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  • Aircraft wing structural detail design (wing, aileron, flaps and subsystems) [microform] : statement of work number 2 / AE421-04 Carbon Copy Design Inc. (TEAM 1), Robert Downs, lead engineer ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Numerical design of advanced multi-element airfoils [microform] : final report / Donovan L. Mathias, Russell M. Cummings.

    • Text
    • San Luis Obispo, CA : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing [microform] / by Michelle Therese Martuccio.

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

  • Flow over swept flaps and flap tips [microform] : final technical report to NASA Langley Research Center on NAG-1-1614 / Peter Bradshaw, principal investigator; Carl U. Buice.

    • Text
    • [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computation of lifting wing-flap configurations [microform] : NASA grant NCC2-5070, final report ... funding dates: July 1, 1994 to June 30, 1995 / Brian Cantwell, Dochan Kwak.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • A final report on the NASA grant NAG-1-1612 of large-vortex capture by a wing at very high angles of attack [microform] / prepared by J.M. Wu ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Velocity and temperature decay characteristics of inverted-profile jets [microform] / U. von Glahn, J. Goodykoontz, and C. Wasserbauer.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • An aerodynamic analysis computer program and design notes for low speed wing flap systems [microform] / Harry W. Carlson and Kenneth B. Walkley ; prepared for Langley Research Center under contract NAS1-16000.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983.
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104929

  • Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques / Kenneth M. Jones, Robert T. Biedron, Mark Whitlock.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77771

  • Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques / Kenneth M. Jones, Robert T. Biedron, Mark Whitlock.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995

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