Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism-Reference-Cited by-同舟云学术

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Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism

Published:2014-01 Issue:1 Volume:51 Page:129-143
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Knowles James A. C.¹,Krauskopf Bernd²,Lowenberg Mark H.³,Neild Simon A.³,Thota P.⁴

Affiliation:

1. Department of Mechanical Engineering and Mathematical Sciences, Oxford Brookes University, Oxford, England OX33 1HX, United Kingdom

2. Department of Mathematics, University of Auckland, Auckland 1142, New Zealand

3. Faculty of Engineering, University of Bristol, Bristol, England BS8 1TR, United Kingdom

4. Physical Systems, Airbus, Bristol, England BS99 7AR, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032130

Reference12 articles.

1. ConwayH. G., Landing Gear Design, Chapman and Hall, London, 1958, pp. 218–265.

3. Simulation of Aircraft Landing Gears with a Nonlinear Dynamic Finite Element Code

4. Aircraft Landing Gear Dynamics: Simulation and Control

5. DanielsJ. N. “A Method for Landing Gear Modeling and Simulation with Experimental Validation,” NASA CR-201601, 1996.

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