Research Catalog

  • Effects of spoiler surfaces on the aeroelastic behavior of a low-spect-ratio rectangular wing [microform] / Stanley R. Cole.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
  • Some buffet response characteristics of a twin-vertical-tail configuration [microform] / Stanley R. Cole, Steven W. Moss, and Robert V. Doggett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
  • The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel [microform] / Stanley R. Cole, José A. Rivera, Jr.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Dynamic response of a hammerhead launch vehicle wind-tunnel model [microform] / Stanley R. Cole, Thomas L. Henning.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64065
  • Exploratory flutter test in a cryogenic wind tunnel [microform] / Stanley R. Cole.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

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