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  • A wall interference assessment/correction system [microform] / Dr. C.F. Lo, principal investigator.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An experimental study of an adaptive-wall wind tunnel [microform] / by Zeki Celik and Leonard Roberts.

    • Text
    • Stanford, CA : Joint Institute for Aeronautics and Acoustics, Stanford University, Dept. of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Flow in out-of-plane double s-bends [microform] / by M.C. Schmidt, J.H. Whitelaw and M. Yianneskis.

    • Text
    • London, England : Imperial College of Science and Technology, Fluids Section, Mechanical Enginering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Derivation of jack movement influence coefficients as a basis for selecting wall contours giving reduced levels of interference in flexible walled test sections [microform] / M.J. Goodyer.

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • Analytical studies of boundary layer generated aircraft interior noise [microform] / M.S. Howe and P.L. Shah.

    • Text
    • Boston, MA : Boston University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel [microform] / Norbert Ulbrich.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Computer simulation of a wind tunnel test section with discrete finite-length wall slots [microform] / William B. Kemp, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT [microform] : final memorandum report.

    • Text
    • [Tullahoma, Tenn. : The University of Tennessee-Calspan Center Aerospace Research (CAR) ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61599

  • Use of adaptive walls in 2D tests [microform] / J.P. Archambaud and J.P. Chevallier.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1984]
    • 1984

  • Sidewall boundary-layer effects in two-dimensional airfoil testing [microform] : progress report for the period ending June 1985 / by A.V. Murthy ; principal investigator: G.L. Goglia ; prepared for the National Aeronautics and Space Administration, Langley Research Center ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, [1985]
    • 1985

  • Data reduction functions for the Langley 14- by 22-foot subsonic tunnel / Andy D. Boney.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2014.
    • 2014-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54991

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