See also Engineering Index 1947 p 56.


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    Title :

    Effects of mach number up to 0.34 and Reynolds number up to 8×106 on maximum lift coefficient of wing of NACA 66-series airfoil sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    43 pages


    Remarks:

    Illustrations, Diagrams


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :