O. SCHRENK's method for finding wing lift distribution can be taken further in order to determine pitching moment coefficient about quarter-chord point of mean chord at no-lift; fore and aft position of standard mean chord. See also Engineering Index 1944 p 57.


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    Title :

    Wing pitching moment coefficient


    Additional title:

    Aircraft Eng


    Contributors:
    Morse, W.L. (author)

    Published in:

    Publication date :

    1945


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wing Pitching Moment Coefficient

    Morse, W.L. | Emerald Group Publishing | 1945


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