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    Title :

    Effects of Mach number up to 0.34 and Reynolds number up to 8 x 10 6 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections


    Contributors:


    Publication date :

    1950


    Size :

    43 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