Effects of Independent Variations of Mach Number and Reynolds Number on Maximum Lift Coefficients of Four NACA 6-Series Airfoil Sections.


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    Title :

    Effects of independent variations of mach number and Reynolds number on maximum lift coefficients of four NACA 6-series airfoil sections


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1952


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :