Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure
Description:
"The effects of interaction between a landing gear and a flexible airplane structure on the behavior of the landing gear and the loads in the structure have been studied by treating the equations of motion of the airplane and the landing gear as a coupled system. The landing gear is considered to have nonlinear characteristics typical of conventional gears, namely, velocity-squared damping, polytropic air-compression springing, and exponential tire force-deflection characteristics. For the case…
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Date:
May 5, 1955
Creator:
Cook, Francis E. & Milwitzky, Benjamin
Item Type:
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