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Pressure

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• Force and energy

• Pressure -- Measurement
• Atmospheric pressure
• Body fluids -- Pressure
• Compressibility
• Earth pressure
• High pressure (Science)
• Hydrostatic pressure
• Low pressure (Science)
• Radiation pressure
• Reservoir oil pressure
• Sound pressure
• Thermomolecular pressure
• Wind-pressure

• Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Ralph L. Schacht, Arthur W. Goldstein, Richard R. Cullom, and Lewis Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Jr. Stallings, Paige B. Burbank, and Langley Research Center (page images at HathiTrust)
• Interface test for evaluating ability of pressure-suited subjects to perform lunar scientific tasks / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1965), by Earl V. LaFevers, Curtis C. Mason, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Effects of pressure, oxygen concentration, and forced convection on flame spread rate of Plexiglas, nylon, and Teflon / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Julius J. Notardonato, Thomas H. Cochran, Leo A. Burkhardt, and Lewis Research Center (page images at HathiTrust)
• Sluice pressures, gate vibrations and stilling basin wall pressures, Libby Dam, Kootenai River, Montana : final report / (Vicksburg, Miss. : Dept. of Defense, Army, Corps of Engineers, Waterways Experiment Station, 1976), by E. Dale Hart, Allen R. Tool, Vicksburg United States. Waterways Experiment Station, and United States. Army. Corps of Engineers. Seattle District (page images at HathiTrust)
• Instrumentation, field operations, and data processing for PMEL deep ocean bottom pressure measurements / (Seattle, Wash. : U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Pacific Marine Environmental Laboratory ; Springfield, VA : For sale by the National Technical Information Service, [1989]), by M. C Eble and Pacific Marine Environmental Laboratory (U.S.) (page images at HathiTrust)
• Analysis of condensing pressure control for SNAP-8 system / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Donald R. Packe and Lewis Research Center (page images at HathiTrust)
• Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Robert S. Osborne, Virginia C. Stafford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of Mach number on pitot-probe displacment in a turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jerry M. Allen and Langley Research Center (page images at HathiTrust)
• An investigation of a 0.05-scale model of the XSM-64A Navaho missile and booster at supersonic mach numbers. (Washington : National Aeronautics and Space Administration, [1959]), by James D. Church, Nancy L. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of geometric variables on the performance of a probe for direct measurement of free-stream stagnation pressure in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Lana M. Couch and Langley Research Center (page images at HathiTrust)
• Condensing pressure drop by improved Lockhart-Martinelli method / ([Washington] : National Aeronautics and Space Administration, [1964]), by Fred L. Robson, Winthrop E. Hilding, University of Connecticut, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by Lloyd S. Jernell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by James Wayne Sawyer, Charles F. Whitcomb, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental determination of pressure drop and flow characteristics of dilute gas-solid suspensions / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by Robert Pfeffer, Salvatore J. Rossetti, Lewis Research Center, and City University of New York. City College (page images at HathiTrust)
• Panel flutter tests on full-scale X-15 lower vertical stabilizer at Mach number of 3.0 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1962), by Herman L. Bohon, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Liquid-filled transient pressure measuring systems : a method for determining frequency respose / ([Washington, D.C.] : National Aeronautics and Space Administration, [Scientific and Technical Information Branch], [1971?]), by Robert C. Anderson, David R. Englund, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Pressure-viscosity measurements for several lubricants to 5.5 x 10⁸ newtons per square meter (8 x 10⁴ psi) and 149 ̊C (300 ̊F) / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by William R. Jones and Lewis Research Center (page images at HathiTrust)
• Investigation of an anomalous flow condition of the Langley pilot model expansion tube / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Wilfred J. Friesen and Langley Research Center (page images at HathiTrust)
• Flight-measured inlet pressure transients accompanying engine compressor surges on the F-111A airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jack Nugent, Jon K. Holzman, and Flight Research Center (U.S.) (page images at HathiTrust)
• Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Morton Cooper, Charles R. Gunn, and Langley Research Center (page images at HathiTrust)
• Lateral pressure of grain in bins / (June 1903), by Albert Grafton Varnes (page images at HathiTrust; US access only)
• Time and pressure measurments [sic] in the corona / (1920), by Charles Stever Fazel (page images at HathiTrust; US access only)
• Laboratory tests of a hydraulic pressure surge reliever / (Denver, Colo. : Hydraulics Branch, Division of Research, Engineering and Research Center, U.S. Dept. of the Interior, Bureau of Reclamation, [1983]), by B. W. Mefford and Engineering and Research Center (U.S.). Hydraulics Branch (page images at HathiTrust)
• Hazard summary report on the Experimental Boiling Water Reactor (EBWR) / (Argonne, Ill. : Argonne National Laboratory, [1958]), by J. M. West and Argonne National Laboratory (page images at HathiTrust)
• Boiling water reactor technology status of the art report : Volume 1. Heat transfer and hydraulics / (Argonne, Ill. : Argonne National Laboratory, Reactor Engineering Division, 1962), by P. A. Lottes and Argonne National Laboratory (page images at HathiTrust)
• Zone therapy, or, Relieving pain and disease / (Hartford, Conn. : M.C. Hillery, 1919), by Wm. H. Fitzgerald and Edwin F. Bowers (page images at HathiTrust)
• Prototype filling and emptying system measurements, New Bankhead Lock, Black Warrior River, Alabama / (Vicksburg, Miss. : U.S. Army Engineer Waterways Experiment Station, [1980]), by Allen R. Tool, U.S. Army Engineer Waterways Experiment Station, U.S. Army Engineer Waterways Experiment Station. Hydraulics Laboratory, and United States. Army. Corps of Engineers. Mobile District (page images at HathiTrust)
• Piëzodynamische onderzoekingen. (Amsterdam, [1914]), by H. F. G. Kaiser (page images at HathiTrust; US access only)
• Pressure loss and heat transfer for turbulent flow. ([Oak Ridge, Tenn.] U. S. Atomic Energy Commission, Office of Technical Information, 1960), by Rudolph Koch (page images at HathiTrust)
• The effect of different homogenization process on the physical properties of an ice cream mixture and the resulting ice crem when the percentage of fat is varied and the solids not fat remain constant / (Columbia, Mo. : University of Missouri, College of Agriculture, Agricultural Experiment Station, 1930), by William Herbert Eddy Reid and L. B. Russell (page images at HathiTrust; US access only)
• Research directed toward the use of synoptic simulation to develop forecast models compatible for use in system 433L. (Ft. Belvoir : Defense Technical Information Center, 14 Jun 1962), by J. T. Hilworth, P. W. Funke, W. R. Biggers, S. J. Donaldson, R. J. Shafer, and Inc. Eastern Air Lines (page images at HathiTrust; US access only)
• Investigations on the basic theory of static and dynamic pressure phenomena in grain under conditions of storage (Hyattsville, Md.] : U.S. Agricultural Research Service, 1971), by Joel D. Isaacson (page images at HathiTrust)
• An experimental study of the pressure and heat-transfer distribution on a 70° sweep slab delta wing in hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1963), by Mitchel H. Bertram, Philip E. Everhart, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• On the dynamics of short pressure probes : some design factors affecting frequency response / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Ted W. Nyland, Robert C. Anderson, David R. Englund, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Calculated pressure-induced vibrational absorption in H₂ - H₂ collisions in hydrogen gas / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by R. W. Patch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Simon C. Sommer and Ames Research Center (page images at HathiTrust)
• Analysis of developing laminar flow and heat transfer in a tube for a gas with cooling / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Alden F. Presler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Pressure distribution on models of the SL-7 containership and Great Lakes bulk carrier S.J. Cort in waves. ([Washington, D.C.] : Ship Structure Committee ; [Springfield, Va. : National Technical Information Service, distributor], 1983), by University of Michigan. Dept. of Naval Architecture and Marine Engineering and United States. Ship Structure Committee (page images at HathiTrust)
• A method of rating fumigation chambers for tightness / ([Washington, D.C. : U.S. Department of Agriculture, Bureau of Entomology and Plant Quarantine, 1945]), by R. D. Chisholm, Louis Koblitsky, and United States. Bureau of Entomology and Plant Quarantine (page images at HathiTrust)
• Simulation of turbulent wall pressure / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Information Service, 1978), by Robert L. Ash, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,), by Terry J. Larson and Ames Research Center (page images at HathiTrust)
• Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream mach numbers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : for sale by the National Technical Information Service], 1979), by Mary L. Mason, Lawrence E. Putnam, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Charles B. Johnson, P. Calvin Stainback, and Langley Research Center (page images at HathiTrust)
