Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 204
Fig. 110. Aileron Lever on Torque Tube184 Art. 132 Investigation of Bell Crank Lever … Fig. 111. Section A-A Through Aileron Lever By the method of trial it is found that B is the most stressed pointon the cross-section A—A, Fig. 111. 2580 X -90fbl = = 31,300 fb2 .0741740 X -14 .0281 3,700 Resultant stress = 35,000 lbs. per sq. in. . 55,000 Coefficient = = 1.57 (satisfactory) 35,000…
Airplanes
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