Access

    Redirect to SLUB

    Check availability in my library


    Export, share and cite



    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.


    Type of media :

    Miscellaneous


    Type of material :

    Print


    Language :

    English



    Classification :

    RVK:    ZO 7000
    BKL:    55.50 / 50.34