• The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Elizabeth B. Plentovich and Langley Research Center (page images at HathiTrust)
• Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Elizabeth B. Plentovich, Blair B. Gloss, and Langley Research Center (page images at HathiTrust)
• Flight measurements of surface pressures on a flexible supercritical research wing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Clinton V. Eckstrom and Langley Research Center (page images at HathiTrust)
• Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by John B. McDevitt, Arthur F. Okuno, and Ames Research Center (page images at HathiTrust)
• Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Charles G. Miller, Peter A. Gnoffo, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optical zero-differential pressure switch and its evaluation in a multiple-pressure measuring system / (Washington : National Aeronautics and Space Adinistration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by J. Anthony Powell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of effect of jet decay rate on jet-induced pressures on a flat plate / (Washington : National Aeronautics and Space Administration, Scientfic and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by John M. Kuhlman, Ronald W. Warcup, Don S. Ousterhout, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Study of wetting and nonwetting mercury condensing pressure drops / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Alfred Koestel, Robert T. Wainwright, Martin U. Gutstein, and Lewis Research Center (page images at HathiTrust)
• Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Joesph W. Jewel and Langley Research Center (page images at HathiTrust)
• Effect of cover gas pressures on accelerated cavitation damage in sodium / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1867]), by Stanley G. Young, James R. Johnston, and Lewis Research Center (page images at HathiTrust)
• Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1962), by P. Calvin Stainback and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Structural feasibility study of pressurized tanks for liquid-methane fueled supersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Rene E. Chambellan, William A. Bevevino, Joseph F. Lubomski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mixing of supersonic jets including the effects of transvere pressure gradient using difference methods / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Anatole P. Kurkov, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Correction of pressure data for thermal transpiration effects in pneumatic lines / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by James A. Daggerhart, Langley Research Center, and North Carolina State University (page images at HathiTrust)
• Tests of a single-tube-in-shell water boiler with helical-wire insert, inlet nozzle, and two different inlet-region plugs / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by James R. Stone, Nick J. Sekas, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Survey of literature on flow characteristics of a single turbulent jet impinging on a flat plate. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1970]), by James W. Gauntner, Peter Hrycak, John N. B. Livingood, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of fluid temperature on the cavitation performance of a high hub-tip ratio axial flow pump in water to 250 ̊F (394 K) (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], [1969]), by Walter S. Cunnan, Dean C. Reemsnyder, George Kovich, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An improved method for calculating supersonic pressure fields about bodies of revolution / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Robert J. Mack, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of trailing edge geometry and thickness on the performance of certain turbine stator blading. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1972]), by Herman W. Prust, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 ̊to 15 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by Robert L. Stallings, Dorothy T. Howell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of composition on combustion of solid propellants during a rapid pressure decrease / (Washington, D.C. : National Aeronautics and Space Administration, 1962), by Carl C. Ciepluch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Base heat transfer, pressure ratios, and configuration effects obtained on a 1/27 scall saturn (C-1) model at mach numbers from 0.1 to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by John L. Allen, Robert A. Wasko, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Approximate treatment of V/STOL wall interference for closed circular tunnels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Harry H. Heyson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Zone therapy; or, Relieving pain at home, (Columbus, O. : I. W. Long, 1917), by Wm. H. Fitzgerald and Edwin F. Bowers (page images at HathiTrust; US access only)
