Research Catalog

  • Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration [microform] / Donald R. Riley and Jay M. Brandon, Louis J. Glaab.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept [microform] / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS72303
  • Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method / Donald R. Riley.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67295
  • Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration / Donald R. Riley and Jay M. Brandon, Louis J. Glaab.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1994.
    • 1994-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157689

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