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    Title :

    Wind-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes


    Contributors:

    Published in:

    Publication date :

    1945


    Size :

    12 S.


    Remarks:

    Ill., graph. Darst.
    Originally issued April 1945 as Advance restricted report L5B17


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik