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    Title :

    Effects of Plan Form, Airfoil Section, and Angle of Attack on the Pressures Along the Base of Blunt-trailing-edge Wings at Mach Numbers of 1.41, 1.62, and 1.96


    Contributors:

    Publication date :

    1952-09-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English