Research Catalog

  • Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques [microform] / Raymond E. Mineck.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992
  • Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Raymond E. Mineck and Acquilla S. Hill.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
  • Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip [microform] / by Raymond Edward Mineck.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992
  • Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line [microform] / Raymond E. Mineck, Paul M. H. W. Vijgen.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993
  • Application of two procedures for dual-point design of transonic airfoils [microform] / Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Study of potential aerodynamic benefits from spanwise blowing at wingtip [microform] / Raymond E. Mineck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000
  • Reynolds number effects on the performance of lateral control devices / Raymond E. Mineck.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2000.
    • 2000-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86203

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