Research Catalog

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  • 1700 [degree] C optical temperature sensor [microform] : final report / P.W. Mossey, principal investigator, W.M. Shaffernocker, A.R. Mulukutla.

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

  • Summary of investigations of engine response to distorted inlet conditions [microform] / Thomas J. Biesiadny ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1986?]
    • 1986

  • Heat transfer computations of internal flows with combined hydraulic and thermal developing length [microform] / C.R. Wang ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • SRM internal flow test and computational fluid dynamic analyses [microform] : final report : contract NAS8-39095 / prepared by ERC, Incorporated.

    • Text
    • Huntsville, AL : ERC, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995- ]
    • 1995-present

  • Prediction of nonuniform inlet temperature effects on vane and rotor heat transfer [microform] / R.J. Boyle, P.W. Giel.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Experimental evaluation of the ignition process of carbon monoxide and oxygen in a rocket engine [microform] / Diane L. Linne.

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

  • Advanced seal technology role in meeting next generation turbine engine goals [microform] / Bruce M. Steinetz and Robert C. Hendricks, John Munson.

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

  • A performance map for ideal air breathing pulse detonation engines [microform] / Daniel E. Paxon.

    • 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/LPS26960

  • Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / Zhuohui J. He [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54279

  • Experimental evaluation of the ignition process of carbon monoxide and oxygen in a rocket engine / Diane L. Linne.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69460

  • Low-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system / Jerrold D. Wear, Arthur M. Trout, and John M. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
    • 1980-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71101

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