Method is developed for calculating spanwise lift distribution and other aerodynamic characteristics of simple wing; effects of landing flap displacement and aileron displacement considered; worked numerical examples are given in order to explain application as well as to check accuracy of method.


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    Title :

    Simple method of calculating aerodynamic characteristics of monoplane wing


    Additional title:

    Tokyo Imperial Univ -- Aeronautical Research Inst -- Report


    Contributors:
    Tani, I. (author)


    Publication date :

    1940


    Size :

    87 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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