04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT
N. Li¹, H. Wang¹, Z.Q. Li¹, Z.H. Wang¹; ¹Taiyuan University of Technology, China
The kinematic model of the rigid-flexible coupling for the main landing gear was established, the dynamic simulations under extreme working conditions were conducted, and the strength& stiffness models were obtained, so that the performance was reflected more accurately, and the optimization strategies and structural design suggestions were put forward.