Analytical studies of response of vehicles to pilot induced longitudinal maneuvers indicate that vehicles may rapidly approach their structural limits at combinations of high dynamic pressure and Mach number; results of investigation by General Dynamics/ Astronautics; parametric studies to determine effect of vehicle characteristics and operational requirements upon vehicle response; relative influence of design and operational parameters upon vehicle response to control surface deflection is shown and means of alleviating problem during preliminary design.


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    Title :

    Response of hypersonic winged vehicles to abrupt control displacements


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1966


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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