This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Comparison Between Drop Tower Spindown and Aircraft Spinup Tire Wear
ISSN: 0148-7191, e-ISSN: 2688-3627
Published May 01, 1995 by SAE International in United States
Annotation ability available
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.
|Technical Paper||Spin-Up Studies of the Space Shuttle Orbiter Main Gear Tire|
|Technical Paper||Relative Pavement Bearing Strength Requirements of Aircraft|
|Technical Paper||Initial Identification of Aircraft Tire Wear|
CitationPadovan, 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.
- Padovan, J., Kazempour, A., and Kim, Y.H., Aircraft Landing Induced Tire Spinup, Journal of Aircraft, Vol. 28, No. 2, 849-854, 1991.
- Padovan, J., Padovan, P., and Kazempour, A., Modelling Spinup Wear in aircraft Tires, Tire Science and Technology, Vol. 21, No. 3, 138-162, 1993.
- Sobieski, I., “A Theoretical and Experimental Investigation into the Pre-Rotation of Aircraft Tires, AIAA Journal, Vol. 29, No. 1, 40, 1991.
- Daugherty, R.H., and Stubbs, S., Spinup Studies of the Space Shuttle Orbiter main Gear Tire, SAE 881360, Aerospace Technology Conference, Col. Oct. 1988.
- Lay, M.K. and Macy, W.W., The Improved Tire Life Program, Final Report For Period May 1993-August 1994, WL-TR-94-3122, Aug. 1994.
- Padovan, J., and 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, Vol. 16, 351-372, 1993, Vol. 17, 1-20, 1994.