New method, based on lifting line theory, makes use of lift distribution due to angle of attack and takes into account aspect ratio of wing.


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    Title :

    Improved approximate methods for calculating lift distributions due to twist


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1951


    Size :

    35 pages


    Remarks:

    Charts


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :