J. WEISSINGER method used to find lift-curve slope, spanwise center of pressure, aerodynamic center location, and span loading coefficients of untwisted and uncambered wings having wide range of plan forms; results presented in graphical form; methods for determining induced drag and approximate effects of compressibility.


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    DeYoung, J. (author)


    Publication date :

    1947


    Size :

    17 pages


    Remarks:

    20 Supp plates, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :