Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 215
this tube with its applied loads. Maximum bending moment = 509.5 X 12 — 422 X H = 1470 in. lbs.Maximum torsional moment = 2110 in. lbs.Tube is U/4 X -049 in. Polar I — .1901470X-875fb = : =13,550 lbs. per sq. in. .0952110X.875 9,720 lbs. per sq. in. .190 Combined Stresses. 13,550 Maximum fb = 1- 2… … Fig. 121. Forces Acting on Rear Stick and Transverse Torque Tube 196 Art. 141 Pursuit Airplane Control System 141. Pursuit Airplane Control System—Fig. 122 illustrates diagram-matically the functioning of a control system which has certain goodpoints. For the design in question, the aileron and…
Airplanes
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