Application is made of O. SCHRENK'S approximate method (indexed in Engineering Index 1940 p 54, from Nat Advisory Committee Aeronautics -- Tech Memo n 948 Aug 1940) to two cases, one wing without twist and other, same wing with twist.


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    Title :

    Wing lift distribution


    Additional title:

    Aircraft Eng


    Contributors:
    Morse, W.L. (author)

    Published in:

    Publication date :

    1944


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wing Lift Distribution

    Morse, W.L. | Emerald Group Publishing | 1944



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