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    Title :

    Effects of Mach number and Reynolds number on the maximum lift coefficient of a wing of NACA 230-series airfoil sections


    Contributors:


    Publication date :

    1947


    Size :

    14, [29] S.


    Remarks:

    Ill., graph. Darst.


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik