An 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 ca...
The braking performance of a nine-place, light, twin-engine airplane was evaluated on comparative gr...
Dynamic hydroplaning, viscous hydroplaning, and tire tread rubber reversion effects on tire traction...
Statistics show that the likelihood of a runway excursion during takeoff or landing is much higher o...
The characteristics, which include the cornering-force and drag-force friction coefficients and self...
An experimental investigation was conducted to study the performance of an aircraft tire under cycli...
Comparative braking performance of various aircraft on grooved and ungrooved pavement
Damage to aircraft tires produced by grooved runway surfaces when impacted at various sink rates, ve...
Problems associated with aircraft ground handling operations on wet runways are discussed and major ...
An investigation to determine the effects of pavement surface condition on the cornering forces deve...
A limited test program was conducted to extend and supplement the braking and cornering data on a 30...
Aircraft stopping and directional control performance on wet runways is discussed. The major element...
A series of taxiing tests was conducted at the Langley landing loads track with both braked and unbr...
An investigation was conducted at the Langley aircraft landing loads and traction facility to determ...
A test program was conducted to evaluate friction performance and wear characteristics on wet runway...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77386/1/AIAA-1974-967-540.pd
The braking performance of a nine-place, light, twin-engine airplane was evaluated on comparative gr...
Dynamic hydroplaning, viscous hydroplaning, and tire tread rubber reversion effects on tire traction...
Statistics show that the likelihood of a runway excursion during takeoff or landing is much higher o...
The characteristics, which include the cornering-force and drag-force friction coefficients and self...
An experimental investigation was conducted to study the performance of an aircraft tire under cycli...
Comparative braking performance of various aircraft on grooved and ungrooved pavement
Damage to aircraft tires produced by grooved runway surfaces when impacted at various sink rates, ve...
Problems associated with aircraft ground handling operations on wet runways are discussed and major ...
An investigation to determine the effects of pavement surface condition on the cornering forces deve...
A limited test program was conducted to extend and supplement the braking and cornering data on a 30...
Aircraft stopping and directional control performance on wet runways is discussed. The major element...
A series of taxiing tests was conducted at the Langley landing loads track with both braked and unbr...
An investigation was conducted at the Langley aircraft landing loads and traction facility to determ...
A test program was conducted to evaluate friction performance and wear characteristics on wet runway...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77386/1/AIAA-1974-967-540.pd
The braking performance of a nine-place, light, twin-engine airplane was evaluated on comparative gr...
Dynamic hydroplaning, viscous hydroplaning, and tire tread rubber reversion effects on tire traction...
Statistics show that the likelihood of a runway excursion during takeoff or landing is much higher o...