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    Title :

    Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25.c slotted flap for the fleetwings XA-39 airplane


    Contributors:

    Published in:

    Publication date :

    1944


    Size :

    11 S., [15] Bl


    Remarks:

    graph. Darst
    Originally issued November 1944 as Memorandum report L4K21


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik




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