Effects of compressibility on lift and load characteristics of tapered wing of NACA 64-210 airfoil sections up to Mach number of 0.60.


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    Title :

    Effects of compressibility on lift and load characteristics of tapered wing of NACA 64-210 airfoil sections up to Mach number of 0.60


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    West, Jr., F.E. (author) / Himka, T. (author)


    Publication date :

    1949


    Size :

    48 pages


    Remarks:

    Illus, Charts, Diagrs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :