Agrawal, S. K. (1981). The Braking Performance of an Aircraft Tire on Concrete Surfaces (Report No. FAA-CT-81-185). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/91129
Agrawal, Satish K.. The Braking Performance of an Aircraft Tire on Concrete Surfaces. Report no. FAA-CT-81-185. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1981. https://rosap.ntl.bts.gov/view/dot/91129.
Agrawal, Satish K. The Braking Performance of an Aircraft Tire on Concrete Surfaces. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1981, Report no. FAA-CT-81-185, ROSA P. https://rosap.ntl.bts.gov/view/dot/91129.
The braking and cornering performance of an aircraft tire during landing operations depends upon the magnitude of the friction forces developed at the tire/runway interface. The presence of water on the runways significantly reduces the available friction at this interface and results in loss of braking and directional control of the aircraft. An extreme case of loss of control is hydroplaning.
Agrawal, S. K. (1981). The Braking Performance of an Aircraft Tire on Concrete Surfaces (Report No. FAA-CT-81-185). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/91129
Agrawal, Satish K.. The Braking Performance of an Aircraft Tire on Concrete Surfaces. Report no. FAA-CT-81-185. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1981. https://rosap.ntl.bts.gov/view/dot/91129.
Agrawal, Satish K. The Braking Performance of an Aircraft Tire on Concrete Surfaces. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1981, Report no. FAA-CT-81-185, ROSA P. https://rosap.ntl.bts.gov/view/dot/91129.
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