International audienceLight aircrafts are designed to be used in both developed and undeveloped areas of a country. Hard landingconditions such as shocks and rebounds may occur. In this context, a good, efficient, robust and easy to maintainlanding gear is vital. Its main role is to dissipate the energy of the impact. The aim of this work is to study aninnovative light aircraft landing gear equipped with a damper. The study includes comparing its dissipationperformance with two traditional light aircraft landing gears: a classical flat spring landing gear and a landing gearwith Sandow cords. These systems’ modeling is carried out through three steps. Firstly, Bush tire is modeled withfinite elements considering tire geometry and material specificities. Secondly, combined finite elements withstructural elements are used to model the different landing gear systems. Thus, stress, deformation and energywithin landing gears components could be obtained. Finally, aircraft rolling simulations are conducted. Systems’transient responses while rolling over ramp are evaluated, as well as the efforts and rebound displacementstransmitted to the aircraft. A dissipation efficiency comparative study between the landing gears is conducted. Inaddition, the influence of simulation’ conditions such as inflation pressure, rolling velocity or runway flatness isinvestigated
