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An Overview of Landing Gear DynamicsOne of the problems facing the aircraft community is landing gear dynamics, especially shimmy and brake-induced vibration. Shimmy and brake-induced vibrations can lead to accidents due to excessive wear and shortened life of gear parts and contribute to pilot and passenger discomfort. To increase understanding of these problems, a literature survey was performed. The major focus is on work from the last ten years. Some older publications are included to understand the longevity of the problem and the background from earlier researchers. The literature survey includes analyses, testing, modeling, and simulation of aircraft landing gear; and experimental validation and characterization of shimmy and brake-induced vibration of aircraft landing gear. The paper presents an overview of the problem, background information, and a history of landing gear dynamics problems and solutions. Based on the survey an assessment and recommendations of the most critically needed enhancements to the state of the art will be presented. The status of Langley work contributing to this activity will be given.
Document ID
19990047095
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Pritchard, Jocelyn I.
(Army Research Lab. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-17840
ARL-TR-1976
NAS 1.15:209143
NASA/TM-1999-209143
Report Number: L-17840
Report Number: ARL-TR-1976
Report Number: NAS 1.15:209143
Report Number: NASA/TM-1999-209143
Funding Number(s)
PROJECT: RTOP 522-18-11-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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