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    Title :

    Low-speed Pressure-distribution Investigation of a Spoiler and a Spoiler-slot-deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section


    Contributors:

    Publication date :

    1956-01-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English