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26 x 6.6 radial-belted aircraft tire performancePreliminary results from testing of 26 x 6.6 radial-belted and bias-ply aircraft tires at NASA Langley's Aircraft Landing Dynamics Facility (ALDF) are reviewed. The 26 x 6.6 tire size evaluation includes cornering performance tests throughout the aircraft ground operational speed range for both dry and wet runway surfaces. Static test results to define 26 x 6.6 tire vertical stiffness properties are also presented and discussed.
Document ID
19920057368
Document Type
Conference Paper
Authors
Davis, Pamela A. (NASA Langley Research Center Hampton, VA, United States)
Martinson, Veloria J. (NASA Langley Research Center Hampton, VA, United States)
Yager, Thomas J. (NASA Langley Research Center Hampton, VA, United States)
Stubbs, Sandy M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1991
Subject Category
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number
SAE PAPER 912157
Distribution Limits
Public
Copyright
Other