Research Catalog

  • High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions [microform] / Julio Chu and Pierce L. Lawing.

    • 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
  • Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996- ]
    • 1996-present

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