• Absorption rate sticking probabilities for oxygen on columbium and dilute columbium-zirconium alloys / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), by Charles A. Barrett, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Heat-transfer and pressure distributions due to sinusoidal distortions on a flat plate at Mach 20 in helium / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by James P. Arrington, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Random pressure excitation of shells and statistical dependence effect of normal mode response / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by Robert E. Davis (page images at HathiTrust; US access only)
• Study of new methods to measure low pressure. ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1968]), by Richard Hecht, Langley Research Center, and National Research Corporation (U.S.) (page images at HathiTrust; US access only)
• Effects of pressure and dielectric constant on sound absorption in magnesium sulfate solutions / (Cambridge, Mass. : Acoustics Research Laboratory, Division of Engineering and Applied Physics, Harvard University, [1962]), by Frederick Hendrick Fisher (page images at HathiTrust; US access only)
• Untersuchungen über den Drucksinn vermittlest der von Prof. Dr. Landois angegebenen Quecksilberdruckwage. (Greifswald, J. Abel, 1881), by Matthias Theodor Kruth and L. Landois (page images at HathiTrust)
• Om det osmotiske tryks natur /, by Ferdinand Barmwater (page images at HathiTrust; US access only)
• Experimental base pressures on 9 ̊spherically blunted cones at Mach numbers from 10.5 to 20 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Charles G. Miller and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Bibliography and index on vacuum and low pressure measurement. ([Washington], 1961), by W. G. Brombacher (page images at HathiTrust)
• A test method for determining the effect of thermal transients on pressure-transducer response / (Washington : U.S. Dept. of Commerce, National Bureau of Standards, Institute for Applied Technology, Electronic Technology Division : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1976), by John S. Hilten, Sandia Laboratories, United States. Naval Air Systems Command, and Institute for Applied Technology (U.S.). Electronic Technology Division (page images at HathiTrust)
• LOFT experimental measurements uncertainty analyses / (Washington, D.C. : The Commission, [1978- ]), by Gordon D. Lassahn, Idaho National Engineering Laboratory, EG & G Idaho, United States. Department of Energy. Idaho Operations Office, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• An investigation of certain thermodynamic and transport properties of water and water vapor in the critical region / (Lemont, Ill. : Argonne National Laboratory, 1959), by E. S. Nowak, R. J. Grosh, and Argonne National Laboratory (page images at HathiTrust)
• Development of dynamic calibration methods for pogo pressure transducers / (Washington : Dept. of Commerce, National Bureau of Standards. Institute for Applied Technology, Electronic Technology Division : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1976), by John S. Hilten and Institute for Applied Technology (U.S.). Electronic Technology Division (page images at HathiTrust)
• Surface pressure fluctuations near an axisymmetric stagnation point / (Washington : U.S. National Bureau of Standards : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1971), by Richard D. Marshall (page images at HathiTrust)
• Steam chugging in pressure suppression containment : final report, July 1976 - July 1979 / (Washington, D.C. : The Commission : Available from GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 1980), by C. K. B. Lee, C. K. Chan, Nuclear Regulatory Commission. Division of Reactor Safety Research, and Los Angeles. Chemical University of California (page images at HathiTrust)
• Summary report of pressure sensor for the loss of fluid test (LOFT) reactor / (Washington, D.C. : The Division, 1981), by T. R. Billeter, Hanford Engineering Development Laboratory, and Fuel Cycle U.S. Nuclear Regulatory Commission. Division of Safeguards (page images at HathiTrust)
• Theoretical investigation of pressure pulse development during steam condensation in the pressure reducing system of boiling water reactors : - computer program KONDAS - / (Washington, D.C. : U.S. Nuclear Regulatory Commission, 1978), by G. Class, U.S. Nuclear Regulatory Commission, and Kernforschungszentrum Karlsruhe. Institut für Reaktorentwicklung. Projekt Nukleare Sicherheit (page images at HathiTrust)
• Research program for basic and plant-oriented pressure suppression tests on the PSS test stand = (Versuchsprogramm für grundlegende und anlagenorientierte Druckabbauversuche auf dem PSS-Versuchsstand der GKSS) : draft / (Washington, D.C. : U.S. Nuclear Regulatory Commission, 1978), by E. Aust, U.S. Nuclear Regulatory Commission, and Gesellschaft für Kernenergieverwertung in Schiffbau und Schiffahrt (Germany) (page images at HathiTrust)
• Calculation of convection heat transfer to non-isothermal surfaces exposed to a fluid stream with wedge type surface pressure gradient /, by J. P. Hartnett, E. R. G. Eckert, Roland Birkebak, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, and Wright Air Development Center (page images at HathiTrust)
