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    Title :

    Effects of Mach Number up to 0.34 and Reynolds Number up to 8 X 10(exp 6) Power on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections


    Contributors:

    Publication date :

    1950-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English