Continuation Analysis of Aircraft Ground Loads During High-Speed Turns
Author:
Affiliation:
1. Airbus, Bristol, England BS99 7AR, United Kingdom
2. Department of Mathematics, University of Auckland, Auckland 1142, New Zealand
3. Department of Aerospace Engineering, 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.C031883
Reference12 articles.
1. CoetzeeE. “Nonlinear Aircraft Ground Dynamics,” Master’s Thesis, Univ. of Bristol, Bristol, England, 2006.
2. TippsD.RustenburgJ.SkinnD.DeFioreT. “Side Load Factor Statistics From Commercial Aircraft Ground Operations,” Federal Aviation Administration UDR-TR 2002-00119, Washington, DC, Jan. 2003.
3. Application of Bifurcation Methods to the Prediction of Low-Speed Aircraft Ground Performance
4. Bifurcation and Stability Analysis of Aircraft Turning on the Ground
5. Operational Parameter Study of Aircraft Dynamics on the Ground
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