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    Title :

    Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively


    Contributors:


    Publication date :

    1961


    Size :

    86 S.


    Remarks:

    graph. Darst.
    Supersedes NACA technical note 4322


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik