Alternate Launch and Recovery Surface Traction Characteristics
Date Published: 1986-10-01
Paper Number:861627
DOI: 10.4271/861627
Citation:
Carter, T., Treanor, D., and Lewis, M., "Alternate Launch and Recovery Surface Traction Characteristics," SAE Technical Paper 861627, 1986, doi:10.4271/861627.
Author(s):
Thomas J. Carter - Wright-Patterson AFB
David H. Treanor - Wright-Patterson AFB
Martin D. Lewis - Air Force Engineering Services Center, Tyndall AFB
Abstract:
The rapid repair of bomb-damaged runways is of increasing concern to the U.S. Air Force, therefore, expedient repair concepts are being developed. Aircraft performance effects imposed by the repair treatments include: tire flotation, aircraft weight, landing dynamics, and the forces generated at the tire/runway surface interface. This study focuses on tire/runway surface interface forces and was initiated to evaluate several surfaces with respect to their relative tractive and lateral force potential. Three damage repair surface materials, a baseline concrete surface, and a ceramic aluminized marking strip were tested. Quasi-static tests were run at seven tire yaw angles, with and without braking under dry, wet, and icy conditions.
File Size: 478K
Product Status: In Stock
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