Tests on airfoil sections in modified open-throat type wind tunnel developed for purpose of obtaining 2-dimensional airfoil data at transonic speeds.


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    Title :

    Effect of thickness, camber, and thickness distribution on airfoil characteristics at mach numbers up to 1.0


    Additional title:

    NACA -- Tech Note


    Contributors:
    Daley, B.N. (author) / Dick, R.S. (author)


    Publication date :

    1956


    Size :

    75 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :