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    Title :

    Free-flight Longitudinal-stability Investigation Including Some Effects of Wing Elasticity from Mach Numbers of 0.85 to 1.34 of a Tailless Missile Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 5.5


    Contributors:

    Publication date :

    1953-08-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English