Research Catalog

  • Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment [microform] / Stephen A. Whitmore and Timothy Moes.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994
  • Vehicle integration effects on hypersonic waveriders [microform] / Charles Edward Cockrell, Jr.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • 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
  • Design and evaluation of candidate pressure ports for the HYFLITE experiment [microform] / John E. Teter, Jr., and Craig S. Cleckner, Alfred E. Von Theumer.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Waverider. Volume II [microform] : final report, 1987-1988.

    • Text
    • Pomona, Calif. : California State Polytechnic University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Propulsion over a wide Mach number range [microform] / Edwin L. Resler, Jr., and Barry M. Greenberg.

    • Text
    • Ithaca, NY : Cornell University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment [microform] / Herbert J. Gladden and Matthew E. Melis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • 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
  • Particle kinetic simulation of high altitude hypervelocity flight [microform] / Iain Boyd and Brian L. Haas.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation [microform] / Robert D. Quinn and Leslie Gong.

    • 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
  • A computational fluid dynamics simulation of the hypersonic flight of the Pegasus (TM) vehicle using an artificial viscosity model and a nonlinear filtering method [microform] / John Cadiz Mendoza.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995
  • [Nonlinear issues in the aerothermochemistry of gases and materials and the associated physics and dynamics of interfaces] [microform] : final report, NASA-FAMU University Research Center, January 1, 1992 - December 31, 1996, NAGW-2930 / submitted by Joseph A. Johnson III.

    • Text
    • Tallahassee, Fla. : Florida A&M University, Laboratory for Modern Fluid Physics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Improving the performance of two-stage gas guns by adding a diaphragm in the pump tube [microform] / D.W. Bogdanoff and Robert J. Miller.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system [microform] : final report : under contract NAG3-1500 / Ing Chuang, Louis G. Hunter.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Investigation of piloting aids for manual control of hypersonic maneuvers [microform] / David L. Raney, Michael R. Phillips, and Lee H. Person, Jr.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54049
  • Transpiration cooling in hypersonic flight [microform] / Domingo Tavelia and Leonard Roberts.

    • 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/LPS62036
  • Optimal trajectories for an aerospace plane [microform] / by A. Miele, W.Y. Lee, and G.D. Wu.

    • Text
    • Houston, Tex. : Rice University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 2 Resources

    Available Online

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  • Selections from "Flug Revue und Flugwelt International" [microform] / Penner, H. ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986
  • 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
  • A comprehensive analysis of the X-15 flight 3-65 accident / Cornelius J. Dennehy [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55652
  • Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / W. Lance Richards.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66583
  • Extraction of stability and control derivatives from orbiter flight data / Kenneth W. Iliff and Mary F. Shafer.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1993.
    • 1993-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71191
  • Status of turbulence modeling for hypersonic propulsion flowpaths.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo29114
  • Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / Lancert E. Foster [and three others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo38254
  • X-15 research results, with a selected bibliography / by Wendell H. Stillwell.

    • Text
    • Washington, DC : Scientific and Technical Information Division, National Aeronautics and Space Administration : United States Government Printing Office, 1965.
    • 1965
    • 1 Item
    FormatCall NumberItem Location
    Text 92513.882Off-site
  • High-speed flight propulsion systems / edited by S.N.B. Murthy, E.T. Curran.

    • Text
    • Washington, DC. : American Institute of Aeronautics and Astronautics, ©1991.
    • 1991
    • 1 Item
    FormatCall NumberItem Location
    Text TL570 .H533 1991Off-site

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