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    Title :

    An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line desined to produce a high critical mach number


    Contributors:


    Publication date :

    1948


    Size :

    33 S.


    Remarks:

    graph. Darst.


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik