Dynamometer Simulation of Aircraft Tire Wear Due to Braking

2001-01-3028

09/11/2001

Event
World Aviation Congress & Exposition
Authors Abstract
Content
Laboratory and aircraft flight testing indicates that braking is the primary driver of tire wear on tactical aircraft, and that steps can be taken to significantly improve the tire wear performance. The effects of numerous other factors including aircraft characteristics, runway surface texture, tire tread compound, tire pressure, and environmental conditions were also evaluated under the Air Force’s Improved Tire Life and Extended Life Tire programs. Laboratory testing of tire wear performance using the new 168i internal roadwheel dynamometer was successfully demonstrated.
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DOI
https://doi.org/10.4271/2001-01-3028
Pages
12
Citation
Medzorian, J., and Shea, M., "Dynamometer Simulation of Aircraft Tire Wear Due to Braking," SAE Technical Paper 2001-01-3028, 2001, https://doi.org/10.4271/2001-01-3028.
Additional Details
Publisher
Published
Sep 11, 2001
Product Code
2001-01-3028
Content Type
Technical Paper
Language
English