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  • 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

  • Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique [microform] : progress report for the period ended June 30, 1994 / by J.K. Ahuja, D.J. Singh, and S.N. Tiwari, principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Parametric study of shock-induced combustion in a hydrogen air system [microform] / by J.K. Ahuja and S.N. Tiwari (principal investigator).

    • Text
    • Norfolk, Va. : Institute for Computational and Applied Mechanics, Old Dominion University ; Hampton, Va. : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Spectral solution of the viscous blunt body problem. II, Multidomain approximation [microform] / David A. Kopriva.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • [Numerical computation of viscous flow around bodies and wings moving at supersonic speeds] [microform] : final report, NASA grant NGR 16-002-003, November 15, 1971 - March 31, 1984 / J.C. Tannehill.

    • Text
    • Ames, Iowa ; Engineering Research Institute, Iowa State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1984

  • 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

  • Aerodynamics of 3-dimensional bodies in transitional flow [microform] / by J. Leith Potter.

    • Text
    • Nashville, TN : Vanderbilt University, School of Engineering, Dept. of Mechanical & Materials Engineering ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Transition and turbulence modeling for blunt-body wake flows [microform] : abstract of paper proposed for the 32nd AIAA Thermophysics Conference, June 23-25, 1997, Atlanta, Georgia / Robert P. Nance, Thomas J. Horvath, H.A. Hassan.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • 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

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies [microform] / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • 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

  • 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

  • Equilibrium radiative heating tables for aerobraking in the Martian atmosphere [microform] / Lin C. Hartung, Kenneth Sutton, Frank Brauns.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59860

  • Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields [microform] : semiannual progress report, January 1990--June 1990 / Leland A. Carlson.

    • Text
    • College Station, TX : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64094

  • Equilibrium radiative heating tables for earth entry [microform] / Kenneth Sutton, Lin C. Hartung.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68893

  • Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics [microform] / prepared by Sivaram Arepalli.

    • Text
    • Houston, Tex. : Lockheed Engineering and Sciences Company : Structures and Mechanics Division and Advanced Programs Office, National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS71812

  • A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 / George C. Ashby, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71442

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

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79359

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Texas : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83038

  • Uniform foam crush testing for multi-mission earth entry vehicle impact attenuation / Byron W. Patterson and Louis J. Glaab.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41043

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