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  • Numerical flux formulas for the Euler and Navier-Stokes equations [microform] / William J. Coirier and Bram van Leer.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor], <1991- >
    • 1991-present

  • Experimental studies of shock-wave/wall-jet interaction in hypersonic flow [microform] / Michael S. Holden, Kathleen Rodriguez.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Center, distributor, 1994]
    • 1994

  • Development and application of computational aerothermodynamics flowfield computer codes [microform] / Ethiraj Venkatapathy.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1994]
    • 1994

  • Shock-tunnel combustor testing for hypersonic vehicles [microform] / Mark Loomis.

    • Text
    • San Jose, Calif. : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Three dimensional viscous analysis of a hypersonic inlet [microform] / D.R. Reddy ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1989?]
    • 1989

  • High-order polynomial expansions (HOPE) for flux-vector splitting [microform] / Meng-Sing Liou and Chris J. Steffen, Jr.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991?]
    • 1991

  • In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows [microform] : design and development / Kon-Sheng Charles Wang.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids [microform] / Guruaja R. Vemaganti.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Experimental results for a hypersonic nozzle/afterbody flow field [microform] / Frank W. Spaid, Earl R. Keener, Frank C.L. Hui.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Application of pressure sensitive paint in hypersonic flows [microform] / Kenol Jules and Mario Carbonaro and Stephan Zemsch.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Development of computer models for correlating data of film cooling of nose cone under hypersonic flow [microform] : semi-annual status report (April 1, 1986 to September 30, 1986) / principal investigator, L. Sharpe, Jr.

    • Text
    • Greensboro, NC : North Carolina A&T State University : [Washington, D.C. : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Semi-implicit and fully implicit shock-capturing methods for hyperbolic conservation laws with stiff source terms [microform] / H.C. Yee, Judy L. Shinn.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • DSMC calcuations for a 70⁰ blunted cone at 3.2km/s in nitrogen [microform] / J.N. Moss and J.M. Price, V.K. Dogra .

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Experimental investigation of hypersonic aerodynamics [microform] : semi-annual research report for the period April 1, 1987 - September 30, 1987 / prepared by Eloret Institute ; K. Heinemann, Peter F. Intrieri, principal investigator.

    • Text
    • Sunnyvale, CA : The Institute ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • High-resolution shock capturing scheme for high Mach number internal flow [microform] / Seokkwan Yoon and Antony Jameson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Turbulence modeling [microform] / Jorge E. Bardina.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12 [microform].

    • Text
    • [Brisbane, Australia] : University of Queensland ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hypersonic flows as related to the national aerospace plane [microform] / Marvin Kussoy, George P.-G. Huang, F. Menter.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers [microform] : final grant report / Eric F. Spina.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Development of an upwind, finite-volume code with finite-rate chemistry [microform] / Gregory A. Molvik.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Electron-beam diagnostic methods for hypersonic flow diagnostics [microform] : final NASA report grant no. 2-718.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Parallelization of a parabolized Navier-Stokes solver with a design optimizer [microform] : 34th AIAA Aerospace Sciences Meeting and Exhibit / J.M. Pallis and J.J. Chattot, S.L. Lawrence.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes [microform] / Zheng-Tao Deng ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Review of blunt body wake flows at hypersonic low density conditions [microform] / J.N. Moss and J.M. Price.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Applications of quantum theory of atomic and molecular scattering to problems in hypersonic flow [microform] : final report / F. Bary Malik.

    • Text
    • Carbondale, Ill. : Southern Illinois University at Carbondale ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Effects of chemistry on blunt-body wake structure [microform] / V.K. Dogra ... [et al.].

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone [microform] : final report / principal investigator, Gregory V. Selby ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.
    • 1996

  • Hypersonic pitching-moment shift for stardust reentry capsule forebody [microform] / William A. Wood.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • Computational aeroheating predictions for X-34 [microform] / William L. Kleb, William A. Wood, and Peter A. Gnoffo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Pegasus wing-glove experiment to document hypersonic crossflow transition [microform] : measurement system and selected flight results / Arild Bertelrud ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Hypersonic flows about a 25̊ sharp cone [microform] / James N. Moss.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27166

  • Validation of WIND for a series of inlet flows [microform] / John W. Slater, John M. Abbott, and Richard H. Cavicchi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS46512

  • Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 [microform] / Don E. Avery.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985

  • Comparison of nonequilibrium solution algorithms applied to chemically stiff hypersonic flows [microform] / G. Palmer and E. Venkatapathy.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54368

  • Optimum shape of a blunt forebody in hypersonic flow [microform] / L. Maestrello, L. Ting.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58433

  • On the instability of hypersonic flow past a flat plate [microform] / Nicholas Blackaby, Stephen Cowley, Philip Hall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60955

  • Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows [microform] : progress report for the period ended December 31, 1989 / by D. J. Singh and S. N. Tiwari ; prepared for National Aeronautics and Space Administration, Langley Research Center.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63194

  • An approximate method for calculating three-dimensional inviscid hypersonic flow fields [microform] / Christopher J. Riley, Fred R. DeJarnette.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65619

  • Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows [microform] / A.R. Porro ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67809

  • The stability of two-dimensional wakes and shear-layers at high Mach numbers [microform] / D.T. Papageorgiou.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69039

  • Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations [microform] / Gregory M. Gatlin.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68634

  • Application of CFD to aerothermal heating problems [microform] / Michele G. Macaraeg.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • Experimental program for real gas flow code validation at NASA Ames Research Center [microform] / George S. Deiwert ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : For sale by the National Technical Information Service, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92592

  • Particle kinetic simulation of high altitude hypervelocity flight [microform] : periodic research report for the period February 1, 1992 - December 31, 1992 / Iain Boyd and Brian L. Haas.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center, [1993]
    • 1993
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98071

  • Mutual effect of thermochemical surface decomposition and viscous interaction during hypersonic flow past a sharp cone [microform] / A.V. Limanskiy, V.I. Timoshenko.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • High speed corner and gap seal computations using an LU-SGS scheme / William J. Coirier.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108391

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