• Correlations between transverse and torsional shear creep deformations /, by Joseph Marin, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center (page images at HathiTrust)
• Semiscale blowdown and emergency core cooling (ECC) project test report -- test 803 through 820 /, by Harry W. Heiselmann, J. F. Whitbeck, D. J. Olson, sponsor U.S. Atomic Energy Commission. Idaho Operations Office, issuing body Allied Chemical Corporation, and issuing body Aerojet-General Corporation (page images at HathiTrust)
• Performance of trailing aerodynamic decelerators at high dynamic pressures : Phases V and VI /, by B. A. Engstrom, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
• Pilot plant studies of atmospheric and pressure leaching of uranium ores in alkaline solutions : topical report WIN-73 /, by R. G. Beverly, W. A. Millsap, G. Winslow, National Lead Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effects of temperature and pressure on gypsum and anhydrite /, by Marie Farnsworth and United States Bureau of Mines (page images at HathiTrust)
• Piezoelectric polymer transducers for dynamic pressure measurements. Final report. (1977), by Aime S. DeReggi, Scymour Edelman, and Steven C. Roth (page images at HathiTrust)
• Evaluation of the performance of child restraint systems. Final report. (1988), by K. N. Naab (page images at HathiTrust)
• Dynamic pressure measurement devices in nuclear reactors / ([Idaho Falls, Idaho] : U.S. Atomic Energy Commission, Idaho Operations Office, 1964), by P. H. Hofhine, Phillips Petroleum Company. Atomic Energy Division, and Idaho National Reactor Testing Station (page images at HathiTrust)
• A piezo-electric method for the instantaneous measurement of high pressures / ([Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1922]), by John Clarence Karcher and United States. National Bureau of Standards. Scientific Papers (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Alexander Mendelson, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• An inlet design concept to reduce flow distortion at angle of attack / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Carl F. Schueller, Leonard E. Stitt, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Louis W. Habel, Donald R. Bowman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Leonard W. Putland, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Charts of pressure rise obtainable with airfoil-type axial-flow cooling fans / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1947), by A. Kahane and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transient behavior of lumped-constant systems for sensing gas pressures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Gene J. Delio, Richard S. Cesaro, Glennon V. Schwent, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Momentum transport in packed columns using stochastic models / (Ames, Iowa : Ames Laboratory, Iowa State University of Science and Technology, 1963), by Charles Burrell Schriver, Raymond W. Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Correlation of data for pressure loss in a cannular J-73 combustor / (Cincinnati, OH. : Technical Publications, 1957), by R. E. Motsinger, U.S. Atomic Energy Commission, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
• Vibration effects on the Taylor 206R pressure transmitter,, by A. H. Fowler, G. H. Job, Carbide and Carbon Chemicals Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Vibration effects on the Taylor 206R pressure transmitter., by G. H. Job, J. A. Owen, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Comparative measurements of total temperature in a supersonic turbulent boundary layer using a conical equilibrium and combined temperature-pressure probe. /, by R. L. P. Voisinet, H. U. Meier, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Piezoelectric polymer transducer for impact pressure measurement. Final report. (1975), by Aime S. DeReggi (page images at HathiTrust)
• Experimental investigation of truck tire inflation pressure on pavement-tire contact area and pressure distribution. Interim report. (1985), by Kurt M. Marshek, W. Ronald Hudson, R. B. Connell, H. H. Chen, and C. L. Saraf (page images at HathiTrust)
• Truck tire pavement contact pressure distribution characteristics for super single 18-22.5 and smooth 11R24.5 tires. Interim report. (1989), by Rex William Hansen, C. Bertrand, Kurt M. Marshek, and W. Ronald Hudson (page images at HathiTrust)
• Air pumps at U.S. gas stations: an investigation into factors associated with gauge accuracy. (Washington, D.C.: National Center for Statistics and Analysis, Research and Development ; Springfield, Va. : National Technical Information Service, 2002), by J. A. Stevano (page images at HathiTrust)
• Making ventilation-pressure surveys with altimeters / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1957), by G. E. McElroy, D. S. Kingery, and United States Bureau of Mines (page images at HathiTrust)
• Pressure-relieving capacities of diaphragms and other devices for venting dust explosions / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1950), by John Nagy, Irving Hartmann, and J. E. Zellinger (page images at HathiTrust)
