Shimmy performance analysis and parameter optimization of a dual-wheel nose landing gear coupled with torsional nonlinear energy sink and considering structural nonlinear factor

Author:

Wang Yong,Zhang Tao,Bian Hanyan,Yin Yin,Wei Xiaohui

Funder

Jiangsu Provincial Key Laboratory of Electrochemical Energy Storage Technologies, Nanjing University of Aeronautics and Astronautics

Outstanding Youth Scientist Foundation of Hunan Province

Natural Science Foundation for Young Scientists of Shanxi Province

China Postdoctoral Science Foundation

Senior Talent Foundation of Jiangsu University

National Natural Science Foundation of China

State Key Laboratory of Mechatronics Engineering and Control

Tianjin Postdoctoral Science Foundation

National Aerospace Science Foundation of China

Publisher

Elsevier BV

Reference44 articles.

1. Shimmy in aircraft landing gear;Coetzee,2007

2. Linear stability analysis and dynamic response of shimmy dampers for main landing gears;Arreaza;J Appl Mech,2016

3. Describing function analysis of nonlinear nose gear shimmy;Burton,1981

4. Perturbation analysis of nonlinear wheel shimmy;Gordon;J Aircr,2002

5. Incremental harmonic balance method for predicting amplitudes of a multi-d.o.f. non-linear wheel shimmy system with combined Coulomb and quadratic damping;Zhou;J Sound Vib,2005

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