Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 250
al 2035 59.5 121,090 Without Wing 1730 58.5 101,265 Fig. 157 indicates the loads and their position relative to the verticalfuselage trusses as taken from the balance drawing. In computing thestresses in the fuselage it is considered as composed of two trusses loadedat the panel points. Fig. 158… … Fuselage Art. 156 ill
Airplanes
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