Procedure based upon J.WEISSINGER method presented so that basic span loading, angle of zero lift, and pitching moment due to twist can be readily predicted for wide range of plan forms.


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    Title :

    Theoretical basic span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    33 pages


    Remarks:

    Illus, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :