Research Catalog

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  • 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop [microform] : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999 / edited by David E. Hahne.

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

  • Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 [microform] / Ira J. Walker, Peter F. Covell And Dana K. Forrest.

    • 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

  • Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails [microform] / Jerry M. Allen and Carolyn B. Watson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system [microform] / Daniel W. Banks and John W. Paulson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
    • 1987

  • Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport [microform] / Christopher A. Lee.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail [microform] / by Matthew Robert Whiting.

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

  • Numerical study of steady and unsteady canard-wing-body aerodynamics [microform] / Eugene L. Tu.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Parametric study of a canard-configured transport using conceptual design optimization [microform] / P. Douglas Arbuckle and Steven M. Sliwa.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Space shuttle orbiter trimmed center-of-gravity extension study [microform] : summary report / William I. Scallion and W. Pelham Phillips.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Wind-tunnel investigation of a full-scale canard-configured general aviation airplane [microform] / Long P. Yip.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54941

  • A computer module used to calculate the horizontal control surface size of a conceputal aircraft design [microform] / principal investigator, Doral R. Sandlin ; student assistant, Stephen Mark Swanson..

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69281

  • Unsteady transonic flow calculations for two-dimensional canard-wing configurations with aeroelastic applications [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Space shuttle orbiter trimmed center-of-gravity extension study. Volume ix. Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 / W. Pelham Phillips and Roger H. Fournier.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January1985.
    • 1985-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59036

  • Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds / Gary E. Erickson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40586

  • Effect of canard position and wing leading-edge flap deflection on wing buffet at transonic speeds / by Blair B. Gloss, William P. Henderson, and Jarrett K. Huffman.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1975.
    • 1975-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157696

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