Research Catalog

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  • Some characteristics of bypass transition in a heated boundary layer [microform] / K.H. Sohn, J.E. O'Brien, and E. Reshotko.

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

  • Ultra-high bypass ratio jet noise [microform] / John K.C. Low.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Stress analysis method for clearance-fit joints with bearing-bypass loads [microform] / R.A. Naik and J.H. Crews, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Wave rotor-enhanced gas turbine engines [microform] / Gerard E. Welch, Scott M. Jones, and Daniel E. Paxson.

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

  • Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report [microform] / Joseph R. Hauser, Steven H. Zysman, and Thomas J. Barber.

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

  • Ultra-efficient engine diameter study [microform] / David L. Daggett, Stephen T. Brown, and Ron T. Kawai.

    • 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, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55129

  • Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / Christopher E. Hughes, John A. Gazzaniga.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Langley Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50535

  • HYTESS, a Hypothetical Turbofan Engine Simplified Simulation / Walter C. Merrill [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1984.
    • 1984-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52059

  • 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

  • Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / Richard F. Bozak.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.
    • 2017-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82411

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