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Static mechanical properties of 30 x 11.5-14.5, type VII, aircraft tires of bias-ply and radial-belted designAn investigation was conducted to determine the static mechanical characteristics of 30 x 115-14.5 bias-ply and radial aircraft tires. The tires were subjected to vertical and lateral loads and mass moment of inertia tests were conducted. Static load deflection curves, spring rates, hysteresis losses, and inertia data are presented along with a discussion of the advantages and disadvantages of one tire over the other.
Document ID
19880043595
Document Type
Conference Paper
Authors
Davis, Pamela A. (NASA Langley Research Center Hampton, VA, United States)
Lopez, Mercedes C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Subject Category
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number
SAE PAPER 871868
Distribution Limits
Public
Copyright
Other