SCHRENK'S method for finding the wing lift distribution which has already been given in AIRCRAFT ENGINEERING can be taken further in order to determine the Pitching Moment Coefficient, CM0, about the quarter-chord point of the mean chord at no-lift.


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    Title :

    Wing Pitching Moment Coefficient


    Contributors:
    Morse, W.L. (author)

    Published in:

    Publication date :

    1945-07-01


    Size :

    2 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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