Numerical Continuation Applied to Landing Gear Mechanism Analysis
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031247
Reference12 articles.
1. Subject Index
2. Aircraft Landing Gear Dynamics: Simulation and Control
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