Authors demonstrate that under given incident flow conditions, forces on airfoil depend only on characteristics of trailing vortex sheet, i.e., on potential flow due to this sheet at considerable downstream distance. Brief English abstract from Luftfahrtforschung v 20 n 2 Feb 27 1943 p 48-56. (Abstract Sec)


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    Title :

    Theory of lifting wing


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Nikuradse, J. (author) / Mohr, E. (author)

    Published in:

    Publication date :

    1943


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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