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.)
Aileron arrangement
Aviation
Aviation ; 26 , n 7
1929
2 pages
4 Figs.
Article (Journal)
English
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