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  1. 1
    Numerical study of steady and unsteady canard-wing-body aerodynamics

    Numerical study of steady and unsteady canard-wing-body aerodynamics by Tu, Eugene L.

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


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  2. 2
    Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system

    Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system by Banks, Daniel W.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  3. 3
    Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

    Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 by Walker, Ira J.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  4. 4
    1999 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999

    1999 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C.,...

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Conference Proceeding Book


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  5. 5
    Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail

    Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail by Whiting, Matthew Robert

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  6. 6
    Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails

    Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails by Allen, Jerry M.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  7. 7
    Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport

    Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport by Lee, Christopher A.

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


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