• A discussion of the transpiration method for determining vapor pressure / (Oak Ridge, Tenn. : Technical Information Division, Atomic Energy Commission, [1948]), by J. V. Lepore, J. R. Van Wazer, U.S. Atomic Energy Commission, and Carbide and Carbon Chemicals Corporation (page images at HathiTrust)
• Some effects of pressure on the hydrocracking of crude shale oil over cobalt molybdate catalyst / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, [1973]), by Clyde M. Frost, Philip L. Cottingham, Laramie Energy Research Center, University of Wyoming, and United States Bureau of Mines (page images at HathiTrust)
• A correlation of pressure buildup in oil wells with completion practice for a deep California field / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1957), by Frank C. Morris (page images at HathiTrust)
• Pressure development in laboratory dust explosions / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1964), by John Nagy, Joseph M. Stupar, and Austin R. Cooper (page images at HathiTrust)
• 100-ton test : mechanical impulse meter / (Oak Ridge, Tenn. : U.S. Atomic Energy Commission, Technical Information Division, 1950), by Theodore P. Jorgensen, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An experimental verification of a computer program for the calculation of oscillatory pressure attenuation in pneumatic transmission lines / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1965), by Geoffrey P. Watts, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Pressure drop and gas residence time for a four foot core / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, [1955]), by Leon Cooper, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Tests of a small-scale NACA submerged inlet at transonic Mach numbers / (Washington, D.C. : National Advisory Committee for Aeronautics, [1950]), by L. Stewart Rolls, George A. Rathert, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jet diffuser for simulating ram conditions on a turbojet-engine static test stand / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Robert H. Essig, David S. Gabriel, H. R. Bohanon, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Preliminary attempts at isothermal compression of a supersonic air stream / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by E. Perchonok, F. Wilcox, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by H. George Krull, William T. Beale, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by R. I. Sears, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects on adjacent surfaces from the firing of rocket jets / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Walter E. Bressette, Abraham Leiss, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The mechanism of pressure bonding / (Columbus, OH : Battelle Memorial Institute ; Washington, D.C. : Available from the Office of Technical Services, U.S. Dept. of Commerce, [1961]), by G. W. Cunningham, Joseph W. Spretnak, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Bernard N. Daley, Lillian E. Hanna, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Improvement of accuracy of balanced-pressure indicators and development of an indicator calibrating machine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by James C. Livengood and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of ejector thrust by integration of calculated surface pressures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by John C. Sanders, Virginia L. Brightwell, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight investigation of the variation of static-pressure error of a static-pressure tube with distance ahead of a wing and a fuselage / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by William Gracey, Elwood F. Scheithauer, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The near noise field of static jets and some model studies of devices for noise reduction / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Leslie W. Lassiter, Harvey H. Hubbard, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Efficacy of bentonite for control of seepage. (Vicksburg, Miss. : Waterways Experiment Station, 1938), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Leak rate versus absolute pressure studies completion report (Project D-P-0131) / (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Union Carbide Nuclear Company, 1961), by Joseph H. Keith, Oak Ridge Y-12 Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Pressure tests in flood-control conduits : Summersville Dam, Gauley River, West Virginia / (Vicksburg, Miss. : Waterways Experiment Station, 1968), by E. Dale Hart (page images at HathiTrust)
• Response of linear elastic transverse-isotropic media to borehole pressuremeter loadings : final report / (Vicksburg, Miss. : Waterways Experiment Station, 1978), by George Y. Baladi, Michael E. George, and United States. Defense Nuclear Agency (page images at HathiTrust)
• Instrumentation for granite test No. 1 / (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Division of Technical Information, [1974]), by Bert R. Dennis, Robert M. Potter, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• The effect of inlet temperature and pressure on the efficiency of a single-stage impulse turbine having a 13.2-inch pitch-line diameter wheel / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by Ernest R. Chanes, L. Robert Carman, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by David S. Gabriel, L. Robert Carman, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. 1 - Performance of a highly supercharged compression-ignition engine / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by J. C. Sanders, Alexander Mendelson, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine - 2 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1946]), by Henry E. Alquist, John C. Evvard, Leon O'Dell, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Pressure testing of zircaloy tubing /, by L. F. Cochrun, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• An absolute mass rate flowmeter /, by F. A. Guevara, W. E. Wageman, R. M. Potter, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Production of well known pressures of pure and mixed gases in the high-vacuum range /, by G. Schneppe and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• FFTF sodium service pressure measurement : state-of-the-art report /, by T. J. Crocker, Battelle Memorial Institute. Pacific Northwest Division. issuing body, U.S. Atomic Energy Commission, and Pacific Northwest Laboratory (page images at HathiTrust)
• Evaluation of a telemetry system for use in shock interaction experiments /, by David L. Merritt, Philip M. Aronson, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Handbook of blunt-body aerodynamics: volume 1 - static stability. /, by John A. Darling and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Quarterly technical progress report : fuels, materials, and coolant chemistry programs, January-March 1970 /, by Rockwell International. Atomics International Division and U.S. Atomic Energy Commission (page images at HathiTrust)
• High pressure technology. (New York : McGraw-Hill, 1956), by Edward W. Comings (page images at HathiTrust)
• Pressure and flow-field study at Mach number 8 of flow separation on a flat plate with deflected trailing-edge flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• STD observation from the R/V COLUMBUS ISELIN during Phase III of GATE / (Miami, Fla. : U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William McLeish, S. Michael Minton, Environmental Research Laboratories (U.S.), and Atlantic Oceanographic and Meteorological Laboratories (page images at HathiTrust)
• Pressure response in a long tube which is closed at one end / ([Albuquerque, N.M. : Sandia Corporation ;, 1961]), by M. D. Bennett, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Theoretical investigation at subsonic speeds of the flow ahead of a slender inclinded parabolic-arc body of revolution and correlation with experimental data obtained at low speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by William Letko, Edward C. B. Danforth, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A study of the effect of aftercooling on the power and the weight of a 2000-horsepower air-cooled engine installation / (Washington, D.C. : National Advisory Committee for Aeronautics, [1942]), by George P. Wood, D. E. Brimley, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The calculation of pressure drop and flow distribution within a reactor vessel in a pressurized water nuclear reactor system /, by J. S. Busch, C. F. Bonilla, L. L. Lynn, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Project Pre-GONDALA III : Phase II : microbarograph measurements /, by Jack W Reed, U.S. Army Engineer Nuclear Cratering Group, U.S. Atomic Energy Commission, Sandia Laboratories, and Project Plowshare (U.S.) (page images at HathiTrust)
• Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Harvey H. Hubbard, Leslie W. Lassiter, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• PM development : task 5.0, local boiling heat transfer tests : single tube heat transfer and pressure drop tests / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Division of Technical Information ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, 1961), by J. J. Jicha, S. Frank, Martin Company. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Pressure drop in two-phase flow / (Argonne, Ill. : Argonne National Laboratory, Reactor Engineering Division, 1952), by D. H. Weiss and Argonne National Laboratory (page images at HathiTrust)
• Two-phase flow through abrupt expansions and contractions : final report volume III on a study of convection boiling inside channels : June 1966 /, by J. K. Ferrell, John William McGee, and U.S. Atomic Energy Commission. Division of Technical Information. issuing body (page images at HathiTrust)
