Impingement of Water Droplets on NACA 65A004 Airfoil and Effect of Change in Airfoil Thickness From 12 to 4 Percent at 4° Angle of Attack.


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    Title :

    Impingement of water droplets on NACA 65A004 airfoil and effect of change in airfoil thickness from 12 to 4 percent at 4° angle of attack


    Additional title:

    NACA -- Tech Note


    Contributors:
    Brun, R.J. (author) / Gallagher, H.M. (author) / Vogt, D.E. (author)


    Publication date :

    1953


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :