Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 203
r—Refer to Figs. 110 and 111. 5160 Vertical force on outer end of arm = 397 lbs. 2X6.5 Since the rods connecting the ends of the arm with the bell cranksmake an angle of 16 degs. with the vertical, a horizontal component ispresent which produces a moment about the long axis of any cross-section of… … Fig. 110. Aileron Lever on Torque Tube184 Art. 132 Investigation of Bell Crank Lever
Airplanes
Internet Archive · Library of Congress · Public Domain Mark 1.0. Free to use for anything.
