Research Catalog

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  • Automotive gas turbine power system-performance analysis code [microform] / Albert J. Juhasz.

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

  • Development of advanced in-cylinder components and tribological systems for low heat rejection diesel engines [microform] : phases 2, 3, and 4 final report / T.M. Yonushonis ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application [microform] / Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt.

    • 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/LPS23306

  • Probabilistic analysis of solid oxide fuel cell based hybrid gas turbine system [microform] / Rama S.R. Gorla, Shantaram S. Pai and Jeffrey J. Rusick.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59604

  • Natural environment design criteria for the space station program definition phase [microform] / by William W. Vaughan.

    • Text
    • [ Huntsville, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99119

  • The influence of unsteadiness on the analysis of pressure gain combustion devices / Daniel E. Paxson, Tom Kaemming.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2013.
    • 2013-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51821

  • NASA Fixed Wing Project propulsion research and technology development activities to reduce thrust specific energy consumption / Michael D. Hathaway and Ruben Del Rosario, Nateri K. Madavan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53623

  • Probabilistic analysis of gas turbine field performance / Rama S.R. Gorla, Shantaram S. Pai and Jeffrey J. Rusick.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2002.
    • 2002-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo61359

  • Automotive gas turbine power system-performance analysis code / Albert J. Juhasz.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January1997.
    • 1997-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70917

  • Performance of semi-transpiration-cooled liner in high-temperature-rise combustor / Jerrold D. Wear, Arthur M. Trout and John M. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, March 1981.
    • 1981-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71512

  • Overview of NASA Lewis Research Center free-piston Stirling engine activities / Jack G. Slaby.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77204

  • Overview of NASA Lewis Research Center free-piston Stirling engine activities / Jack G. Slaby.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application / Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2001.
    • 2001-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23306

  • Performance of an Advanced Stirling Convertor based on heat flux sensor measurements / Scott D. Wilson.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37970

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