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Aircraft nose gear shimmy studiesAn overview of previous studies involving aircraft nose gear shimmy behavior is given together with some test results identifying the influence of different factors inducing shimmy. A NASA Langley test program conducted at the Landing Loads Track (LLT) facility to evaluate shimmy characteristics of an actual Space Shuttle nose gear is described together with some of the test results. Based on results from these various evaluations, recommendations are made concerning nose gear design features, such as corotating wheels, to minimize the occurence of shimmy.
Document ID
19950062072
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yager, Thomas J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
ISSN: 0148-7191
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 931401
Report Number: SAE PAPER 931401
ISSN: 0148-7191
Meeting Information
Meeting: SAE, Aerospace Atlantic Conference & Exposition
Location: Dayton, OH
Country: United States
Start Date: April 20, 1993
End Date: April 23, 1993
Accession Number
95A93671
Distribution Limits
Public
Copyright
Other

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