Research Catalog

  • Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction [microform] : final report / by H.T. Nagamatsu and R. Dyer.

    • Text
    • [Hampton, Va.? : National Aeronautics and Space Administration, Langley Research Center, 1984]
    • 1984
  • Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction [microform] : semi-annual report for the period March 16, 1983 to September 14, 1983 / by H.T. Nagamatsu, R. Ficarra, R. Orozco.

    • Text
    • [Hampton, Va.?] : NASA Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS86568
  • Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
    • 1984

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