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    Title :

    Wing-flow Measurements of Longitudinal Stability and Control Characteristics of a Supersonic Airplane Configuration Having a 42.8 Degree Sweptback Circular Arc Wing with Aspect Ratio 4.0, Taper Ratio 0.50, and Sweptback Tail Surfaces


    Contributors:

    Publication date :

    1950-04-03


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English