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    Title :

    High-speed-wind-tunnel tests on an NACA 16-009 airfoil having a 32.9-percent-chord flap with an overhang 20.7 percent of the flap chord


    Contributors:


    Publication date :

    1947


    Size :

    8 S., [16] Bl


    Remarks:

    Ill., graph. Darst


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik