Dynamic Analysis of Aircraft Landing Impact Using Landing-Region-Based Model
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.6801
Reference21 articles.
1. Vibration Control of a Landing Gear System Featuring Electrorheological/Magnetorheological Fluids
2. Control Aspects of Aerospace Plane Docking with Ekranoplane for Water Landing
3. 5Milwitzky, B., and Cook, F. E. "Analysis of Landing-Gear Behavior," NACA Report 1154, 1953.
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