This SAE Aerospace Information Report (AIR) describes the current process for performing comparative wear testing on aircraft tires in a laboratory environment. This technique is applicable to both radial and bias tires, and is pertinent for all aircraft tire sizes. This AIR describes a technique based upon “wear” energy. In this technique, side wear energy and drag wear energy are computed as the tire is run through a prescribed test program. The specifics that drive the test setup conditions are discussed in Sections 4 through 7. In general, the technique follows this process: A test profile is developed from measured mechanical property data of the tires under study. Each tire is repeatedly run to the test profile until it is worn to the maximum wear limit (MWL). Several tires, typically 5 to 10, of each tire design are tested. Wear energy is computed for each test cycle and then summed to determine total absorbed wear energy. An index is calculated for each tire design.
SAE AIR5797-2013 history
2018SAE AIR5797A-2018 Aircraft Tire Wear Profile Development and Execution for Laboratory Testing
2013SAE AIR5797-2013 Aircraft Tire Wear Profile Development and Execution for Laboratory Testing
2008SAE AIR5797-2008 Aircraft Tire Wear Profile Development and Execution for Laboratory Testing