This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Aircraft Landing Induced Tire Spinup
Annotation ability available
Sector:
Language:
English
Abstract
Based on the appropriate stiffness and inertial properties of prototypical aircraft landing gear suspension systems, a tire spinup model is developed. Due to its generality, the model can define the various governing dynamical fields. Here the effects of such factors as sink rate, runway friction and aircraft landing speed are considered. Main attention is given to defining the tire deflection-rotation-skidding history as well as the net and pointwise rate of work due to interfacial friction as it effects the growth of rotary inertia and slip work. To quantify the influence of such environmental factor as sink rate, friction and landing speed, a case study involving the shuttle main tires is included.
Recommended Content
| Technical Paper | The Aircraft Tire Wear Problem |
| Technical Paper | Autoflight and Powerplant Integration of Last Generation Commuter Aircraft |
Authors
Topic
Citation
Padovan, J., Kazempour, A., and Kim, T., "Aircraft Landing Induced Tire Spinup," SAE Technical Paper 901910, 1990, https://doi.org/10.4271/901910.Also In
References
- Currey, Norman S. Landing Gear: Design Handbook 1st Edition Lockheed Georgia Company Marietta, Georgia 30063 Jan. 1983
- Captain, K.M. Stokes, V.K. Edwards, J.H. Friction and Wear Test for Aircraft Tires Technical report ASR-TR-72-85 Aeronautical Systems Division Air Force System Command Wright Patterson Air Force Base, Ohio Nov. 1972
- Tanner, J.A. Drchet, R.C. Stubbs, S.M. Smith, E.G. Tire Temperatures During Antiskid Braking and Cornering Over Dry Runway NASA Technical Paper 2009 May 1982
- Dougherty, R.H. Stubbs, S.M. Spinup Studies of the Space Shuttle Orbiter Main Gear Tire NASA Langley Research Center 1988
- Chung, T.J. Continuum Mechanics Prentice Hall Englewood Cliffs, New Jersey 1988
- Clark, S. Mechanics of Pneumatic Tires U.S. Government Priority Office Washington, D.C. Department of Transportation National Highway Traffic Safety Administration 1980
- Padovan, J. Kennedy, R. Nakajima, Y. Finite Element Analysis of Steady and Transiently Moving/Rolling Nonlinear Viscoelastic Structure: Part 1, 2, 3 Completers and Structures 27 249 286 1987
- Padovan, J. Kazempour, A. Multibody Instantly Centered Moving Lagrangian Observer Schemes Computers and Structures 32 93 111 1989
- Hughes, T.J.R. The Finite Element Method Prentice-Hall, Inc. Englewood Cliffs, New Jersey 1987
- Baker, C.T.H. The Numerical Treatment of Integral Equations Clarendon Press Oxford 1977
- Bevington, P.R. Data Reduction and Error Analysis for the Physical Sciences McGraw Hill New York 1969