Aircraft Landing Gear of a Dynamic Research and Computer Simulation
by the MSC Adams / Aircraft software features, setting pillar-type landing gear as the prototype, and using ADAMS software modules prior to the establishment of a certain type of aircraft landing gear model, then calculate the air buffer spring force oil, damping force and the structural constraints force curve based on dynamics model, At the end of paper we will analyze the model drop-test results. The results proved that we used this method was feasible.
S. S. Li et al., "Aircraft Landing Gear of a Dynamic Research and Computer Simulation", Advanced Materials Research, Vols. 383-390, pp. 2426-2429, 2012