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    Title :

    Test of NACA 66,2-116, a=0.6 airfoil section fitted with pressure balance and slotted flaps fot the wing of the XP-63 airplane


    Contributors:

    Published in:

    Publication date :

    1942


    Size :

    6 S., [7] Bl


    Remarks:

    graph. Darst
    Originally issued May 1942 as Memorandum report


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik