Some early experimental results from a combined experimental and analytical study being conducted at NASA-Langley of the transonic flutter characterisitics of a generic arrow wing configuration are presented. The planned study includes the parametric variation of a variety of structural and geometric characteristics. Presented here are flutter results of the basic arrow wing, for the basic wing with the addition of two simulated lower-surface-mounted engine nacelles, and for the basic wing with the addition of both the fin and the engine nacelles.


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    Title :

    Parametric flutter studies of an arrow-wing configuration: Some early results



    Publication date :

    1988-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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