Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 258
Art. 161 Flying Conditions with Rudder Turned ->66? … Fig. 162. Stress Diagram for Front Portion of Fuselage in MaximumAir Load Condition assumption and a simple one. The tail post will then act as a beamloaded at the level of the center of gravity of the vertical surfaces, andsupported at two points by the longerons. It is then a simple matterto…
Airplanes
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