Research Catalog

  • Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft [microform] / Richard J. Re and George T. Carson, Jr.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
  • Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993
  • A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986
  • A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / Richard J. Re and William K. Abeyounis.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68006

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