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    Title :

    Effect of Wing Camber and Twist at Mach Numbers from 1.4 to 2.1 on the Lift, Drag, and Longitudinal Stability of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces


    Contributors:

    Publication date :

    1956-05-07


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English