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    Title :

    Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degree, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination with a Fuselage at High Subsonic Mach Numbers and Mach Num


    Contributors:

    Publication date :

    1951-06-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English