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Stagnation point

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• Fluid mechanics

• Ballistic Range Measurements of Stagnation-Point Heat Transfer in Air and Carbon Dioxide at Velocities up to 18,000 Feet per Second (NASA technical note D-777; Washington: National Aeronautics and Space Administration, 1961), by Layton Yee, Harry E. Bailey, and Henry T. Woodward (page images at HathiTrust)
• The NATA code : theory and analysis / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by W. L. Bade, Jerrold M. Yos, Lyndon B. Johnson Space Center, and Avco Systems Division (page images at HathiTrust)
• Photographic study of a bromine jet flowing in a coaxial airstream and impinging on a stagnation surface / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by Charles C. Masser, Maynard F. Taylor, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Radiative heat transfer during atmosphere entry at parabolic velocity / (Washington, [D.C.] : National Aeronautical and Space Administration, 1961), by Kenneth K. Yoshikawa, Bradford H. Wick, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Effect of localized mass transfer near the stagnation region of blunt bodies in hypersonic flight / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
• Radiative coupled viscous flow with massive blowing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Charts depicting kinematic and heating parameters for a ballistic reentry at speeds of 26,000 to 45,000 feet per second / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Uriel M. Lovelace, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Shielding of partially reflecting stagnation surfaces against radiation by transpiration of an absorbing gas / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Supt. of Docs., U.S. G.P.O., Washington 25, D.C. 22151], 1961), by John Thomas Howe and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A Digital computer program for calculating steady temperature and density distributions in gas containing heat sources / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Harry W. Davison, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust; US access only)
• Stagnation point heat transfer during hypervelocity atmospheric entry / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by W. S. Rigdon, M. Thomas, R. B. Dirling, McDonnell Douglas Astronautics Company. Western Division, and Langley Research Center (page images at HathiTrust)
• Numerical calculations of viscous compressible fluid flow around a stationary cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Comparison of convective stagnation heat transfer in air, CO₂-N₂, and CO₂-Ar gas mixtures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Clifford M. Akin, Joseph G. Marvin, and Ames Research Center (page images at HathiTrust)
• A program for equilibrium normal shock and stagnation point solutions for arbitrary gas mixtures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Linwood B. Callis, Jane T. Kemper, and Langley Research Center (page images at HathiTrust)
• A comparison of the theoretical and experimental stagnation-point heat transfer in an arc-heated subsonic stream / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1964]), by Ronald D. Brown and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of corner radius on stagnation-point velocity gradients on blunt axisymmetric bodies / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by Ernest V. Zoby, Edward M. Sullivan, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Louis S. Stivers and Ames Research Center (page images at HathiTrust)
• Shielding stagnation surfaces of finite catalytic activity by air injection in hypersonic flight / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
• Pressure distributions on 140, ̊ 160, ̊ and 180 ̊cones at Mach numbers from 2.30 to 4.63 and angles of attack from 0 ̊to 20 ̊/ (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by James F. Campbell, Dorothy H. Tudor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Leonard Roberts and Langley Research Center (page images at HathiTrust)
• Solutions of the laminar compressible boundary-layer equations with transpiration which are applicable to the stagnation regions of axisymmetric blunt bodies / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by John T. Howe, William A. Mersman, and Ames Research Center (page images at HathiTrust)
• Blunt-body stagnation-region flow with nongray radiation heat transfer : a singular perturbation solution / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Stagnation-point solutions for inviscid radiating shock layers / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Laminarization of a turbulent boundary layer as observed from heat-transfer and boundary-layer measurements in conical nozzles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Donald R. Boldman, Anne K. Gallagher, James F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of substructure heating on cracked ablative heat shields /, by Erhard M Winkler, M. T. Madden, J. A. Koenig, Richard L. Humphrey, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Supersonic ablation studies with teflon /, by Erhard M Winkler, J. A. Koenig, Richard L. Humphrey, M. T. Madden, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Charts of equilibrium real-gas stagnation point conditions on a sphere for altitudes to 200,000 feet and velocities to 15,000 feet per second /, by P. D. Fisher and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Stagnation point heat transfer from a viscous nongray radiating shock layer : including the applicability of step model absorption coefficients and sensitivity to uncertainties in transport properties /, by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An equation for rapid calculation of stagnation point radiative heat transfer : including shock layer radiative cooling and nongray self-absorption /, by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A hot-wire stagnation temperature probe /, by William Joseph Yanta and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Transpiration cooling experiments near the stagnation line of a cylinder in cross flow /, by Richard L. Humphrey and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A fine-wire stagnation temperature probe /, by William Joseph Yanta and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Inhibition of flow separation at high speed., by Frederick K. Goodwin, Larry L. Lynes, Jack Norman Nielsen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Nielsen Engineering & Research (page images at HathiTrust)
• Inviscid flow in the stagnation point region of very blunt-nosed bodies at hypersonic flight speeds /, by Ronald F. Probstein, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor Brown University. Division of Engineering (page images at HathiTrust)
• Inhibition of flow separation at high speed., by Frederick K. Goodwin, Larry L. Lynes, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Nielsen Engineering & Research (page images at HathiTrust)
• Stagnation point heat transfer in a relaxing gas /, by Robert E. Wilson, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation (page images at HathiTrust)
• Highly nonequilibrium boundary layer flows of a multicomponent dissociated gas mixture /, by G. I. Inger, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation (page images at HathiTrust)
• Nonequilibrium hypersonic stagnation flow at low reynolds numbers /, by G. I. Inger, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation. Laboratory Operations (page images at HathiTrust)
• Stagnation point flow and heat transfer under free-stream turbulence /, by Zhongmin Xiong, Sanjiva K. Lele, Stanford University. Department of Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Stagnation point boundary layer with large wall-to-freestream enthalpy ratio /, by Harold Mirels, William E Welsh, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)

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

• Fluid Mechanics (New York et al.: Wiley, c1961), by Richard H. F. Pao (page images at HathiTrust)
• Hydrodynamics: A Study in Logic, Fact, and Similitude (New York, Dover Publications, 1955), by Garrett Birkhoff (page images at HathiTrust)
• Elementary treatise on hydromechanics, with numerous examples [electronic resource] / (New York : D. Van Nostrand, 1889), by Edward A. Bowser (page images at HathiTrust)
• A treatise on hydromechanics. (Cambridge [Eng.] Deighton, Bell and Co., 1883), by W. H. Besant (page images at HathiTrust)
• Mechanics of fluids for practical men, comprising hydrostatics, descriptive and constructive: the whole illustrated by numerous examples and appropriate diagrams. (London, Williams, 1848), by Alexander Jamieson (page images at HathiTrust)
• A treatise on hydromechanics / (London : G. Bell, 1904-1913), by W. H. Besant and A. S. Ramsey (page images at HathiTrust; US access only)
• Fluid mechanics laboratory manual / (Bethelem, Pennsylvania : Lehigh University, Civil Engineering Dept., 1960), by John B. Herbich, Hydraulics Division Lehigh University. Fritz Engineering Laboratory, and Lehigh University. Dept. of Civil Engineering (page images at HathiTrust)
• Report on Forum 2000 : fluid properties for new technologies : connecting virtual design with physical reality / (Boulder, Colo. : U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology ; Washington : For sale by the Supt. of Docs., U.S. G.P.O., 2001), by James C. Rainwater, National Institute of Standards and Technology (U.S.), and Colo.) Symposium on Thermophysical Properties (14th : 2000 : Boulder (page images at HathiTrust)
• Numerical simulations of three-dimensional laminar flow over a backward facing step; flow near side walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by Erlendur Steinthorsson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical study of shock-induced combustion in methane-air mixtures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by Shaye Yungster, Martin J. Rabinowitz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Rodrick V. Chima, Anthony J. Strazisar, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Traité de l'équilibre et du mouvement des fluides, pour servir de suite au traité de dynamique. Paris, Chez David, 1744. ([Bruxelles, Culture et Civilisation, 1966]), by Jean Le Rond d' Alembert (page images at HathiTrust; US access only)
• An elementary treatise on hydromechanics, with numerous examples. (New York, D. Van Nostrand, 1899), by Edward A. Bowser (page images at HathiTrust; US access only)
• A new definition of a fluid. (Washington, Naval Research Laboratory, 1949), by C. Truesdell (page images at HathiTrust)
• Liquids and gases. (New York, J.F. Rider, [1958]), by Alexander Efron (page images at HathiTrust; US access only)
• Technische Hydromechanik. (München : Oldenburg, 1910), by Hans Lorenz (page images at HathiTrust; US access only)
• A near-wall turbulence model and its application to fully developed turbulent channel and pipe flows ([Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]), by S. W. Kim and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Conservative-variable average states for equilibrium gas multi-dimensional fluxes / (Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]), by G. S. Iannelli and Lewis Research Center (page images at HathiTrust)
• The effect of small streamwise velocity distortion on the boundary layer flow over a thin flat plate with application to boundary layer stability theory ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]), by M. E. Goldstein, Stephen J. Cowley, S. J. Leib, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical investigation of an internal layer in turbulent flow over a curved hill / ([Cleveland, Ohio : NASA Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1989]), by S. W. Kim and Lewis Research Center (page images at HathiTrust)
• Forced-convection peak heat flux on cylindrical heaters in water and refrigerant 113 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Thomas H. Cochran, Charles R. Andracchio, and Lewis Research Center (page images at HathiTrust)
• A cubic spline approximation for problems in fluid mechanics / (Washington : U.S. National Aeronautics and Space Administration, 1975), by Stanley G. Rubin and Randolph A. Graves (page images at HathiTrust)
• Supersonic turbulent boundary-layer flows with mass injection through slots and/or porous walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Alvin L. Murray, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• A general form of the co-moving tensorial derivative / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Earle K. Huckins, Richard E. Turner, and Langley Research Center (page images at HathiTrust)
• Unified analysis of turbulent jet mixing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Joseph A. Schetz, Johns Hopkins University, University of Maryland at College Park, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Turbulent mixing of coaxial compressible hydrogen-air jets / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by James M. Eggers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Experimental study of one- and two-component low-turbulence confined coaxial flows / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by John C. Bennett, Bruce V. Johnson, Lewis Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data / (Washington, D.C., : U.S. G.P.O., 1962), by William R. Wells, William O. Armstrong, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Analysis of internal flow characteristics of a smooth-disk water-brake dynamometer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by David G. Evans and Lewis Research Center (page images at HathiTrust)
• An experimental and numerical study of wave motion and upstream influence in a stratified fluid / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by David A. Hurdis and Goddard Space Flight Center (page images at HathiTrust)
• Cavitation performance of an 83° helical inducer operated in liquid hydrogen / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by George W. Lewis, D. M. Sandercock, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Numerical study of axisymmetric vortex breakdowns / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by K. E. Torrance, R. N. Kopecky, United States National Aeronautics and Space Administration, and Cornell University (page images at HathiTrust)
• Hydromechanics : an elementary treatise prepared for the use of the cadets at the United States Naval Academy / (Baltimore, Md. : Lord Baltimore Press, 1902), by Philip R. Alger (page images at HathiTrust)
• Hydrostatics and pneumatics. By the Rev. Dionysius Lardner. (Philadelphia : Carey and Lea, 1832), by Dionysius Lardner and Benjamin F. Joslin (page images at HathiTrust)
• Nuova raccolta d'autori, che trattano del moto dell'acque. (Parma : F. Carmignani, 1766-1768), by Antonio Cavagna Sangiuliani di Gualdana (page images at HathiTrust)
• Raccolta d'autori che trattano del moto dell'acque : divisa in tre tomi (In Firenze : Nella Stamperia di S.A.R. per gli Tartini e Franchi, 1723), by Antonio Cavagna Sangiuliani di Gualdana (page images at HathiTrust)
• Theory of energetic activities for fluid carriers through channels of continuous flow transformers / (1916), by Walter Jacob Wohlenberg (page images at HathiTrust; US access only)
• On some general features of turbulent flows with large Reynolds numbers / (Upton, N.Y. : Brookhaven National Laboratory, Dept. of Nuclear Energy, Nuclear Waste Research Group; Springfield, Va. : available from NTIS, 1982), by Arnold Levin and Brookhaven National Laboratory. Atmospheric Sciences Division. org (page images at HathiTrust)
• Control of surging in low-pressure pipelines / (Denver, Colo. : Bureau of Reclamation, Engineering and Research Center, 1972), by John J. Cassidy and Engineering and Research Center (U.S.) (page images at HathiTrust)
• Dynamic flow model for low-BTU gasification of coal for electric power systems / ([Washington] : Dept. of Energy ; Springfield, Va. : for sale by the National Technical Information Service, 1977, i.e. 1979-), by J. D. Bianca, J. G. McGowan, W. P. Bauver, United States. Department of Energy, and inc. Power Systems Combustion Engineering (page images at HathiTrust)
• Experimental researches into the properties and motions of fluids. With theoretical deductions therefrom. (London, New York, E. & F.N.Spon, 1881), by William Ford Stanley (page images at HathiTrust)
• A treatise on hydromechanics : part I. Hydrostatics / (Cambridge, Eng. : Deighton, Bell & Co., 1883), by W. H. Besant (page images at HathiTrust)
• Application of the hydraulic analogy to internal subsonic flow. (Redstone Arsenal, Ala., Army Inertial Guidance and Control Laboratory, Research and Development Directorate, U.S. Army Missile Command, 1967), by Carl Hugh Warren (page images at HathiTrust)
• Traité théorique et expérimental d'hydrodynamique. (Paris, Larau, l'an IV, [1796]), by Charles Bossut (page images at HathiTrust)
• The equations of motion of sea water, (La Jolla, Calif., [1959]), by Carl Eckart (page images at HathiTrust)
• A treatise on hydromechanics, (London, G. Bell, 1877), by W. H. Besant, A. S. Ramsey, and A. S. Ramsey (page images at HathiTrust)
• A Treatise on hydromechanics. (Cambridge : [s.n.], 1891-1913), by W. H. Besant and A. S. Ramsey (page images at HathiTrust)
• Time domain numerical calculations of unsteady vortical flows about a flat plate airfoil ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]), by S. I. Hariharan, J. R. Scott, Yu Ping, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fluid mechanics (New York, Prentice-Hall, 1943), by Raymond C. Binder (page images at HathiTrust)
• A treatise on hydromechanics ... (London, G. Bell and Sons, Ltd., 1919-20), by W. H. Besant and A. S. Ramsey (page images at HathiTrust; US access only)
• Tables of the function H(u,₎)=[reproduction of equation for the function] / (Socorro : New Mexico Institute of Mining & Technology, 1961), by Mahdi S. Hantush (page images at HathiTrust; US access only)
• A preliminary study of sediment transport parameters, Rio Puerco near Bernardo, New Mexico, by Carl F. Nordin, Jr. (Washington, U. S. Govt. Print. Off., 1963), by Carl F. Nordin (page images at HathiTrust)
• Transverse dispersion in liquid flow through porous media. (Washington, U.S.Govt.Print.Off., 1962), by Eugene Sidney Simpson (page images at HathiTrust)
• Fenn-i mihanik / ([İstanbul] : Kasbar Matbaası, 1324 [1906 or 1907]), by Ahmet Cemil (page images at HathiTrust; US access only)
• Treatise on hydromechanics. (London, Bell, 1867), by William Henry Besant and Arthur Stanley Ramsey (page images at HathiTrust)
• Flow into a stratified reservoir / (Berkeley, Calif. : Univ. of California, 1971), by Antonio Alfonso Zuluaga-Angel and Berkeley University of California (page images at HathiTrust; US access only)
• Fish screen head loss, perforated 16-gage steel plate (5/32-inch holes staggered on 7/32-inch centers) versus 5-mesh, 19-gage galvanized wire, Tracy Pumping Plant intake, Central Valley Project / (Denver : U.S. Dept. of the Interior, Bureau of Reclamation, Branch of Design and Construction, 1950), by Wiley J. Karrh and United States. Bureau of Reclamation. Research and Geology Division (page images at HathiTrust)
• The motion of a floating sphere in surface waves / (Berkeley : University of California, Institute of Engineering Research, Waves Research Laboratory, 1954), by R. C. MacCamy, Berkeley. Institute of Engineering Research University of California, and United States. Office of Naval Research (page images at HathiTrust)
• Outflow hydrograph resulting from sudden release of ponded water through a large opening / (Washington : U.S. Department of the Interior, Geological Survey, 1960), by Vujica M. Yevjevich and United States. Army Map Service (page images at HathiTrust)
• Engineering applications of fluid mechanics, (New York, McGraw-Hill Book Co., 1947), by Jerome Clarke Hunsaker and B. G. Rightmire (page images at HathiTrust)
• Fluid mechanics, acoustics, and design of turbomachinery : a symposium held at the Pennsylvania State University, University Park, Pennsylvania, August 31 to September 3, 1970 and sponsored by the National Aeronautics and Space Administration, the Pennsylvania State University and the U.S. Navy / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration : [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1974), by Werner R. Britsch, Walter S. Gearhart, B. Lakshminarayana, and Pennsylvania State University (page images at HathiTrust)
• Extension of Preston's shear measurement technique to rough boundaries / (1962), by L. Hwang (page images at HathiTrust; US access only)
• Fluid power. (Milwaukee : [The Oilgear company, 1937-1946]), by Oilgear Company (page images at HathiTrust; US access only)
• Turbulent skin-friction and heat-transfer coefficients for an inclined flat plate at high hypersonic speeds in terms of free-stream flow properties. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James F. Schmidt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Mary W. Jackson, K. R. Czatnecki, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation procedure for the thermodynamic, transport, and flow properties of the combustion products of a hydrocarbon fuel mixture burned in air with results for ethylene-air and methane-air mixtures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by E. W. Leyhe, R. R. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure loads produced on a flate-plate wing by rocket jets exhausting in a spanwise direction below the wing and perpendicular to a free-stream flow of mach number 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ralph A. Falanga, Joseph J. Janos, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fluid oscillations in the containers of a space vehicle and their influence upon stability / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Helmut F. Bauer, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Approximation for distribution of flow properties in the angle-of-attack plane of conical flows / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Joseph W. Cleary, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Liquid drops: numerical and asymptotic solutions of their shapes, ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1968]), by Kenneth J. Baumeister and Thomas D. Hamill (page images at HathiTrust; US access only)
• Hydrodynamics; a study in logic, fact, and similitude. ([Princeton] Princeton University Press for University of Cincinnati, 1950), by Garrett Birkhoff (page images at HathiTrust)
• A Treatise on hydraulics for use in technical schools / (New York : John Wiley ; London : Chapman and Hall, 1908, c1890), by Irving P. Church (page images at HathiTrust; US access only)
• Shortcuts and special problems in aquifer tests / (Washington, D.C. : U.S. G.P.O., 1963), by Ray Bentall (page images at HathiTrust)
• A treatise on hydrostatics and pneumatics. (Philadelphia : Cary, Lea, and Blanchard, 1836), by Dionysius Lardner and Benjamin F. Joslin (page images at HathiTrust)
• Oeuvres de m. Mariotte, de l'Académie royale des sçiences; (La Haye, Jean Neaulme, M,DCC,XL), by Edmé Mariotte (page images at HathiTrust)
• Numerical simulation of three-dimensional self-gravitating flow / (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1993), by John V. Shebalin and Langley Research Center (page images at HathiTrust)
• Thermally-sustained structure in convectively unstable systems / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by Robert J. Deissler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computation of confined coflow jets with three turbulence models / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by J. Zhu and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling [electronic resource] / (Langley Field, VA : Langley Research Center ; Springfield, Va. : for sale by the National Technical Information Service, 1959), by Ivan E. Beckwith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Internal-performance evaluation of a two-position divergent shroud ejectro / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James R. Mihaloew, Andrew J. Stofan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cold-air investigation of prototype Snap-8 turbine (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William J. Nusbaum, Donald E. Holeski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the liquid level at the wall of a spinning tank (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by David M. Winch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Volume-energy parameters and turbulent-flow density fluctuations / (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 Robert C. Hendricks and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Charles P. Shore, Irving Weinstein, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A second-order accurate kinetic-theory-based method for inviscid compressible flows / (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 S. M. Deshpande and Langley Research Center (page images at HathiTrust)
• Some recent developments in the prediction of shock interaction phenomena at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Davis H. Crawford, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Phase control during reconstruction of holographically recorded flow fields using real-time holographic interferometry / (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 Alpheus W. Burner, William K. Goad, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fluid surface behavior in low gravity : Center Discretionary Fund no. 83-21, final report / (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 Fred Leslie, Charles F. Schafer, Roger F. Gans, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 / (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 Theodore R. Creel, W. E. Zorumski, Ivan E. Beckwith, Barbara B. Holley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium / ([Washington] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by George C. Ashby, V. T. Helms, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Draining characteristics of hemispherically bottomed cylinders in a low-gravity environment / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Eugene P. Symons, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Correlation of laser velocimeter measurements over a wing with results of two prediction techniques / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Danny R. Hoad and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Oil-flow study of a space shuttle orbiter tip-fin controller / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by V. T. Helms and Langley Research Center (page images at HathiTrust)
• A numerical solution of the Navier-Stokes equations for chemically nonequilibrium, merged stagnation shock layers on spheres and two-dimensional cylinders in air / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Kenneth D. Johnston and William L. Hendricks (page images at HathiTrust)
• Flow through aligned sequential orifice-type inlets / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Robert C. Hendricks, T. Trent Stetz, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental measurement of the orbital paths of particles sedimenting within a rotating viscous fluid as influenced by gravity / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David A. Wolf, Ray P. Schwarz, and Lyndon B. Johnson Space Center. Astronaut Office/CB. (page images at HathiTrust)
• Three-step cylindrical seal for high-performance turbomachines / ([Washington, D.C.] : National Aeronautics and Space Administration, [1987]), by Robert C. Hendricks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Straight cylindrical seal for high-performance turbomachines / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Robert C. Hendricks (page images at HathiTrust)
• Some flow phenomena associated with aligned, sequential apertures with borda-type inlets / (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 Robert C. Hendricks, T. Trent Stetz, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental data and model for the turbulent boundary layer on a convex, curved surface / (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 J. C. Gillis, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A variational principle for compressible fluid mechanics : discussion of the multi-dimensional theory / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Robert Joel Prozan, Inc Continuum, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert T. Swann, Jerry C. South, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic interaction effects ahead of a sonic jet exhausting perpendicularly from a flat plate into a mach number 6 free stream / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by David J. Romeo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James L. Amick and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the damping of liquid oscillations in cylindrical tanks with various baffles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Milton A. Silveira, H. Wayne Leonard, David G. Stephens, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William J. Monta, K. R. Czarnecki, Paul W. Howard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures from 1,295 degrees F to 2,910 degrees F / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Bernard Rashis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of a high-speed hydrofoil with parabolic thickness distribution and an aspect ration of 3 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kenneth W. Christopher and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Two-dimensional ion beams with small lateral spreading / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Harold Mirels and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A one-dimensional analysis of magnetohydrodynamic energy conversion / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert G. Deissler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and theoretical study of heat conduction for air up to 5000 degrees F / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Tzy-Cheng Peng, Warren F. Ahtye, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Surface pressures and heat transfer on unswept blunt plates in helium at high mach numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph G. Marvin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The flow field over blunted flat plates and its effect on turbulent boundary-layer growth and heat transfer at a mach number of 4.7 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Thorval Tendeland, Melvin J. Fohrman, Helmer L. Nielsen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kenneth K. Yoshikawa, Elliott D. Katzen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shock impingement on the distribution of heat-transfer coefficients on a right circular cylinder at mach numbers of 2.65, 3.51, and 4.44 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Robert A. Newlander and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Loads induced on a flat-plate wing by an air jet exhausting perpendicularly through the wing and normal to a free-stream flow of mach number 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph J. Janos and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interaction of a charged satellite with the ionosphere by A. H. Davis and I. Harris. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by A. H. Davis, I. Harris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Approximations for the thermodynamic and transport properties of high-temperature nitrogen with shock-tube applications / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Warren F. Ahtye, Tzy-Cheng Peng, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The determination of ablative properties of materials in free-flight ranges / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Raymond C. Savin, Richard G. Dahms, Hermilo R. Gloria, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The theoretical enthalpy distribution of air in steady flow along the axis of a direct-current electric arc / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Howard A. Stine, Velvin R. Watson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Secondary flow fields embedded in hypersonic shock layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Alvin Seiff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert T. Swann, C. M. Pittman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bruce E. Tinling, Clyde Q. Allen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Electron diffusion in a turbulent plasma / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Harold R. Kaufman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Andrew J. Stofan, Albert J. Pavli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of melting boundary layers on decelerating bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Simon Ostrach, Jesse Hamman, Arthur W. Goldstein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boiling heat transfer to liquid hydrogen and nitrogen in forced flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by James P. Lewis, John F. Kline, Jack H. Goodykoontz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the damping of liquids in right-circular cylindrical tanks, including the effects of a time-variant liquid depth / David G. Stephens, H. Wayne Leonard and Tom W. Perry Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by David G. Stephens, Tom W. Perry, H. Wayne Leonard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interaction of highly underexpanded jets with simulated lunar surfaces / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Leonard E. Stitt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the electron density distribution about the F2 peak / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by S. J. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gary T. Chapman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Recovery temperature transition and heat-transfer measurements at mach 5 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul F. Brinich and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Estimate of shock standoff distance ahead of a general stagnation point / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Eli Reshotko and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Radiation emission effects of the equilibrium boundary layer in the stagnation region / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John Thomas Howe and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Arthur Henderson, Dorothy O. Braswell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Two instruments for measuring distributions of low-energy charged particles in space / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Michel Bader, Fred C. Witteborn, Thomas B. Fryer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tests of an asymmetrical baffle for fuel-sloshing suppression / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Henry A. Cole, Bruno J. Gambucci, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [19 62]), by John L. Sewall, Charles E. Watkins, Robert W. Hess, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Applicability of mixing length theory to a turbulent vortex system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert G. Ragsdale and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical evaluation of hypersonic forces moments and stability derivatives for combinations of flat plates, including effects of blunt leading edges, by Newtonian impact theory / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Walter B. Olstad and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Amos A. Spady and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of geometric parameters on the static performance of an annular nozzle with a concave central base / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles E. Mercer, Albert J. Simonson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Frederick W. Boltz, Clyde Q. Allen, George C. Kenyon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The numerical calculation of flow past conical bodies supporting elliptic conical shock waves at finite angles of incidence / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Benjamin R. Briggs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Exploratory study of the reduction in friction drag due to streamwise injection of helium. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Byron L. Swenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transition Reynolds numbers of separated flows at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Howard K. Larson, Stephen J. Keating, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to surfaces of finite catalytic activity in frozen dissociated hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul M. Chung, Aemer Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the induced flow of an electrically conducting liquid in a rectangular duct by electric and magnetic fields of finite extent / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Vernon J. Rossow, Robert H. Huerta, Wm. Pritchard Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of combined forced and free-laminar convection in a vertical tube / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Theodore M. Hallman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of an axial-flow-pump stage designed by the blade-element theory - blade-element data / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James E. Crouse, John C. Montgomery, Richard F. Soltis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determining inertias by using the amplitude decay rate of a mechanical oscillating system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Gene T. Carpenter, Dan T. Meredith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An accelerated reservoir light-gas gun / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John S. Curtis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of surface recombination on heat transfer to bodies in a high enthalpy stream of partially dissociated nitrogen / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961 ]), by Ernest L. Winkler, Roy N. Griffin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of flow fields from bow wave profiles for the downstrream region of blunt-nosed circular cylinders in axial hypersonic flight / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alvin Seiff, Ellis E. Whiting, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A correlation study of the bow wave profiles of blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962 ]), by Alvin Seiff, Ellis E. Whiting, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal force and moment data at mach numbers from 0.60 to 1.40 for a family of elliptic cones with various semiapex angles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Louis S. Stivers, Lionel L. Levy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-determined aerodynamic-noise environment of an airplane nose cone up to a Mach number of 2 (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Norman J. McLeod and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic properties of hydrogen from room temperature to 100,000 degrees K / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Burt M. Rosenbaum, Leo Levitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nonviscous flow through a pump impeller on a blade-to-blade surface of revolution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James J. Kramer, Ralph J. Bean, Norbert O. Stockman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of a 10-centimeter-diameter electron-bombardment ion rocket (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Paul D. Reader and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Potential-flow analysis of unsteady outflow from a tank and its effect on the dynamics of a fluid system (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William H. Roudebush, I. Irving Pinkel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Thomas H. Einstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A comparison of reverse-feed and porous-tungsten ion engines (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Thaine W. Reynolds and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Accelerator grid tests on an electron-bombardment ion rocket (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William R. Kerslake and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and calibration of an arc-heated, hypersonic, low-density wind tunnel (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Ruth N. Weitmann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of a 78 degree flat-plate helical inducer (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Richard F. Soltis, Donald M. Sandercock, Douglas A. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Incompressible nonviscous blade-to-blade flow through a pump rotor with splitter vanes/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James J. Kramer, Ralph J. Bean, Norbert O. Stockman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determinations of local and instantaneous combustion conditions from acoustic measurements in a rocket combustor and comparison with overall performance/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of the effects of weightlessness on the configuration of mercury and alcohol in spherical tanks/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald A. Petrash, Edward W. Otto, Robert F. Zappa, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Forces and moments on sphere-cone bodies in Newtonian flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert R. Dickey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The performance of ablative materials in a high-energy, partially dissociated, frozen nitrogen stream / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Nick S. Vojvodich and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method for calculating the generalized aerodynamic forces on rectangular wings deforming symmetrically in supersonic flight with indicial or sinusoidal time dependence / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Rueben Bond and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to 0 degree and 75 degree swept blunt leading edges in free flight at mach numbers from 1.90 to 3.07. Robert L. O'Neal and Aleck C. Bond. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert L. O'Neal, Aleck C. Bond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William R. Wehrend and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John V. Becker, Peter F. Korycinski, and United States National Aeronautics and Space Administration (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)
• Comparative measurements of singly and doubly ionized mercury produced by electron-bombardment ion engine / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Nelson L. Milder and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability of three-dimensional compressible boundary layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Eli Reshotko and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald L. Lansing and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Robert D. Witcofski, Arthur Henderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald R. McFarland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a sinuisoidally perturbed flow in a line including a 90 degree elbow with flexible supports / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert J. Blade, Jack H. Goodykoontz, William Lewis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Don W. Jillie, Edward J. Hopkins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer at the reattachment zone of separated laminar boundary layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul M. Chung and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gary T. Chapman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical and experimental evaluation of a two-stage annular air ejector for high-energy wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John A. Sheldon, Henry R. Hunczak, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of flow duration in a low-pressure shock tube / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Virgil A. Sandborn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Similar solutions for turbulent boundary layer with large favorble pressures gradients (nozzle flow with heat transfer) / (Washington : National Aeronautics and Space Administration, 1971), by James F. Schmidt, Carroll Todd, Donald R. Boldman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of surface preparation and gas flow on nitrogen atom surface recombination / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by George M. Prok and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The blunt plate in hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Donald L. Baradell, Mitchel H. Bertram, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William F. Hinson, Ralph A. Falanga, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computation of the perturbation of nearly circular orbits, using a non-sigular set of vectorial elements / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Peter Musen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical and experimental investigation of forces and frequencies resulting from liquid sloshing in a spherical tank Andrew J. Stofan and Alfred L. Armstead. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Andrew J. Stofan, Alfred L. Armstead, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An Empirical correlation of critical boiling heat flux in forced flow upward through uniformly heated tubes Uwe H. von Glahn. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Uwe H. von Glahn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the effect of convective and radiactive heat loads on the performance of subliming and charring ablators / Roger W. Peters and R. Gale Wilson. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Roger W. Peters, R. Gale Wilson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of water-absorbent materials as possible heat sinks for hypersonic and reentry vehicles Robert P. Dengler and Reeves P. Cochran. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert P. Dengler, Reeves P. Cochran, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The earth's free oscillations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Gordon J. F. MacDonald and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Acoustic phenomena observed on rocket-borne high altitude explosions William Nordberg. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William Nordberg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical solution of two-dimensional Possion equation : Theory and application to electrostatic-ion-engine analysis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Vladimir Hamza, Edward A. Richley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Victor L. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Stuart L. Treon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by John C. Montgomery and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of an axial-flow-pump stage designed by the blade-element theory - design and overall performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James E. Crouse, Richard F. Soltis, John C. Montgomery, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Surface-temperature distribution on thin-walled bodies subjected to solar radiation in interplanetary space / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An ion rocket with an electron-bombardment ion source / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Harold R. Kaufman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Liquid management in low gravity using baffled rotating containers / (Washington, D.C. : National Aeronautics and Space Administation, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Roger F. Gans and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Analysis of gravity-induced particle motion and fluid perfusion flow in the NASA-designed rotating zero-head-space tissue culture vessel / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by David A. Wolf, Ray P. Schwarz, and Lyndon B. Johnson Space Center. Medical Sciences Division. Space and Life Sciences (page images at HathiTrust)
• Effects of various assumptions on the calculated liquid fraction in isentropic saturated equilibrium expansions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Joseph W. Bursik, Robert M. Hall, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by J. Philip Drummond and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Flow visualization of discrete-hole film cooling with a spanwise injection over a cylinder / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Louis M. Russell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Contoured tank outlets for draining of cylindrical tanks in low-gravity environment / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Eugene P. Symons, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by K. James Weilmuenster, H. Harris Hamilton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fluid mechanical model of the acoustic impedance of small orifices / (Washington : U.S. National Aeronautics and Space Administration ; Springfield Va. : For sale by the National Technical Information Service, 1976), by Alan S. Hersh, Thomas Rogers, United States National Aeronautics and Space Administration, Lewis Research Center, and Hersh Acoustical Engineering (page images at HathiTrust)
• Effects of unsteady free stream velocity and free stream turbulence on stagnation point heat transfer / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Rama S. R. Gorla, Cleveland State University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• GIM code user's manual for the STAR-100 computer / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Lawrence Spradley, Mark Pearson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• On the question of instabilities upstream of cylindrical bodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Mark V. Morkovin, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Development of a three-dimensional supersonic inlet flow analysis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by R. C. Buggeln, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A simplified model for the viscous crossflow in a slotted test section / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Charlie H. Cooke, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Cryogenic-coolant He⁴-superconductor dynamic and static interactions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by George C. Marshall Space Flight Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Nonparallel stability of three-dimensional compressible boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, Scientifice and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Nabil M. El-Hady, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Internal-performance evaluation of two fixed-divergent-shroud ejectors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James R. Mihaloew and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary study of a solar-probe mission / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Duane W. Dugan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Earl C. Watson, William P. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Film condensation with and without body force in boundary-layer flow of vapor over a flat plate / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul M. Chung and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by K. R. Czarnecki, William J. Monta, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure distributions on two-dimensional sharp-leading-edge flat plates with sweep angles of 0 degrees, 30 degrees, and 45 degrees at a mach number of 6 and angles of attack from 0 degrees to 90 degrees / James G. Hondros. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James G. Hondros and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Use of conformal mapping to determine the apparent additional mass of scalloped and/or clustered cylinder configurations with experimental evaluations of results / Charles E. Watkins, Donald L. Lansing and Frederick W. Gibosn. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Charles E. Watkins, Frederick W. Gibson, Donald L. Lansing, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Influence of the tire tread pattern and runway surface condition on breaking friction and rolling resistance of a modern aircraft tire / Walter B. Horne and Trafford J.W. Leland. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Walter B. Horne, Trafford J.W. Leland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic heating and boundary-layer transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 X 10(6) / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Benjamine J. Garland, Katherine C. Speegle, Andrew G. Swanson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of magnetic triodes for direct-energy conversion having flat-plate cathodes and anodes at an arbitrary angle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by James E. Hatch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harold Ferguson, John W. Schaefer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A 1-foot hypervelocity shock tunnel in which high-enthalpy, real-gas air flows can be generated with flow times of about 180 milliseconds / Bernard E. Cunningham and Samuel Kraus. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard E. Cunningham, Samuel Kraus, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental determination of the dynamic response of a long hydraulic line / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Regetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Regime of frozen boundary layers in stagnation region of blunt reentry bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Norman T. Grier, Norman Sands, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the natural frequencies and mode shapes of liquids in oblate spheroidal tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by H. Wayne Leonard, William C. Walton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by B. H. Little, James M. Cubbage, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Byron L. Swenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of experimental and numerical results for the flow of a perfect gas about blunt-nosed bodies / Mamoru Inouye and Harvard Lomax. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Mamoru Inouye, Harvard Lomax, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of impingement angle on drop-size distribution abd spray pattern of two impinging water jets / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Marcus F. Heidmann, Hampton H. Foster, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to an electrically conducting fluid flowing in a channel with a transverse magnetic field / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Morris Perlmutter, Robert Siegel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard D. Wagner, Arthur Henderson, W. Clint Pine, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Approximate temperature distributions and streamwise heat conduction effects in the transient aerodynamic heating of thin-skinned bodies. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Raul J. Conti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary investigation of an underwater ramjet powered by compressed air / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Elmo J. Mottard, Charles J. Shoemaker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William D. Deveikis, Robert W. Walker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3.55 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Russell W. McDearmon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A cooled-tube pyrometer with experimental results obtained in a high-temperature gas stream. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by George E. Glawe, Krause,LLyod N., Robert C. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the natural frequencies of liquids in toroidal tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by John Locke McCarty, William C. Walton, H. Wayne Leonard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Propagation of free flames in laminar- and turbulent-flow fields / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Ray E. Bolz, Henry Burlage, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of the fluid oscillations in a circular cylindrical ring tank partially filled with liquid / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Helmut F. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-transfer measurements at a mach number of 4.95 on two 60 degree sweot delta wings with blunt leading edges and dihedral angles of 0 degrees and 46 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by P. Calvin Stainback and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some simple solutions to the problem of predicting boundary-layer self-induced pressures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Michael H. Bertram, Thomas A. Blackstock, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by K. R. Czarnecki and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Frederick W. Boltz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100⁰ total-angle cone and a 10⁰ half-angle conical flare section up to a mach number of 4.08 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Bernard Rashis, Aleck C. Bond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Franklyn B. Fuller and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary study of the acoustic transmission loss of two fiberglas nose cone shapes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Vern G. Rollin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of laminar compressible viscous pipe flow accelerated by an axial body force, with application to magnetogasdynamics. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by E. Dale Martin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental evaluation of analytical models for the inertias and natural frequencies of fuel sloshing in circular cylindrical tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert W. Warner, John T. Caldwell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Constant density approximations for the flow behind axisymmetric shock waves. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Albert G. Munson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of an electromagnetic mass accelerator for achieving hypervelocities. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Karlheinz Thom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of aerodynamic heat transfer and boundary-layer transition on a 15⁰ cone in free flight at supersonic mach numbers up to 5.2 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles B. Rumsey, Dorothy B. Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Predicted shock envelopes about two types of vehicles at large angles of attack / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by George E. Kaattari and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Charles L. Ladson, Thomas A. Blackstock, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William R. Wells, Charles H. McLellan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability limits of the premixed stoichiometric cyanogen-oxygen flame / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Irving Fruchtman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combustion instability limits determined by a nonlinear theory and a one-dimensional model / by Richard J. Priem and Donald C. Guentert. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1962), by Richard J. Priem, Donald C. Guentert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles R. Rumsey, Dorothy B. Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ivan E. Beckwith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experiments with plasmas produced by potassium-seeded cyanogen oxygen flames for study of radio transmission at simulated reentry vehicle plasma conditions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul W. Huber, Paul B. Gooderum, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Retrieval of dispersive and convective transport phenomena in fluids using stationary and nonstationary time domain analysis [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by J. Briscoe Stephens, Robert M. St. John, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
• A treatise on hydromechanics / (Cambridge [England] : Deighton, Bell ; London : Bell and Daldy, 1867), by W. H. Besant (page images at HathiTrust)
• The elements of hydrostatics and hydrodynamics. (Cambridge [Eng.] J.& J.J. Deighton; [etc., etc.], 1843), by William Hallows Miller (page images at HathiTrust)
• ... Mécanique des fluides / (Saint-Étienne : Société de l'imprimerie Théolier-J. Thomas & Cie, 1904), by E. Jouguet (page images at HathiTrust; US access only)
• Elements of electricity and magnetism, direct-current dynamos and motors, alternating-current machinery, operation of dynamo-electric machinery, transmission, lighting, and signaling, hydromechanics, mine pumps, first aid to the injured. (Scranton, [Pa.] : International Textbook Co., c1907), by International Textbook Company and International Correspondence Schools (page images at HathiTrust)
• Oeuvres de Mr. Mariotte, de l'Académie royale des sciences; divisées en deux tomes, comprenant tous les traitez de cet auteur; tant ceux qui avoient déja paru séparément que ceux qui n'avoient pas encore été publiez; imprimées sur les exemplaires les plus exacts & les plus complets. (Leide, P. Vander Aa, 1717), by Edmé Mariotte (page images at HathiTrust)
• Microgravity Fluid Management Symposium : proceedings of a symposium held at NASA Lewis Research Center, Cleveland, Ohio, September 9-10, 1986. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Microgravity Fluid Management Symposium (1986 : NASA Lewis Research Center) (page images at HathiTrust)
• X-ray observations of flow patterns in a mercury boiler / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by Alex Vary, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental study of multi-component coaxial-flow jets in short chambers / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Bruce V. Johnson (page images at HathiTrust; US access only)
• A critical evaluation of the status and trends in high speed fluid film lubrication / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by E. S. Kulinski and S. Ostrach (page images at HathiTrust; US access only)
• A treatise on hydromechanics ... (London, G. Bell and Sons, Ltd., 1904-), by W. H. Besant and A. S. Ramsey (page images at HathiTrust; US access only)
• Die Gestalten der Flüssigkeit ; Die Symmetrie : Zwei populäre Vorträte gehalten im Deutschen Casino zu Prag im Winter 1868 und 1871 / (Prag : J. G. Calve, 1872), by Ernst Mach (page images at HathiTrust)
• Idromeccanica piana. (Milano, Cesare Tamburini fu Camillo, 1921-), by Umberto Cisotti (page images at HathiTrust; US access only)
• Sur les figures d'équilibre peu différentes des ellipsoïdes d'une masse liquide homogène douée d'un mouvement de rotation. (St.-Pétersbourg, Imprimerie de l'Acad. impériale des sciences, 1906-14), by Aleksandr Mikhaĭlovich Lyapunov (page images at HathiTrust; US access only)
• A treatise on hydrostatics and pneumatics. (Philadelphia, Cary, Lea, & Co., 1838), by Dionysius Lardner and Benjamin Franklin Joslin (page images at HathiTrust)
• Über das Kitâb al ḥijal--das werk über die sinnreichen Anordnungen--der Benû Mûsâ, (Erlangen, M. Mencke, 1922), by Friedrich Hauser, fl. 9th century Ḥasan ibn Mūsa ibn Shākir, fl. 9th century Aḥmad ibn Mūsa ibn Shākir, and fl. 9th century Muḥammad ibn Mūsa ibn Shākir (page images at HathiTrust; US access only)
• Einleitung in die theoretische physik. Vorlesungen, gehalten an der Universität zu Königsberg von dr. F. Neumann. (Leipzig, B.G. Teubner, 1883), by F. E. Neumann and Carl Johannes Wilhelm Pape (page images at HathiTrust)
• Laboratory instruction in the mechanics of fluids. (Iowa City, The University, 1961), by Hunter Rouse (page images at HathiTrust; US access only)
• Basic fluid mechanics. (New York : McGraw-Hill, 1963), by J. Lister Robinson (page images at HathiTrust)
• The elements of hydrostatics and hydrodynamics. (Cambridge [Eng.] Printed by J. Smith for J. & J. J. Deighton; [etc., etc.], 1831), by W. H. Miller (page images at HathiTrust)
• The motion of fluids, natural and artificial; in particular that of the air and water ... (London, Printed for A. Ward [etc.], 1747), by M. Clare (page images at HathiTrust)
• Comparison of numerical and physical hydraulic models, Masonboro Inlet, North Carolina : Appendix 3, numerical simulation of hydrodynamics (Tracor) / (Fort Belvoir, Va. : Coastal Engineering Research Center ;, 1977), by R. J. Chen, Louis A. Hembree, Inc Tracor, Waterways Experiment Station (U.S.), and Coastal Engineering Research Center (U.S.) (page images at HathiTrust)
• A treatise on hydromechanics ... (London, G. Bell and Sons, Ltd., 1925-'20), by W. H. Besant and A. S. Ramsey (page images at HathiTrust; US access only)
• An elementary treatise on hydromechanics, with numerous examples / (New York : D. Van Nostrand, 1886), by Edward A. Bowser (page images at HathiTrust)
• A treatise on hydrostatics and hydrodynamics: for the use of students in the university. (Cambridge, For T. Stevenson; [etc., etc.], 1830), by Henry Moseley (page images at HathiTrust)
• Selective withdrawal from a stratified reservoir, (Washington [Environmental Protection Agency, Water Quality Office]; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1970), by Jorg Imberger, Hugo B. Fischer, and United States. Environmental Protection Agency (page images at HathiTrust)
• A collection of problems in illustration of the principles of theoretical hydrostatics and hydrodynamics. (Cambridge [Eng.] Deightons, 1847), by William Walton (page images at HathiTrust)
• Principles of fluid mechanics. (New York, Ronald Press Co., [1960]), by Richard A. Kenyon (page images at HathiTrust)
• Fluid flow in pipes; (New York, Industrial Press, [1952]), by Clifford H. McClain (page images at HathiTrust)
• Technical paper. (Minneapolis.), by St. Anthony Falls Hydraulic Laboratory (page images at HathiTrust; US access only)
• Fluid mechanics for engineers (Englewood Cliffs, N.J., Prentice-Hall, 1960), by Maurice L. Albertson (page images at HathiTrust)
• Advanced fluid mechanics (Englewood Cliffs, N.J., Prentice-Hall, 1958), by Raymond C. Binder (page images at HathiTrust)
• Fluid mechanics. (New York, Prentice-Hall, 1949), by Raymond C. Binder (page images at HathiTrust)
• Zur allgemeinen Theorie der Bewegung der Flüssigkeiten. Eine von der philosophischen Facultät der Georgia Augusta am 4.Juni 1861 gekrönte Preisschrift, von Hermann Hankel. (Göttingen, Dieterische Univ.-Buchdruckerei (W.F. Kaestner), [1861]), by Hermann Hankel (page images at HathiTrust)
• Applied fluid mechanics, (New York, London, McGraw-Hill Book Company, inc., 1937), by Morrough P. O'Brien and George Harold Hickox (page images at HathiTrust; US access only)
• Fluid and particle mechanics, (Newark, University of Delaware, 1951), by C. E. Lapple (page images at HathiTrust)
• Fluid mechanics. (New York, Asia Pub. House, [1963-), by Madhav Manohar (page images at HathiTrust)
• Mechanics of fluids. (Scranton, Pa., International textbook company, [1942]), by Glenn Murphy (page images at HathiTrust)
• Elementary theoretical fluid mechanics. (New York, Wiley, [1960]), by Karl Brenkert (page images at HathiTrust)
• Comparison of incompressible flow and isothermal compressible flow formulae / ([Washington, D.C.] : U.S. Dept. of Commerce, National Bureau of Standards, 1967), by Jesse Hord, Institute for Materials Research (U.S.). Cryogenics Division, and United States. National Bureau of Standards. Technical note (page images at HathiTrust)
• Project reports. ([Minneapolis]), by St. Anthony Falls Hydraulic Laboratory (page images at HathiTrust; US access only)
• A treatise on hydromechanics. (Cambridge, Deighton, Bell, 1891), by W. H. Besant (page images at HathiTrust)
• Della fluidità de' corpi, trattato del padre d. Claudio Fromond ... (Livorno, Per A. Santini e compagni, 1754), by Giovanni Claudio Fromond (page images at HathiTrust)
• Hydromechanik, oder Die technische mechanik flüssiger körper, (Hannover, Hahn'sche buchhandlung, 1880), by Moritz Rühlmann (page images at HathiTrust)
• Mechanics of solids and fluids. (Englewood Cliffs, N.J., Prentice-Hall, 1961), by Robert R. Long (page images at HathiTrust)
• On randomly oscillating fluid flows / (Pullman, Wash. : R.L. Albrook Hydraulic Laboratory, Division of Industrial Research : Dept. of Mechanical Engineering, 1963), by John H. Lienhard, Washington State University. Mechanical Engineering Department, and R.L. Albrook Hydraulic Laboratory (page images at HathiTrust; US access only)
• The theory of equilibrium and motion of fluids. (Cambridge [Eng.] For J. & J. J. Deighton; [etc., etc.], 1836), by Thomas Webster (page images at HathiTrust)
• Further studies on liquid sloshing. Final report. (1985), by Y. K. Lou, M. C. Wu, and C. K. Lee (page images at HathiTrust; US access only)
• The status of transport properties of air / (Livermore, CA : University of California Lawrence Radiation Laboratory, 1962), by V. E. Schrock, Lawrence Radiation Laboratory, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Gaseous diffusion at moderate flow rates in circular conduits / (Ames, Iowa : Ames Laboratory, Iowa State University of Science and Technology, 1960), by George Roley, Ray W. Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flow of an aqueous slurry through a vertical tube / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, 1957), by Harold E. Wolfe, Glenn Murphy, Ames Laboratory, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Application of the coupled fluid-structure code PELE-IC to pressure-suppression analysis : annual report to NRC for 1979 /, by William Herbert McMaster, Robert E. Nickell, N. A. Macken, E. Y. Gong, D. M. Norris, C. S. Landram, D. F. Qui©Þnones, Lawrence Livermore Laboratory, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, United States Government Printing Office, and United States. National Technical Information Service (page images at HathiTrust)
• Measurements of a supersonic favorable-pressure-gradient turbulent boundary layer with heat Transfer : part 1 -data compilation. /, by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (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)
• Compressible turbulent skin friction on rough and rough/wavy walls in adiabatic flow. /, by Daniel C Reda and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Analytical procedures used to obtain and evaluate the eddy viscosity and mixing length extracted from incompressible turbulent boundary layer data /, by W. J. Glowacki and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A Program for computing steady inviscid three-dimensional supersonic flow on reentry vehicles : volume I : analysis and programming /, by J. M. Solomon, A. B Wardlaw, J. B. Bell, R. E. Ferguson, M. Ciment, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• A Program for computing steady inviscid three-dimensional supersonic flow on reentry vehicles : volume II - users manual /, by J. M. Solomon, A. B Wardlaw, J. B. Bell, R. E. Ferguson, M. Ciment, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• A Study of the effect of pressure gradient on the eddy viscosity and mixing length for incompressible equilibrium turbulent boundary layers /, by W. J. Glowacki, S. W. Chi, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• an Integral approach to transient heat-conduction problems with phase transition /, by Tse-Fou Zien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Induced side forces on bodies of revolution at high angle of attack /, by Jr. Wardlaw, A. M. Morrison, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Cinématique et mécanismes; potentiel et mécanique des fluides. (Paris, G. Carré et C. Naud, 1899), by Henri Poincaré and A. Guillet (page images at HathiTrust; US access only)
• An assessment of the potential impact of combustion research on internal combustion engine emissions and fuel consumption. Final report. (1979), by Jack L. Kerrebrock and C. E. Kolb (page images at HathiTrust)
• Development of a fluidic antilock brake system for motorcycles. Final report. (1985), by R. R. Purves (page images at HathiTrust)
• The effect of the liquid viscosity in two-phase, two-component flow / (Argonne, Ill. : Argonne National Laboratory, 1960), by Melvin Jerome Fohrman, U.S. Atomic Energy Commission. ANL., and Argonne National Laboratory. ANL. (page images at HathiTrust)
• Vertical flow of oil and gas mixtures in small-diameter siphon-type flowstrings / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1965), by Gerald E. Rennick, R. L. Rough, and United States Bureau of Mines (page images at HathiTrust)
• Application of the Burnett method of compressibility determinations to multiphase fluid mixtures / ([Washington, DC] : Bureau of Mines, U.S. Dep. of the Interior, [1963]), by Earle S. Burnett and United States Bureau of Mines (page images at HathiTrust)
• A survey of experimental methods for determining enthalpies of fluids / ([Washington, D.C.] : United States Dept. of the Interior, Bureau of Mines, [1965]), by Robert E. Barieau and United States Bureau of Mines (page images at HathiTrust)
• Shock hydrodynamics / (Livermore, CA : University of California Lawrence Radiation Laboratory, 1962), by Mark L. Wilkins, Lawrence Radiation Laboratory, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Fluid mechanics and heat transfer for gases (air, He, H₂ and N₂) flowing single phase in closed channels : bibliography / (Livermore, CA : University of California Lawrence Radiation Laboratory, 1962), by Rose Kraft, Lawrence Radiation Laboratory, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Some practical methods of using characteristics in the calculation of non-steady compressible flow / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, 1953), by Douglas R. Hartree, U.S. Atomic Energy Commission, and Harvard University. Department of Mathematics (page images at HathiTrust)
• Pressure loads produced on a flat-plate wing by rocket jets exhausting in a spanwise direction below the wing and perpendicular to a free-stream flow of Mach number 2.0 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Ralph A. Falanga, Joseph J. Janos, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Turbulent mass transfer in liquid streams / (Ames, Iowa : Ames Laboratory , 1961), by Richard Charles Seagrave, R. W. Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A diaphragm pump for liquid metal service / (Ames, Iowa : Ames Laboratory , 1962), by D. E. Westerheide, George Burnet, J. C. Clifford, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Determination of turbulent thermal diffusivities for flow of liquids in pipes / (Ames, Iowa : Ames Laboratory, Iowa State University of Science and Technology, 1963), by William F. Beckwith, Ray Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Selective withdrawal from man-made lakes : Hydraulic Laboratory investigation / (Vicksburg, Miss. : U.S. Army Engineer Waterways Experiment Station, 1973), by Joseph P. Bohan, John L. Grace, United States Army Corps of Engineers, and Waterways Experiment Station (U.S.). Hydraulics Laboratory (page images at HathiTrust)
• Isothermalize : a computer program to size coolant passages / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation., 1962), by S. C. Skirvin, U.S. Atomic Energy Commission, and General Electric Company. Nuclear Materials and Propulsion Operation (page images at HathiTrust)
