Rigidly forced oscillatory dynamic stability method for measuring pitch and yaw damping derivatives in wind tunnels at transonic and supersonic speeds


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    Title :

    The significance of nonlinear damping trends determined for current aircraft configurations


    Contributors:


    Publication date :

    1966-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




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