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    Title :

    Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 2, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic Bump Method


    Contributors:

    Publication date :

    1950-02-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English