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    Title :

    Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 I : Maximum Thickness at 20 Percent of the Chord


    Contributors:

    Publication date :

    1948-11-19


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English