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    Title :

    Chordwise pressure distributions on a 12-foot-span wing of NACA 66-series airfoil sections up to a Mach number of 6.0


    Contributors:


    Publication date :

    1948


    Size :

    147 S


    Remarks:

    Ill., graph. Darst
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik