Treatment of problem of wing of finite span has been on basis of 2-dimensional theory, corrected for effect of wake; problem of 3-dimensional flow considered; correction formulas given.


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    Title :

    Theoretical correction for lift of elliptic wings


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Jones, R.T. (author)


    Publication date :

    1941


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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