Research Catalog

  • On the effects of viscosity on the stability of a trailing-line vortex [microform] / Peter W. Duck, Mehdi R. Khorrami.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991-1991
  • On the linear stability of compressible plane couette flow [microform] / Peter W. Duck, Gordon Erlebacher, M. Yousuff Hussaini.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, [1991]
    • 1991
  • On the interactions between the shock wave attached to a wedge and freestream disturbances [microform] / Peter W. Duck, D. Glenn Lasseigne, M. Y. Hussaini.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge [microform] : NASA contract no. NAS1-19480 / Peter W. Duck, D. Glenn Lasseigne, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity [microform] / Peter W. Duck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59768
  • The inviscid stability of supersonic flow past a sharp cone [microform] / Peter W. Duck, Stephen J. Shaw..

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61720
  • Unsteady three-dimensional marginal separation, including breakdown [microform] / Peter W. Duck.

    • Text
    • [Washington, D.C.] : NASA ; [Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67526

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