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    Title :

    Lift tests of a 0.1536c thick Douglas airfoil section of NACA 7-series type equipped with a lateral-control device for use with a full-span double-slotted flap on the C-74 airplane


    Contributors:

    Published in:

    Publication date :

    1945


    Size :

    9 S., [30] Bl


    Remarks:

    Ill., graph. Darst
    Originally issued March 1945 as Memorandum report L5C24a


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik