VMS calls for the use of commercially available sensor, power, and telecommunication equipment, so that efforts could be focused on integrating all of the equipment into a system that could survive impact and operate thereafter for 30 days, transmitting data on the pre-eruptive state of a target volcano to a monitoring center. In a typical scenario, VMSs would be <span class="hlt">dropped</span> at strategically chosen locations on the flanks of a volcano once the volcano had been identified as posing a hazard from any of a variety of observations that could include eyewitness reports, scientific observations from positions on the ground, synthetic-aperture-radar scans from aircraft, and/or remote sensing from aboard spacecraft. Once <span class="hlt">dropped</span>, the VMSs would be operated as a network of in situ sensors that would transmit data to a local monitoring center. This network would provide observations as part of an integrated volcano-hazard assessment strategy that would involve both remote sensing and timely observations from the in situ sensors. A similar strategy that involves the use of portable sensors (but not <span class="hlt">dropping</span> of sensors from aircraft) is</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20396866','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20396866"><span>Formaldehyde removal from <span class="hlt">air</span> by a biodegradation system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Zhongjun; Hou, Haiping</p> <p>2010-07-01</p> <p>A biodegradation system was used for the treatment of formaldehyde-polluted <span class="hlt">air</span>. <span class="hlt">Air</span> <span class="hlt">pressure</span> <span class="hlt">dropped</span> 12 mm water in the trickling biofilter during the experiment of about 4 months. In the range 20-300 mg m(-3) influent formaldehyde, this biodegradation system obtained 4.0-40.0 mg h(-1) degradation capacity, with 100%-66.7% degradation efficiency. The amount of formaldehyde degraded by the trickling biofilter was more than that by the activated sludge bioreactor below 200 mg m(-3) influent gaseous formaldehyde while the amount by the trickling biofilter was less than that by the activated sludge bioreactor over 200 mg m(-3) influent gaseous formaldehyde.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-157.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title42-vol1/pdf/CFR-2012-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2012-10-01 2012-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-157.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title42-vol1/pdf/CFR-2013-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2013-10-01 2013-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-157.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title42-vol1/pdf/CFR-2014-title42-vol1-sec84-157.pdf"><span>42 CFR 84.157 - Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum...</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-10-01</p> <p>... test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. (a) The static... 42 Public Health 1 2014-10-01 2014-10-01 false Airflow resistance test; Type C supplied-<span class="hlt">air</span> respirator, <span class="hlt">pressure</span>-demand class; minimum requirements. 84.157 Section 84.157 Public Health PUBLIC HEALTH...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083715','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=2&id=EJ1083715"><span>Experimental <span class="hlt">Air</span> <span class="hlt">Pressure</span> Tank Systems for Process Control Education</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Long, Christopher E.; Holland, Charles E.; Gatzke, Edward P.</p> <p>2006-01-01</p> <p>In process control education, particularly in the field of chemical engineering, there is an inherent need for industrially relevant hands-on apparatuses that enable one to bridge the gap between the theoretical content of coursework and real-world applications. At the University of South Carolina, two experimental <span class="hlt">air-pressure</span> tank systems have…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFDG16007M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFDG16007M"><span>Coalescence of a <span class="hlt">Drop</span> inside another <span class="hlt">Drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mugundhan, Vivek; Jian, Zhen; Yang, Fan; Li, Erqiang; Thoroddsen, Sigurdur</p> <p>2016-11-01</p> <p>Coalescence dynamics of a pendent <span class="hlt">drop</span> sitting inside another <span class="hlt">drop</span>, has been studied experimentally and in numerical simulations. Using an in-house fabricated composite micro-nozzle, a smaller salt-water <span class="hlt">drop</span> is introduced inside a larger oil <span class="hlt">drop</span> which is pendent in a tank containing the same liquid as the inner <span class="hlt">drop</span>. On touching the surface of outer <span class="hlt">drop</span>, the inner <span class="hlt">drop</span> coalesces with the surrounding liquid forming a vortex ring, which grows in time to form a mushroom-like structure. The initial dynamics at the first bridge opening up is quantified using Particle Image Velocimetry (PIV), while matching the refractive index of the two liquids. The phenomenon is also numerically simulated using the open-source code Gerris. The problem is fully governed by two non-dimensional parameters: the Ohnesorge number and the diameter ratios of the two <span class="hlt">drops</span>. The validated numerical model is used to better understand the dynamics of the phenomenon. In some cases a coalescence cascade is observed with liquid draining intermittently and the inner <span class="hlt">drop</span> reducing in size.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1987srti.rept.....W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1987srti.rept.....W"><span>Soviet research on the transport of intense relativistic electron beams through high-<span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wells, Nikita</p> <p>1987-05-01</p> <p>Soviet development of intense relativistic electron beams (IREB) through background <span class="hlt">air</span> at <span class="hlt">pressures</span> from 1/100 Torr to atmospheric is analyzed as reflected by Soviet open literature of the last 15 years. Important Soviet findings include: (1) the formation of a plasma channel created by an IREB propagating through background <span class="hlt">air</span> and the effect of beam parameters upon the plasma channel parameters (and vice versa); (2) determination of the background <span class="hlt">air</span> <span class="hlt">pressure</span> for the optimum transport of IREB in two ranges, an ion focused regime at 0.06 to 0.09 Torr and a low <span class="hlt">pressure</span> window at 1 Torr; (3) observation of current enhancement, whereby the IREB-induced current in plasma is higher than the initial beam current; and (4) the effect of resistive hose instability on IREB propagation. This research is characterized by absence of high energy experimentation. A conclusion of the research is that, for optimum beam transport through <span class="hlt">air</span>, it is imperative to ensure conditions that allow full neutralization of the IREB's self-fields along the entire path of the beam's transport.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=respiratory+AND+system&pg=6&id=EJ696527','ERIC'); return false;" href="https://eric.ed.gov/?q=respiratory+AND+system&pg=6&id=EJ696527"><span><span class="hlt">Air</span> <span class="hlt">Pressure</span> Responses to Sudden Vocal Tract <span class="hlt">Pressure</span> Bleeds during Production of Stop Consonants: New Evidence of Aeromechanical Regulation.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Zajac, David J.; Weissler, Mark C.</p> <p>2004-01-01</p> <p>Two studies were conducted to evaluate short-latency vocal tract <span class="hlt">air</span> <span class="hlt">pressure</span> responses to sudden <span class="hlt">pressure</span> bleeds during production of voiceless bilabial stop consonants. It was hypothesized that the occurrence of respiratory reflexes would be indicated by distinct patterns of responses as a function of bleed magnitude. In Study 1, 19 adults…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170008003','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170008003"><span>Creating a Bimodal <span class="hlt">Drop</span>-Size Distribution in the NASA Glenn Icing Research Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>King-Steen, Laura E.; Ide, Robert F.</p> <p>2017-01-01</p> <p>The Icing Research Tunnel at NASA Glenn has demonstrated that they can create a <span class="hlt">drop</span>-size distribution that matches the FAA Part 25 Appendix O FZDZ, MVD <40 microns normalized cumulative volume within 10%. This is done by simultaneously spraying the Standard and Mod1 nozzles at the same nozzle <span class="hlt">air</span> <span class="hlt">pressure</span> and different nozzle water <span class="hlt">pressures</span>. It was also found through these tests that the distributions that are measured when the two nozzle sets are sprayed simultaneously closely matched what was found by combining the two individual distributions analytically. Additionally, distributions were compared between spraying all spraybars and also by spraying only every-other spraybar, and were found to match within 4%. The cloud liquid water content uniformity for this condition has been found to be excellent. It should be noted, however, that the liquid water content for this condition in the IRT is much higher than the requirement specified in Part 25 Appendix O.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170007899','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170007899"><span>Creating a Bimodal <span class="hlt">Drop</span>-Size Distribution in the NASA Glenn Icing Research Tunnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>King-Steen, Laura E.; Ide, Robert F.</p> <p>2017-01-01</p> <p>The Icing Research Tunnel at NASA Glenn has demonstrated that they can create a <span class="hlt">drop</span>-size distribution that matches the FAA Part 25 Appendix O FZDZ, MVD40 m normalized cumulative volume within 10. This is done by simultaneously spraying the Standard and Mod1 nozzles at the same nozzle <span class="hlt">air</span> <span class="hlt">pressure</span> and different nozzle water <span class="hlt">pressures</span>. It was also found through these tests that the distributions that are measured when the two nozzle sets are sprayed simultaneously closely matched what was found by combining the two individual distributions analytically. Additionally, distributions were compared between spraying all spraybars and also by spraying only every-other spraybar, and were found to match within 4. The cloud liquid water content uniformity for this condition has been found to be excellent: 10. It should be noted, however, that the liquid water content for this condition in the IRT is much higher than the requirement specified in Part 25 Appendix O.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1194007','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1194007"><span><span class="hlt">Drop</span> Testing Representative Multi-Canister Overpacks</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Snow, Spencer D.; Morton, Dana K.</p> <p></p> <p>The objective of the work reported herein was to determine the ability of the Multi- Canister Overpack (MCO) canister design to maintain its containment boundary after an accidental <span class="hlt">drop</span> event. Two test MCO canisters were assembled at Hanford, prepared for testing at the Idaho National Engineering and Environmental Laboratory (INEEL), <span class="hlt">drop</span> tested at Sandia National Laboratories, and evaluated back at the INEEL. In addition to the actual testing efforts, finite element plastic analysis techniques were used to make both pre-test and post-test predictions of the test MCOs structural deformations. The completed effort has demonstrated that the canister design is capablemore » of maintaining a 50 psig <span class="hlt">pressure</span> boundary after <span class="hlt">drop</span> testing. Based on helium leak testing methods, one test MCO was determined to have a leakage rate not greater than 1x10 -5 std cc/sec (prior internal helium presence prevented a more rigorous test) and the remaining test MCO had a measured leakage rate less than 1x10 -7 std cc/sec (i.e., a leaktight containment) after the <span class="hlt">drop</span> test. The effort has also demonstrated the capability of finite element methods using plastic analysis techniques to accurately predict the structural deformations of canisters subjected to an accidental <span class="hlt">drop</span> event.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018EPJWC.18002011B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018EPJWC.18002011B"><span>The influence of flow modification on <span class="hlt">air</span> and PCM temperatures in an accumulative heat exchanger</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Borcuch, Marcin; Musiał, Michał; Sztekler, Karol; Kalawa, Wojciech; Gumuła, Stanisław; Stefański, Sebastian</p> <p>2018-06-01</p> <p>The paper presents the influence of flow modification on the operation of an accumulative heat exchanger. This device can be used as a regenerator in ventilation and <span class="hlt">air</span> supply systems. A heat exchanger uses ceresine (a mixture of paraffins) as a phase change material (PCM). The aim of this research was to determine the effect of flow modification on temperature distribution and <span class="hlt">pressure</span> <span class="hlt">drops</span> in the device. The introduction contains a short description of the test stand used, including the accumulative heat exchanger, the guide vanes, and the locations of measurement and control equipment. We found that additional objects limited vortex structures, increased the inside temperature, and <span class="hlt">dropped</span> the <span class="hlt">pressure</span> along the heat exchanger. Guidelines for further research are proposed and briefly discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19940000215&hterms=gas+turbine+blade+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dgas%2Bturbine%2Bblade%2Bdesign','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19940000215&hterms=gas+turbine+blade+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dgas%2Bturbine%2Bblade%2Bdesign"><span>Twisted Vanes Would Enhance Fuel/<span class="hlt">Air</span> Mixing In Turbines</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Nguyen, H. Lee; Micklow, Gerald J.; Dogra, Anju S.</p> <p>1994-01-01</p> <p>Computations of flow show performance of high-shear airblast fuel injector in gas-turbine engine enhanced by use of appropriately proportioned twisted (instead of flat) dome swirl vanes. Resultant more nearly uniform fuel/<span class="hlt">air</span> mixture burns more efficiently, emitting smaller amounts of nitrogen oxides. Twisted-vane high-shear airblast injectors also incorporated into paint sprayers, providing advantages of low <span class="hlt">pressure</span> <span class="hlt">drop</span> characteristic of airblast injectors in general and finer atomization of advanced twisted-blade design.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..MARP37013M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..MARP37013M"><span>The origin of star-shaped oscillations of Leidenfrost <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ma, Xiaolei; Burton, Justin C.</p> <p></p> <p>We experimentally investigate the oscillations of Leidenfrost <span class="hlt">drops</span> of water, liquid nitrogen, ethanol, methanol, acetone and isopropyl alcohol. The <span class="hlt">drops</span> levitate on a cushion of evaporated vapor over a hot, curved surface which keeps the <span class="hlt">drops</span> stationary. We observe star-shaped modes along the periphery of the <span class="hlt">drop</span>, with mode numbers n = 2 to 13. The number of observed modes is sensitive to the properties of the liquid. The <span class="hlt">pressure</span> oscillation frequency in the vapor layer under the <span class="hlt">drop</span> is approximately twice that of the <span class="hlt">drop</span> frequency, which is consistent with a parametric forcing mechanism. However, the Rayleigh and thermal Marangoni numbers are of order 10,000, indicating that convection should play a dominating role as well. Surprisingly, we find that the wavelength and frequency of the oscillations only depend on the thickness of the liquid, which is twice the capillary length, and do not depend on the mode number, substrate temperature, or the substrate curvature. This robust behavior suggests that the wavelength for the oscillations is set by thermal convection inside the <span class="hlt">drop</span>, and is less dependent on the flow in the vapor layer under the <span class="hlt">drop</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880061388&hterms=hanging+drop&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dhanging%2Bdrop','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880061388&hterms=hanging+drop&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dhanging%2Bdrop"><span>Experimental and theoretical analysis of the rate of solvent equilibration in the hanging <span class="hlt">drop</span> method of protein crystal growth</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fowlis, William W.; Delucas, Lawrence J.; Twigg, Pamela J.; Howard, Sandra B.; Meehan, Edward J.</p> <p>1988-01-01</p> <p>The principles of the hanging-<span class="hlt">drop</span> method of crystal growth are discussed, and the rate of water evaporation in a water droplet (containing protein, buffer, and a precipitating agent) suspended above a well containing a double concentration of precipitating agent is investigated theoretically. It is shown that, on earth, the rate of evaporation may be determined from diffusion theory and the colligative properties of solutions. The parameters affecting the rate of evaporation include the temperature, the vapor <span class="hlt">pressure</span> of water, the ionization constant of the salt, the volume of the <span class="hlt">drop</span>, the contact angle between the droplet and the coverslip, the number of moles of salt in the droplet, the number of moles of water and salt in the well, the molar volumes of water and salt, the distance from the droplet to the well, and the coefficient of diffusion of water vapor through <span class="hlt">air</span>. To test the theoretical equations, hanging-<span class="hlt">drop</span> experiments were conducted using various reagent concentrations in 25-microliter droplets and measuring the evaporation times at 4 C and 25 C. The results showed good agreement with the theory.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810012682','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810012682"><span>An investigation of <span class="hlt">air</span> solubility in Jet A fuel at high <span class="hlt">pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Faeth, G. M.</p> <p>1981-01-01</p> <p>Problems concerned with the supercritical injection concept are discussed. Supercritical injection involves dissolving <span class="hlt">air</span> into a fuel prior to injection. A similar effect is obtained by preheating the fuel so that a portion of the fuel flashes when its <span class="hlt">pressure</span> is reduced. Flashing improves atomization properties and the presence of <span class="hlt">air</span> in the primary zone of a spray flame reduces the formation of pollutants. The investigation is divided into three phases: (1) measure the solubility and density properties of fuel/gas mixtures, including Jet A/<span class="hlt">air</span>, at <span class="hlt">pressures</span> and correlate these results using theory; (2) investigate the atomization properties of flashing liquids, including fuel/dissolved gas systems. Determine and correlate the effect of inlet properties and injector geometry on mass flow rates, Sauter mean diameter and spray angles; (3) examine the combustion properties of flashing injection in an open burner flame, considering flame shape and soot production.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=physics+AND+glass&pg=2&id=EJ1025234','ERIC'); return false;" href="https://eric.ed.gov/?q=physics+AND+glass&pg=2&id=EJ1025234"><span>The Jar Magic--Instructional Activities for Teaching <span class="hlt">Air</span> <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Ku, Bing-Hong; Chen, Chyong-Sun</p> <p>2013-01-01</p> <p>There are a variety of impressive activities designed for teaching the concept of <span class="hlt">air</span> <span class="hlt">pressure</span> to junior high school students. Water, glasses, balloons, plastic bottles, and suction cups are some of the items commonly used in these experiments. For example, if we take a glass of water, cover it with a piece of cardboard, and invert the glass,…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091720','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091720"><span>Correction of Temperatures of <span class="hlt">Air</span>-Cooled Engine Cylinders for Variation in Engine and Cooling Conditions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Schey, Oscar W; Pinkel, Benjamin; Ellerbrock, Herman H , Jr</p> <p>1939-01-01</p> <p>Factors are obtained from semiempirical equations for correcting engine-cylinder temperatures for variation in important engine and cooling conditions. The variation of engine temperatures with atmospheric temperature is treated in detail, and correction factors are obtained for various flight and test conditions, such as climb at constant indicated <span class="hlt">air</span> speed, level flight, ground running, take-off, constant speed of cooling <span class="hlt">air</span>, and constant mass flow of cooling <span class="hlt">air</span>. Seven conventional <span class="hlt">air</span>-cooled engine cylinders enclosed in jackets and cooled by a blower were tested to determine the effect of cooling-<span class="hlt">air</span> temperature and carburetor-<span class="hlt">air</span> temperature on cylinder temperatures. The cooling <span class="hlt">air</span> temperature was varied from approximately 80 degrees F. to 230 degrees F. and the carburetor-<span class="hlt">air</span> temperature from approximately 40 degrees F. to 160 degrees F. Tests were made over a large range of engine speeds, brake mean effective <span class="hlt">pressures</span>, and <span class="hlt">pressure</span> <span class="hlt">drops</span> across the cylinder. The correction factors obtained experimentally are compared with those obtained from the semiempirical equations and a fair agreement is noted.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017HMT....53.3119B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017HMT....53.3119B"><span>Experimental investigation of the effect of <span class="hlt">air</span> velocity on a unit cooler under frosting condition: a case study</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bayrak, Ergin; Çağlayan, Akın; Konukman, Alp Er S.</p> <p>2017-10-01</p> <p>Finned tube evaporators are used in a wide range of applications such as commercial and industrial cold/freezed storage rooms with high traffic loading under frosting conditions. In this case study, an evaporator with an integrated fan was manufactured and tested under frosting conditions by only changing the <span class="hlt">air</span> flow rate in an ambient balanced type test laboratory compared to testing in a wind tunnel with a more uniform flow distribution in order to detect the effect of <span class="hlt">air</span> flow rate on frosting. During the test, operation was performed separately based on three different <span class="hlt">air</span> flow rates. The parameters concerning test operation such as the changes of <span class="hlt">air</span> temperature, <span class="hlt">air</span> relative humidity, surface temperature, <span class="hlt">air</span>-side <span class="hlt">pressure</span> <span class="hlt">drop</span> and refrigerant side capacity etc. were followed in detail for each <span class="hlt">air</span> flow rate. At the same time, digital images were captured in front of the evaporator; thus, frost thicknesses and blockage ratios at the course of fan stall were determined by using an image-processing technique. Consequently, the test and visual results showed that the trendline of <span class="hlt">air</span>-side <span class="hlt">pressure</span> <span class="hlt">drop</span> increased slowly at the first stage of test operations, then increased linearly up to a top point and then the linearity was disrupted instantly. This point speculated the beginning of defrost operation for each case. In addition, despite detecting a velocity that needs to be avoided, a test applied at minimum <span class="hlt">air</span> velocity is superior to providing minimum capacity in terms of loss of capacity during test operations.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_20 --> <div id="page_21" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="401"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PlST...18..732W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PlST...18..732W"><span>Thermodynamic and Transport Properties of Real <span class="hlt">Air</span> Plasma in Wide Range of Temperature and <span class="hlt">Pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Chunlin; Wu, Yi; Chen, Zhexin; Yang, Fei; Feng, Ying; Rong, Mingzhe; Zhang, Hantian</p> <p>2016-07-01</p> <p><span class="hlt">Air</span> plasma has been widely applied in industrial manufacture. In this paper, both dry and humid <span class="hlt">air</span> plasmas' thermodynamic and transport properties are calculated in temperature 300-100000 K and <span class="hlt">pressure</span> 0.1-100 atm. To build a more precise model of real <span class="hlt">air</span> plasma, over 70 species are considered for composition. Two different methods, the Gibbs free energy minimization method and the mass action law method, are used to determinate the composition of the <span class="hlt">air</span> plasma in a different temperature range. For the transport coefficients, the simplified Chapman-Enskog method developed by Devoto has been applied using the most recent collision integrals. It is found that the presence of CO2 has almost no effect on the properties of <span class="hlt">air</span> plasma. The influence of H2O can be ignored except in low <span class="hlt">pressure</span> <span class="hlt">air</span> plasma, in which the saturated vapor <span class="hlt">pressure</span> is relatively high. The results will serve as credible inputs for computational simulation of <span class="hlt">air</span> plasma. supported by the National Key Basic Research Program of China (973 Program)(No. 2015CB251002), National Natural Science Foundation of China (Nos. 51521065, 51577145), the Science and Technology Project Funds of the Grid State Corporation (SGTYHT/13-JS-177), the Fundamental Research Funds for the Central Universities, and State Grid Corporation Project (GY71-14-004)</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17687455','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17687455"><span>Elevated plasma endothelin-1 and pulmonary arterial <span class="hlt">pressure</span> in children exposed to <span class="hlt">air</span> pollution.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Calderón-Garcidueñas, Lilian; Vincent, Renaud; Mora-Tiscareño, Antonieta; Franco-Lira, Maricela; Henríquez-Roldán, Carlos; Barragán-Mejía, Gerardo; Garrido-García, Luis; Camacho-Reyes, Laura; Valencia-Salazar, Gildardo; Paredes, Rogelio; Romero, Lina; Osnaya, Hector; Villarreal-Calderón, Rafael; Torres-Jardón, Ricardo; Hazucha, Milan J; Reed, William</p> <p>2007-08-01</p> <p>Controlled exposures of animals and humans to particulate matter (PM) or ozone <span class="hlt">air</span> pollution cause an increase in plasma levels of endothelin-1, a potent vasoconstrictor that regulates pulmonary arterial <span class="hlt">pressure</span>. The primary objective of this field study was to determine whether Mexico City children, who are chronically exposed to levels of PM and O(3) that exceed the United States <span class="hlt">air</span> quality standards, have elevated plasma endothelin-1 levels and pulmonary arterial <span class="hlt">pressures</span>. We conducted a study of 81 children, 7.9 +/- 1.3 years of age, lifelong residents of either northeast (n = 19) or southwest (n = 40) Mexico City or Polotitlán (n = 22), a control city with PM and O(3) levels below the U.S. <span class="hlt">air</span> quality standards. Clinical histories, physical examinations, and complete blood counts were done. Plasma endothelin-1 concentrations were determined by immunoassay, and pulmonary arterial <span class="hlt">pressures</span> were measured by Doppler echocardiography. Mexico City children had higher plasma endothelin-1 concentrations compared with controls (p < 0.001). Mean pulmonary arterial <span class="hlt">pressure</span> was elevated in children from both northeast (p < 0.001) and southwest (p < 0.05) Mexico City compared with controls. Endothelin-1 levels in Mexico City children were positively correlated with daily outdoor hours (p = 0.012), and 7-day cumulative levels of PM <span class="hlt">air</span> pollution < 2.5 mum in aerodynamic diameter (PM(2.5)) before endothelin-1 measurement (p = 0.03). Chronic exposure of children to PM(2.5) is associated with increased levels of circulating endothelin-1 and elevated mean pulmonary arterial <span class="hlt">pressure</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790042626&hterms=anatomy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Danatomy','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790042626&hterms=anatomy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Danatomy"><span>Space Shuttle Solid Rocket Booster Decelerator Subsystem <span class="hlt">Drop</span> Test 3 - Anatomy of a failure</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Runkle, R. E.; Woodis, W. R.</p> <p>1979-01-01</p> <p>A test failure dramatically points out a design weakness or the limits of the material in the test article. In a low budget test program, with a very limited number of tests, a test failure sparks supreme efforts to investigate, analyze, and/or explain the anomaly and to improve the design such that the failure will not recur. The third <span class="hlt">air</span> <span class="hlt">drop</span> of the Space Shuttle Solid Rocket Booster Recovery System experienced such a dramatic failure. On <span class="hlt">air</span> <span class="hlt">drop</span> 3, the 54-ft drogue parachute was totally destroyed 0.7 sec after deployment. The parachute failure investigation, based on analysis of <span class="hlt">drop</span> test data and supporting ground element test results is presented. Drogue design modifications are also discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/873149','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/873149"><span>Simplified configuration for the combustor of an oil burner using a low <span class="hlt">pressure</span>, high flow <span class="hlt">air</span>-atomizing nozzle</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Butcher, Thomas A.; Celebi, Yusuf; Fisher, Leonard</p> <p>2000-09-15</p> <p>The invention relates to clean burning of fuel oil with <span class="hlt">air</span>. More specifically, to a fuel burning combustion head using a low-<span class="hlt">pressure</span>, high <span class="hlt">air</span> flow atomizing nozzle so that there will be a complete combustion of oil resulting in a minimum emission of pollutants. The improved fuel burner uses a low <span class="hlt">pressure</span> <span class="hlt">air</span> atomizing nozzle that does not result in the use of additional compressors or the introduction of <span class="hlt">pressurized</span> gases downstream, nor does it require a complex design. Inventors:</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860015491','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860015491"><span>Measurement of viscosity of gaseous mixtures at atmospheric <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Singh, J. J.; Mall, G. H.; Chegini, H.</p> <p>1986-01-01</p> <p>Coefficients of viscosity of various types of gas mixtures, including simulated natural-gas samples, have been measured at atmospheric <span class="hlt">pressure</span> and room temperature using a modified capillary tube method. <span class="hlt">Pressure</span> <span class="hlt">drops</span> across the straight capillary tube section of a thermal mass flowmeter were measured for small, well-defined, volume flow rates for the test gases and for standard <span class="hlt">air</span>. In this configuration, the flowmeter provides the volumetric flow rates as well as a well-characterized capillary section for differential <span class="hlt">pressure</span> measurements across it. The coefficients of viscosity of the test gases were calculated using the reported value of 185.6 micro P for the viscosity of <span class="hlt">air</span>. The coefficients of viscosity for the test mixtures were also calculated using Wilke's approximation of the Chapman-Enskog (C-E) theory. The experimental and calculated values for binary mixtures are in agreement within the reported accuracy of Wilke's approximation of the C-E theory. However, the agreement for multicomponent mixtures is less satisfactory, possible because of the limitations of Wilkes's approximation of the classical dilute-gas state model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18529171','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18529171"><span>High-Reynolds-number turbulent-boundary-layer wall <span class="hlt">pressure</span> fluctuations with skin-friction reduction by <span class="hlt">air</span> injection.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Winkel, Eric S; Elbing, Brian R; Ceccio, Steven L; Perlin, Marc; Dowling, David R</p> <p>2008-05-01</p> <p>The hydrodynamic <span class="hlt">pressure</span> fluctuations that occur on the solid surface beneath a turbulent boundary layer are a common source of flow noise. This paper reports multipoint surface <span class="hlt">pressure</span> fluctuation measurements in water beneath a high-Reynolds-number turbulent boundary layer with wall injection of <span class="hlt">air</span> to reduce skin-friction drag. The experiments were conducted in the U.S. Navy's Large Cavitation Channel on a 12.9-m-long, 3.05-m-wide hydrodynamically smooth flat plate at freestream speeds up to 20 ms and downstream-distance-based Reynolds numbers exceeding 200 x 10(6). <span class="hlt">Air</span> was injected from one of two spanwise slots through flush-mounted porous stainless steel frits (approximately 40 microm mean pore diameter) at volume flow rates from 17.8 to 142.5 l/s per meter span. The two injectors were located 1.32 and 9.78 m from the model's leading edge and spanned the center 87% of the test model. Surface <span class="hlt">pressure</span> measurements were made with 16 flush-mounted transducers in an "L-shaped" array located 10.7 m from the plate's leading edge. When compared to no-injection conditions, the observed wall-<span class="hlt">pressure</span> variance was reduced by as much as 87% with <span class="hlt">air</span> injection. In addition, <span class="hlt">air</span> injection altered the inferred convection speed of <span class="hlt">pressure</span> fluctuation sources and the streamwise coherence of <span class="hlt">pressure</span> fluctuations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25217332','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25217332"><span>Control of stain geometry by <span class="hlt">drop</span> evaporation of surfactant containing dispersions.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Erbil, H Yildirim</p> <p>2015-08-01</p> <p>Control of stain geometry by <span class="hlt">drop</span> evaporation of surfactant containing dispersions is an important topic of interest because it plays a crucial role in many applications such as forming templates on solid surfaces, in ink-jet printing, spraying of pesticides, micro/nano material fabrication, thin film coatings, biochemical assays, deposition of DNA/RNA micro-arrays, and manufacture of novel optical and electronic materials. This paper presents a review of the published articles on the diffusive <span class="hlt">drop</span> evaporation of pure liquids (water), the surfactant stains obtained from evaporating <span class="hlt">drops</span> that do not contain dispersed particles and deposits obtained from <span class="hlt">drops</span> containing polymer colloids and carbon based particles such as carbon nanotubes, graphite and fullerenes. Experimental results of specific systems and modeling attempts are discussed. This review also has some special subtopics such as suppression of coffee-rings by surfactant addition and "stick-slip" behavior of evaporating nanosuspension <span class="hlt">drops</span>. In general, the <span class="hlt">drop</span> evaporation process of a surfactant/particle/substrate system is very complex since dissolved surfactants adsorb on both the insoluble organic/inorganic micro/nanoparticles in the <span class="hlt">drop</span>, on the <span class="hlt">air</span>/solution interface and on the substrate surface in different extends. Meanwhile, surfactant adsorbed particles interact with the substrate giving a specific contact angle, and free surfactants create a solutal Marangoni flow in the <span class="hlt">drop</span> which controls the location of the particle deposition together with the rate of evaporation. In some cases, the presence of a surfactant monolayer at the <span class="hlt">air</span>/solution interface alters the rate of evaporation. At present, the magnitude of each effect cannot be predicted adequately in advance and consequently they should be carefully studied for any system in order to control the shape and size of the final deposit. Copyright © 2014 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..DFD.S5004A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..DFD.S5004A"><span>Mixing in Sessile <span class="hlt">Drops</span> Merging on a Surface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Anna, Shelley; Zhang, Ying; Oberdick, Samuel; Garoff, Stephen</p> <p>2011-11-01</p> <p>We investigate the mixing of two sessile <span class="hlt">drops</span> that merge on a surface. The <span class="hlt">drops</span> consist of low viscosity glycerol-water mixtures deposited on a silicone elastomer surface with contact angle near 90°. We observe the shape of the <span class="hlt">drops</span> and the location of their intersection by placing a fluorescent dye in one <span class="hlt">drop</span> and using a laser light sheet to image a plane perpendicular to the surface. The initial healing of the meniscus bridge between the merging <span class="hlt">drops</span>, and the damping of capillary waves appearing on their surfaces occur on timescales comparable to the inertio-capillary relaxation time. However, the interface between the two fluids remains sharp, broadening diffusively over several minutes. The shape of the merged <span class="hlt">drops</span> and the boundary between them also continues to evolve on a timescale of minutes. This later motion is controlled by gravity, capillary <span class="hlt">pressure</span>, and viscous stresses. Images of the 3D <span class="hlt">drop</span> shape indicate that small contact line motions are correlated to the slow relaxation. Although the two <span class="hlt">drops</span> contain identical liquids except for the presence of the dye, the shape of the interface consistently evolves asymmetrically, assuming a characteristic crescent shape. We note that very tiny surface tension gradients can produce an asymmetric flow like the one observed here. We characterize the long timescale flow as a function of the <span class="hlt">drop</span> sizes, and we use numerical simulations to aid in elucidating the essential physics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014cosp...40E2560P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014cosp...40E2560P"><span><span class="hlt">Drop</span> Tower Facility at Queensland University of Technology</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Plagens, Owen; Castillo, Martin; Steinberg, Theodore; Ong, Teng-Cheong</p> <p></p> <p>The Queensland University of Technology (QUT) <span class="hlt">Drop</span> Tower Facility is a {raise.17exscriptstyle˜}2.1 second, 21.3 m fall, dual capsule <span class="hlt">drop</span> tower system. The dual capsule comprises of an uncoupled exterior hollow drag shield that experiences drag by the ambient atmosphere with the experimental capsule falling within the drag shield. The dual capsule system is lifted to the top of the <span class="hlt">drop</span> tower via a mechanical crane and the <span class="hlt">dropping</span> process is initiated by the cutting of a wire coupling the experimental package and suspending the drag shield. The internal experimental capsule reaches the bottom of the drag shield floor just prior to the deceleration stage at the <span class="hlt">air</span> bag and during this time experience gravity levels of {raise.17exscriptstyle˜}10textsuperscript{-6} g. The deceleration system utilizes an inflatable airbag where experimental packages can be designed to experience a maximum deceleration of {raise.17exscriptstyle˜}10textsuperscript{18} g for {raise.17exscriptstyle˜}0.1 seconds. The drag shield can house experimental packages with a maximum diameter of 0.8 m and height of 0.9 m. The drag shield can also be used in foam mode, where the walls are lined with foam and small experiments can be <span class="hlt">dropped</span> completely untethered. This mode is generally used for the study of microsatellite manipulation. Payloads can be powered by on-board power systems with power delivered to the experiment until free fall occurs. Experimental data that can be collected includes but is not limited to video, temperature, <span class="hlt">pressure</span>, voltage/current from the power supply, and triggering mechanisms outputs which are simultaneously collected via data logging systems and high speed video recording systems. Academic and commercial projects are currently under investigation at the QUT <span class="hlt">Drop</span> Tower Facility and collaboration is openly welcome at this facility. Current research includes the study of heterogeneously burning metals in oxygen which is aimed at fire safety applications and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19780020155','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19780020155"><span>Experimental study of the effect of cycle <span class="hlt">pressure</span> on lean combustion emissions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Roffe, G.; Venkataramani, K. S.</p> <p>1978-01-01</p> <p>Experiments were conducted in which a stream of premixed propane and <span class="hlt">air</span> was burned under conditions representative of gas turbine operation. Emissions of NOx, CO, and unburned hydrocarbons (UHC) were measured over a range of combustor inlet temperature, <span class="hlt">pressure</span>, and residence time at equivalence ratios from 0.7 down to the lean stability limit. At an inlet temperature of 600 K, observed NOx levels <span class="hlt">dropped</span> markedly with decreasing <span class="hlt">pressure</span> for <span class="hlt">pressures</span> below 20 atm. The NOx levels are proportional to combustor residence time and formation rates were principally a function of adiabatic flame temperature. For adiabatic flame temperatures of 2050 K and higher, CO reached chemical equilibrium within 2 msec. Unburned hydrocarbon species <span class="hlt">dropped</span> to a negligible level within 2 msec regardless of inlet temperature, <span class="hlt">pressure</span>, or equivalence ratio. For a combustor residence time of 2.5 msec, combustion inefficiency became less than 0.01% at an adiabatic flame temperature of 2050 K. The maximum combustion inefficiency observed was on the order of 1% and corresponded to conditions near the lean stability limit. Using a perforated plate flameholder, this limit is well represented by the condition of 1800 K adiabatic flame temperature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810068602','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810068602"><span>A Procedure for the Design of <span class="hlt">Air</span>-Heated Ice-Prevention Systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Neel, C. B.</p> <p>1954-01-01</p> <p>A procedure proposed for use in the design of <span class="hlt">air</span>-heated systems for the continuous prevention of ice formation on airplane components is set forth. Required heat-transfer and <span class="hlt">air-pressure</span>-loss equations are presented, and methods of selecting appropriate meteorological conditions for flight over specified geographical areas and for the calculation of water-<span class="hlt">drop</span>-impingement characteristics are suggested. In order to facilitate the design, a simple electrical analogue was devised which solves the complex heat-transfer relationships existing in the thermal-system analysis. The analogue is described and an illustration of its application to design is given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19870012585&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870012585&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure"><span>Investigation of the reaction of liquid hydrogen with liquid <span class="hlt">air</span> in a <span class="hlt">pressure</span> tube</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Karb, Erich H.</p> <p>1987-01-01</p> <p>A <span class="hlt">pressure</span> tube should protect the FR-2 reactor from the consequences of a hydrogen-<span class="hlt">air</span> reaction, which is conceivable in the breakdown of several safety devices of the planned cold neutron source Project FR-2/16. The magnitudes and time pattern of the <span class="hlt">pressures</span> to be expected were investigated. In the geometry used and the ignition mechanism selected, which is comparable to the strongest ignition process conceivable in the reactor, the reaction proceeds with greater probability than combustion. The combustion is possibly smaller if local limited partial detonations are superimposed. The magnitude of the <span class="hlt">pressure</span> was determined by the masses of the reaction partners, liquid H2 and liquid <span class="hlt">air</span>, and determines their ratio to each other.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26741497','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26741497"><span>Effect of Different Levels of <span class="hlt">Pressure</span> Relieving <span class="hlt">Air</span>-Mattress Firmness on Cough Strength.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kamikawa, Norimichi; Taito, Shunsuke; Takahashi, Makoto; Sekikawa, Kiyokazu; Hamada, Hironobu</p> <p>2016-01-01</p> <p>Cough is an important host-defense mechanism. The elderly and patients who are severely ill cannot cough effectively when lying in the supine position. Furthermore, <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattresses are recommended for preventing the development of <span class="hlt">pressure</span> ulcers. In this study, we clarified whether or not the cough peak flow (CPF), an index of cough strength, is affected by different firmness levels of a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress in healthy volunteers in the supine position. Fifty-two healthy young men participated. All the measurements were carried out on each participant in the supine position on a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress. The participants were assessed at two firmness levels, a "hard" and "soft" mode. The CPF, forced vital capacity (FVC), maximal expiratory <span class="hlt">pressure</span> (PEmax), and maximal inspiratory <span class="hlt">pressure</span> (PImax) were determined for each mode. The sinking distance of the body into the mattress was measured without any activity and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax, and PImax were determined for each mode. The sinking distance of the body into the mattress was measured and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax and PImax values of the participants coughing on the mattress were significantly lower when the mattress was in "soft" than in "hard" mode. The differences between the sinking distances of the mattress in "soft" and "hard" modes were larger for the anterior superior iliac spine. A harder mattress may lead to increased CPF in healthy young men lying in the supine position, and increased CPF may be important for host defense.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29113035','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29113035"><span>Room-Temperature <span class="hlt">Pressure</span>-Induced Optically-Actuated Fabry-Perot Nanomechanical Resonator with Multilayer Graphene Diaphragm in <span class="hlt">Air</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Li, Cheng; Lan, Tian; Yu, Xiyu; Bo, Nan; Dong, Jingyu; Fan, Shangchun</p> <p>2017-11-04</p> <p>We demonstrated a miniature and in situ ~13-layer graphene nanomechanical resonator by utilizing a simple optical fiber Fabry-Perot (F-P) interferometric excitation and detection scheme. The graphene film was transferred onto the endface of a ferrule with a 125-μm inner diameter. In contrast to the pre-tension induced in membrane that increased quality ( Q ) factor to ~18.5 from ~3.23 at room temperature and normal <span class="hlt">pressure</span>, the limited effects of <span class="hlt">air</span> damping on resonance behaviors at 10 -2 and 10⁵ Pa were demonstrated by characterizing graphene F-P resonators with open and micro-<span class="hlt">air</span>-gap cavities. Then in terms of optomechanical behaviors of the resonator with an <span class="hlt">air</span> micro-cavity configuration using a polished ferrule substrate, measured resonance frequencies were increased to the range of 509-542 kHz from several kHz with a maximum Q factor of 16.6 despite the lower Knudsen number ranging from 0.0002 to 0.0006 in damping <span class="hlt">air</span> over a relative <span class="hlt">pressure</span> range of 0-199 kPa. However, there was the little dependence of Q on resonance frequency. Note that compared with the inferior F-P cavity length response to applied <span class="hlt">pressures</span> due to interfacial <span class="hlt">air</span> leakage, the developed F-P resonator exhibited a consistent fitted <span class="hlt">pressure</span> sensitivity of 1.18 × 10⁵ kHz³/kPa with a good linearity error of 5.16% in the tested range. These measurements shed light on the pre-stress-dominated <span class="hlt">pressure</span>-sensitive mechanisms behind <span class="hlt">air</span> damping in in situ F-P resonant sensors using graphene or other 2D nanomaterials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011HMT....47..951R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011HMT....47..951R"><span>Heat transfer, <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow patterns during flow boiling of R407C in a horizontal microfin tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rollmann, P.; Spindler, K.; Müller-Steinhagen, H.</p> <p>2011-08-01</p> <p>The heat transfer, <span class="hlt">pressure</span> <span class="hlt">drop</span> and flow patterns during flow boiling of R407C in a horizontal microfin tube have been investigated. The microfin tube is made of copper with a total fin number of 55 and a helix angle of 15°. The fin height is 0.24 mm and the inner tube diameter at fin root is 8.95 mm. The test tube is 1 m long. It is heated electrically. The experiments have been performed at saturation temperatures between -30°C and +10°C. The mass flux was varied between 25 and 300 kg/m2/s, the heat flux from 20,000 W/m2 down to 1,000 W/m2. The vapour quality was kept constant at 0.1, 0.3, 0.5, 0.7 at the inlet and 0.8, 1.0 at the outlet, respectively. The measured heat transfer coefficient is compared with the correlations of Cavallini et al., Shah as well as Zhang et al. Cavallini's correlation contains seven experimental constants. After fitting these constants to our measured values, the correlation achieves good agreement. The measured <span class="hlt">pressure</span> <span class="hlt">drop</span> is compared to the correlations of Pierre, Kuo and Wang as well as Müller-Steinhagen and Heck. The best agreement is achieved with the correlation of Kuo and Wang. Almost all values are calculated within an accuracy of ±30%. The flow regimes were observed. It is shown, that changes in the flow regime affect the heat transfer coefficient significantly.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25559870','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25559870"><span>A randomized comparison of the i-gel with the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q intubating laryngeal airway in children.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kim, Min-Soo; Lee, Jae Hoon; Han, Sang Won; Im, Young Jae; Kang, Hyo Jong; Lee, Jeong-Rim</p> <p>2015-04-01</p> <p>Supraglottic airway devices with noninflatable cuff have advantages in omitting the cuff <span class="hlt">pressure</span> monitoring and reducing potential pharyngolaryngeal complications. Typical devices without cuff inflation available in children are the i-gel and the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q intubating laryngeal airway (<span class="hlt">air</span>-Q SP). To date, there is no comparative study between these devices in pediatric patients. The purpose of this randomized study was to compare the i-gel(™) and the self-<span class="hlt">pressurized</span> <span class="hlt">air</span>-Q(™) intubating laryngeal airway (<span class="hlt">air</span>-Q SP) in children undergoing general anesthesia. Eighty children, 1-108 months of age, 7-30 kg of weight, and scheduled for elective surgery in which supraglottic airway devices would be suitable for airway management, were randomly assigned to either the i-gel or the <span class="hlt">air</span>-Q SP. Oropharyngeal leak <span class="hlt">pressure</span> and fiberoptic view were assessed three times as follows: after insertion and fixation of the device, 10 min after initial assessment, and after completion of surgery. We also assessed insertion parameters and complications. Insertion of the i-gel was regarded as significantly easier compared to the <span class="hlt">air</span>-Q SP (P = 0.04). Compared to the <span class="hlt">air</span>-Q SP group, the i-gel group had significantly higher oropharyngeal leak <span class="hlt">pressures</span> at all measurement points and significantly lower frequencies of gastric insufflation at 10 min after initial assessment and completion of surgery. The <span class="hlt">air</span>-Q SP group had better fiberoptic views than the i-gel group at all measurement points. Our results showed that the i-gel had easier insertion and better sealing function, and the <span class="hlt">air</span>-Q SP provided improved fiberoptic views in children requiring general anesthesia. © 2015 John Wiley & Sons Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25179108','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25179108"><span>Fabrication of an anti-viral <span class="hlt">air</span> filter with SiO₂-Ag nanoparticles and performance evaluation in a continuous airflow condition.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Joe, Yun Haeng; Woo, Kyoungja; Hwang, Jungho</p> <p>2014-09-15</p> <p>In this study, SiO2 nanoparticles surface coated with Ag nanoparticles (SA particles) were fabricated to coat a medium <span class="hlt">air</span> filter. The <span class="hlt">pressure</span> <span class="hlt">drop</span>, filtration efficiency, and anti-viral ability of the filter were evaluated against aerosolized bacteriophage MS2 in a continuous <span class="hlt">air</span> flow condition. A mathematical approach was developed to measure the anti-viral ability of the filter with various virus deposition times. Moreover, two quality factors based on the anti-viral ability of the filter, and a traditional quality factor based on filtration efficiency, were calculated. The filtration efficiency and <span class="hlt">pressure</span> <span class="hlt">drop</span> increased with decreasing media velocity and with increasing SA particle coating level. The anti-viral efficiency also increased with increasing SA particle coating level, and decreased by with increasing virus deposition time. Consequently, SA particle coating on a filter does not have significant effects on filtration quality, and there is an optimal coating level to produce the highest anti-viral quality. Copyright © 2014 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006JPS...156..232B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006JPS...156..232B"><span>Modeling and optimization of the <span class="hlt">air</span> system in polymer exchange membrane fuel cell systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bao, Cheng; Ouyang, Minggao; Yi, Baolian</p> <p></p> <p>Stack and <span class="hlt">air</span> system are the two most important components in the fuel cell system (FCS). It is meaningful to study their properties and the trade-off between them. In this paper, a modified one-dimensional steady-state analytical fuel cell model is used. The logarithmic mean of the inlet and the outlet oxygen partial <span class="hlt">pressure</span> is adopted to avoid underestimating the effect of <span class="hlt">air</span> stoichiometry. And the <span class="hlt">pressure</span> <span class="hlt">drop</span> model in the grid-distributed flow field is included in the stack analysis. Combined with the coordinate change preprocessing and analog technique, neural network is used to treat the MAP of compressor and turbine in the <span class="hlt">air</span> system. Three kinds of <span class="hlt">air</span> system topologies, the pure screw compressor, serial booster and exhaust expander are analyzed in this article. A real-code genetic algorithm is programmed to obtain the global optimum <span class="hlt">air</span> stoichiometric ratio and the cathode outlet <span class="hlt">pressure</span>. It is shown that the serial booster and expander with the help of exhaust recycling, can improve more than 3% in the FCS efficiency comparing to the pure screw compressor. As the net power increases, the optimum cathode outlet <span class="hlt">pressure</span> keeps rising and the <span class="hlt">air</span> stoichiometry takes on the concave trajectory. The working zone of the proportional valve is also discussed. This presented work is helpful to the design of the <span class="hlt">air</span> system in fuel cell system. The steady-state optimum can also be used in the dynamic control.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18639301','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18639301"><span><span class="hlt">Air</span> charged and microtip catheters cannot be used interchangeably for urethral <span class="hlt">pressure</span> measurement: a prospective, single-blind, randomized trial.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zehnder, Pascal; Roth, Beat; Burkhard, Fiona C; Kessler, Thomas M</p> <p>2008-09-01</p> <p>We determined and compared urethral <span class="hlt">pressure</span> measurements using <span class="hlt">air</span> charged and microtip catheters in a prospective, single-blind, randomized trial. A consecutive series of 64 women referred for urodynamic investigation underwent sequential urethral <span class="hlt">pressure</span> measurements using an <span class="hlt">air</span> charged and a microtip catheter in randomized order. Patients were blinded to the type and sequence of catheter used. Agreement between the 2 catheter systems was assessed using the Bland and Altman 95% limits of agreement method. Intraclass correlation coefficients of <span class="hlt">air</span> charged and microtip catheters for maximum urethral closure <span class="hlt">pressure</span> at rest were 0.97 and 0.93, and for functional profile length they were 0.9 and 0.78, respectively. Pearson's correlation coefficients and Lin's concordance coefficients of <span class="hlt">air</span> charged and microtip catheters were r = 0.82 and rho = 0.79 for maximum urethral closure <span class="hlt">pressure</span> at rest, and r = 0.73 and rho = 0.7 for functional profile length, respectively. When applying the Bland and Altman method, <span class="hlt">air</span> charged catheters gave higher readings than microtip catheters for maximum urethral closure <span class="hlt">pressure</span> at rest (mean difference 7.5 cm H(2)O) and functional profile length (mean difference 1.8 mm). There were wide 95% limits of agreement for differences in maximum urethral closure <span class="hlt">pressure</span> at rest (-24.1 to 39 cm H(2)O) and functional profile length (-7.7 to 11.3 mm). For urethral <span class="hlt">pressure</span> measurement the <span class="hlt">air</span> charged catheter is at least as reliable as the microtip catheter and it generally gives higher readings. However, <span class="hlt">air</span> charged and microtip catheters cannot be used interchangeably for clinical purposes because of insufficient agreement. Hence, clinicians should be aware that <span class="hlt">air</span> charged and microtip catheters may yield completely different results, and these differences should be acknowledged during clinical decision making.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25625652','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25625652"><span>Prenatal <span class="hlt">air</span> pollution exposure and newborn blood <span class="hlt">pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>van Rossem, Lenie; Rifas-Shiman, Sheryl L; Melly, Steven J; Kloog, Itai; Luttmann-Gibson, Heike; Zanobetti, Antonella; Coull, Brent A; Schwartz, Joel D; Mittleman, Murray A; Oken, Emily; Gillman, Matthew W; Koutrakis, Petros; Gold, Diane R</p> <p>2015-04-01</p> <p><span class="hlt">Air</span> pollution exposure has been associated with increased blood <span class="hlt">pressure</span> in adults. We examined associations of antenatal exposure to ambient <span class="hlt">air</span> pollution with newborn systolic blood <span class="hlt">pressure</span> (SBP). We studied 1,131 mother-infant pairs in a Boston, Massachusetts, area pre-birth cohort. We calculated average exposures by trimester and during the 2 to 90 days before birth for temporally resolved fine particulate matter (≤ 2.5 μm; PM2.5), black carbon (BC), nitrogen oxides, nitrogen dioxide, ozone (O3), and carbon monoxide measured at stationary monitoring sites, and for spatiotemporally resolved estimates of PM2.5 and BC at the residence level. We measured SBP at a mean age of 30 ± 18 hr with an automated device. We used mixed-effects models to examine associations between <span class="hlt">air</span> pollutant exposures and SBP, taking into account measurement circumstances; child's birth weight; mother's age, race/ethnicity, socioeconomic position, and third-trimester BP; and time trend. Estimates represent differences in SBP associated with an interquartile range (IQR) increase in each pollutant. Higher mean PM2.5 and BC exposures during the third trimester were associated with higher SBP (e.g., 1.0 mmHg; 95% CI: 0.1, 1.8 for a 0.32-μg/m3 increase in mean 90-day residential BC). In contrast, O3 was negatively associated with SBP (e.g., -2.3 mmHg; 95% CI: -4.4, -0.2 for a 13.5-ppb increase during the 90 days before birth). Exposures to PM2.5 and BC in late pregnancy were positively associated with newborn SBP, whereas O3 was negatively associated with SBP. Longitudinal follow-up will enable us to assess the implications of these findings for health during later childhood and adulthood.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_21 --> <div id="page_22" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="421"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013OptFT..19...83H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013OptFT..19...83H"><span>Micro-controller based <span class="hlt">air</span> <span class="hlt">pressure</span> monitoring instrumentation system using optical fibers as sensor</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hazarika, D.; Pegu, D. S.</p> <p>2013-03-01</p> <p>This paper describes a micro-controller based instrumentation system to monitor <span class="hlt">air</span> <span class="hlt">pressure</span> using optical fiber sensors. The principle of macrobending is used to develop the sensor system. The instrumentation system consists of a laser source, a beam splitter, two multi mode optical fibers, two Light Dependent Resistance (LDR) based timer circuits and a AT89S8252 micro-controller. The beam splitter is used to divide the laser beam into two parts and then these two beams are launched into two multi mode fibers. One of the multi mode fibers is used as the sensor fiber and the other one is used as the reference fiber. The use of the reference fiber is to eliminate the environmental effects while measuring the <span class="hlt">air</span> <span class="hlt">pressure</span> magnitude. The laser beams from the sensor and reference fibers are applied to two identical LDR based timer circuits. The LDR based timer circuits are interfaced to a micro-controller through its counter pins. The micro-controller samples the frequencies of the timer circuits using its counter-0 and counter-1 and the counter values are then processed to provide the measure of <span class="hlt">air</span> <span class="hlt">pressure</span> magnitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/70035760','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/70035760"><span><span class="hlt">Air-dropped</span> sensor network for real-time high-fidelity volcano monitoring</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Song, W.-Z.; Huang, R.; Xu, M.; Ma, A.; Shirazi, B.; LaHusen, R.</p> <p>2009-01-01</p> <p>This paper presents the design and deployment experience of an <span class="hlt">air-dropped</span> wireless sensor network for volcano hazard monitoring. The deployment of five stations into the rugged crater of Mount St. Helens only took one hour with a helicopter. The stations communicate with each other through an amplified 802.15.4 radio and establish a self-forming and self-healing multi-hop wireless network. The distance between stations is up to 2 km. Each sensor station collects and delivers real-time continuous seismic, infrasonic, lightning, GPS raw data to a gateway. The main contribution of this paper is the design and evaluation of a robust sensor network to replace data loggers and provide real-time long-term volcano monitoring. The system supports UTC-time synchronized data acquisition with 1ms accuracy, and is online configurable. It has been tested in the lab environment, the outdoor campus and the volcano crater. Despite the heavy rain, snow, and ice as well as gusts exceeding 120 miles per hour, the sensor network has achieved a remarkable packet delivery ratio above 99% with an overall system uptime of about 93.8% over the 1.5 months evaluation period after deployment. Our initial deployment experiences with the system have alleviated the doubts of domain scientists and prove to them that a low-cost sensor network system can support real-time monitoring in extremely harsh environments. Copyright 2009 ACM.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.925a2006B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.925a2006B"><span>Fluid flow inside and outside an evaporating sessile <span class="hlt">drop</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bouchenna, C.; Aitsaada, M.; Chikh, S.; Tadrist, L.</p> <p>2017-11-01</p> <p>The sessile <span class="hlt">drop</span> evaporation is a phenomena which is extensively studied in the literature, but the governing effects are far from being well understood especially those involving movements taking place in both liquid and gas phases. The present work numerically studies the flow within and around an evaporating sessile <span class="hlt">drop</span>. The flow is induced by the strong mass loss at contact line, the thermo-capillary effect and the buoyancy effect in the surrounding <span class="hlt">air</span>. The results showed that buoyancy-induced flow in gas phase weakly influences thermo-capillarity-induced flow in the liquid phase. Buoyancy effect can strongly modify the temperature distribution at liquid-gas interface and thus the overall evaporation rate of the <span class="hlt">drop</span> when the substrate is heated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130011132','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130011132"><span>Analysis of an Aircraft Honeycomb Sandwich Panel with Circular Face Sheet/Core Disbond Subjected to Ground-<span class="hlt">Air</span> <span class="hlt">Pressurization</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rinker, Martin; Krueger, Ronald; Ratcliffe, James</p> <p>2013-01-01</p> <p>The ground-<span class="hlt">air</span> <span class="hlt">pressurization</span> of lightweight honeycomb sandwich structures caused by alternating <span class="hlt">pressure</span> differences between the enclosed <span class="hlt">air</span> within the honeycomb core and the ambient environment is a well-known and controllable loading condition of aerospace structures. However, initial face sheet/core disbonds intensify the face sheet peeling effect of the internal <span class="hlt">pressure</span> load significantly and can decrease the reliability of the sandwich structure drastically. Within this paper, a numerical parameter study was carried out to investigate the criticality of initial disbonds in honeycomb sandwich structures under ground-<span class="hlt">air</span> <span class="hlt">pressurization</span>. A fracture mechanics approach was used to evaluate the loading at the disbond front. In this case, the strain energy release rate was computed via the Virtual Crack Closure Technique. Special attention was paid to the <span class="hlt">pressure</span>-deformation coupling which can decrease the <span class="hlt">pressure</span> load within the disbonded sandwich section significantly when the structure is highly deformed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/863741','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/863741"><span><span class="hlt">Air</span> ejector augmented compressed <span class="hlt">air</span> energy storage system</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Ahrens, Frederick W.; Kartsounes, George T.</p> <p>1980-01-01</p> <p>Energy is stored in slack demand periods by charging a plurality of underground reservoirs with <span class="hlt">air</span> to the same peak storage <span class="hlt">pressure</span>, during peak demand periods throttling the <span class="hlt">air</span> from one storage reservoir into a gas turbine system at a constant inlet <span class="hlt">pressure</span> until the <span class="hlt">air</span> <span class="hlt">pressure</span> in the reservoir falls to said constant inlet <span class="hlt">pressure</span>, thereupon permitting <span class="hlt">air</span> in a second reservoir to flow into said gas turbine system while drawing <span class="hlt">air</span> from the first reservoir through a variable geometry <span class="hlt">air</span> ejector and adjusting said variable geometry <span class="hlt">air</span> ejector, said <span class="hlt">air</span> flow being essentially at the constant inlet <span class="hlt">pressure</span> of the gas turbine system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27579835','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27579835"><span>A Preliminary Investigation of the <span class="hlt">Air</span>-Bone Gap: Changes in Intracochlear Sound <span class="hlt">Pressure</span> With <span class="hlt">Air</span>- and Bone-conducted Stimuli After Cochlear Implantation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Banakis Hartl, Renee M; Mattingly, Jameson K; Greene, Nathaniel T; Jenkins, Herman A; Cass, Stephen P; Tollin, Daniel J</p> <p>2016-10-01</p> <p>A cochlear implant electrode within the cochlea contributes to the <span class="hlt">air</span>-bone gap (ABG) component of postoperative changes in residual hearing after electrode insertion. Preservation of residual hearing after cochlear implantation has gained importance as simultaneous electric-acoustic stimulation allows for improved speech outcomes. Postoperative loss of residual hearing has previously been attributed to sensorineural changes; however, presence of increased postoperative ABG remains unexplained and could result in part from altered cochlear mechanics. Here, we sought to investigate changes to these mechanics via intracochlear <span class="hlt">pressure</span> measurements before and after electrode implantation to quantify the contribution to postoperative ABG. Human cadaveric heads were implanted with titanium fixtures for bone conduction transducers. Velocities of stapes capitulum and cochlear promontory between the two windows were measured using single-axis laser Doppler vibrometry and fiber-optic sensors measured intracochlear <span class="hlt">pressures</span> in scala vestibuli and tympani for <span class="hlt">air</span>- and bone-conducted stimuli before and after cochlear implant electrode insertion through the round window. Intracochlear <span class="hlt">pressures</span> revealed only slightly reduced responses to <span class="hlt">air</span>-conducted stimuli consistent with previous literature. No significant changes were noted to bone-conducted stimuli after implantation. Velocities of the stapes capitulum and the cochlear promontory to both stimuli were stable after electrode placement. Presence of a cochlear implant electrode causes alterations in intracochlear sound <span class="hlt">pressure</span> levels to <span class="hlt">air</span>, but not bone, conducted stimuli and helps to explain changes in residual hearing noted clinically. These results suggest the possibility of a cochlear conductive component to postoperative changes in hearing sensitivity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19790015294&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19790015294&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dair%2Bpressure"><span><span class="hlt">Air</span> <span class="hlt">pressure</span> measurement</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ballard, H. N.</p> <p>1978-01-01</p> <p>The <span class="hlt">pressure</span> measurement was made by a Model 830J Rosemont sensor which utilized the principle of a changing <span class="hlt">pressure</span> to change correspondingly the capacitance of the <span class="hlt">pressure</span> sensitive element. The sensor's range was stated to be from zero to 100 Torr (14 km); however, the sensor was not activated until an altitude of 20 km (41 Torr) was reached during the balloon ascent. The resolution of the sensor was specified by the manufacturer as infinitesimal; however, associated electronic and <span class="hlt">pressure</span> readout systems limit the resolution to .044 Torr. Thus in the vicinity of an altitude of 30 km the <span class="hlt">pressure</span> resolution corresponded to an altitude resolution of approximately 33 meters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005PhFl...17j0606K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005PhFl...17j0606K"><span>Characterization of surface roughness effects on <span class="hlt">pressure</span> <span class="hlt">drop</span> in single-phase flow in minichannels</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kandlikar, Satish G.; Schmitt, Derek; Carrano, Andres L.; Taylor, James B.</p> <p>2005-10-01</p> <p>Roughness features on the walls of a channel wall affect the <span class="hlt">pressure</span> <span class="hlt">drop</span> of a fluid flowing through that channel. This roughness effect can be described by (i) flow area constriction and (ii) increase in the wall shear stress. Replotting the Moody's friction factor chart with the constricted flow diameter results in a simplified plot and yields a single asymptotic value of friction factor for relative roughness values of ɛ /D>0.03 in the fully developed turbulent region. After reviewing the literature, three new roughness parameters are proposed (maximum profile peak height Rp, mean spacing of profile irregularities RSm, and floor distance to mean line Fp). Three additional parameters are presented to consider the localized hydraulic diameter variation (maximum, minimum, and average) in future work. The roughness ɛ is then defined as Rp+Fp. This definition yields the same value of roughness as obtained from the sand-grain roughness [H. Darcy, Recherches Experimentales Relatives au Mouvement de L'Eau dans les Tuyaux (Mallet-Bachelier, Paris, France, 1857); J. T. Fanning, A Practical Treatise on Hydraulic and Water Supply Engineering (Van Nostrand, New York, 1877, revised ed. 1886); J. Nikuradse, "Laws of flow in rough pipes" ["Stromungsgesetze in Rauen Rohren," VDI-Forschungsheft 361 (1933)]; Beilage zu "Forschung auf dem Gebiete des Ingenieurwesens," Ausgabe B Band 4, English translation NACA Tech. Mem. 1292 (1937)]. Specific experiments are conducted using parallel sawtooth ridge elements, placed normal to the flow direction, in aligned and offset configurations in a 10.03mm wide rectangular channel with variable gap (resulting hydraulic diameters of 325μm-1819μm with Reynolds numbers ranging from 200 to 7200 for <span class="hlt">air</span> and 200 to 5700 for water). The use of constricted flow diameter extends the applicability of the laminar friction factor equations to relative roughness values (sawtooth height) up to 14%. In the turbulent region, the aligned and offset</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20222654','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20222654"><span>Determination of 1-octanol-<span class="hlt">air</span> partition coefficient using gaseous diffusion in the <span class="hlt">air</span> boundary layer.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ha, Yeonjeong; Kwon, Jung-Hwan</p> <p>2010-04-15</p> <p>Exact determination of the partition coefficient between 1-octanol and <span class="hlt">air</span> (K(OA)) is very important because it is a key descriptor for describing the thermodynamic partitioning between the <span class="hlt">air</span> and organic phases. In spite of its importance, the number and quality of experimental K(OA) values for hydrophobic organic chemicals are limited because of experimental difficulties. Thus, to measure K(OA) values, a high-throughput method was developed that used liquid-phase extraction with 1-octanol <span class="hlt">drop</span> at the tip of a microsyringe needle. The concentration in the headspace surrounding the 1 muL octanol <span class="hlt">drop</span> was equilibrated with liquid octanol containing polycyclic aromatic hydrocarbons (PAHs). The change in concentrations of PAHs in the octanol <span class="hlt">drop</span> was measured to obtain mass transfer rate constants, and these rate constants were then converted into K(OA) values using a film diffusion model. Thirteen polycyclic aromatic hydrocarbons with log K(OA) between 5 and 12 were chosen for the proof of the principle. Experimental determination of log K(OA) was accomplished in 30 h for PAHs with their log K(OA) less than 11. The measured log K(OA) values were very close to those obtained by various experimental and estimation methods in the literature, suggesting that this new method can provide a fast and easy determination of log K(OA) values for many chemicals of environmental interests. In addition, the applicability of the method can be extended to determine Henry's law constant for compounds with low vapor <span class="hlt">pressure</span> and to estimate gaseous transfer rate of semivolatile compounds for environmental fate modeling.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/871473','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/871473"><span>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Sinha, Dipen N.</p> <p>1998-01-01</p> <p>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids. The present invention includes the use of two closely spaced transducers, or one transducer and a closely spaced reflector plate, to form an interferometer suitable for ultrasonic characterization of droplet-size and smaller samples without the need for a container. The droplet is held between the interferometer elements, whose distance apart may be adjusted, by surface tension. The surfaces of the interferometer elements may be readily cleansed by a stream of solvent followed by purified <span class="hlt">air</span> when it is desired to change samples. A single <span class="hlt">drop</span> of liquid is sufficient for high-quality measurement. Examples of samples which may be investigated using the apparatus and method of the present invention include biological specimens (tear <span class="hlt">drops</span>; blood and other body fluid samples; samples from tumors, tissues, and organs; secretions from tissues and organs; snake and bee venom, etc.) for diagnostic evaluation, samples in forensic investigations, and detection of drugs in small quantities.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/644439','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/644439"><span>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Sinha, D.N.</p> <p>1998-04-14</p> <p>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids is disclosed. The present invention includes the use of two closely spaced transducers, or one transducer and a closely spaced reflector plate, to form an interferometer suitable for ultrasonic characterization of droplet-size and smaller samples without the need for a container. The droplet is held between the interferometer elements, whose distance apart may be adjusted, by surface tension. The surfaces of the interferometer elements may be readily cleansed by a stream of solvent followed by purified <span class="hlt">air</span> when it is desired to change samples. A single <span class="hlt">drop</span> of liquid is sufficient for high-quality measurement. Examples of samples which may be investigated using the apparatus and method of the present invention include biological specimens (tear <span class="hlt">drops</span>; blood and other body fluid samples; samples from tumors, tissues, and organs; secretions from tissues and organs; snake and bee venom, etc.) for diagnostic evaluation, samples in forensic investigations, and detection of drugs in small quantities. 5 figs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/644439-ultrasonic-characterization-single-drops-liquids','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/644439-ultrasonic-characterization-single-drops-liquids"><span>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sinha, D.N.</p> <p></p> <p>Ultrasonic characterization of single <span class="hlt">drops</span> of liquids is disclosed. The present invention includes the use of two closely spaced transducers, or one transducer and a closely spaced reflector plate, to form an interferometer suitable for ultrasonic characterization of droplet-size and smaller samples without the need for a container. The droplet is held between the interferometer elements, whose distance apart may be adjusted, by surface tension. The surfaces of the interferometer elements may be readily cleansed by a stream of solvent followed by purified <span class="hlt">air</span> when it is desired to change samples. A single <span class="hlt">drop</span> of liquid is sufficient for high-qualitymore » measurement. Examples of samples which may be investigated using the apparatus and method of the present invention include biological specimens (tear <span class="hlt">drops</span>; blood and other body fluid samples; samples from tumors, tissues, and organs; secretions from tissues and organs; snake and bee venom, etc.) for diagnostic evaluation, samples in forensic investigations, and detection of drugs in small quantities. 5 figs.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MeScT..29f4002S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MeScT..29f4002S"><span>Measurement of the refractive index of <span class="hlt">air</span> in a low-<span class="hlt">pressure</span> regime and the applicability of traditional empirical formulae</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schödel, René; Walkov, Alexander; Voigt, Michael; Bartl, Guido</p> <p>2018-06-01</p> <p>The refractive index of <span class="hlt">air</span> is a major limiting factor in length measurements by interferometry, which are mostly performed under atmospheric conditions. Therefore, especially in the last century, measurement and description of the <span class="hlt">air</span> refractive index was a key point in order to achieve accuracy in the realisation of the length by interferometry. Nevertheless, interferometric length measurements performed in vacuum are much more accurate since the wavelength of the light is not affected by the <span class="hlt">air</span> refractive index. However, compared with thermal conditions in <span class="hlt">air</span>, in high vacuum heat conduction is missing. In such a situation, dependent on the radiative thermal equilibrium, a temperature distribution can be very inhomogeneous. Using a so-called contact gas instead of high vacuum is a very effective way to enable heat conduction on nearly the same level as under atmospheric <span class="hlt">pressure</span> conditions whereby keeping the effect of the <span class="hlt">air</span> refractive index on a small level. As physics predicts, and as we have demonstrated previously, helium seems like the optimal contact gas because of its large heat conduction and its refractive index that can be calculated from precisely known parameters. On the other hand, helium gas situated in a vacuum chamber could easily be contaminated, e.g. by <span class="hlt">air</span> leakage from outside. Above the boiling point of oxygen (‑183 °C) it is therefore beneficial to use dry <span class="hlt">air</span> as a contact gas. In such an approach, the <span class="hlt">air</span> refractive index could be calculated based on measured quantities for <span class="hlt">pressure</span> and temperature. However, existing formulas for the <span class="hlt">air</span> refractive index are not valid in the low-<span class="hlt">pressure</span> regime. Although it seems reasonable that the refractivity (n  ‑  1) of dry <span class="hlt">air</span> simply downscales with the <span class="hlt">pressure</span>, to our knowledge there is no experimental evidence for the applicability of any empirical formula. This evidence is given in the present paper which reports on highly accurate measurements of the <span class="hlt">air</span> refractive index for the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4704731','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4704731"><span>Effect of Different Levels of <span class="hlt">Pressure</span> Relieving <span class="hlt">Air</span>-Mattress Firmness on Cough Strength</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Kamikawa, Norimichi; Taito, Shunsuke; Takahashi, Makoto; Sekikawa, Kiyokazu; Hamada, Hironobu</p> <p>2016-01-01</p> <p>Cough is an important host-defense mechanism. The elderly and patients who are severely ill cannot cough effectively when lying in the supine position. Furthermore, <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattresses are recommended for preventing the development of <span class="hlt">pressure</span> ulcers. In this study, we clarified whether or not the cough peak flow (CPF), an index of cough strength, is affected by different firmness levels of a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress in healthy volunteers in the supine position. Fifty-two healthy young men participated. All the measurements were carried out on each participant in the supine position on a <span class="hlt">pressure</span> relieving <span class="hlt">air</span>-mattress. The participants were assessed at two firmness levels, a “hard” and “soft” mode. The CPF, forced vital capacity (FVC), maximal expiratory <span class="hlt">pressure</span> (PEmax), and maximal inspiratory <span class="hlt">pressure</span> (PImax) were determined for each mode. The sinking distance of the body into the mattress was measured without any activity and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax, and PImax were determined for each mode. The sinking distance of the body into the mattress was measured and the difference between the sinking distances of the two firmness levels was determined. The CPF, FVC, PEmax and PImax values of the participants coughing on the mattress were significantly lower when the mattress was in “soft” than in “hard” mode. The differences between the sinking distances of the mattress in “soft” and “hard” modes were larger for the anterior superior iliac spine. A harder mattress may lead to increased CPF in healthy young men lying in the supine position, and increased CPF may be important for host defense. PMID:26741497</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1893c0088S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1893c0088S"><span>Multi-hole <span class="hlt">pressure</span> probes to wind tunnel experiments and <span class="hlt">air</span> data systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shevchenko, A. M.; Shmakov, A. S.</p> <p>2017-10-01</p> <p>The problems to develop a multihole <span class="hlt">pressure</span> system to measure flow angularity, Mach number and dynamic head for wind tunnel experiments or <span class="hlt">air</span> data systems are discussed. A simple analytical model with separation of variables is derived for the multihole spherical <span class="hlt">pressure</span> probe. The proposed model is uniform for small subsonic and supersonic speeds. An error analysis was performed. The error functions are obtained, allowing to estimate the influence of the Mach number, the pitch angle, the location of the <span class="hlt">pressure</span> ports on the uncertainty of determining the flow parameters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/3657482','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/3657482"><span><span class="hlt">Drop</span> jumping. II. The influence of <span class="hlt">dropping</span> height on the biomechanics of <span class="hlt">drop</span> jumping.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bobbert, M F; Huijing, P A; van Ingen Schenau, G J</p> <p>1987-08-01</p> <p>In the literature, athletes preparing for explosive activities are recommended to include <span class="hlt">drop</span> jumping in their training programs. For the execution of <span class="hlt">drop</span> jumps, different techniques and different <span class="hlt">dropping</span> heights can be used. This study was designed to investigate for the performance of bounce <span class="hlt">drop</span> jumps the influence of <span class="hlt">dropping</span> height on the biomechanics of the jumps. Six subjects executed bounce <span class="hlt">drop</span> jumps from heights of 20 cm (designated here as DJ20), 40 cm (designated here as DJ40), and 60 cm (designated here as DJ60). During jumping, they were filmed, and ground reaction forces were recorded. The results of a biomechanical analysis show no difference between DJ20 and DJ40 in mechanical output about the joints during the push-off phase. Peak values of moment and power output about the ankles during the push-off phase were found to be smaller in DJ60 than in DJ40 (DJ20 = DJ60). The amplitude of joint reaction forces increased with <span class="hlt">dropping</span> height. During DJ60, the net joint reaction forces showed a sharp peak on the instant that the heels came down on the ground. Based on the results, researchers are advised to limit <span class="hlt">dropping</span> height to 20 or 40 cm when investigating training effects of the execution of bounce <span class="hlt">drop</span> jumps.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19880009190','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19880009190"><span>Three-dimensional trajectory analyses of two <span class="hlt">drop</span> sizing instruments: PMS OAP and PMS FSSP</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Norment, Hillyer G.</p> <p>1988-01-01</p> <p>Flow induced distortions of water <span class="hlt">drop</span> fluxes and speeds seen by the instruments were predicted by use of three dimensional flow and trajectory calculation methods. Sensitivities were determined for the instruments, in isolation and mounted under the wing of an airplane, to: water <span class="hlt">drop</span> diameter (2 to 1000 microns), angle of attack and free stream <span class="hlt">air</span> speed. For the optical array probe in isolation and on the airplane at 0 deg angle of attack, flux distortions of practical consequence are not found. At 4 deg airplane angle of attack, partial flow stagnation under the uptilted wing causes significant decreases in both flux and speed for cloud size droplets. For the forward scattering spectrometer probe in isolation, only marginally significant sensitivities to free stream <span class="hlt">air</span> speed are found, and no sensitivity is found to angle of attack. Both speed and flux of cloud size droplets are predicted to be undermeasured by from 12 to 24 percent depending on airplane angle of attack. For the wing-mounted instruments, effects of flow about the instruments themselves are found to be equal in importance to effects of flow about the airplane. Preferred orientation (canting) angles of distorted water <span class="hlt">drops</span> are found to be functions of <span class="hlt">drop</span> size, angle of attack and <span class="hlt">air</span> speed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=128602&Lab=NRMRL&keyword=investment+AND+management&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50','EPA-EIMS'); return false;" href="https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=128602&Lab=NRMRL&keyword=investment+AND+management&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50"><span>SOIL-<span class="hlt">AIR</span> PERMEABILITY MEASUREMENT WITH A TRANSIENT <span class="hlt">PRESSURE</span> BUILDUP METHOD</span></a></p> <p><a target="_blank" href="http://oaspub.epa.gov/eims/query.page">EPA Science Inventory</a></p> <p></p> <p></p> <p>An analytical solution for transient <span class="hlt">pressure</span> change in a single venting well was derived from mass conservation of <span class="hlt">air</span>, Darcy's law of flow in porous media, and the ideal gas law equation of state. Slopes of plots of Pw2 against ln (t+Δt)/Δt similar to Homer's plot were used to ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890032478&hterms=Acoustic+levitation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DAcoustic%2Blevitation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890032478&hterms=Acoustic+levitation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DAcoustic%2Blevitation"><span>Acoustic measurement of the surface tension of levitated <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Trinh, E. H.; Marston, P. L.; Robey, J. L.</p> <p>1988-01-01</p> <p>The measurement of the frequency of the fundamental mode of shape oscillation of acoustically levitated <span class="hlt">drops</span> has been carried out to determine the surface tension of the <span class="hlt">drop</span> material. Sound fields of about 20 kHz in frequency allow the suspension of <span class="hlt">drops</span> a few millimeters in size, as well as the necessary drive for oscillations. The surface tension of water, hexadecane, silicone oil, and aqueous solutions of glycerin levitated in <span class="hlt">air</span> has been measured, and the results have been compared with those obtained with standard ring tensiometry. The two sets of data are in good agreement, the largest discrepancy being about 10 percent. Uncertainties in the effects of the nonspherical static shape of <span class="hlt">drops</span> levitated in the earth's gravitational field and the rotation state of the sample are the major contributors to the experimental error. A decrease of the resonance frequency of the fundamental mode indicates a soft nonlinearity as the oscillation amplitude increases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20815439','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20815439"><span>A micro-machined piezoelectric flexural-mode hydrophone with <span class="hlt">air</span> backing: a hydrostatic <span class="hlt">pressure</span>-balancing mechanism for integrity preservation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Choi, Sungjoon; Lee, Haksue; Moon, Wonkyu</p> <p>2010-09-01</p> <p>Although an <span class="hlt">air</span>-backed thin plate is an effective sound receiver structure, it is easily damaged via <span class="hlt">pressure</span> unbalance caused by external hydrostatic <span class="hlt">pressure</span>. To overcome this difficulty, a simple <span class="hlt">pressure</span>-balancing module is proposed. Despite its small size and relative simplicity, with proper design and operation, micro-channel structure provides a solution to the <span class="hlt">pressure</span>-balancing problem. If the channel size is sufficiently small, the gas-liquid interface may move back and forth without breach by the hydrostatic <span class="hlt">pressure</span> since the surface tension can retain the interface surface continuously. One input port of the device is opened to an intermediate liquid, while the other port is connected to the <span class="hlt">air</span>-backing chamber. As the hydrostatic <span class="hlt">pressure</span> increases, the liquid in the micro-channel compresses the <span class="hlt">air</span>, and the <span class="hlt">pressure</span> in the backing chamber is then equalized to match the external hydrostatic <span class="hlt">pressure</span>. To validate the performance of the proposed mechanism, a micro-channel prototype is designed and integrated with the piezoelectric micro-machined flexural sensor developed in our previous work. The working principle of the mechanism is experimentally verified. In addition, the effect of hydrostatic <span class="hlt">pressure</span> on receiving sensitivity is evaluated and compared with predicted behavior.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_22 --> <div id="page_23" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="441"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1159352','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1159352"><span>Low-Flow Liquid Desiccant <span class="hlt">Air</span> Conditioning: General Guidance and Site Considerations</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kozubal, E.; Herrmann, L.; Deru, M.</p> <p>2014-09-01</p> <p>Dehumidification or latent cooling in buildings is an area of growing interest that has been identified as needing more research and improved technologies for higher performance. Heating, ventilating, and <span class="hlt">air</span>-conditioning (HVAC) systems typically expend excessive energy by using overcool-and-reheat strategies to dehumidify buildings. These systems first overcool ventilation <span class="hlt">air</span> to remove moisture and then reheat the <span class="hlt">air</span> to meet comfort requirements. Another common strategy incorporates solid desiccant rotors that remove moisture from the <span class="hlt">air</span> more efficiently; however, these systems increase fan energy consumption because of the high airside <span class="hlt">pressure</span> <span class="hlt">drop</span> of solid desiccant rotors and can add heat of absorptionmore » to the ventilation <span class="hlt">air</span>. Alternatively, liquid desiccant <span class="hlt">air</span>-conditioning (LDAC) technology provides an innovative dehumidification solution that: (1) eliminates the need for overcooling and reheating from traditional cooling systems; and (2) avoids the increased fan energy and <span class="hlt">air</span> heating from solid desiccant rotor systems.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA513823','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA513823"><span>Lighter-Than-<span class="hlt">Air</span> and <span class="hlt">Pressurized</span> Structures Technology for Unmanned Aerial Vehicles (UAVs)</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2010-01-01</p> <p>through lighter-than-<span class="hlt">air</span> or <span class="hlt">pressurized</span> structures-based ( PSB ) technologies. Basically, we examined how to construct the UAV in such a way that a...considerable percentage of its weight will be supported by or composed of inflatable structures containing <span class="hlt">air</span> or helium. In this way, PSB technology...will reduce the amount of energy required to keep the UAV aloft, thus allowing the use of smaller, slower, and quieter motors. Using PSB technology</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/4627496-adiabatic-dispersed-two-phase-flow-further-results-influence-physical-properties-pressure-drop-film-thickness-topical-report','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/4627496-adiabatic-dispersed-two-phase-flow-further-results-influence-physical-properties-pressure-drop-film-thickness-topical-report"><span>ADIABATIC DISPERSED TWO-PHASE FLOW: FURTHER RESULTS ON THE INFLUENCE OF PHYSICAL PROPERTIES ON <span class="hlt">PRESSURE</span> <span class="hlt">DROP</span> AND FILM THICKNESS. Topical Report No. 6</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Casagrande, I.; Cravarolo, L.; Hassid, A.</p> <p>1963-05-01</p> <p>A discussion is given of the experimental data obtained at CISE on two- phase adiabatic flow under the following conditions: vertical upward (dispersed regime) flow; circular conduit (15 to 25 mm diameter); gaseous phase argon or nitrogen; liquid phase water or ethyl alcohol-water solution (,90% by wt. of alcohol); gas fiow rate of 15 to 82 g/ cm/sup 2/; liquid flow rate of 20 to 208 g/ cm/sup 2/ sec; temperature of 18 to 20 deg C; <span class="hlt">pressure</span> of up to approximates 22 kg/cm/sup 2/. The measured quantities are <span class="hlt">pressure</span> <span class="hlt">drop</span> and liquid film thickness on the wall of themore » conduit. The <span class="hlt">pressure</span> loss and film flow rate are evaluated. The experimental data are discussed and the influence of surface tension and gas and liquid viscosity investigated. A simple relationship for the <span class="hlt">pressure</span> loss over a wide range of experimental conditions in adiabatic dispersed regime is given. (auth)« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://medlineplus.gov/ency/article/007278.htm','NIH-MEDLINEPLUS'); return false;" href="https://medlineplus.gov/ency/article/007278.htm"><span>Low blood <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://medlineplus.gov/">MedlinePlus</a></p> <p></p> <p></p> <p>Hypotension; Blood <span class="hlt">pressure</span> - low; Postprandial hypotension; Orthostatic hypotension; Neurally mediated hypotension; NMH ... Blood <span class="hlt">pressure</span> varies from one person to another. A <span class="hlt">drop</span> as little as 20 mmHg, can cause ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810013600','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810013600"><span>Investigation of <span class="hlt">air</span> solubility in jet A fuel at high <span class="hlt">pressures</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rupprecht, S. D.; Faeth, G. M.</p> <p>1981-01-01</p> <p>The solubility and density properties of saturated mixtures of fuels and gases were measured. The fuels consisted of Jet A and dodecane, the gases were <span class="hlt">air</span> and nitrogen. The test range included <span class="hlt">pressures</span> of 1.03 to 10.34 MPa and temperatures of 298 to 373 K. The results were correlated successfully, using the Soave equation of state. Over this test range, dissolved gas concentrations were roughly proportional to <span class="hlt">pressure</span> and increased slightly with increasing temperature. Mixture density was relatively independent of dissolved gas concentration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009TePhL..35.1012K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009TePhL..35.1012K"><span>Generation of subnanosecond electron beams in <span class="hlt">air</span> at atmospheric <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kostyrya, I. D.; Tarasenko, V. F.; Baksht, E. Kh.; Burachenko, A. G.; Lomaev, M. I.; Rybka, D. V.</p> <p>2009-11-01</p> <p>Optimum conditions for the generation of runaway electron beams with maximum current amplitudes and densities in nanosecond pulsed discharges in <span class="hlt">air</span> at atmospheric <span class="hlt">pressure</span> are determined. A supershort avalanche electron beam (SAEB) with a current amplitude of ˜30 A, a current density of ˜20 A/cm2, and a pulse full width at half maximum (FWHM) of ˜100 ps has been observed behind the output foil of an <span class="hlt">air</span>-filled diode. It is shown that the position of the SAEB current maximum relative to the voltage pulse front exhibits a time shift that varies when the small-size collector is moved over the foil surface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS.955a2002D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS.955a2002D"><span>The study of the effects of sea-spray <span class="hlt">drops</span> on the marine atmospheric boundary layer by direct numerical simulation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Druzhinin, O.; Troitskaya, Yu; Zilitinkevich, S.</p> <p>2018-01-01</p> <p>The detailed knowledge of turbulent exchange processes occurring in the atmospheric marine boundary layer are of primary importance for their correct parameterization in large-scale prognostic models. These processes are complicated, especially at sufficiently strong wind forcing conditions, by the presence of sea-spray <span class="hlt">drops</span> which are torn off the crests of sufficiently steep surface waves by the wind gusts. Natural observations indicate that mass fraction of sea-spray <span class="hlt">drops</span> increases with wind speed and their impact on the dynamics of the <span class="hlt">air</span> in the vicinity of the sea surface can become quite significant. Field experiments, however, are limited by insufficient accuracy of the acquired data and are in general costly and difficult. Laboratory modeling presents another route to investigate the spray-mediated exchange processes in much more detail as compared to the natural experiments. However, laboratory measurements, contact as well as Particle Image Velocimetry (PIV) methods, also suffer from inability to resolve the dynamics of the near-surface <span class="hlt">air</span>-flow, especially in the surface wave troughs. In this report, we present a first attempt to use Direct Numerical Simulation (DNS) as tool for investigation of the <span class="hlt">drops</span>-mediated momentum, heat and moisture transfer in a turbulent, droplet-laden <span class="hlt">air</span> flow over a wavy water surface. DNS is capable of resolving the details of the transfer processes and do not involve any closure assumptions typical of Large-Eddy and Reynolds Averaged Navier-Stokes (LES and RANS) simulations. Thus DNS provides a basis for improving parameterizations in LES and RANS closure models and further development of large-scale prognostic models. In particular, we discuss numerical results showing the details of the modification of the <span class="hlt">air</span> flow velocity, temperature and relative humidity fields by multidisperse, evaporating <span class="hlt">drops</span>. We use Eulerian-Lagrangian approach where the equations for the <span class="hlt">air</span>-flow fields are solved in a Eulerian frame whereas</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950007192','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950007192"><span><span class="hlt">Pressure</span> measurements of a three wave journal <span class="hlt">air</span> bearing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dimofte, Florin; Addy, Harold E., Jr.</p> <p>1994-01-01</p> <p>In order to validate theoretical predictions of a wave journal bearing concept, a bench test rig was assembled at NASA Lewis Research Center to measure the steady-state performance of a journal <span class="hlt">air</span> bearing. The tester can run up to 30,000 RPM and the spindle has a run out of less than 1 micron. A three wave journal bearing (50 mm diameter and 58 mm length) has been machined at NASA Lewis. The <span class="hlt">pressures</span> at 16 ports along the bearing circumference at the middle of the bearing length were measured and compared to the theoretical prediction. The bearing ran at speeds up to 15,000 RPM and certain loads. Good agreement was found between the measured and calculated <span class="hlt">pressures</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920041111&hterms=Sound+levitation&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DSound%2Blevitation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920041111&hterms=Sound+levitation&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DSound%2Blevitation"><span>The behavior of a liquid <span class="hlt">drop</span> levitated and drastically flattened by an intense sound field</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lee, C. P.; Anilkumar, A. V.; Wang, Taylor G.</p> <p>1992-01-01</p> <p>The deformation and break-up are studied of a liquid <span class="hlt">drop</span> in levitation through the radiation <span class="hlt">pressure</span>. Using high-speed photography ripples are observed on the central membrane of the <span class="hlt">drop</span>, atomization of the membrane by emission of satellite <span class="hlt">drops</span> from its unstable ripples, and shattering of the <span class="hlt">drop</span> after upward buckling like an umbrella, or after horizontal expansion like a sheet. These effects are captured on video. The ripples are theorized to be capillary waves generated by the Faraday instability excited by the sound vibration. Atomization occurs whenever the membrane becomes so thin that the vibration is sufficiently intense. The vibration leads to a destabilizing Bernoulli correction in the static <span class="hlt">pressure</span>. Buckling occurs when an existent equilibrium is unstable to a radial (i.e., tangential) motion of the membrane because of the Bernoulli effect. Besides, the radiation stress at the rim of the <span class="hlt">drop</span> is a suction stress which can make equilibrium impossible, leading to the horizontal expansion and the subsequent break-up.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21246066','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21246066"><span>Effect of cleaning methods after reduced-<span class="hlt">pressure</span> <span class="hlt">air</span> abrasion on bonding to zirconia ceramic.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Attia, Ahmed; Kern, Matthias</p> <p>2011-12-01</p> <p>To evaluate in vitro the influence of different cleaning methods after low-<span class="hlt">pressure</span> <span class="hlt">air</span> abrasion on the bond strength of a phosphate monomer-containing luting resin to zirconia ceramic. A total of 112 zirconia ceramic disks were divided into 7 groups (n = 16). In the test groups, disks were <span class="hlt">air</span> abraded at low <span class="hlt">pressure</span> (L) 0.05 MPa using 50-μm alumina particles. Prior to bonding, the disks were ultrasonically (U) cleaned either in isopropanol alcohol (AC), hydrofluoric acid (HF), demineralized water (DW), or tap water (TW), or they were used without ultrasonic cleaning. Disks <span class="hlt">air</span> abraded at a high (H) <span class="hlt">pressure</span> of 0.25 MPa and cleaned ultrasonically in isopropanol served as positive control; original (O) milled disks used without <span class="hlt">air</span> abrasion served as the negative control group. Plexiglas tubes filled with composite resin were bonded with the adhesive luting resin Panavia 21 to the ceramic disks. Prior to testing tensile bond strength (TBS), each main group was further subdivided into 2 subgroups (n=8) which were stored in distilled water either at 37°C for 3 days or for 30 days with 7500 thermal cycles. Statistical analyses were conducted with two- and one-way analyses of variance (ANOVA) and Tukey's HSD test. Initial tensile bond strength (TBS) ranged from 32.6 to 42.8 MPa. After 30 days storage in water with thermocycling, TBS ranged from 21.9 to 36.3 MPa. Storage in water and thermocycling significantly decreased the TBS of test groups which were not <span class="hlt">air</span> abraded (p = 0.05) or which were <span class="hlt">air</span> abraded but cleaned in tap water (p = 0.002), but not the TBS of the other groups (p > 0.05). Also, the TBS of <span class="hlt">air</span>-abraded groups were significantly higher than the TBS of the original milled (p < 0.01). Cleaning procedures did not significantly affect TBS either after 3 days or 30 days storage in water and thermocycling (p > 0.05). <span class="hlt">Air</span> abrasion at 0.05 MPa and ultrasonic cleaning are important factors for improving bonding to zirconia ceramic.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5502603','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5502603"><span>Heat exchange between a bouncing <span class="hlt">drop</span> and a superhydrophobic substrate</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Shiri, Samira; Bird, James C.</p> <p>2017-01-01</p> <p>The ability to enhance or limit heat transfer between a surface and impacting <span class="hlt">drops</span> is important in applications ranging from industrial spray cooling to the thermal regulation of animals in cold rain. When these surfaces are micro/nanotextured and hydrophobic, or superhydrophobic, an impacting <span class="hlt">drop</span> can spread and recoil over trapped <span class="hlt">air</span> pockets so quickly that it can completely bounce off the surface. It is expected that this short contact time limits heat transfer; however, the amount of heat exchanged and precise role of various parameters, such as the <span class="hlt">drop</span> size, are unknown. Here, we demonstrate that the amount of heat exchanged between a millimeter-sized water <span class="hlt">drop</span> and a superhydrophobic surface will be orders of magnitude less when the <span class="hlt">drop</span> bounces than when it sticks. Through a combination of experiments and theory, we show that the heat transfer process on superhydrophobic surfaces is independent of the trapped gas. Instead, we find that, for a given spreading factor, the small fraction of heat transferred is controlled by two dimensionless groupings of physical parameters: one that relates the thermal properties of the <span class="hlt">drop</span> and bulk substrate and the other that characterizes the relative thermal, inertial, and capillary dynamics of the <span class="hlt">drop</span>. PMID:28630306</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24651271','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24651271"><span>Gas-liquid-liquid three-phase flow pattern and <span class="hlt">pressure</span> <span class="hlt">drop</span> in a microfluidic chip: similarities with gas-liquid/liquid-liquid flows.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Yue, Jun; Rebrov, Evgeny V; Schouten, Jaap C</p> <p>2014-05-07</p> <p>We report a three-phase slug flow and a parallel-slug flow as two major flow patterns found under the nitrogen-decane-water flow through a glass microfluidic chip which features a long microchannel with a hydraulic diameter of 98 μm connected to a cross-flow mixer. The three-phase slug flow pattern is characterized by a flow of decane droplets containing single elongated nitrogen bubbles, which are separated by water slugs. This flow pattern was observed at a superficial velocity of decane (in the range of about 0.6 to 10 mm s(-1)) typically lower than that of water for a given superficial gas velocity in the range of 30 to 91 mm s(-1). The parallel-slug flow pattern is characterized by a continuous water flow in one part of the channel cross section and a parallel flow of decane with dispersed nitrogen bubbles in the adjacent part of the channel cross section, which was observed at a superficial velocity of decane (in the range of about 2.5 to 40 mm s(-1)) typically higher than that of water for each given superficial gas velocity. The three-phase slug flow can be seen as a superimposition of both decane-water and nitrogen-decane slug flows observed in the chip when the flow of the third phase (viz. nitrogen or water, respectively) was set at zero. The parallel-slug flow can be seen as a superimposition of the decane-water parallel flow and the nitrogen-decane slug flow observed in the chip under the corresponding two-phase flow conditions. In case of small capillary numbers (Ca ≪ 0.1) and Weber numbers (We ≪ 1), the developed two-phase <span class="hlt">pressure</span> <span class="hlt">drop</span> model under a slug flow has been extended to obtain a three-phase slug flow model in which the 'nitrogen-in-decane' droplet is assumed as a pseudo-homogeneous droplet with an effective viscosity. The parallel flow and slug flow <span class="hlt">pressure</span> <span class="hlt">drop</span> models have been combined to obtain a parallel-slug flow model. The obtained models describe the experimental <span class="hlt">pressure</span> <span class="hlt">drop</span> with standard deviations of 8% and 12% for the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhRvF...1e4102B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhRvF...1e4102B"><span><span class="hlt">Pressure</span> driven flow of superfluid 4He through a nanopipe</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Botimer, Jeffrey; Taborek, Peter</p> <p>2016-09-01</p> <p><span class="hlt">Pressure</span> driven flow of superfluid helium through single high-aspect-ratio glass nanopipes into a vacuum has been studied for a wide range of <span class="hlt">pressure</span> <span class="hlt">drop</span> (0-30 bars), reservoir temperature (0.8-2.5 K), pipe lengths (1-30 mm), and pipe radii (131 and 230 nm). As a function of <span class="hlt">pressure</span> <span class="hlt">drop</span> we observe two distinct flow regimes above and below a critical <span class="hlt">pressure</span> <span class="hlt">drop</span> Pc. For P <Pc , the critical velocity is approximately the Feynman critical velocity. As the <span class="hlt">pressure</span> <span class="hlt">drop</span> approaches Pc, there is a sudden transition to a new flow state with a critical velocity more than an order of magnitude higher. The position of the transition is explained by a simple model that accounts for the fountain <span class="hlt">pressure</span> generated by evaporative cooling at the outlet of the nanopipe.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010cosp...38.3588K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010cosp...38.3588K"><span>The <span class="hlt">Drop</span> Tower Bremen -Experiment Operation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Könemann, Thorben; von Kampen, Peter; Rath, Hans J.</p> <p></p> <p>The idea behind the <span class="hlt">drop</span> tower facility of the Center of Applied Space Technology and Micro-gravity (ZARM) in Bremen is to provide an inimitable technical opportunity of a daily access to short-term weightlessness on earth. In this way ZARM`s european unique ground-based microgravity laboratory displays an excellent economic alternative for research in space-related conditions at low costs comparable to orbital platforms. Many national and international ex-perimentalists motivated by these prospects decide to benefit from the high-quality and easy accessible microgravity environment only provided by the <span class="hlt">Drop</span> Tower Bremen. Corresponding experiments in reduced gravity could open new perspectives of investigation methods and give scientists an impressive potential for a future technology and multidisciplinary applications on different research fields like Fundamental Physics, Astrophysics, Fluid Dynamics, Combus-tion, Material Science, Chemistry and Biology. Generally, realizing microgravity experiments at ZARM`s <span class="hlt">drop</span> tower facility meet new requirements of the experimental hardware and may lead to some technical constraints in the setups. In any case the ZARM <span class="hlt">Drop</span> Tower Operation and Service Company (ZARM FAB mbH) maintaining the <span class="hlt">drop</span> tower facility is prepared to as-sist experimentalists by offering own <span class="hlt">air</span>-conditioned laboratories, clean rooms, workshops and consulting engineers, as well as scientific personal. Furthermore, ZARM`s on-site apartment can be used for accommodations during the experiment campaigns. In terms of approaching <span class="hlt">drop</span> tower experimenting, consulting of experimentalists is mandatory to successfully accomplish the pursued <span class="hlt">drop</span> or catapult capsule experiment. For this purpose there will be a lot of expertise and help given by ZARM FAB mbH in strong cooperation to-gether with the experimentalists. However, in comparison to standard laboratory setups the <span class="hlt">drop</span> or catapult capsule setup seems to be completely different at first view. While defining a</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/5319244','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/5319244"><span><span class="hlt">Air</span> ejector augmented compressed <span class="hlt">air</span> energy storage system</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Ahrens, F.W.; Kartsounes, G.T.</p> <p></p> <p>Energy is stored in slack demand periods by charging a plurality of underground reservoirs with <span class="hlt">air</span> to the same peak storage <span class="hlt">pressure</span>, during peak demand periods throttling the <span class="hlt">air</span> from one storage reservoir into a gas turbine system at a constant inlet <span class="hlt">pressure</span> until the <span class="hlt">air</span> presure in the reservoir falls to said constant inlet <span class="hlt">pressure</span>, thereupon permitting <span class="hlt">air</span> in a second reservoir to flow into said gas turbine system while drawing <span class="hlt">air</span> from the first reservoir through a variable geometry <span class="hlt">air</span> ejector and adjusting said variable geometry <span class="hlt">air</span> ejector, said <span class="hlt">air</span> flow being essentially at the constant inlet <span class="hlt">pressure</span> of the gas turbine system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010APS..DFD.CS007S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010APS..DFD.CS007S"><span>An evaporation model of multicomponent solution <span class="hlt">drops</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sartori, Silvana; Liñán, Amable; Lasheras, Juan C.</p> <p>2010-11-01</p> <p>Solutions of polymers are widely used in the pharmaceutical industry as tablets coatings. These allow controlling the rate at which the drug is delivered, taste or appearance. The coating is performed by spraying and drying the tablets at moderate temperatures. The wetting of the coating solution on the pill's surface depends on the droplet Webber and Re numbers, angle of impact and on the rheological properties of the droplet. We present a model for the evaporation of multicomponent solutions droplets in a hot <span class="hlt">air</span> environment with temperatures substantially lower than the boiling temperature of the solvent. As the liquid vaporizes from the surface the fluid in the <span class="hlt">drop</span> increases in concentration, until reaching its saturation point. After saturation, precipitation occurs uniformly within the <span class="hlt">drop</span>. As the surface regresses, a compacting front formed by the precipitate at its maximum packing density advances into the <span class="hlt">drop</span>, while the solute continues precipitating uniformly. This porous shell grows fast due to the double effect of surface regression and precipitation. The evaporation rate is determined by the rates at which heat is transported to the droplet surface and at which liquid vapor diffuses away from it. When the <span class="hlt">drop</span> is fully compacted, the evaporation is drastically reduced.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/873546','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/873546"><span>Vehicle cabin cooling system for capturing and exhausting heated boundary layer <span class="hlt">air</span> from inner surfaces of solar heated windows</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Farrington, Robert B.; Anderson, Ren</p> <p>2001-01-01</p> <p>The cabin cooling system includes a cooling duct positioned proximate and above upper edges of one or more windows of a vehicle to exhaust hot <span class="hlt">air</span> as the <span class="hlt">air</span> is heated by inner surfaces of the windows and forms thin boundary layers of heated <span class="hlt">air</span> adjacent the heated windows. The cabin cooling system includes at least one fan to draw the hot <span class="hlt">air</span> into the cooling duct at a flow rate that captures the hot <span class="hlt">air</span> in the boundary layer without capturing a significant portion of the cooler cabin interior <span class="hlt">air</span> and to discharge the hot <span class="hlt">air</span> at a point outside the vehicle cabin, such as the vehicle trunk. In a preferred embodiment, the cooling duct has a cross-sectional area that gradually increases from a distal point to a proximal point to the fan inlet to develop a substantially uniform <span class="hlt">pressure</span> <span class="hlt">drop</span> along the length of the cooling duct. Correspondingly, this cross-sectional configuration develops a uniform suction <span class="hlt">pressure</span> and uniform flow rate at the upper edge of the window to capture the hot <span class="hlt">air</span> in the boundary layer adjacent each window.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29576128','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29576128"><span>Non-invasive positive-<span class="hlt">pressure</span> ventilation with positive end-expiratory <span class="hlt">pressure</span> counteracts inward <span class="hlt">air</span> leaks during preoxygenation: a randomised crossover controlled study in healthy volunteers.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hanouz, J-L; Le Gall, F; Gérard, J-L; Terzi, N; Normand, H</p> <p>2018-04-01</p> <p>During preoxygenation, the lack of tight fit between the mask and the patient's face results in inward <span class="hlt">air</span> leak preventing effective preoxygenation. We hypothesized that non-invasive positive-<span class="hlt">pressure</span> ventilation and positive end-expiratory <span class="hlt">pressure</span> (PEEP) could counteract inward <span class="hlt">air</span> leak. Healthy volunteers were randomly assigned to preoxygenated through spontaneous breathing without leak (SB), spontaneous breathing with a calibrated <span class="hlt">air</span> leak (T-shaped piece between the mouth and the breathing system; SB-leak), or non-invasive positive inspiratory <span class="hlt">pressure</span> ventilation (inspiratory support +6 cm H 2 O; PEEP +5 cm H 2 O) with calibrated leak (PPV-leak). The volunteers breathed through a mouthpiece connected to an anaesthesia ventilator. The expired oxygen fraction (FeO 2 ) and <span class="hlt">air</span>-leak flow (ml s -1 ) were measured. The primary end point was the proportion of volunteers with FeO 2 >90% at 3 min. The secondary end points were FeO 2 at 3 min, time to reach FeO 2 of 90%, and the inspiratory <span class="hlt">air</span>-leak flow. Twenty healthy volunteers were included. The proportion of volunteers with FeO 2 >90% at 3 min was 0% in the SB-leak group, 95% in the SB group, and 100% in the PPV-leak group (P<0.001). At 3 min, the mean [standard deviation (sd)] FeO 2 was 89 (1)%, 76 (1)%, and 90 (0)% in the SB, SB-leak, and PPV-leak groups, respectively (P<0.001). The mean (sd) inward <span class="hlt">air</span> leak was 59 (12) ml s -1 in the SB-leak group, but 0 (0) ml s -1 in the PPV-leak group (P<0.001). Preoxygenation through non-invasive positive-<span class="hlt">pressure</span> ventilation and PEEP provided effective preoxygenation despite an inward <span class="hlt">air</span> leak. NCT03087825. Copyright © 2017 British Journal of Anaesthesia. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011PlPhR..37..409T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011PlPhR..37..409T"><span>Parameters of a supershort avalanche electron beam generated in atmospheric-<span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tarasenko, V. F.</p> <p>2011-05-01</p> <p>Conditions under which the number of runaway electrons in atmospheric-<span class="hlt">pressure</span> <span class="hlt">air</span> reaches ˜5 × 1010 are determined. Recommendations for creating runaway electron accelerators are given. Methods for measuring the parameters of a supershort avalanche electron beam and X-ray pulses from gas-filled diodes, as well as the discharge current and gap voltage, are described. A technique for determining the instant of runaway electron generation with respect to the voltage pulse is proposed. It is shown that the reduction in the gap voltage and the decrease in the beam current coincide in time. The mechanism of intense electron beam generation in gas-filled diodes is analyzed. It is confirmed experimentally that, in optimal regimes, the number of electrons generated in atmospheric-<span class="hlt">pressure</span> <span class="hlt">air</span> with energies T > eU m , where U m is the maximum gap voltage, is relatively small.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19670000291','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19670000291"><span>Remotely operated high <span class="hlt">pressure</span> valve protects test personnel</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Howland, B. T.</p> <p>1967-01-01</p> <p>High <span class="hlt">pressure</span> valve used in testing certain spacecraft systems is safely opened and closed by a remotely stationed operator. The valve is self-regulating in that if the incoming <span class="hlt">pressure</span> <span class="hlt">drops</span> below a desired value the valve will automatically close, warning the operator that the testing <span class="hlt">pressure</span> has <span class="hlt">dropped</span> to an undesired level.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_23 --> <div id="page_24" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="461"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28555683','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28555683"><span>Foamed emulsion drainage: flow and trapping of <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Schneider, Maxime; Zou, Ziqiang; Langevin, Dominique; Salonen, Anniina</p> <p>2017-06-07</p> <p>Foamed emulsions are ubiquitous in our daily life but the ageing of such systems is still poorly understood. In this study we investigate foam drainage and measure the evolution of the gas, liquid and oil volume fractions inside the foam. We evidence three regimes of ageing. During an initial period of fast drainage, both bubbles and <span class="hlt">drops</span> are very mobile. As the foam stabilises drainage proceeds leading to a gradual decrease of the liquid fraction and slowing down of drainage. Clusters of oil <span class="hlt">drops</span> are less sheared, their dynamic viscosity increases and drainage slows down even further, until the <span class="hlt">drops</span> become blocked. At this point the oil fraction starts to increase in the continuous phase. The foam ageing leads to an increase of the capillary <span class="hlt">pressure</span> until the oil acts as an antifoaming agent and the foam collapses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930091453','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930091453"><span>Static, <span class="hlt">Drop</span>, and Flight Tests on Musselman Type Airwheels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Peck, William C; Beard, Albert P</p> <p>1932-01-01</p> <p>The purpose of this investigation was to obtain quantitative information on the shock-reducing and energy-dissipating qualities of a set of 30 by 13-6 Musselman type airwheels. The investigation consisted of static, <span class="hlt">drop</span>, and flight tests. The static tests were made with inflation <span class="hlt">pressures</span> of approximately 0, 5, 10, 15, 20, and 25 pounds per square inch and loadings up to 9,600 pounds. The <span class="hlt">drop</span> tests were with the inflation <span class="hlt">pressures</span> approximately 5, 10, 15, 20, and 25 pounds per square inch and loadings of 1,840, 2,440, 3,050, and 3,585 pounds. The flight tests were made with VE-7 airplane weighing 2,153 pounds, with the tires inflated to 5, 10, and 15 pounds per square inch. The landing gears used in conjunction with airwheels were practically rigid structures. The results of the tests showed that the walls of the tires carried a considerable portion of the load, each tire supporting a load of 600 pounds with a depression of approximately 6 inches. The shock-reducing qualities, under severe tests, and the energy dissipating characteristics of the tires, under all tests, were poor. The latter was evidenced by the rebound present in all landings made. In the severe <span class="hlt">drop</span> tests, the free rebound reached as much as 60 per cent of the free <span class="hlt">drop</span>. The results indicate that a shock-reducing and energy-dissipating mechanism should be used in conjunction with airwheels.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18299098','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18299098"><span>Reduced injection <span class="hlt">pressures</span> using a compressed <span class="hlt">air</span> injection technique (CAIT): an in vitro study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tsui, Ban C H; Knezevich, Mark P; Pillay, Jennifer J</p> <p>2008-01-01</p> <p>High injection <span class="hlt">pressures</span> have been associated with intraneural injection and persistent neurological injury in animals. Our objective was to test whether a reported simple compressed <span class="hlt">air</span> injection technique (CAIT) would limit the generation of injection <span class="hlt">pressures</span> to below a suggested 1,034 mm Hg limit in an in vitro model. After ethics board approval, 30 consenting anesthesiologists injected saline into a semiclosed system. Injection <span class="hlt">pressures</span> using 30 mL syringes connected to a 22 gauge needle and containing 20 mL of saline were measured for 60 seconds using: (1) a typical "syringe feel" method, and (2) CAIT, thereby drawing 10 mL of <span class="hlt">air</span> above the saline and compressing this to 5 mL prior to and during injections. All anesthesiologists performed the syringe feel method before introduction and demonstration of CAIT. Using CAIT, no anesthesiologist generated <span class="hlt">pressures</span> above 1,034 mm Hg, while 29 of 30 produced <span class="hlt">pressures</span> above this limit at some time using the syringe feel method. The mean <span class="hlt">pressure</span> using CAIT was lower (636 +/- 71 vs. 1378 +/- 194 mm Hg, P = .025), and the syringe feel method resulted in higher peak <span class="hlt">pressures</span> (1,875 +/- 206 vs. 715 +/- 104 mm Hg, P = .000). This study demonstrated that CAIT can effectively keep injection <span class="hlt">pressures</span> under 1,034 mm Hg in this in vitro model. Animal and clinical studies will be needed to determine whether CAIT will allow objective, real-time <span class="hlt">pressure</span> monitoring. If high <span class="hlt">pressure</span> injections are proven to contribute to nerve injury in humans, this technique may have the potential to improve the safety of peripheral nerve blocks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20170003842','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20170003842"><span>A Modified Triples Algorithm for Flush <span class="hlt">Air</span> Data Systems that Allows a Variety of <span class="hlt">Pressure</span> Port Configurations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Millman, Daniel R.</p> <p>2017-01-01</p> <p><span class="hlt">Air</span> Data Systems (FADS) are becoming more prevalent on re-entry vehicles, as evi- denced by the Mars Science Laboratory and the Orion Multipurpose Crew Vehicle. A FADS consists of flush-mounted <span class="hlt">pressure</span> transducers located at various locations on the fore-body of a flight vehicle or the heat shield of a re-entry capsule. A <span class="hlt">pressure</span> model converts the <span class="hlt">pressure</span> readings into useful <span class="hlt">air</span> data quantities. Two algorithms for converting <span class="hlt">pressure</span> readings to <span class="hlt">air</span> data have become predominant- the iterative Least Squares State Estimator (LSSE) and the Triples Algorithm. What follows herein is a new algorithm that takes advantage of the best features of both the Triples Algorithm and the LSSE. This approach employs the potential flow model and strategic differencing of the Triples Algorithm to obtain the defective flight angles; however, the requirements on port placement are far less restrictive, allowing for configurations that are considered optimal for a FADS.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820018419','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820018419"><span>Investigation of spray characteristics for flashing injection of fuels containing dissolved <span class="hlt">air</span> and superheated fuels</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Solomon, A. S. P.; Chen, L. D.; Faeth, G. M.</p> <p>1982-01-01</p> <p>The flow, atomization and spreading of flashing injector flowing liquids containing dissolved gases (jet/<span class="hlt">air</span>) as well as superheated liquids (Freon II) were considered. The use of a two stage expansion process separated by an expansion chamber, ws found to be beneficial for flashing injection particularly for dissolved gas systems. Both locally homogeneous and separated flow models provided good predictions of injector flow properties. Conventional correlations for <span class="hlt">drop</span> sizes from <span class="hlt">pressure</span> atomized and airblast injectors were successfully modified, using the separated flow model to prescribe injector exit conditions, to correlate <span class="hlt">drop</span> size measurements. Additional experimental results are provided for spray angle and combustion properties of sprays from flashing injectors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EPJWC.14302054K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EPJWC.14302054K"><span>Experimental investigation of cavitation induced <span class="hlt">air</span> release</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kowalski, Karoline; Pollak, Stefan; Hussong, Jeanette</p> <p></p> <p>Variations in cross-sectional areas may lead to <span class="hlt">pressure</span> <span class="hlt">drops</span> below a critical value, such that cavitation and <span class="hlt">air</span> release are provoked in hydraulic systems. Due to a relatively slow dissolution of gas bubbles, the performance of hydraulic systems will be affected on long time scales by the gas phase. Therefore predictions of <span class="hlt">air</span> production rates are desirable to describe the system characteristics. Existing investigations on generic geometries such as micro-orifice flows show an outgassing process due to hydrodynamic cavitation which takes place on time scales far shorter than diffusion processes. The aim of the present investigation is to find a correlation between global, hydrodynamic flow characteristics and cavitation induced undissolved gas fractions generated behind generic flow constrictions such as an orifice or venturi tube. Experimental investigations are realised in a cavitation channel that enables an independent adjustment of the <span class="hlt">pressure</span> level upstream and downstream of the orifice. Released <span class="hlt">air</span> fractions are determined by means of shadowgraphy imaging. First results indicate that an increased cavitation activity leads to a rapid increase in undissolved gas volume only in the choking regime. The frequency distribution of generated gas bubble size seems to depend only indirectly on the cavitation intensity driven by an increase of downstream coalescence events due to a more densely populated bubbly flow.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820020566','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820020566"><span>Method of forming frozen spheres in a force-free <span class="hlt">drop</span> tower</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kendall, J. M., Jr. (Inventor)</p> <p>1982-01-01</p> <p>Hollow glass spheres are shaped by the effects of surface tension acting on bubbles of glass in its molten state. A downwardly flowing stream of <span class="hlt">air</span> accelerated at a one-G rate of acceleration is established through a <span class="hlt">drop</span> bubbles on molten glass are introduced into the stream of <span class="hlt">air</span> and frozen and as they are accelerated at a one-G rate of acceleration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29440184','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29440184"><span>Household <span class="hlt">air</span> pollution and measures of blood <span class="hlt">pressure</span>, arterial stiffness and central haemodynamics.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Baumgartner, Jill; Carter, Ellison; Schauer, James J; Ezzati, Majid; Daskalopoulou, Stella S; Valois, Marie-France; Shan, Ming; Yang, Xudong</p> <p>2018-02-09</p> <p>We evaluated the exposure-response associations between personal exposure to <span class="hlt">air</span> pollution from biomass stoves and multiple vascular and haemodynamic parameters in rural Chinese women. We analysed the baseline information from a longitudinal study in southwestern China. Women's brachial and central blood <span class="hlt">pressure</span> and pulse <span class="hlt">pressure</span>, carotid-femoral pulse wave velocity and augmentation index, and their 48-hour personal exposures to fine particulate matter (PM 2.5 ) and black carbon were measured in summer and winter. We evaluated the associations between exposure to <span class="hlt">air</span> pollution and haemodynamic parameters using mixed-effects regression models adjusted for known cardiovascular risk factors. Women's (n=205, ages 27-86 years) exposures to PM 2.5 and black carbon ranged from 14 µg/m 3 to 1405 µg/m 3 and 0.1-121.8 µg/m 3 , respectively. Among women aged ≥50 years, increased PM 2.5 exposure was associated with higher systolic (brachial: 3.5 mm Hg (P=0.05); central: 4.4 mm Hg (P=0.005)) and diastolic blood <span class="hlt">pressure</span> (central: 1.3 mm Hg (P=0.10)), higher pulse <span class="hlt">pressure</span> (peripheral: 2.5 mm Hg (P=0.05); central: 2.9 mm Hg (P=0.008)) and lower peripheral-central pulse <span class="hlt">pressure</span> amplification (-0.007 (P=0.04)). Among younger women, the associations were inconsistent in the direction of effect and not statistically significant. Increased PM 2.5 exposure was associated with no difference in pulse wave velocity and modestly higher augmentation index though the CI included zero (1.1%; 95% CI -0.2% to 2.4%). Similar associations were found for black carbon exposure. Exposure to household <span class="hlt">air</span> pollution was associated with higher blood <span class="hlt">pressure</span> and central haemodynamics in older Chinese women, with no associations observed with pulse wave velocity. © Article author(s) (or their employer(s) unless otherwise stated in the text of the article) 2018. All rights reserved. No commercial use is permitted unless otherwise expressly granted.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23433896','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23433896"><span>Hanging <span class="hlt">drop</span>: an in vitro <span class="hlt">air</span> toxic exposure model using human lung cells in 2D and 3D structures.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Liu, Faye F; Peng, Cheng; Escher, Beate I; Fantino, Emmanuelle; Giles, Cindy; Were, Stephen; Duffy, Lesley; Ng, Jack C</p> <p>2013-10-15</p> <p>Using benzene as a candidate <span class="hlt">air</span> toxicant and A549 cells as an in vitro cell model, we have developed and validated a hanging <span class="hlt">drop</span> (HD) <span class="hlt">air</span> exposure system that mimics an <span class="hlt">air</span> liquid interface exposure to the lung for periods of 1h to over 20 days. Dose response curves were highly reproducible for 2D cultures but more variable for 3D cultures. By comparing the HD exposure method with other classically used <span class="hlt">air</span> exposure systems, we found that the HD exposure method is more sensitive, more reliable and cheaper to run than medium diffusion methods and the CULTEX(®) system. The concentration causing 50% of reduction of cell viability (EC50) for benzene, toluene, p-xylene, m-xylene and o-xylene to A549 cells for 1h exposure in the HD system were similar to previous in vitro static <span class="hlt">air</span> exposure. Not only cell viability could be assessed but also sub lethal biological endpoints such as DNA damage and interleukin expressions. An advantage of the HD exposure system is that bioavailability and cell concentrations can be derived from published physicochemical properties using a four compartment mass balance model. The modelled cellular effect concentrations EC50cell for 1h exposure were very similar for benzene, toluene and three xylenes and ranged from 5 to 15 mmol/kgdry weight, which corresponds to the intracellular concentration of narcotic chemicals in many aquatic species, confirming the high sensitivity of this exposure method. Copyright © 2013 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JInst..13.1004Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JInst..13.1004Z"><span>The conceptual design of high temporal resolution HCN interferometry for atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> plasmas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, J. B.; Liu, H. Q.; Jie, Y. X.; Wei, X. C.; Hu, L. Q.</p> <p>2018-01-01</p> <p>A heterodyne interferometer operating at the frequency f = 890 GHz has been designed for measuring the electron density of atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span> plasmas, it's density range is from 1015 to 3×1019 m-3 and the <span class="hlt">pressure</span> range is from 1 Pa to 20 kPa. The system is configured as a Mach\</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhD...50.5202L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhD...50.5202L"><span>Gas heating dynamics during leader inception in long <span class="hlt">air</span> gaps at atmospheric <span class="hlt">pressure</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Lipeng; Becerra, Marley</p> <p>2017-08-01</p> <p>The inception of leader discharges in long <span class="hlt">air</span> gaps at atmospheric <span class="hlt">pressure</span> is simulated with a thermo-hydrodynamic model and a detailed kinetic scheme for N2/O2/H2O mixtures. In order to investigate the effect of humidity, the kinetic scheme includes the most important reactions with the H2O molecule and its derivatives, resulting in a scheme with 45 species and 192 chemical reactions. The heating of a thin plasma channel in front of an anode electrode during the streamer to leader transition is evaluated with a detailed 1D radial model. The analysis includes the simulation of the corresponding streamer bursts, dark periods and aborted leaders that may occur prior to the inception of a propagating leader discharge. The simulations are performed using the time-varying discharge current in two laboratory discharge events of positive polarity reported in the literature as input. Excellent agreement between the simulated and the experimental time variation of the thermal radius for a 1 m rod-plate <span class="hlt">air</span> gap discharge event reported in the literature has been found. The role of different energy transfer and loss mechanisms prior to the inception of a stable leader is also discussed. It is found that although a small percentage of water molecules can accelerate the vibrational-translational relaxation to some extent, this effect leads to a negligible temperature increase during the streamer-to-leader transition. It is also found that the gas temperature should significantly exceed 2000 K for the transition to lead to the inception of a propagating leader. Otherwise, the strong convection loss produced by the gas expansion during the transition causes a <span class="hlt">drop</span> in the translational temperature below 2000 K, aborting the incepted leader. Furthermore, it is shown that the assumptions used by the widely-used model of Gallimberti do not hold when evaluating the streamer-to-leader transition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011SPIE.8058E..11T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011SPIE.8058E..11T"><span>Heart-rate monitoring by <span class="hlt">air</span> <span class="hlt">pressure</span> and causal analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tsuchiya, Naoki; Nakajima, Hiroshi; Hata, Yutaka</p> <p>2011-06-01</p> <p>Among lots of vital signals, heart-rate (HR) is an important index for diagnose human's health condition. For instance, HR provides an early stage of cardiac disease, autonomic nerve behavior, and so forth. However, currently, HR is measured only in medical checkups and clinical diagnosis during the rested state by using electrocardiograph (ECG). Thus, some serious cardiac events in daily life could be lost. Therefore, a continuous HR monitoring during 24 hours is desired. Considering the use in daily life, the monitoring should be noninvasive and low intrusive. Thus, in this paper, an HR monitoring in sleep by using <span class="hlt">air</span> <span class="hlt">pressure</span> sensors is proposed. The HR monitoring is realized by employing the causal analysis among <span class="hlt">air</span> <span class="hlt">pressure</span> and HR. The causality is described by employing fuzzy logic. According to the experiment on 7 males at age 22-25 (23 on average), the correlation coefficient against ECG is 0.73-0.97 (0.85 on average). In addition, the cause-effect structure for HR monitoring is arranged by employing causal decomposition, and the arranged causality is applied to HR monitoring in a setting posture. According to the additional experiment on 6 males, the correlation coefficient is 0.66-0.86 (0.76 on average). Therefore, the proposed method is suggested to have enough accuracy and robustness for some daily use cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25959867','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25959867"><span>Two types of Cassie-to-Wenzel wetting transitions on superhydrophobic surfaces during <span class="hlt">drop</span> impact.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lee, Choongyeop; Nam, Youngsuk; Lastakowski, Henri; Hur, Janet I; Shin, Seungwon; Biance, Anne-Laure; Pirat, Christophe; Kim, Chang-Jin C J; Ybert, Christophe</p> <p>2015-06-21</p> <p>Despite the fact that superhydrophobic surfaces possess useful and unique properties, their practical application has remained limited by durability issues. Among those, the wetting transition, whereby a surface gets impregnated by the liquid and permanently loses its superhydrophobicity, certainly constitutes the most limiting aspect under many realistic conditions. In this study, we revisit this so-called Cassie-to-Wenzel transition (CWT) under the broadly encountered situation of liquid <span class="hlt">drop</span> impact. Using model hydrophobic micropillar surfaces of various geometrical characteristics and high speed imaging, we identify that CWT can occur through different mechanisms, and at different impact stages. At early impact stages, right after contact, CWT occurs through the well established dynamic <span class="hlt">pressure</span> scenario of which we provide here a fully quantitative description. Comparing the critical wetting <span class="hlt">pressure</span> of surfaces and the theoretical <span class="hlt">pressure</span> distribution inside the liquid <span class="hlt">drop</span>, we provide not only the CWT threshold but also the hardly reported wetted area which directly affects the surface spoiling. At a later stage, we report for the first time to our knowledge, a new CWT which occurs during the <span class="hlt">drop</span> recoil toward bouncing. With the help of numerical simulations, we discuss the mechanism underlying this new transition and provide a simple model based on impulse conservation which successfully captures the transition threshold. By shedding light on the complex interaction between impacting water <span class="hlt">drops</span> and surface structures, the present study will facilitate designing superhydrophobic surfaces with a desirable wetting state during <span class="hlt">drop</span> impact.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25853278','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25853278"><span>Thermal activation of superheated lipid-coated perfluorocarbon <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mountford, Paul A; Thomas, Alec N; Borden, Mark A</p> <p>2015-04-28</p> <p>This study explored the thermal conditions necessary for the vaporization of superheated perfluorocarbon nanodrops. Droplets C3F8 and C4F10 coated with a homologous series of saturated diacylphosphatidylcholines were formed by condensation of 4 μm diameter microbubbles. These <span class="hlt">drops</span> were stable at room temperature and atmospheric <span class="hlt">pressure</span>, but they vaporized back into microbubbles at higher temperatures. The vaporization transition was measured as a function of temperature by laser light extinction. We found that C3F8 and C4F10 <span class="hlt">drops</span> experienced 90% vaporization at 40 and 75 °C, respectively, near the theoretical superheat limits (80-90% of the critical temperature). We therefore conclude that the metastabilty of these phase-change agents arises not from the droplet Laplace <span class="hlt">pressure</span> altering the boiling point, as previously reported, but from the metastability of the pure superheated fluid to homogeneous nucleation. The rate of C4F10 <span class="hlt">drop</span> vaporization was quantified at temperatures ranging from 55 to 75 °C, and an apparent activation energy barrier was calculated from an Arrhenius plot. Interestingly, the activation energy increased linearly with acyl chain length from C14 to C20, indicating that lipid interchain cohesion plays an important role in suppressing the vaporization rate. The vaporized <span class="hlt">drops</span> (microbubbles) were found to be unstable to dissolution at high temperatures, particularly for C14 and C16. However, proper choice of the fluorocarbon and lipid species provided a nanoemulsion that could undergo at least ten reversible condensation/vaporization cycles. The vaporization properties presented in this study may facilitate the engineering of tunable phase-shift particles for diagnostic imaging, targeted drug delivery, tissue ablation, and other applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28713524','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28713524"><span>Forced-<span class="hlt">Air</span> Warming Discontinued: Periprosthetic Joint Infection Rates <span class="hlt">Drop</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Augustine, Scott D</p> <p>2017-06-23</p> <p>Several studies have shown that the waste heat from forced-<span class="hlt">air</span> warming (FAW) escapes near the floor and warms the contaminated <span class="hlt">air</span> resident near the floor. The waste heat then forms into convection currents that rise up and contaminate the sterile field above the surgical table. It has been shown that a single airborne bacterium can cause a periprosthetic joint infection (PJI) following joint replacement surgery. We retrospectively compared PJI rates during a period of FAW to a period of <span class="hlt">air</span>-free conductive fabric electric warming (CFW) at three hospitals. Surgical and antibiotic protocols were held constant. The pooled multicenter data showed a decreased PJI rate of 78% following the discontinuation of FAW and a switch to <span class="hlt">air</span>-free CFW (n=2034; P=0.002). The 78% reduction in joint implant infections observed when FAW was discontinued suggests that there is a link between the waste FAW heat and PJIs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880056230&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880056230&hterms=air+pressure&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dair%2Bpressure"><span><span class="hlt">Air</span>-broadened Lorentz halfwidths and <span class="hlt">pressure</span>-induced line shifts in the nu(4) band of C-13H4</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Devi, V. Malathy; Benner, D. Chris; Rinsland, Curtis P.; Smith, Mary Ann H.</p> <p>1988-01-01</p> <p><span class="hlt">Air</span>-broadened halfwidths and <span class="hlt">pressure</span>-induced line shifts in the nu(4) fundamental of C-13H4 were determined from spectra recorded at room temperature and at 0.01/cm resolution using a Fourier transform spectrometer. Halfwidths and <span class="hlt">pressure</span> shifts were determined for over 180 transitions belonging to J-double prime values of less than or = to 16. Comparisons of <span class="hlt">air</span>-broadened halfwidths and <span class="hlt">pressure</span>-induced line shifts made for identical transitions in the nu(4) bands of C-12H4 and C-13H4 have shown that C-13H4 <span class="hlt">air</span>-broadened halfwidths are about 5 percent smaller than the corresponding C-12H4 halfwidths, and the <span class="hlt">pressure</span> shifts for C-13H4 lines are about 5-15 percent larger than those for C-12H4.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5505092','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5505092"><span>Forced-<span class="hlt">Air</span> Warming Discontinued: Periprosthetic Joint Infection Rates <span class="hlt">Drop</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Augustine, Scott D.</p> <p>2017-01-01</p> <p>Several studies have shown that the waste heat from forced-<span class="hlt">air</span> warming (FAW) escapes near the floor and warms the contaminated <span class="hlt">air</span> resident near the floor. The waste heat then forms into convection currents that rise up and contaminate the sterile field above the surgical table. It has been shown that a single airborne bacterium can cause a periprosthetic joint infection (PJI) following joint replacement surgery. We retrospectively compared PJI rates during a period of FAW to a period of <span class="hlt">air</span>-free conductive fabric electric warming (CFW) at three hospitals. Surgical and antibiotic protocols were held constant. The pooled multicenter data showed a decreased PJI rate of 78% following the discontinuation of FAW and a switch to <span class="hlt">air</span>-free CFW (n=2034; P=0.002). The 78% reduction in joint implant infections observed when FAW was discontinued suggests that there is a link between the waste FAW heat and PJIs. PMID:28713524</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24199602','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24199602"><span>Effects of setting under <span class="hlt">air</span> <span class="hlt">pressure</span> on the number of surface pores and irregularities of dental investment materials.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tourah, Anita; Moshaverinia, Alireza; Chee, Winston W</p> <p>2014-02-01</p> <p>Surface roughness and irregularities are important properties of dental investment materials that can affect the fit of a restoration. Whether setting under <span class="hlt">air</span> <span class="hlt">pressure</span> affects the surface irregularities of gypsum-bonded and phosphate-bonded investment materials is unknown. The purpose of this study was to investigate the effect of <span class="hlt">air</span> <span class="hlt">pressure</span> on the pore size and surface irregularities of investment materials immediately after pouring. Three dental investments, 1 gypsum-bonded investment and 2 phosphate-bonded investments, were investigated. They were vacuum mixed according to the manufacturers' recommendations, then poured into a ringless casting system. The prepared specimens were divided into 2 groups: 1 bench setting and the other placed in a <span class="hlt">pressure</span> pot at 172 kPa. After 45 minutes of setting, the rings were removed and the investments were cut at a right angle to the long axis with a diamond disk. The surfaces of the investments were steam cleaned, dried with an <span class="hlt">air</span> spray, and observed with a stereomicroscope. A profilometer was used to evaluate the surface roughness (μm) of the castings. The number of surface pores was counted for 8 specimens from each group and the means and standard deviations were reported. Two-way ANOVA was used to compare the data. Specimens that set under atmospheric <span class="hlt">air</span> <span class="hlt">pressure</span> had a significantly higher number of pores than specimens that set under increased <span class="hlt">pressure</span> (P<.05). No statistically significant differences for surface roughness were found (P=.078). Also, no significant difference was observed among the 3 different types of materials tested (P>.05). Specimens set under positive <span class="hlt">pressure</span> in a <span class="hlt">pressure</span> chamber presented fewer surface bubbles than specimens set under atmospheric <span class="hlt">pressure</span>. Positive <span class="hlt">pressure</span> is effective and, therefore, is recommended for both gypsum-bonded and phosphate-bonded investment materials. Copyright © 2014 Editorial Council for the Journal of Prosthetic Dentistry. Published by Mosby, Inc. All</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930087025','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930087025"><span>Variation of the <span class="hlt">pressure</span> limits of flame propagation with tube diameter for propane-<span class="hlt">air</span> mixtures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Belles, Frank E; Simon, Dorothy M</p> <p>1951-01-01</p> <p>An investigation was made of the variation of the <span class="hlt">pressure</span> limits of flame propagation with tube diameter for quiescent propane with tube diameter for quiescent propane-<span class="hlt">air</span> mixtures. <span class="hlt">Pressure</span> limits were measured in glass tubes of six different inside diameters, with a precise apparatus. Critical diameters for flame propagation were calculated and the effect of <span class="hlt">pressure</span> was determined. The critical diameters depended on the <span class="hlt">pressure</span> to the -0.97 power for stoichiometric mixtures. The <span class="hlt">pressure</span> dependence decreased with decreasing propane concentration. Critical diameters were related to quenching distance, flame speeds, and minimum ignition energy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=air+AND+pressure&pg=6&id=EJ490036','ERIC'); return false;" href="https://eric.ed.gov/?q=air+AND+pressure&pg=6&id=EJ490036"><span>The Impact of a Science Demonstration on Children's Understanding of <span class="hlt">Air</span> <span class="hlt">Pressure</span>.</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Shepardson, Damiel P.; And Others</p> <p>1994-01-01</p> <p>Examines 52 fifth graders' written and oral responses to determine the impact of a scientific demonstration on their understanding of <span class="hlt">air</span> <span class="hlt">pressure</span>. For one-third of the children, the demonstration reinforced previous understanding. Recommendations for using demonstrations to promote children's scientific understanding are presented. (ZWH)</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_24 --> <div id="page_25" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="481"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24514078','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24514078"><span>Effects of hydraulic <span class="hlt">pressure</span> on the performance of single chamber <span class="hlt">air</span>-cathode microbial fuel cells.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cheng, Shaoan; Liu, Weifeng; Guo, Jian; Sun, Dan; Pan, Bin; Ye, Yaoli; Ding, Weijun; Huang, Haobin; Li, Fujian</p> <p>2014-06-15</p> <p>Scaling up of microbial fuel cells (MFCs) without losing power density requires a thorough understanding of the effect of hydraulic <span class="hlt">pressure</span> on MFC performance. In this work, the performance of an activated carbon <span class="hlt">air</span>-cathode MFC was evaluated under different hydraulic <span class="hlt">pressures</span>. The MFC under 100 mmH2O hydraulic <span class="hlt">pressure</span> produced a maximum power density of 1260 ± 24 mW m(-2), while the power density decreased by 24.4% and 44.7% as the hydraulic <span class="hlt">pressure</span> increased to 500 mmH2O and 2000 mmH2O, respectively. Notably, the performance of both the anode and the cathode had decreased under high hydraulic <span class="hlt">pressures</span>. Electrochemical impedance spectroscopy tests of the cathode indicated that both charge transfer resistance and diffusion transfer resistance increased with the increase in hydraulic <span class="hlt">pressure</span>. Denaturing gradient gel electrophoresis of PCR-amplified partial 16S rRNA genes demonstrated that the similarity among anodic biofilm communities under different hydraulic <span class="hlt">pressures</span> was ≥ 90%, and the communities of all MFCs were dominated by Geobacter sp. These results suggested that the reduction in power output of the single chamber <span class="hlt">air</span>-cathode MFC under high hydraulic <span class="hlt">pressures</span> can be attributed to water flooding of the cathode and suppression the metabolism of anodic exoelectrogenic bacteria. Copyright © 2014 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhNan..29...42S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhNan..29...42S"><span>Hanging colloidal <span class="hlt">drop</span>: A new photonic crystal synthesis route</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sandu, Ion; Dumitru, Marius; Fleaca, Claudiu Teodor; Dumitrache, Florian</p> <p>2018-05-01</p> <p>High-quality photonic crystals (hundreds of micrometres in thickness) were grown by the free evaporation of a colloidal <span class="hlt">drop</span> consisting of silica and polystyrene nanospheres with dimensions of 300 nm, 500 nm, and 1000 nm. The essence of experimental findings is that the <span class="hlt">drop</span> has to hang on a pillar. This leads to the inhibition of the droplet spreading, the minimisation of the convective force, and the zeroing of the static frictional force between nanospheres and the liquid/<span class="hlt">air</span> interface, where the first layer is formed. The theoretical essence is the continuous adjustment of nanospheres positions during the growth of photonic crystal, a key condition of the self-assembling phenomenon.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28664905','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28664905"><span><span class="hlt">Air</span> <span class="hlt">pressure</span> changes in the creation and bursting of the type-1 big bubble in deep anterior lamellar keratoplasty: an ex vivo study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>AlTaan, S L; Mohammed, I; Said, D G; Dua, H S</p> <p>2018-01-01</p> <p>PurposeTo measure the <span class="hlt">pressure</span> and volume of <span class="hlt">air</span> required to create a big bubble (BB) in simulated deep anterior lamellar keratoplasty (DALK) in donor eyes and ascertain the bursting <span class="hlt">pressure</span> of the BB.Patients and methodsTwenty-two human sclera-corneal discs were used. <span class="hlt">Air</span> was injected into the corneal stroma to create a BB and the <span class="hlt">pressure</span> measured by means of a <span class="hlt">pressure</span> converter attached to the system via a side port. A special clamp was designed to prevent <span class="hlt">air</span> leak from the periphery of the discs. The <span class="hlt">pressure</span> at which <span class="hlt">air</span> emerged in the corneal tissue; the bursting <span class="hlt">pressure</span> measured after advancing the needle into the bubble cavity and injecting more <span class="hlt">air</span>; the volume of <span class="hlt">air</span> required to create a BB and the volume of the BB were ascertained.ResultsType-1 BB were achieved in 19 and type-2 BB in 3 eyes. The maximum <span class="hlt">pressure</span> reached to create a BB was 96.25+/- 21.61 kpa; the mean type-1 intrabubble <span class="hlt">pressure</span> was 10.16 +/- 3.65 kpa. The mean bursting <span class="hlt">pressure</span> of a type-1 BB was 66.65 +/- 18.65 kpa, while that of a type-2 BB was 14.77 +/- 2.44 kpa. The volume of <span class="hlt">air</span> required to create a type-1 BB was 0.54 ml and the volume of a type-1 BB was consistently 0.1 ml.ConclusionsDua's layer baring DALK can withstand high intraoperative <span class="hlt">pressures</span> compared to Descemet's membrane baring DALK. The study suggests that it could be safe to undertake procedures such as DALK-triple with a type-1 BB but not with a type-2 BB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006APS..DFD.EF004M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006APS..DFD.EF004M"><span>Dynamics of Oscillating and Rotating Liquid <span class="hlt">Drop</span> using Electrostatic Levitator</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Matsumoto, Satoshi; Awazu, Shigeru; Abe, Yutaka; Watanabe, Tadashi; Nishinari, Katsuhiro; Yoda, Shinichi</p> <p>2006-11-01</p> <p>In order to understand the nonlinear behavior of liquid <span class="hlt">drop</span> with oscillatory and/or rotational motions, an experimental study was performed. The electrostatic levitator was employed to achieve liquid <span class="hlt">drop</span> formation on ground. A liquid <span class="hlt">drop</span> with about 3 mm in diameter was levitated. The oscillation of mode n=2 along the vertical axis was induced by an external electrostatic force. The oscillatory motions were observed to clarify the nonlinearities of oscillatory behavior. A relationship between amplitude and frequency shift was made clear and the effect of frequency shift on amplitude agreed well with the theory. The frequency shift became larger with increasing the amplitude of oscillation. To confirm the nonlinear effects, we modeled the oscillation by employing the mass-spring-damper system included the nonlinear term. The result indicates that the large-amplitude oscillation includes the effect of nonlinear oscillation. The sound <span class="hlt">pressure</span> was imposed to rotate the liquid <span class="hlt">drop</span> along a vertical axis by using a pair of acoustic transducers. The <span class="hlt">drop</span> transited to the two lobed shape due to centrifugal force when nondimensional angular velocity exceeded to 0.58.