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Some effects of grooved runway configurations on aircraft tire braking traction under flooded runway conditionsAn experimental investigation was conducted to study the effect of grooved runway configurations on aircraft tire braking traction on flooded runway surfaces. The investigation was performed, utilizing size 49 x 17, type VII, aircraft tires with an inflation pressure of 170 lb per square inch at ground speeds up to approximately 120 knots. The results of this investigation indicate that when the runway is flooded, grooved surfaces provide better braking traction than an ungrooved surface and, in general, the level of braking traction was found to improve as the tire bearing pressure was increased because of an increase in the groove area of either the surface or the tire tread. Rounding the groove edges tended to degrade the tire braking capability from that developed on the same groove configuration with sharp edges. Results also indicate that braking friction coefficients for the test tires and runway surfaces decreased as ground speed was increased because of the hydroplaning effects.
Document ID
19730012330
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Byrdsong, T. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1973
Subject Category
Aircraft
Report/Patent Number
L-8227
NASA-TN-D-7215
Report Number: L-8227
Report Number: NASA-TN-D-7215
Accession Number
73N21057
Funding Number(s)
PROJECT: RTOP 501-38-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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