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Thermomolecular pressure

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• Gas dynamics
• Pressure
• Thermodynamics

• Optimization of mechanical/corrosion properties of TI-CODE-12 plate and sheet : part II: thermomechanical processing effects (stage II final report) (Sandia National Laboratories ;, 1988), by R. W. Schutz, J. A. Hall, Sandia National Laboratories, and Sandia Laboratories (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Molecular Flow of Gases (New York: J. Wiley and Sons; London: Chapman and Hall, c1956), by Gordon N. Patterson (page images at HathiTrust)
• Salmonid bioassay of supersaturated dissolved air in water (U.S. Environmental Protection Agency, Office of Research and Development, Environmental Research Laboratory ;, 1976), by United States. Environmental Protection Agency. Office of Research and Development, Earl Dawley, and United States. National Marine Fisheries Service (page images at HathiTrust)
• Theoretical evaluation of chemical propellants. (Prentice-Hall, 1963), by Roger Lawrence Wilkins (page images at HathiTrust)
• Design data for aeronautics and astronautics; a compilation of existing data. (Wiley, 1962), by Richard Boyd Morrison (page images at HathiTrust)
• Viscous hypersonic flow : theory of reacting and hypersonic boundary layers. (McGraw-Hill, 1962), by William H. Dorrance (page images at HathiTrust)
• Studies in physical gas dynamics (National Aeronautics and Space Administration ;, 1968), by A. S. Predvoditelev (page images at HathiTrust)
• Shock capturing using flux-corrected transport algorithms with adaptive gridding (Naval Research Laboratory, 1981), by M. Fry (page images at HathiTrust)
• Coupled gasdynamics and kinetics during condensation by a rarefaction wave (Dept. of the Interior, Bureau of Mines, 1977), by David R. Forshey and Welby G. Courtney (page images at HathiTrust)
• Hot gas ignition temperatures of hydrocarbon fuel vapor-air mixtures (U.S. Dept. of the Interior, Bureau of Mines, 1966), by J. M. Kuchta, Ralph J. Cato, Air Force Aero Propulsion Laboratory (U.S.), and United States Bureau of Mines (page images at HathiTrust)
• Die thermodynamische Berechnung chemischer Affinitäten von homogenen und heterogenen Gasreaktionen (Kommissionsverlag von R. Friedländer, 1916), by Ivar W. Cederberg (page images at HathiTrust; US access only)
• Procedures for digital computer analysis of one-dimensional fluid flow processes involving real gases (University of California Lawrence Radiation Laboratory, 1964), by Michael D. Mintz, D. P. Jordan, Lawrence Radiation Laboratory, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Recherches expérimentales et analytiques sur les lois d'écoulement et du choc des gaz en fonction de la température. (Gauthier-Villars, 1886), by Gustave Adolphe Hirn (page images at HathiTrust)
• Gas dynamics in space exploration. ([U. S. Govt. Print. Off.], 1962), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of current-voltage and flow characteristics of an electric discharge across the exit of the AFFDL 1-Mw arc air heater (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966), by STD Research Corporation and S. T. Demetriades (page images at HathiTrust)
• Gasdynamic theory of heat (Headquarters, Air Materiel Command, Wright-Patterson Air Force Base, 1949), by L. E. Kalikhman (page images at HathiTrust)
• Application of the characteristics method to numerical solution of unidimensional problems in gas dynamics (National Aeronautics and Space Administration ;, 1967), by Anatoliĭ Ivanovich Zhukov (page images at HathiTrust; US access only)
• Shock waves in real gases (National Aeronautics and Space Administration, for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), by T. V. Bazhenova (page images at HathiTrust)
• Venting characteristics of gaseous helium and nitrogen discharging into a free stream at Mach numbers from 0.60 to 1.57 (National Aeronautics and Space Administration ;, 1974), by Albert L. Johns, Merle L. Jones, and Lewis Research Center (page images at HathiTrust)
• Experimental perfect-gas study of expansion-tube flow characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Judy L. Shinn, Charles G. Miller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance tests of a gas blending system based on mass-flow controllers (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Albert Evans, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Nonequilibrium gasdynamics (National Aeronautics and Space Administration ;, 1969), by William S. Watt and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Non-equilibrium Arc Tunnel Analysis : theory and analysis (National Aeronautics and Space Administration ;, 1975), by W. L. Bade, Jerrold M. Yos, Lyndon B. Johnson Space Center, and Avco Systems Division (page images at HathiTrust)
• Vorticity interaction effects on blunt bodies (National Aeronautics and Space Administration ;, 1977), by E. Clay Anderson, David C. Wilcox, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• High-velocity explosively driven guns (National Aeronautics and Space Administration ;, 1970), by J. D. Watson, Ames Research Center, and Physics International Company (page images at HathiTrust)
• Real-gas correction factors for hypersonic flow parameters in helium. (National Aeronautics and Space Administration :, 1960), by Wayne D. Erickson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A comparison of measured and predicted test flow in an expansion tube with air and oxygen test gases (National Aeronautics and Space Administration ;, 1975), by Kenneth V. Haggard, William K. Goad, and Langley Research Center (page images at HathiTrust)
• Measured effects of gaseous flow system dynamics on acoustic-mode combustion instability (National Aeronautics and Space Administration ;, 1969), by John F. Groeneweg, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Tornadolike gravity-driven vortex model (National Aeronautics and Space Administration ;, 1974), by Robert G. Deissler, Donald R. Boldman, and Lewis Research Center (page images at HathiTrust)
• Application of various techniques for determining local heat-transfer coefficients in a rocket engine from transient experimental data (National Aeronautics and Space Administration, 1960), by Curt H. Liebert, Ronald W. Grant, James E. Hatch, and Lewis Research Center (page images at HathiTrust)
• Radiation shielding of the stagnation region by transpiration of an opaque gas (National Aeronautics and Space Administration, 1960), by John T. Howe and Ames Research Center (page images at HathiTrust; US access only)
• An estimate of the chemical kinetics behind normal shock waves in mixtures of carbon dioxide and nitrogen for conditions of Mars entry (National Aeronautics and Space Administration ;, 1966), by Robert L. McKenzie and Ames Research Center (page images at HathiTrust)
• Determination of molecular contamination performance for space chamber tests (National Aeronautics and Space Administration ;, 1973), by John J. Scialdone and Goddard Space Flight Center (page images at HathiTrust)
• Calculation of transport properties and heat-transfer parameters of dissociating hydrogen (National Aeronautics and Space Administration ;, 1962), by Norman T. Grier, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1632 (National Aeronautics and Space Administration, 1963), by Wayne D. Erickson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic properties of carbon-dioxide and nitrogen mixtures behind a normal shock wave (National Aeronautics and Space Administration ;, 1963), by Henry T. Woodward, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Contact-surface tailoring in real shock tubes (National Aeronautics and Space Administration ;, 1965), by Theodore A. Brabbs, Frank E. Belles, and Lewis Research Center (page images at HathiTrust)
• A method for computing chemical-equilibrium compositions of reacting-gas mixtures by reduction to a single interation equation (National Aeronautics and Space Administration, 1966), by Wayne D. Erickson, Jane T. Kemper, and Dennis O. Allison (page images at HathiTrust)
• NASA TN D-1761 (National Aeronautics and Space Administration, 1963), by Stefan Schreier, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Velocity lag of solid particles in oscillating gases and in gases passing through normal shock waves (National Aeronautics and Space Administration ;, 1974), by Barry R. Maxwell, Richard G. Seasholtz, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-7050 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Robert L. McKenzie, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Vacuum testing at SAM Laboratories (U.S. Atomic Energy Commission, Technical Information Division, 1948), by S. Bashkin, C. R. A. Rice, F. S. Stein, J. E. Binns, Columbia University, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Theoretisch untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten (NACA, 1948), by K. Oswatitsch, K. Wieghardt, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Primer tochnogo reshenia ploskoi vikhrevoi zadachi gazovoi dinamiki (National Advisory Committee for Aeronautics, 1950), by I. A. Kiebel and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Pressure-temperature relation for constant-area compressible flow of a gas, considering heat transfer and friction with constant wall temperatures (Los Alamos Scientific Laboratory of the University of California, 1957), by Franklin P. Durham, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Collision integrals and transport properties for gases obeying an exponential repulsive potential : application to hydrogen and helium. (Los Alamos Scientific Laboratory of the University of California, 1960), by Joseph B. Mann, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Calculations of the coefficients of viscosity, diffusion, and thermal conductivity for dissociating hydrogen for a range of temperatures and pressures (Los Alamos Scientific Laboratory of the University of California, 1961), by David G. Clifton, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• HUG : a FORTRAN-FAP code for computing normal shock and detonation wave parameters in gases (Los Alamos Scientific Laboratory of the University of California, 1964), by Paul F. Bird, Garry L. Schott, Russell E. Duff, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Interaction of moving shocks and hot layers (National Advisory Committee for Aeronautics, 1957), by Robert V. Hess, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The effect of wall friction on the strength of shock waves in tubes and hydraulic jumps in channels (National Advisory Committee for Aeronautics, 1949), by Coleman duP. Donaldson, Roger D. Sullivan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Rise through the atmosphere of a hot bubble (Los Alamos Scientific Laboratory of the University of California, 1962), by Francis H. Harlow, Billy D. Meixner, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effect of dissociation on thermodynamic properties of pure diatomic gases (National Advisory Committee for Aeronautics, 1955), by Harold W. Woolley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Molecular physics of equilibrium gases : a handbook for engineers (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), by C. Frederick Hansen (page images at HathiTrust)
• Separation of gaseous mixtures by a non-uniform barrier (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1957), by Stephen Prager, Oak Ridge Gaseous Diffusion Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), by Cearcy D. Miller, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air-water mixture flow through orifices, bends, and other fittings in a horizontal pipe (St. Anthony Falls Hydraulic Laboratory, University of Minnesota, 1960), by Edward Silberman, Lorenz G. Straub, St. Anthony Falls Hydraulic Laboratory, Naval Surface Warfare Center (U.S.). Carderock Division, and United States Navy Department Bureau of Ships (page images at HathiTrust)
• Sandia Corporation bibliography (Sandia Corporation, Technical Information Division ;, 1961), by D. E. Randall, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Analysis of mechanical and gasdynamic loadings during sabot discard from gun launched projectiles (Aberdeen Proving Ground, Maryland : USA Armament Research and Development Command, USA Ballistic Research Laboratory, 1977., 1977), by Peter Crimi, David Siegelman, U.S. Army Ballistic Research Laboratory, and Avco Corporation. Systems Division (page images at HathiTrust)
• Deviations from thermal equilibrium in shock waves ([publisher not identified], 1940), by Hans A. Bethe and Edward Teller (page images at HathiTrust)
• Charts for equiibrium flow properties of carbon dioxide in hypervelocity nozzles (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1965), by Leland H. Jorgensen and Robert J. Redmond (page images at HathiTrust)
• Gasdynamics of combustion (National Aeronautics and Space Administration, 1964), by K. I. Shchelkin and Ya. K. Troshin (page images at HathiTrust)
• Hypersonic gas dynamic charts for equilibrium air. (Avco Research Laboratory, Avco Manufacturing Corporation, 1927), by Saul Feldman and Avco Corporation (page images at HathiTrust)
• A relativistic treatment of strong shock waves in a classical gas. (Thermal Radiation Laboratory, Geophysics Research Directorate, Air Force Cambridge Research Center, 1959), by Arnold W. Guess (page images at HathiTrust; US access only)
• Les machines des service pneumatique au nouvel hotel des postes a Paris (Vve. Ch. Dunod, 1886), by M. Wünschendorff (page images at HathiTrust)
• Extended hypervelocity gas dynamic charts for equilibrium air (Los Angeles, California : Physical Research Laboratory, Space Technology Laboratories, 1960., 1960), by Richard W. Hales and Los Angeles. Physical Research Laboratory Space Technology Laboratories (page images at HathiTrust)
• Probes in a plasma from a gas dynamic point of view with application to the problem of satellite charging (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1976), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Gas dispersion in porous media : Peclet-Reynolds number correlations (University of California, Sanitary Engineering Research Laboratory, 1967), by W. Emmett Bolch, Warren J. Kaufman, Robert E. Selleck, and Berkeley. Sanitary Engineering Research Laboratory University of California (page images at HathiTrust; US access only)
• Computation of equilibrium hypersonic flow about blunt axisymmetric bodies with sharp concers : (Final Report) (Buffalo, New York : Sandia Corporation, Cornell Aeronautical Laboratory, Inc., 1967., 1967), by J. T. Curtis, C. R. Strom, Sandia Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Photoionization of N₂ and O₂ ahead of strong shock waves in a shock tube (Albuquerque, New Mexico : Sandia Laboratories, Experimental Aerophysics Division, 1971., 1971), by A. J. Mulac, Sandia Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Interactions between a multicomponent flow and a laser beam : part II - separation of particles from a carrier gas in a hypersonic two-phase flow (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Kuei-Yuan Chien and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Shock-tube diagnostics utilizing laser raman spectroscopy (Silver Spring, Maryland : illustrations, 1975., 1975), by Anthony A. Boiarski and Naval Surface Weapons Center. : White Oak Laboratory (page images at HathiTrust)
• Kinetics of reactions in shock tubes (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by S. H. Bauer, Cornell University, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• The High temperature hypersonic gasdynamics facility (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Robert W. Milling, United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Extension of Belotserkovskii's direct method to reacting gas in thermodynamic equilibrium (Inglewood, California : Space Systems Division, Air Force Systems Command, United States Air Force, 1964., 1964), by S. T. Chu, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
• The Development of a small Mach 10 hypersonic wind tunnel (Princeton, New Jersey : Princeton University, Department of Aeronautical Engineering, 1963., 1963), by Neil A. Zarin, I. E. Vas, United States. Air Force. Office of Scientific Research, and Princeton University. Department of Aeronautical Engineering (page images at HathiTrust)
• Stagnation point heat transfer in a relaxing gas (Inglewood, California : Space Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Robert E. Wilson, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
• Exact solutions for nonequilibrium expansions of air with coupled chemical reactions (Washington, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1961., 1961), by Alan Q. Eschenroeder, J. Gordon Hall, Donald W. Boyer, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Research on nonisentropic gas dynamics (Cornell Aeronautical Laboratory of Cornell University, 1970), by Robert J. Vidal, Gordon E. Merritt, John A. Bartz, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)

More items available under broader and related terms at left.