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22599927-generation-large-area-glow-like-surface-discharge-atmospheric-pressure-air','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22599927-generation-large-area-glow-like-surface-discharge-atmospheric-pressure-air"><span>Generation of large-area and glow-like surface discharge in atmospheric <span class="hlt">pressure</span> <span class="hlt">air</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Song, Ying; Bi, Zhenhua; Wang, Xueyang</p> <p>2016-08-15</p> <p>A large-area (6 cm × 6 cm) <span class="hlt">air</span> surface dielectric barrier discharge has been generated at atmospheric <span class="hlt">pressure</span> by using well-aligned and micron-sized dielectric tubes with tungsten wire electrodes. Intensified CCD images with an exposure time of 5 ns show that the uniform surface <span class="hlt">air</span> discharge can be generated during the rising and falling time of pulsed DC voltage. Current and voltage and optical measurements confirm the formation of glow-like <span class="hlt">air</span> discharges on the surface of micron-sized dielectric tubes. Simulation results indicate that the microelectrode configuration contributes to the formation of strong surface electric field and plays an important role in the generation of uniformmore » surface <span class="hlt">air</span> discharge.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800023881','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800023881"><span>Use of nose cap and fuselage <span class="hlt">pressure</span> orifices for determination of <span class="hlt">air</span> data for space shuttle orbiter below supersonic speeds</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Larson, T. J.; Siemers, P. M., III</p> <p>1980-01-01</p> <p>Wind tunnel <span class="hlt">pressure</span> measurements were acquired from orifices on a 0.1 scale forebody model of the space shuttle orbiter that were arranged in a preliminary configuration of the shuttle entry <span class="hlt">air</span> data system (SEADS). <span class="hlt">Pressures</span> from those and auxiliary orifices were evaluated for their ability to provide <span class="hlt">air</span> data at subsonic and transonic speeds. The orifices were on the vehicle's nose cap and on the sides of the forebody forward of the cabin. The investigation covered a Mach number range of 0.25 to 1.40 and an angle of attack range from 4 deg. to 18 deg. An <span class="hlt">air</span> data system consisting of nose cap and forebody fuselage orifices constitutes a complete and accurate <span class="hlt">air</span> data system at subsonic and transonic speeds. For Mach numbers less than 0.80 orifices confined to the nose cap can be used as a complete and accurate <span class="hlt">air</span> data system. <span class="hlt">Air</span> data systems that use only flush <span class="hlt">pressure</span> orifices can be used to determine basic <span class="hlt">air</span> data on other aircraft at subsonic and transonic speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3986987','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3986987"><span>Effects of Moderate Strength Cold <span class="hlt">Air</span> Exposure on Blood <span class="hlt">Pressure</span> and Biochemical Indicators among Cardiovascular and Cerebrovascular Patients</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Zhang, Xiakun; Zhang, Shuyu; Wang, Chunling; Wang, Baojian; Guo, Pinwen</p> <p>2014-01-01</p> <p>The effects of cold <span class="hlt">air</span> on cardiovascular and cerebrovascular diseases were investigated in an experimental study examining blood <span class="hlt">pressure</span> and biochemical indicators. Zhangye, a city in Gansu Province, China, was selected as the experimental site. Health screening and blood tests were conducted, and finally, 30 cardiovascular disease patients and 40 healthy subjects were recruited. The experiment was performed during a cold event during 27–28 April 2013. Blood <span class="hlt">pressure</span>, catecholamine, angiotensin II (ANG-II), cardiac troponin I (cTnI), muscle myoglobin (Mb) and endothefin-1 (ET-1) levels of the subjects were evaluated 1 day before, during the 2nd day of the cold exposure and 1 day after the cold <span class="hlt">air</span> exposure. Our results suggest that cold <span class="hlt">air</span> exposure increases blood <span class="hlt">pressure</span> in cardiovascular disease patients and healthy subjects via the sympathetic nervous system (SNS) that is activated first and which augments ANG-II levels accelerating the release of the norepinephrine and stimulates the renin-angiotensin system (RAS). The combined effect of these factors leads to a rise in blood <span class="hlt">pressure</span>. In addition, cold <span class="hlt">air</span> exposure can cause significant metabolism and secretion of Mb, cTnI and ET-1 in subjects; taking the patient group as an example, ET-1 was 202.7 ng/L during the cold <span class="hlt">air</span> exposure, increased 58 ng/L compared with before the cold <span class="hlt">air</span> exposure, Mb and cTnI levels remained relatively high (2,219.5 ng/L and 613.2 ng/L, increased 642.1 ng/L and 306.5 ng/L compared with before the cold <span class="hlt">air</span> exposure, respectively) 1-day after the cold exposure. This showed that cold <span class="hlt">air</span> can cause damage to patients’ heart cells, and the damage cannot be rapidly repaired. Some of the responses related to the biochemical markers indicated that cold exposure increased cardiovascular strain and possible myocardial injury. PMID:24583830</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24583830','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24583830"><span>Effects of moderate strength cold <span class="hlt">air</span> exposure on blood <span class="hlt">pressure</span> and biochemical indicators among cardiovascular and cerebrovascular patients.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zhang, Xiakun; Zhang, Shuyu; Wang, Chunling; Wang, Baojian; Guo, Pinwen</p> <p>2014-02-27</p> <p>The effects of cold <span class="hlt">air</span> on cardiovascular and cerebrovascular diseases were investigated in an experimental study examining blood <span class="hlt">pressure</span> and biochemical indicators. Zhangye, a city in Gansu Province, China, was selected as the experimental site. Health screening and blood tests were conducted, and finally, 30 cardiovascular disease patients and 40 healthy subjects were recruited. The experiment was performed during a cold event during 27-28 April 2013. Blood <span class="hlt">pressure</span>, catecholamine, angiotensin II (ANG-II), cardiac troponin I (cTnI), muscle myoglobin (Mb) and endothefin-1 (ET-1) levels of the subjects were evaluated 1 day before, during the 2nd day of the cold exposure and 1 day after the cold <span class="hlt">air</span> exposure. Our results suggest that cold <span class="hlt">air</span> exposure increases blood <span class="hlt">pressure</span> in cardiovascular disease patients and healthy subjects via the sympathetic nervous system (SNS) that is activated first and which augments ANG-II levels accelerating the release of the norepinephrine and stimulates the renin-angiotensin system (RAS). The combined effect of these factors leads to a rise in blood <span class="hlt">pressure</span>. In addition, cold <span class="hlt">air</span> exposure can cause significant metabolism and secretion of Mb, cTnI and ET-1 in subjects; taking the patient group as an example, ET-1 was 202.7 ng/L during the cold <span class="hlt">air</span> exposure, increased 58 ng/L compared with before the cold <span class="hlt">air</span> exposure, Mb and cTnI levels remained relatively high (2,219.5 ng/L and 613.2 ng/L, increased 642.1 ng/L and 306.5 ng/L compared with before the cold <span class="hlt">air</span> exposure, respectively) 1-day after the cold exposure. This showed that cold <span class="hlt">air</span> can cause damage to patients' heart cells, and the damage cannot be rapidly repaired. Some of the responses related to the biochemical markers indicated that cold exposure increased cardiovascular strain and possible myocardial injury.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24705688','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24705688"><span>Organization of microbeads in Leidenfrost <span class="hlt">drops</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Maquet, Laurent; Colinet, Pierre; Dorbolo, Stéphane</p> <p>2014-06-21</p> <p>We investigated the organization of micrometric hydrophilic beads (glass or basalt) immersed in Leidenfrost <span class="hlt">drops</span>. Starting from a large volume of water compared to the volume of the beads, while the liquid evaporates, we observed that the grains are eventually trapped at the interface of the droplet and accumulate. At a moment, the grains entirely cover the droplet. We measured the surface area at this moment as a function of the total mass of particles inserted in the droplet. We concluded that the grains form a monolayer around the droplet assuming (i) that the packing of the beads at the surface is a random close packing and (ii) that the initial surface of the <span class="hlt">drop</span> is larger than the maximum surface that the beads can cover. Regarding the evaporation dynamics, the beads are found to reduce the evaporation rate of the <span class="hlt">drop</span>. The slowdown of the evaporation is interpreted as being the consequence of the dewetting of the particles located at the droplet interface which makes the effective surface of evaporation smaller. As a matter of fact, contact angles of the beads with the water deduced from the evaporation rates are consistent with contact angles of beads directly measured at a flat <span class="hlt">air</span>-water interface of water in a container.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/56232','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/56232"><span><span class="hlt">Dropping</span> fire retardants by helicopter: tests of three new helitanks</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>James B. Davis</p> <p>1963-01-01</p> <p>Late model helicopters equipped with new helitanks and adequately supplied can accurately deliver as much fire retardant as most fixed-wing <span class="hlt">air</span> tankers at a potentially lower cost. Viscous water <span class="hlt">dropped</span> from helicopters clung to fuel surfaces and was concentrated in a narrower pattern than plain water.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27729399','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27729399"><span>Stability and Agreement of a Microtransducer and an <span class="hlt">Air</span>-Filled Balloon Esophageal Catheter in the Monitoring of Esophageal <span class="hlt">Pressure</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Augusto, Renan Maloni; Albuquerque, André Luis Pereira; Jaeger, Thomas; de Carvalho, Carlos Roberto Ribeiro; Caruso, Pedro</p> <p>2017-02-01</p> <p>The use of esophageal catheters with microtransducer promises advantages over traditional catheters with <span class="hlt">air</span>-filled balloons. However, performance comparisons between these 2 types of catheters are scarce and incomplete. A catheter with a 9.5-cm <span class="hlt">air</span>-filled balloon at the distal tip and a catheter with a microtransducer mounted within a flexible silicone rubber were tested in vitro and in vivo. In vitro, the response times of both catheters were compared, and the drift of the baseline <span class="hlt">pressure</span> of the microtransducer catheter was evaluated over a 6-h period. In vivo, 11 healthy volunteers had both catheters inserted, and the drift of the baseline esophageal <span class="hlt">pressure</span> was measured over a 3-h period. Also, the correlation and agreement of the baseline and changes in the esophageal <span class="hlt">pressure</span> of both catheters were evaluated. In vitro, the microtransducer catheter had a response time significantly higher (262 × 114 Hz, P < .01) and a good <span class="hlt">pressure</span> stability, with a mean baseline <span class="hlt">pressure</span> drift of 1.4 cm H 2 O. In vivo, both catheters presented a small and similar baseline esophageal <span class="hlt">pressure</span> drift (P = 0.08). For measurements of baseline and changes in esophageal <span class="hlt">pressure</span>, the correlation and agreement between the catheters were poor, with a large bias between them. The catheter with the microtransducer had a small baseline <span class="hlt">pressure</span> drift, similar to the <span class="hlt">air</span>-filled balloon catheter. The low agreement between the catheters does not allow the microtransducer catheter to be used as a surrogate for the traditional <span class="hlt">air</span>-filled balloon catheter. Copyright © 2017 by Daedalus Enterprises.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23710577','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23710577"><span>Intraoperative assessment of intraocular <span class="hlt">pressure</span> in vitrectomized <span class="hlt">air</span>-filled and fluid-filled eyes.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Moon, Chan Hee; Choi, Kyung Seek; Rhee, Mi Ri; Lee, Sung Jin</p> <p>2013-11-01</p> <p>To ascertain the difference of intraocular <span class="hlt">pressure</span> (IOP) measurement between vitrectomized <span class="hlt">air</span>-filled and fluid-filled eyes. Thirty-one eyes of 31 consecutive patients who underwent conventional vitrectomy and intraocular gas tamponade were assessed. After vitrectomy, IOP of the fluid-filled eyes was measured by Tono-Pen. Thereafter, fluid-<span class="hlt">air</span> exchange was performed, and IOP of the <span class="hlt">air</span>-filled eyes was measured again. The IOP within each fluid- and <span class="hlt">air</span>-filled eye was varied by selecting settings on the vitrectomy system, from 10 to 50 mmHg with 5-mmHg increments. Postoperatively, IOP was assessed by both Tono-Pen and Goldmann applanation tonometry (GAT). Linear and nonlinear regression analyses were conducted between intraoperatively measured Tono-Pen readings and actual IOPs. Bland-Altman plot was used to assess the agreements between postoperatively measured Tono-Pen readings and GAT readings. The discrepancy between Tono-Pen readings and actual IOP in fluid-filled eyes was not significant, except for the profound high <span class="hlt">pressures</span> over 45 mmHg. However, Tono-Pen readings in <span class="hlt">air</span>-filled eyes were significantly lower than actual IOPs in all ranges, and Tono-Pen increasingly underestimates IOP at higher levels. Intraoperative Tono-Pen readings were correlated significantly with actual IOP and a quadratic equation evidenced the best fit (R(2) = 0.996). Postoperatively, difference of the measurements between Tono-Pen and GAT was not significant. Tono-Pen and GAT significantly underestimate actual IOP in <span class="hlt">air</span>-filled eyes. It should be considered that actual IOP would be greater than the measured IOP in gas-filled eyes, even though the IOP is measured as normal. © 2013 Acta Ophthalmologica Scandinavica Foundation. Published by John Wiley & Sons Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012JBIS...65...71O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012JBIS...65...71O"><span>Short Duration Reduced Gravity <span class="hlt">Drop</span> Tower Design and Development</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Osborne, B.; Welch, C.</p> <p></p> <p>The industrial and commercial development of space-related activities is intimately linked to the ability to conduct reduced gravity research. Reduced gravity experimentation is important to many diverse fields of research in the understanding of fundamental and applied aspects of physical phenomena. Both terrestrial and extra-terrestrial experimental facilities are currently available to allow researchers access to reduced gravity environments. This paper discusses two <span class="hlt">drop</span> tower designs, a 2.0 second facility built in Australia and a proposed 2.2 second facility in the United Kingdom. Both <span class="hlt">drop</span> towers utilise a drag shield for isolating the falling experiment from the drag forces of the <span class="hlt">air</span> during the test. The design and development of The University of Queensland's (Australia) 2.0 second <span class="hlt">drop</span> tower, including its specifications and operational procedures is discussed first. Sensitive aspects of the design process are examined. Future plans are then presented for a new short duration (2.2 sec) ground-based reduced gravity <span class="hlt">drop</span> tower. The new <span class="hlt">drop</span> tower has been designed for Kingston University (United Kingdom) to support teaching and research in the field of reduced gravity physics. The design has been informed by the previous UQ <span class="hlt">drop</span> tower design process and utilises a catapult mechanism to increase test time and also incorporates features to allow participants for a variety of backgrounds (from high school students through to university researchers) to learn and experiment in reduced gravity. Operational performance expectations for this new facility are also discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27324623','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27324623"><span>Quasi-adiabatic vacuum-based column housing for very high-<span class="hlt">pressure</span> liquid chromatography.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Gritti, Fabrice; Gilar, Martin; Jarrell, Joseph A</p> <p>2016-07-22</p> <p>A prototype vacuum-based (10(-6)Torr) column housing was built to thermally isolate the chromatographic column from the external <span class="hlt">air</span> environment. The heat transfer mechanism is solely controlled by surface radiation, which was minimized by wrapping the column with low-emissivity aluminum tape. The adiabaticity of the column housing was quantitatively assessed from the measurement of the operational <span class="hlt">pressure</span> and fluid temperature at the outlet of a 2.1mm×100mm column (sub-2 μm particles). The <span class="hlt">pressure</span> <span class="hlt">drop</span> along the column was raised up to 1kbar. The enthalpy balance of the eluent (water, acetonitrile, and one water/acetonitrile mixture, 70/30, v/v) showed that less than 1% of the viscous heat generated by friction of the fluid against the packed bed was lost to the external <span class="hlt">air</span> environment. Such a vacuum-based column oven minimizes the amplitude of the radial temperature gradients across the column diameter and maximizes its resolving power. Copyright © 2016 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2010-title14-vol1/pdf/CFR-2010-title14-vol1-sec29-1325.pdf','CFR'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2010-title14-vol1/pdf/CFR-2010-title14-vol1-sec29-1325.pdf"><span>14 CFR 29.1325 - Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2010&page.go=Go">Code of Federal Regulations, 2010 CFR</a></p> <p></p> <p>2010-01-01</p> <p>... between <span class="hlt">air</span> <span class="hlt">pressure</span> in the static <span class="hlt">pressure</span> system and true ambient atmospheric static <span class="hlt">pressure</span> is not... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter...: Installation § 29.1325 Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems. (a) Each instrument with static <span class="hlt">air</span> case...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2011-title14-vol1/pdf/CFR-2011-title14-vol1-sec29-1325.pdf','CFR2011'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2011-title14-vol1/pdf/CFR-2011-title14-vol1-sec29-1325.pdf"><span>14 CFR 29.1325 - Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2011&page.go=Go">Code of Federal Regulations, 2011 CFR</a></p> <p></p> <p>2011-01-01</p> <p>...: Installation § 29.1325 Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems. (a) Each instrument with static <span class="hlt">air</span> case... between <span class="hlt">air</span> <span class="hlt">pressure</span> in the static <span class="hlt">pressure</span> system and true ambient atmospheric static <span class="hlt">pressure</span> is not... 14 Aeronautics and Space 1 2011-01-01 2011-01-01 false Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2012-title14-vol1/pdf/CFR-2012-title14-vol1-sec29-1325.pdf','CFR2012'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2012-title14-vol1/pdf/CFR-2012-title14-vol1-sec29-1325.pdf"><span>14 CFR 29.1325 - Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2012&page.go=Go">Code of Federal Regulations, 2012 CFR</a></p> <p></p> <p>2012-01-01</p> <p>...: Installation § 29.1325 Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems. (a) Each instrument with static <span class="hlt">air</span> case... between <span class="hlt">air</span> <span class="hlt">pressure</span> in the static <span class="hlt">pressure</span> system and true ambient atmospheric static <span class="hlt">pressure</span> is not... 14 Aeronautics and Space 1 2012-01-01 2012-01-01 false Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2013-title14-vol1/pdf/CFR-2013-title14-vol1-sec29-1325.pdf','CFR2013'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2013-title14-vol1/pdf/CFR-2013-title14-vol1-sec29-1325.pdf"><span>14 CFR 29.1325 - Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2013&page.go=Go">Code of Federal Regulations, 2013 CFR</a></p> <p></p> <p>2013-01-01</p> <p>...: Installation § 29.1325 Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems. (a) Each instrument with static <span class="hlt">air</span> case... between <span class="hlt">air</span> <span class="hlt">pressure</span> in the static <span class="hlt">pressure</span> system and true ambient atmospheric static <span class="hlt">pressure</span> is not... 14 Aeronautics and Space 1 2013-01-01 2013-01-01 false Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.gpo.gov/fdsys/pkg/CFR-2014-title14-vol1/pdf/CFR-2014-title14-vol1-sec29-1325.pdf','CFR2014'); return false;" href="https://www.gpo.gov/fdsys/pkg/CFR-2014-title14-vol1/pdf/CFR-2014-title14-vol1-sec29-1325.pdf"><span>14 CFR 29.1325 - Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems.</span></a></p> <p><a target="_blank" href="http://www.gpo.gov/fdsys/browse/collectionCfr.action?selectedYearFrom=2014&page.go=Go">Code of Federal Regulations, 2014 CFR</a></p> <p></p> <p>2014-01-01</p> <p>...: Installation § 29.1325 Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter systems. (a) Each instrument with static <span class="hlt">air</span> case... between <span class="hlt">air</span> <span class="hlt">pressure</span> in the static <span class="hlt">pressure</span> system and true ambient atmospheric static <span class="hlt">pressure</span> is not... 14 Aeronautics and Space 1 2014-01-01 2014-01-01 false Static <span class="hlt">pressure</span> and <span class="hlt">pressure</span> altimeter...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=fourier&pg=5&id=EJ1008062','ERIC'); return false;" href="https://eric.ed.gov/?q=fourier&pg=5&id=EJ1008062"><span>A Comparative Study of Sound Speed in <span class="hlt">Air</span> at Room Temperature between a <span class="hlt">Pressure</span> Sensor and a Sound Sensor</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Amrani, D.</p> <p>2013-01-01</p> <p>This paper deals with the comparison of sound speed measurements in <span class="hlt">air</span> using two types of sensor that are widely employed in physics and engineering education, namely a <span class="hlt">pressure</span> sensor and a sound sensor. A computer-based laboratory with <span class="hlt">pressure</span> and sound sensors was used to carry out measurements of <span class="hlt">air</span> through a 60 ml syringe. The fast Fourier…</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_25 --> <div class="footer-extlink text-muted" style="margin-bottom:1rem; text-align:center;">Some links on this page may take you to non-federal websites. 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