The experimental and analytical techniques used in free rolling motion of vehicles are summarized. The flight dynamics at significant angles of attack are discussed in relation to nonlinear aerodynamic characteristics and pitch-yaw-roll coupling. The problem of nonoscillatory free-flight motion analysis is addressed. Equations for roll data reduction applicable to aircraft configurations are presented.


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    Titel :

    Rolling Motion of Canard Missiles in Wind Tunnel Free-Flight Tests


    Beteiligte:
    M. E. Beyers (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    32 pages



    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch