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    Title :

    Wind-tunnel investigation of an NACA 23012 airfoil with a 30-percent-chord Maxwell slat and with trailing-edge flaps


    Contributors:

    Published in:

    Publication date :

    1941


    Size :

    10 S., [8] Bl


    Remarks:

    graph. Darst
    Originally issued June 1941 as Memorandum report


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik