1993-04-01

Aircraft Nose Gear Shimmy Studies 931401

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.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

The Experimental Measurement of the T-46 Nose Landing Gear Shimmy Parameters

961313

View Details

TECHNICAL PAPER

Realistic Evaluation of Landing Gear Shimmy Stabilization by Test and Analysis

760496

View Details

TECHNICAL PAPER

Some Controls and Accessories Design Approaches to Technical Requirements for Gas Turbine Engines

690739

View Details

X