Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 251
Fig. 157. Load Positions Relative to Fuselage Trusses IgJV//sy /?eoctiOnS2^M … Fig. 158. Panel Loads Due to Dead Weight Station 0 Station 1 Station 2 Engine 1 Engine 1 Engine ) Radiator }. . . . 379 Radiator [.... 197 Radiator L... 74Propeller J Propeller J Propeller J Fuselage 45 Oil and tank Oil and tank 11 5 For two trusses 424 45 X— 31 45 X— 14 For one truss.. 212 16 16…
Airplanes
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