Aircraft Landing Gear of a Dynamic Research and Computer Simulation

Abstract:

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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.

Info:

Periodical:

Advanced Materials Research (Volumes 383-390)

Edited by:

Wu Fan

Pages:

2426-2429

DOI:

10.4028/www.scientific.net/AMR.383-390.2426

Citation:

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

Online since:

November 2011

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Price:

$35.00

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