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    Title :

    Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps


    Contributors:


    Publication date :

    1948


    Size :

    53 S


    Remarks:

    graph. Darst


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik