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Simulation of Shock Absorber in Landing Gear

Application 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.

Ce modèle a été construit avec les éléments suivants:

Multibody Dynamics Module

The combination of COMSOL® products required to model your application depends on the physics interfaces that define it. Particular physics interfaces may be common to several products (see the Specification Chart for more details). To determine the right combination of products for your project, you should evaluate all of your needs in light of each product\'s capabilities, consultation with the COMSOL Sales and Support teams, and the use of an evaluation license.