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Low-Speed Yawed-Rolling Characteristics of a Pair of 56-Inch-Diameter, 32-Ply-Rating, Type 7 Aircraft TiresThe low-speed (up to 4 miles per hour) yawed-rolling characteristics of two 56 x 16 32-ply-rating, type 7 aircraft tires under straight-yawed rolling were determined over a range of inflation pressures and yaw angles for a vertical load approximately equal to 75 percent of the rated vertical load. The quantities measured or determined included cornering force, drag force self-alining torque, pneumatic caster vertical tire deflection, yaw angle, and relaxation length. During straight-yawed rolling the normal force generally increased with increasing yaw angle within the test range. The self-alining torque increased to a maximum value and then decreased with increasing angle of yaw. The pneumatic caster tended to decrease with increasing yaw angle.
Document ID
19980231043
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Thompson, Wilbur E.
(NASA Langley Research Center Hampton, VA United States)
Horne, Walter B.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1959
Subject Category
Mechanical Engineering
Report/Patent Number
L-171
NASA-MEMO-2-7-59L
Report Number: L-171
Report Number: NASA-MEMO-2-7-59L
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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