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    Title :

    Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 30-percent-chord plain flap and three tabs


    Contributors:


    Publication date :

    1940


    Size :

    14 S


    Remarks:

    graph. Darst


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik