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Comparison Between Drop Tower Spindown and Aircraft Spinup Tire Wear
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English
Abstract
This paper will highlight the wear process associated with spinup and its easier to experimentally achieve drop tower spindown counterpart. Overall, such issues as net wear, wear distribution, potential thermal rise, tire construction and runway surface effects will be discussed along with an assessment-correlation study of a theoretical formulation of the problem.
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Authors
Citation
Padovan, J., Ananthaswamy, V., Lay, M., Macy, B. et al., "Comparison Between Drop Tower Spindown and Aircraft Spinup Tire Wear," SAE Technical Paper 951393, 1995, https://doi.org/10.4271/951393.Also In
References
- Padovan, J. Kazempour, A. Kim, Y.H. Aircraft Landing Induced Tire Spinup Journal of Aircraft 28 2 849 854 1991
- Padovan, J. Padovan, P. Kazempour, A. Modelling Spinup Wear in aircraft Tires Tire Science and Technology 21 3 138 162 1993
- Sobieski, I. “A Theoretical and Experimental Investigation into the Pre-Rotation of Aircraft Tires AIAA Journal 29 1 1991
- Daugherty, R.H. Stubbs, S. Spinup Studies of the Space Shuttle Orbiter main Gear Tire SAE 881360 , Aerospace Technology Conference Oct. 1988
- Lay, M.K. Macy, W.W. The Improved Tire Life Program Final Report For Period May 1993 August 1994 WL-TR-94-3122 Aug. 1994
- Padovan, J. Padovan, P. Thermomechanically Induced Wear at High Slip Rate Interfaces Between Deforming Composite Media Part 1, Problem Formulation Part 2, Numerical Simulation Journal of Thermal Stresses 16 351 372 1993 17 1 20 1994