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    Title :

    Wind-tunnel tests of ailerons at various speeds ; 4: Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil


    Contributors:

    Published in:

    Publication date :

    1943


    Size :

    17 S., [30] Bl


    Remarks:

    Ill., graph. Darst
    Originally issued August 1943 as Advance confidential report 3H28


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik