Stresses and Heat Generation in a Landing Gear Mechanism
Model ID: 14045
This model simulates the dynamics of the shock absorber used in a landing gear mechanism of an aircraft.
It analyses the stresses, as well as the heat generated in the landing gear components due to the energy dissipated in the shock absorber. A prismatic joint, with spring and damper, is used to model the shock absorber assembly.
This model was built using the following:Multibody Dynamics Module