Effect of Torsional Damping on Aircraft Nose Landing-Gear Shimmy-Reference-Cited by-同舟云学术

Effect of Torsional Damping on Aircraft Nose Landing-Gear Shimmy

Published:2015-03 Issue:2 Volume:52 Page:561-568
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Feng Fei¹,Nie Hong¹,Zhang Ming¹,Peng Yiming¹

Affiliation:

1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032772

Reference24 articles.

1. PritchardJ. I. “An Overview of Landing Gear Dynamics,” NASA/TM, 1999.

2. von SchlippeB.DietrichR. “Shimmying of a Pneumatic Wheel,” NACA TM-1365, 1947.

3. MorelandW. J. “Landing Gear Vibration,” Wright Air Development Center Air Force TR-6590, Wright–Patterson AFB, OH, 1951.

4. The Story of Shimmy

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