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    Title :

    An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.59


    Contributors:

    Publication date :

    1950-05-23


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English