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    Title :

    High-speed Wind-tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-percent-chord Flap with an Overhang 20.1 Percent of the Flap Chord


    Contributors:

    Publication date :

    1947-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English