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Structural analysis and design of airplanes (1920)

United States. Army. Air Corps · [Washington] · leaf 201

An illustration from Structural analysis and design of airplanes, 1920, leaf 201
0766 6380 lbs. per sq. in. (satisfactory) Bearing of 5/16 in. bolt Bearing area = 2 X -312 X -125 = .078 978 = 12,500 lbs. per sq. in. (satisfactory) .078 The short torque tube to which the control stick is attached is heldin place by a 3/16 in. bolt passing through a collar on the tube. Shearing… … Fig. 109. Section Through Control Stick at Torque Tube 182 Art. 129 Investigation of Control Stick for Aileron Loads 129. Investigation of Control Stick for Aileron Loads—Referenceshould be made to Fig. 109, which shows a section through the controlstick and torque tube. The total aileron moment is…

Airplanes

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