Anderson, R. (1996). Tire Test Correlation: Radial Versus Bias-Ply Tires (Report No. DOT/FAA AR-TN 95/97). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89551
Anderson, Richard. Tire Test Correlation: Radial Versus Bias-Ply Tires. Report no. DOT/FAA AR-TN 95/97. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89551.
Anderson, Richard Tire Test Correlation: Radial Versus Bias-Ply Tires. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN 95/97, ROSA P. https://rosap.ntl.bts.gov/view/dot/89551.
The temperature performance of a radial tire was correlated with a bias-ply tire of identical size under controlled laboratory dynamometer conditions. The general effects of increases in load and ground speed on the temperature profiles of each tire were compared. The results indicated that the bias-ply tire used during the tests was more adversely affected by increases in load and speed than the radial tire. ever, to further quantify the temperature profile distinction between the radial and bias-ply tires, additional data and effort would be required.
Anderson, R. (1996). Tire Test Correlation: Radial Versus Bias-Ply Tires (Report No. DOT/FAA AR-TN 95/97). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89551
Anderson, Richard. Tire Test Correlation: Radial Versus Bias-Ply Tires. Report no. DOT/FAA AR-TN 95/97. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89551.
Anderson, Richard Tire Test Correlation: Radial Versus Bias-Ply Tires. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN 95/97, ROSA P. https://rosap.ntl.bts.gov/view/dot/89551.
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