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  1. 1
    Wake shape and its effects on aerodynamic characteristics

    Wake shape and its effects on aerodynamic characteristics by Emdad, Homayoun

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  2. 2
    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements

    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements by Lamb, Milton

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Format: Government Document Book


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  3. 3
    Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow

    Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow by Kandil, Osama A.

    [Washington, D.C.] : [National Aeronautics and Space Administration], 1997
    Format: Government Document Book


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  4. 4
    Development of a reduced area horizontal tail for a wide body jet aircraft

    Development of a reduced area horizontal tail for a wide body jet aircraft by Rising, Jerry J.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1984
    Format: Government Document Book


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  5. 5
    Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

    Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics by Leavitt, Laurence D.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Format: Government Document Book


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  6. 6
    Development of a reduced area horizontal tail for a wide body jet aircraft

    Development of a reduced area horizontal tail for a wide body jet aircraft by Rising, Jerry J.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1984
    Format: Government Document Book


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  7. 7
    Computation and validation of fluid/structure twin tail buffet response

    Computation and validation of fluid/structure twin tail buffet response by Kandil, Osama A.

    [Washington, D.C.] : [National Aeronautics and Space Administration], 1997
    Format: Government Document Conference Proceeding Book


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  8. 8
    Prediction of light aircraft horizontal tail onset flows : a review and analysis

    Prediction of light aircraft horizontal tail onset flows : a review and analysis by Summey, Delbert C.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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