Paper Title:
Aircraft Landing Gear of a Dynamic Research and Computer Simulation
  Abstract

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)
Chapter
Chapter 8: Modeling, Analysis, and Simulation of Manufacturing Processes
Edited by
Wu Fan
Pages
2426-2429
DOI
10.4028/www.scientific.net/AMR.383-390.2426
Citation
S. S. Li, X. M. Liu, Z. G. Zhu, F. Yang, "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
$32.00
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