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    Title :

    High-speed-wind-tunnel tests on 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


    Size :

    33 S


    Remarks:

    Ill., graph. Darst
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik