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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    Titel :

    Response of hypersonic winged vehicles to abrupt control displacements


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Wollner, B.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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