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  1. 1
    Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /
    by Mason, Mary L
    Published 1983

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  2. 2
    Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft /
    by Capone, Francis J
    Published 1983

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  3. 3
    Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers /
    by Blair, A. B
    Published 1983

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  4. 4
    Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft /
    by Capone, Francis J
    Published 1983

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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  5. 5
    Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /
    by Mason, Mary L
    Published 1983

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    Government Document Book
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  6. 6
    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /
    by Pittman, Jimmy L
    Published 1984

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  7. 7
    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization
    by Carlson, Harry W
    Published 1990

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  8. 8
    Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
    by Satran, Dale R
    Published 1986

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  9. 9
    An in-flight interaction of the X-29A canard and flight control system /
    by Kehoe, M. W
    Published 1990

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  10. 10
    High-angle-of-attack stability characteristics of a three-surface fighter configuration /
    by Grafton, Sue B
    Published 1983

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