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    Title :

    The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section


    Contributors:

    Publication date :

    1953-05-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English