Inerter-Based Configurations for Main-Landing-Gear Shimmy Suppression-Reference-Cited by-同舟云学术

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Inerter-Based Configurations for Main-Landing-Gear Shimmy Suppression

Published:2017-03 Issue:2 Volume:54 Page:684-693
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Li Yuan¹,Jiang Jason Zheng¹,Neild Simon¹

Affiliation:

1. University of Bristol, Bristol, England BS8 1TR, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033964

Reference33 articles.

1. WoernerP.NoelO. “Influence of Nonlinearity on the Shimmy Behaviour of Landing Gear,” AGARD-R-800, 1996.

2. The Story of Shimmy

3. SmileyR. F. “Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy,” NACA Rept. 1299, 1957.

4. Von SchlippeV. B.DietrichR. “Shimmying of a Pneumatic Wheel,” NACA TM-1365, 1954, pp. 125–160.

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