United States. National Advisory Committee for Aeronautics, United States. National Aeronautics and Space Administration · Washington : G.P.O. · leaf 278
ncies in all, iucludin<; tho two staj^ger wires whi(;li aro actinj^. One s(a<^{<er wire ateach panel ])()int always comes into j)lay, but the load may shift from one diaf^onal to tli(! otheras the type of loadinf;; chanii^es. In tho particular case under consideration it is tlu; lonj^… … FiG. 4. quently has a larger deflection. The long stagger wire accordingly comes into play to equalizethe deflections. Tlie distrihution of the drag load also acts to stress the same wire, as the wireNo. 20 acts as a partial support for the upper wing at the inner panel point, and the length ofthe…
Aeronautics
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