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Influence of Tire Tread Pattern and Runway Surface Condition on Braking Friction and Rolling Resistance of a Modern Aircraft TireA series of taxiing tests was conducted at the Langley landing­ loads track with both braked and unbraked (freely rolling) single and tandem wheels equipped with 32x8.8 type VII aircraft tires of dif­ferent tread designs to obtain data on tire and braking characteristics during operation on dry and on contaminated concrete and asphalt run­ ways. Contaminants used were water, slush, JP-4 jet fuel, and organic and detergent fire-extinguishing foams. Forward velocities for the tests ranged from approximately 13 to 104 knots. Vertical loads of approximately 9,000 to 22,000 pounds and tire inflation pressures of 85 to 350 pounds per square inch were used. Results indicated that the unbraked tire rolling resistance increased with increasing forward velocity on dry and on contaminated runway surfaces. Peak tire-ground friction coefficients developed during wheel braking decreased rapidly with increasing velocity on contaminated runways but remained relatively unchanged on dry runways as the forward velocity was increased. Dry-runway friction coeffi­cients were found to be relatively insensitive to tire tread pattern. However, the magnitude of the friction coefficients developed by tires on contaminated runways was extremely sensitive to the tire tread pat­ tern used, with circumferential-groove treads developing the highest values of friction coefficient, and smooth and dimple treads the lowest values for the tread patterns and runway conditions investigated.
Document ID
19620005764
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Horne, Walter B.
(NASA Langley Research Center Hampton, VA, United States)
Leland, Trafford J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
September 1, 1962
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TN-D-1376
Accession Number
62N15764
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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