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  • Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.].

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

  • Computational study of generic hypersonic vehicle flow field [microform] / Johnny R. Narayan.

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

  • NASA's hypersonic research engine project [microform] : a review / Earl H. Andrews, Ernest A. Mackley.

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

  • Research in robust control for hypersonic vehicles [microform] : progress report #1 / principal investigator: A.J. Calise.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Supersonic combustion engine testbed [microform] : heat lightning / D. Hoying ... [et al.]

    • Text
    • Houston, Tex. : Universities Space Research Association ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • OVRhyp : scramjet test aircraft [microform] / J. Aslan ... [et al.].

    • Text
    • Houston, Tex. : Universities Space Research Association ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • 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

  • Numerical study of supersonic combustors by multi-block grids with mismatched interfaces [microform] / Young J. Moon.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The effect of exhaust plume/afterbody interaction on installed scramjet performance [microform] / Thomas A. Edwards.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]
    • 1988

  • Air-breathing aerospace plane development essential [microform] : hypersonic propulsion flight tests / Unmeel B. Mehta.

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

  • Investigation of ramp injectors for supersonic mixing enhancement [microform] / Y. Haimovitch, E. Gartenberg, and A.S. Roberts.

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

  • A first scramjet study [microform] / George Emmanuel.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Aeropropulsion '87. Session 6, High-speed propulsion technology [microform].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

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

  • Operating capability and current status of the reactivated NASA Lewis Research Center hypersonic tunnel facility [microform] / Scott R. Thomas, Charles J. Trefny, and William D. Pack.

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

  • 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

  • Design of a ram accelerator mass launch system [microform] : spacecraft System Design, AA 420/499C. NASA/USRA Advanced Space Design Program / prepared by Michael Aarnio ... [at al.].

    • Text
    • Seattle, WA : Dept. of Aeronautics and Astronautics University of Washington ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Shock tunnel studies of scramjet phenomena 1993 [microform] : supplement 10 / R.J. Stalker ... [et al.].

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

  • Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.].

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

  • Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations [microform] / by Tawit Chitsomboon, Surendra N. Tiwari.

    • Text
    • Norfolk, Va. : Dept. of Chemical Sciences, College of Sciences, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Heat pipe cooling for scramjet engines [microform] / Calvin C. Silverstein.

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

  • Scramjet sidewall burning, preliminary shock tunnel results, NASA contract no. NAGW-674 [microform] / by R.G. Morgan ... [et al.].

    • Text
    • [Brisbane, Australia] : University of Queensland, Dept. of Mechanical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • 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

  • Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion [microform] / Stanley K. Borowski, Donald W. Culver, and Melvin J. Bulman.

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

  • Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems [microform] : final report / Mark D. Ardema, principal investigator.

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

  • Supersonic reacting internal flow fields [microform] / J. Philip Drummond.

    • Text
    • [Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990?]
    • 1990

  • High-speed engine/component performance assessment using exergy and thrust-based methods [microform] / D.W. Riggins.

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

  • Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris.

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

  • Options for flight testing rocket-based combined-cycle (RBCC) engines [microform] / J. Olds.

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

  • Shock tunnel studies of scramjet phenomena [microform] : final technical report, NAGW-674.

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

  • Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE [microform] / C.Y. Tsai.

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

  • Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system [microform] / Nicholas J. Georgiadis, James F. Walker, and Charles J. Trefny.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Hyper-X wind tunnel program [microform] / C.R. McClinton ... [et al.].

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Computational analysis of the combustion process in an axisymmetric RBCC flowpath [microform] / Christopher J. Steffen, Shaye Yungster.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23048

  • Multidisciplinary analysis of a hypersonic engine [microform] / M.E.M. Stewart ... [et al.] ; prepared for the 11th International Conference on Space Planes and Hypersonic Systems and Technologies ... September 29-October 4, 2002.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS42592

  • Advanced fabrication techniques for hydrogen-cooled engine structures [microform] : [final report] / O. A. Buchmann ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54527

  • Fuel injector design optimization for an annular scramjet geometry [microform] / Christopher J. Steffen, Jr.

    • Text
    • [Cleveland, Ohio : NASA Glenn Research Center, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS56848

  • Mach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60779

  • Turbulent transport models for scramjet flowfields [microform] / M.M. Sindir and P.T. Harsha.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • A comprehensive model to determine the effects of temperature and species fluctuations on reaction rates in turbulent reacting flows [microform] : semi-annual status report : period covered August 1, 1983 - January 31, 1984 / F. Magnotti ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, High-Speed Aerodynamics Division, Hypersonic Propulsion Branch, [1984]
    • 1984

  • User's guide for NASCRIN--a vectorized code for calculating two-dimensional supersonic internal flow fields [microform] / Ajay Kumar.

    • Text
    • [Washington, D.C]. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1984.
    • 1984

  • Langley mach 4 scramjet test facility [microform] / Earl H. Andrews, Jr. ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96480

  • Further shock tunnel studies of scramjet phenomena / R. G. Morgan ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS112727

  • Further shock tunnel studies of scramjet phenomena [microform] / R. G. Morgan ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112727

  • Investigation of chemically-reacting supersonic internal flows [microform] / T. Chitsomboon and S.N. Tiwari.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, [1985]
    • 1985

  • Computational analyses of the LIMX TBCC inlet high-speed flowpath / Vance F. Dippold, III.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo25003

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