Research Catalog

  • On the nonlinear stability of a high-speed, axisymmetric boundary layer [microform] / C. David Pruett, Lian L. Ng, Gordon Erlebacher.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991-1991
  • On the wall-normal velocity of the compressible boundary-layer equations [microform] / C. David Pruett; prepared for Langley Research Center under contract NAS1-18599.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1991.
    • 1991
  • A spectrally accurate boundary-layer code for infinite swept wings [microform] / C. David Pruett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994
  • Simulation of crossflow instability on a supersonic highly swept wing [microform] / C. David Pruett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Computational investigations of noise suppression in subsonic round jets [microform] : final report for NASA grant NAG1-1802 / principal investigator, C. David Pruett.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

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