Aircraft Nose Gear Shimmy Studies

931401

04/01/1993

Event
Aerospace Atlantic Conference & Exposition
Authors Abstract
Content
An 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 occurrence of shimmy.
Meta TagsDetails
DOI
https://doi.org/10.4271/931401
Pages
8
Citation
Yager, T., "Aircraft Nose Gear Shimmy Studies," SAE Technical Paper 931401, 1993, https://doi.org/10.4271/931401.
Additional Details
Publisher
Published
Apr 1, 1993
Product Code
931401
Content Type
Technical Paper
Language
English