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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    Title :

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


    Contributors:

    Publication date :

    1974


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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