Research Catalog

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  • Numerical investigation of the effects of icing on fixed and rotary wing aircraft [microform] : progress report for the period January 1, 1992-June 30, 1992 / prepared by L.N. Sankar.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Numerical investigation of the effects of icing on fixed and rotary wing aircraft [microform] : progress report for the period January 1, 1992 - June 30, 1992 / prepared by L.N. Sankar.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Flight simulation software at NASA Dryden Flight Research Center [microform] / Ken A. Norlin.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Linthicum Heights, MD : Available from the NASA Center for AeroSpace Information ; Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • System identification methods for aircraft flight control development and validation [microform] / Mark B. Tischler.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, Aeroflightdynamics Directorate ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Extension of a three-dimensional viscous wing flow analysis [microform] / Bernard C. Weinberg ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68268

  • Rotor systems research aircraft [microform] : fixed-wing simulations results / Robert M. Kufeld.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • NASA collaborative research on the ultra high bypass engine cycle and potential benefits for noise, performance, and emissions / Christopher E. Hughes.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo50534

  • 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

  • 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

  • Performance and weight estimates for an advanced open rotor engine / Eric S. Hendricks and Michael T. Tong.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33031

  • Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model / by Edward J. Ray and Robert T. Taylor.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, March 1966.
    • 1966-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo219374

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