• Air blast in an arctic environment. (Vicksburg, Miss. : U.S. Army Engineer Waterways Experiment Station, 1962), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Stresses under moving vehicles : report 2 : wheeled vehicles (M135), lean and fat clay, 1957. (Vicksburg, Miss. : Army Engineer Waterways Experiment Station, 1960), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Stresses under moving vehicles : report 3 : tracked vehicles (M29C, D4 and D7), on fat clay, 1956. (Vicksburg, Miss. : Army Engineer Waterways Experiment Station, 1960), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Investigation of instruments for measuring pore pressures in concrete : literature review and preliminary laboratory tests. (Vicksburg, Miss. : Waterways Experiment Station, 1964), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Sluice pressures, gate vibrations and stilling basin wall pressures, Libby Dam, Kootenai River, Montana / (Vicksburg, Miss. : U.S. Waterways Experiment Station, 1976), by E. Dale Hart, Allen R. Tool, and United States. Army. Corps of Engineers. Seattle District (page images at HathiTrust; US access only)
• Prediction of the pressure loss and density factors for two-phase annular flow with or without heat generation / (Schenectady, N.Y. : Knolls Atomic Power Laboratory, General Electric Company, [1957]), by J. C. Westmoreland, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
• Lock culvert valve loss coefficients : hydraulic laboratory investigation / (Vicksburg, Mississippi : Waterways Experiment Station ;, 1981), by Glenn A. Pickering, Hydraulics Laboratory (U.S.), and United States Army Corps of Engineers (page images at HathiTrust)
• Fixed-cone valve prototype tests, New Melones Dam, California / (Vicksburg, Mississippi : Waterways Experiment Station ;, 1983), by Timothy L. Fagerburg and United States. Army. Corps of Engineers. Sacramento District (page images at HathiTrust)
• Pressure and temperature instrumentation for dynamic measurements in the KEWB Program : a summary report / (Canoga Park, California : Atomics International, [1960]), by Sigmund P. Harris, Carle F. Bumpus, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Subsurface accelerations and strains from an underground detonation. ([Sandia Base, Alburquerque, New Mexico], [Armed Forces Special Weapons Project, U.S. Headquarters Field Command], [1959]), by F. A. Pieper, R. H. Sievers, A. C. Tiemann, United States. Army. Engineer Research and Development Laboratories, U.S. Army Ballistic Research Laboratory, and United States. Defense Atomic Support Agency (page images at HathiTrust)
• Test results from automatic yield indicators : Operation Hardtack - project 43.10 /, by M. Cowan, H. H. Sander, D. N. Munro, Sandia Corporation, and U.S. Atomic Energy Commission. Albuquerque Operations Office (page images at HathiTrust)
• Pressure sensor for use in the Loss-of-Fluid-Test (LOFT) reactor /, by T. R. Billeter, United States. National Technical Information Service, Hanford Engineering Development Laboratory, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• Summary report of fuel rod displacement sensor for LOFT /, by T. R Billeter, United States. National Technical Information Service, United States Government Printing Office, Hanford Engineering Development Laboratory, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963-1964), by Louis G. Kaufman, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• A measurement of the static aeroelastic deformation and loading of a wing in supersonic flow /, by Frank H. Durgin, C. J. Bartlett, sponsor United States. Air Force. Systems Command. Research and Technology Division, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor Massachusetts Institute of Technology, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Optical spectra excited in the noble gases at high pressures by polonium alpha particles. (New York : Columbia University, Dept. of Physics, 1959), by William Ralph Bennett, Columbia University, and U.S. Atomic Energy Commission (page images at HathiTrust; US access only)
• Measurement of the pressure fluctuations in the test section of the 1-foot transonic tunnel in the frequency range from 5 to 1250 cps /, by J. E. Robertson, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• An influence of the orifice on measured pressures in rarefied flow /, by J. Leith Potter, David E. Boylan, Max Kinslow, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Detonation induction distances in combustible gaseous mixtures at atmospheric and elevated initial ressures., by Loren E. Bollinger, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and sponsor Ohio State University. Department of Aeronautical Engineering (page images at HathiTrust)
• Compressible flow through a porous plate /, by George Emanuel, John P. Jones, sponsor Aerospace Corporation. Laboratory Operations, and issuing body United States. Air Force. Systems Command. Space Systems Division (page images at HathiTrust)
• Development of a miniature pressure transducer for application to airfoil studies in the shock tube /, by J. Ray Ruetenik, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
• The use of the p-V-diagram for ramjet calculations /, by E. R. G. Eckert and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Corrugated metal diaphragms for aircraft pressure-measuring instruments / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1939), by W. A. Wildhack, V. H. Goerke, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)

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