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  • An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

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

  • Steady and unsteady three-dimensional transonic flow computations by integral equation method [microform] : final technical report / by Hong Hu, principal investigator.

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

  • Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing [microform] / M.D. Klinge, S.O. Kjelgaard and J.N. Perkins.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A theory for lateral wing-tip blowing [microform] / by D. Tavella and L. Roberts.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Measurements of wing-tip blowing [microform] / by D. Tavella, N. Wood and P. Harrits.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data [microform] / C.M. Tan and L.W. Carr.

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

  • Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Study of the unsteady flow features on a stalled wing [microform] / S. Yon and J. Katz.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A parametric study of accelerations of an airplane due to a wake vortex system [microform] / Eric C. Stewart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Measurements of supersonic wing tip vortices [microform] : 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO / M.K. Smart, I.M. Kalkhoran and J. Bentson.

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

  • On the flow processes in sharply inclined and stalled airfoils in parallel movement and rotation [microform] / M. Kohler.

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

  • Rapid state space modeling tool for rectangular wing aeroservoelastic studies / Peter M. Suh, Howard J. Conyers, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65159

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