Several examples are presented in which flutter involving interaction between flight mechanics modes and elastic wind bending occurs for a forward swept wing flight vehicle. These results show the basic mechanism by which the instability occurs and form the basis for attempts to actively control such a vehicle.


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    Title :

    Interactive Aircraft Flight Control and Aeroelastic Stabilization


    Contributors:

    Publication date :

    1981


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English