Showing 1 - 7 results of 7 for search 'Hoffler, Keith D.', query time: 0.04s Refine Results
  1. 1
    Generic airplane model concept and four specific models developed for use in piloted simulation studies

    Generic airplane model concept and four specific models developed for use in piloted simulation studies by Hoffler, Keith D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  2. 2
    Investigation of the "vortex tab"

    Investigation of the "vortex tab" by Hoffler, Keith D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985
    Format: Government Document Book


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  3. 3
    A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration

    A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration by Rao, Dhanvada M.

    Hampton, Va. : [Springfield, Va.?] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service [distributor], 1992
    Other Authors: “…Hoffler, Keith D.…”
    Format: Government Document Book


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  4. 4
    A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps

    A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps by Rao, Dhanvada M.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1988
    Other Authors: “…Hoffler, Keith D.…”
    Format: Government Document Book


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  5. 5
    A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps

    A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps by Rao, Dhanvada M.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1988
    Other Authors: “…Hoffler, Keith D.…”
    Format: Government Document Book


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  6. 6
    High-Alpha Research Vehicle (HARV) longitudinal controller : design, analyses, and simulation results

    High-Alpha Research Vehicle (HARV) longitudinal controller : design, analyses, and simulation results by Ostroff, Aaron J.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Other Authors: “…Hoffler, Keith D.…”
    Format: Government Document Book


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  7. 7
    Simulation model of a twin-tail, high performance airplane

    Simulation model of a twin-tail, high performance airplane by Buttrill, Carey S.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992
    Other Authors:
    Format: Government Document Book


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