• General flow passage : a computer program to calculate aerothermal performance of an arbitrary flow passage of fixed geometry / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation, 1961), by S.C. Skirvin, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Correlation of liquid fraction in two-phase flow with application to liquid metals /, by C. J. Baroczy, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Measurement of electron concentrations in an axisymmetric nonequilibrium shock layer /, by F. H. Oertel and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Apparatus for study of fluid motion in a spinning cylinder /, by Harold M. Stoller and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Propagation of internal gravity waves in a medium of weak random vertical shear / (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by J. M. Forbes and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• COCHISE studies., by G. E. Caledonia, F. P. Delgreco, A. Corman, F. X. Robert, J. P. Kennealy, G. A. Simons, B. D. Green, and U.S. Air Force Geophysics Laboratory. Optical Physics Division (page images at HathiTrust)
• An approximate method for the calculation of the reynolds analogy factor for a compressible turbulent boundary layer in a pressure gradient /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Normal impingement of a supersonic jet on a plane : a basic study of shock-interference heating /, by Kuei-Yuan Chien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Effect of nose diameter on the erosion of spherical nosetip reentry bodies /, by Jr. Sheetz, John E. Holmes, and Naval Surface Weapons Center. White Oak Laboratory (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)
• Interacting supersonic turbulent boundary layers over a two-dimensional protuberance. /, by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Interactions between a multicomponent flow and a laser beam : part I - vaporization of liquid-air droplets by high-power laser beams /, by Kuei-Yuan Chien and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Approximate analysis of heat transfer in transpired boundary layers at limiting Prandtl numbers /, by Tse-Fou Zien and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Experimental investigation of a fin-cone interference flow field at Mach 5 /, by Jr. Gillerlain and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Temperature-step effects on direct measurement of skin-friction drag /, by Robert L. P. Voisinet and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• an Investigation of the use of holography in studying supersonic flow in inlets. /, by III Spring, W. C. Ragsdale, and Md.) Naval Ordnance Laboratory (White Oak (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 /, by Kuei-Yuan Chien and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Wind-tunnel study of oscillating flow-induced surface pressures on a tension-cone geometry model /, by Frank P. Baltakis and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range /, by Daniel C Reda, Robert A. Leverance, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Prediction of impact pressures, forces, and moments during vertical and oblique water entry /, by Jr. Wardlaw, John L. Baldwin, A. M. Morrison, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Fluid-solid surface interactions : proceedings, second symposium, June 5-6, 1974 / (Bethesda, Md. : The Center, [1974]), by Md.) Symposium on Fluid-Solid Surface Interactions (2nd : 1974 : Bethesda, Hans J Lugt, and Naval Ship Research and Development Center. Computation and Mathematics Dept (page images at HathiTrust)
• Drop coalescence / (page images at HathiTrust; US access only)
• Investigation of the mechanics of cavitation and cavitation damage / (Pasadena : California Institute of Technology, Hydrodynamics Laboratory, 1957), by Robert T. Hydrodynamics Laboratory Knapp, United States. Office of Naval Research, and Pasadena. org California Institute of Technology. Hydrodynamics Laboratory (page images at HathiTrust; US access only)
• Idromeccanica piana. ... (Milano, Libreria editrice politechnica di C. Tamburini fu Camillo, 1921-), by Umberto Cisotti (page images at HathiTrust; US access only)
• Principles of fluid mechanics. (Boston, Allyn and Bacon, 1962), by Salamon Eskinazi (page images at HathiTrust)
• Advanced fluid dynamics and fluid machinery. (New York, Prentice-Hall, 1951), by Raymond C. Binder (page images at HathiTrust)
• Marangoni convection in a gravity-free silicon float zone / (Bethesda, Md. : Carderock Division, Naval Surface Warfare Center, 1994), by Samuel Ohring, Hans J. Lugt, and Naval Surface Warfare Center (U.S.). Carderock Division (page images at HathiTrust)
• Selected topics in fluid mechanics, Summer session 1946 [New York University?] ([New York?], 1946), by K. O. Friedrichs (page images at HathiTrust)
• Die gesetze des gleichgewichts und der bewegung flüssiger körper. (Leipzig. S.L. Crusius, 1806), by Leonhard Euler, trans. by H. W. Brandes (page images at HathiTrust)
• A treatise on hydromechanics, (London, G. Bell, 1911-1913), by W. H. Besant and A. S. Ramsey (page images at HathiTrust; US access only)
• Mechanics of flow from stratified reservoirs in the interest of water quality : hydraulic laboratory investigation / (Vicksburg, Miss. : U.S. Army Engineer Waterways Experiment Station, 1969), by Joseph P. Bohan and John L. Grace (page images at HathiTrust)
• Summary of reported droplet size distribution data in dispersed two-phase flow / ([Washington, D. C.] : Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, Division of Reactor Safety Research ; Springfield, Virginia. : For sale by the National Technical Information Service, 1978), by R. V. Smith, B. J. Azzopardi, England) Atomic Energy Research Establishment (Harwell, Wichita State University, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Trattato teorico e pratico di idromeccanica. (Milano : U. Hoepli, 1915-), by Donato Spataro (page images at HathiTrust; US access only)
• Elemente der technischen hydromechanik, (Leipzig und Berlin, B. G. Teubner, 1914-), by Richard Von Mises (page images at HathiTrust; US access only)
• Traité de l'équilibre et du mouvement des fluides, pour servir de suite au traité de dynamique. (Paris : Briasson, 1770), by Jean Le Rond d' Alembert (page images at HathiTrust)
• 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)
• Electrofluidmechanics : a study of electrokinetic actions in fluids /, by Henry R. Velkoff and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division. Propulsion Laboratory (page images at HathiTrust)
• Fluid mechanics and tankage design for low gravity environments /, by Robert G. Clodfelter, sponsor Air Force Aero Propulsion Laboratory (U.S.), sponsor Wright-Patterson Air Force Base (Ohio), and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• A study of flow fields about some typical blunt-nosed slender bodies /, by Roberto Vaglio-Laurin, Massimo Trella, United States. Air Force. Office of Scientific Research. issuing body, and Polytechnic Institute of Brooklyn. Department of Aerospace Engineering and Applied Mechanics. sponsor (page images at HathiTrust)
• Point heat sources and the temperature-vorticity analogy in compressible boundary layers /, by W. J. McCroskey, United States. Air Force. Office of Scientific Research. issuing body, and Princeton University. Department of Aeronautical Engineering. sponsor (page images at HathiTrust)
• Some mass transfer effects on the wall jet /, by Herbert Fox, Martin H. Steiger, United States. Air Force. Office of Scientific Research. issuing body, and Polytechnic Institute of Brooklyn. Department of Aerospace Engineering and Applied Mechanics. sponsor (page images at HathiTrust)
• Laboratory studies of the motion of freely floating bodies in non-uniform and uniform long crested waves / (Berkeley : University of California, Institute of Engineering Research, Waves Research Laboratory, 1953), by Osvald Sibul, Berkeley. Institute of Engineering Research. Waves Investigation Laboratory. org University of California, and United States. Office of Naval Research (page images at HathiTrust; US access only)
• Experimental determination of pressures exerted by waves on a rigidly supported box of small draft / (Berkeley : University of California, Hydraulic Engineering Laboratory, Wave Research Laboratory, 1954), by K. E. Beebe, United States. Office of Naval Research, and Berkeley. Wave Research Laboratory. org University of California (page images at HathiTrust; US access only)
• A treatise on hydrostatics and pneumatics, (London, Printed from Longman, Reese, Orme, Brown & Green [etc.], 1831), by Dionysius Lardner (page images at HathiTrust)
• Stagnation point heat transfer in a relaxing gas /, by Robert E. Wilson, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation (page images at HathiTrust)
• Compressible flow modeling with the Lagrangian averaged Navier-Stokes equations /, by Paul E. Dimotakis, Kamran Mohseni, Jerrold E. Marsden, sponsor California Institute of Technology, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• An elastic tube theory of pulse transmission and oscillatory flow in mammalian arteries /, by John R. Womersley, United States. Wright Air Development Center. sponsor, and United States. Air Force. Air Research and Development Command. issuing body (page images at HathiTrust)
• Ultra high pressure air properties and CFD code /, by C. L. Merkle, sponsor Purdue University. School of Mechanical Engineering, sponsor Purdue University. School of Aeronautics and Astronautics, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Flow into a stratified reservoir /, by Antonio A. Zuluaga-Angel, Hugo B. Fischer, Rufus Benton Darden, United States. Environmental Protection Agency. Office of Research and Monitoring. issuing body, and Berkeley. sponsor University of California (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)
• Opposed jet turbulent diffusion flames /, by Lawrence Talbot, Berkeley. Department of Mechanical Engineering. sponsor University of California, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Calculated aerodynamics of wings in severe maneuver /, by J. E. McCune, Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• An elementary treatise on hydrostatics and hydrodynamics. (Dublin, W. Curry, jun., and company; [etc., etc.], 1846), by Andrew Searle Hart (page images at HathiTrust)
• Mechanics of fluids for practical men : comprising hydrostatics, descriptive and constructive ; the whole illustrated by numerous examples and appropriate diagrams / (London : William S. Orr, 1837), by Alexander Jamieson (page images at HathiTrust)
• An introduction to the mechanics of fluids / (London ; New York : Longmans, Green, 1915), by Edwin H. Barton (page images at HathiTrust)
• An introduction to fluid motion, (London, E. Arnold, 1925), by W. N. Bond (page images at HathiTrust; US access only)
• Experimental researches into the properties and motions of fluids. With theoretical deductions therefrom. (London, New York, E. & F.N. Spon, [1882]), by William Ford Robinson Stanley (page images at HathiTrust)
• Chemical evolution and estimated flow velocity of water in the Trinity aquifer, south-central Texas / (Austin, Tex. (8011 Cameron Rd., Austin 78754-3898) : U.S. Dept. of the Interior, U.S. Geological Survey ; Denver, CO : Branch of Information Services [distributor], 1997), by S. A. Jones, John F. Busby, Roger W. Lee, and Geological Survey (U.S.) (page images at HathiTrust)

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