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    Title :

    Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections


    Contributors:
    Pearson, E. O. (author) / Evans, A. J. (author) / West, F. E. (author)

    Publication date :

    1945


    Size :

    13 S., [15] Bl


    Remarks:

    Ill., graph. Darst
    Advance confidential report L5G10
    Auch als: Wartime report ; L-51


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik