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  • 3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions [microform] / D.R. Reddy.

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

  • 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

  • A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field [microform] / by Scott Douglas Holland.

    • Text
    • Raleligh, NC : North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Computational analysis in support of the SSTO flowpath test [microform] / Beverly S. Duncan and Charles J. Trefny.

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

  • Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code [microform] / Kamlesh Kapoor, Bernhard H. Anderson, and Robert J. Shaw.

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

  • Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 [microform] / Scott D. Holland.

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

  • Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland.

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

  • Numerical simulation of supersonic and hypersonic inlet flow fields [microform] : final report / D. Scott McRae.

    • Text
    • Raleigh, N.C. : Mars Mission Research Center, North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computational modeling and validation for hypersonic inlets [microform] / Louis A. Povinelli ; prepared for the 75th Symposium on Hypersonic Combined Cycle Propulsion sponsored by the Propulsion and Energetics Panel of AGARD, Madrid, Spain, May 28-June 1, 1990.

    • Text
    • [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/LPS62529

  • Investigation of "6X" scramjet inlet configurations / Stephen J. Alter.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33458

  • Design of three-dimensional hypersonic inlets with rectangular to elliptical shape transition / M.K. Smart.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], [January 1998]
    • 1998-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174914

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