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    Title :

    Effects of independent variations of mach number and Reynolds number of the maximum lift coefficients of four NACA 6-series airfoil sections


    Contributors:


    Publication date :

    1952


    Size :

    32 S.


    Remarks:

    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
    RVK:    ZO 7000