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    Title :

    Effects of a Leading-edge Slat and a Trailing-edge Split Flap on the Aerodynamic Characteristics of a Wing-fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers from 0.60 to 0.92


    Contributors:

    Publication date :

    1958-01-12


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English