Research Catalog

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  • Hot-jet simulation in cryogenic wind tunnels [microform] / Keisuke Asai.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989

  • Radiation from advanced solid rocket motor plumes [microform] / by: Richard C. Farmer, Sheldon D. Smith, Bryan L. Myruski.

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

  • High-altitude plume computer code development [microform] : final report / by Beverly J. Audeh, Jesse E. Murph.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center, [1985]
    • 1985

  • Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / by Marc W. Kniskern.

    • Text
    • Raleigh, [N.C.] : North Carolina State University, Dept. of Mechanical and Aerospace Engineering, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69058

  • Analysis of internal flow in a ventral nozzle for STOVL aircraft [microform] / C. Frederic Smith and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69189

  • Simulation investigation of the effect of the NASA Ames 80- by 120-foot wind tunnel exhaust flow on light aircraft operating in the Moffett Field traffic pattern [microform] / Barry G. Streeter.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104852

  • Impact of an exhaust throat on semi-idealized rotating detonation engine performance / Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.
    • 2016-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68694

  • Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / Jeffery A. Yetter, Laurance D. Leavitt.

    • 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/gpo71384

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