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  • 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

  • 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

  • Entropy jump across an inviscid shock wave [microform] / Manuel D. Salas, Angelo Iollo.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Reentry-F flowfield solutions at 80,000 ft. [microform] / W.A. Wood, C.J. Riley, and F.M. Cheatwood.

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

  • Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes [microform] / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1989 [microform] / William B. Jones, Jr., Stanley H. Goldstein, eds.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 2 Resources

    Available Online

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  • 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

  • Gas-jet and tangent-slot film cooling tests of a 12.5⁰ cone at Mach number of 6.7 [microform] / Robert J. Nowak.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
    • 1 Resource

    Available Online

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

  • 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

  • Molecular processes in a high temperature shock layer [microform] : semi-annual status report, May 1, 1984-October 31, 1984 / Steven L. Guberman.

    • Text
    • Stoneham, MA : Institute for Scientific Research ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984]
    • 1984

  • Detection of bump-on-tail reduced electron velocity distributions at the electron foreshock boundary [microform] / R. J. Fitzenreiter, A. J. Klmas, and J. D. Scudder.

    • Text
    • Greenbelt, Md. : National Aeronautics and Space Administration, Goddard Space Flight Center, [1984]
    • 1984

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