Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System-Reference-Cited by-同舟云学术

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Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System

Published:2012-08-13 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Terkovics Nándor¹,Neild Simon¹,Lowenberg Mark¹,Krauskopf Bernd²,Sharma Sanjiv³

Affiliation:

1. University of Bristol

2. University of Auckland

3. Airbus

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4731

Reference13 articles.

1. 1von Schlippe, B. and Dietrich, R. “Shimmying of a pneumatic wheel,” Tech. Rep. NACATM 1365, National Advisory Committee for Aeronautics, 1947.

2. 2Smiley, R. F. “Correlation, evaluation, and extension of linearized theories for tyre motion and wheel shimmy,” Tech. Rep. 1299, National Advisory Committee for Aeronautics, 1957.

3. Shimmy analysis of a simple aircraft nose landing gear model using different mathematical methods

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear analysis of a shimmying wheel with contact-force characteristics featuring higher-order discontinuities;Nonlinear Dynamics;2017-08-04

2. Tyre induced vibrations of the car–trailer system;Journal of Sound and Vibration;2016-02

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