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    Title :

    Lift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces


    Contributors:

    Publication date :

    1955-04-25


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English