Report of conclusions reached after series of tests on rolling moments on models of complete airplanes, made at Massachusetts Institute of Technology; variation of rolling moment with angle of attack; ratio of aileron area to wing area; even when lower wing is of somewhat smaller span and chord there should be ailerons on lower wing as well as upper; differential action explained. (Aeronautical Eng. Sec.)


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    Title :

    Aileron arrangement


    Additional title:

    Aviation


    Contributors:
    Ober, S. (author)

    Published in:

    Aviation ; 26 , n 7


    Publication date :

    1929


    Size :

    2 pages


    Remarks:

    4 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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