THE present article is the application of Schrenk's approximate method to two cases, one a wing without twist and the other the same wing with twist, the nomenclature of Schrenk's article having been altered to conform to British usage, and a certain amount of explanatory matter added in order to make the method more easily understood.


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    Title :

    Wing Lift Distribution


    Contributors:
    Morse, W.L. (author)

    Published in:

    Publication date :

    1944-05-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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