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    Title :

    Aerodynamic Characteristics at a Mach Number of 1.25 of a 6-percent-thick Triangular Wing and 6- and 9-percent-thick Triangular Wings in Combination with a Fuselage : Wing Aspect Ratio 2.31, Biconvex Airfoil Sections


    Contributors:

    Publication date :

    1950-05-05


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English