Research Catalog

  • The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data [microform] / C.M. Tan and L.W. Carr.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme [microform] / Dennis L. Huff, Timothy W. Swafford, and T.S.R. Reddy.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58957
  • Transonic steady- and unsteady-pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and F.W. Cazier, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
    • 1980
  • Theory of wing rock [microform] / by Chung-Hao Hsu and C. Edward Lan.

    • Text
    • Hamptan, VA : Langley Research Center, National Aeronautics and Space Administration, [1984]
    • 1984
  • An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71147

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