This document presents symmetric flutter analyses conducted on the all-movable horizontal tail of the Boeing-designed SST. Interaction effects on flutter speed that are produced by the wing, fuselage, control systems and elevator gear ratio are included. Failure conditions of the horizontal-tail actuators are covered. (Author)


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    Titel :

    Flutter Analysis of an All-Movable Horizontal Tail with Geared Elevator on a Supersonic Transport


    Beteiligte:
    J. L. Stelma (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    60 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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