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    Title :

    An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.59


    Contributors:

    Publication date :

    1950-06-29


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English