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    Title :

    Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 2, Taper Ratio 0.78, and NACA 65A004 Airfoil Section - Transonic Bump Method


    Contributors:

    Publication date :

    1950


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English