Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 256
Fig. 159. Panel Loads in Maximum Air Load Condition C hC^d of tY,n^\ 5to ? … 429 1346 Fig. 160. Wing Spar Reaction in Maximum Air Load Condition designers. This method is to decrease the panel loads to the rear ofthe center of gravity and increase those forward of it so that the centerof gravity of the air load and the modified panel loads will be at thecenter of gravity of…
Airplanes
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