Research Catalog

  • Three-dimensional cavity flow fields at subsonic and transonic speeds [microform] / E.B. Plentovich.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
    • 1990
  • Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel [microform] / E.B. Plentovich and Blair B. Gloss.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986
  • The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers [microform] / E.B. Plentovich.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
    • 1986
  • Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds [microform] / E.B. Plentovich, Julio Chu, and M.B. Tracy.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67795
  • Tests of a NACA 65₁-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel [microform] / E.B. Plentovich, Charles L. Ladson, Acquilla S. Hill.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

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