This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Computing Remaining Fatigue Life Under Incrementally Updated Loading Histories
Technical Paper
2018-01-0623
ISSN: 0148-7191, e-ISSN: 2688-3627
This content contains downloadable datasets
Annotation ability available
Sector:
Language:
English
Abstract
After manufacture, every military vehicle experiences a unique history of dynamic loads, depending on loads carried, missions completed, etc. Damage accumulates in vehicle structures and components accordingly, leading eventually to failures that can be difficult to anticipate, and to unpredictable consequences for mission objectives. The advent of simulation-based fatigue life prediction tools opens a path to Digital Twin based solutions for tracking damage, and for gaining control over vehicle reliability. An incremental damage updating feature has now been implemented in the Endurica CL fatigue solver with the aim of supporting such applications for elastomer components. The incremental updating feature is demonstrated via the example of a simple transmission mount component. The damage state of the mount is computed as it progresses towards failure under a series of typical loading histories. The incremental updating feature enables both more realism in anticipating maintenance demands, and better planning of availability/readiness for specific mission demands.
Recommended Content
Technical Paper | High Efficiency Low Cost Vacuum Fluorescent Display Power Supply |
Technical Paper | Process Simulation to Improve Quality and Increase Productivity in Rolling, Ring Rolling and Forging |
Authors
Topic
Citation
Mars, W., Suter, J., and Bauman, M., "Computing Remaining Fatigue Life Under Incrementally Updated Loading Histories," SAE Technical Paper 2018-01-0623, 2018, https://doi.org/10.4271/2018-01-0623.Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 |
Also In
References
- Glaessgen , Edward H. , and David Stargel The Digital Twin Paradigm for Future NASA and US Air Force Vehicles 53rd Struct. Dyn. Mater. Conf Honolulu, HI, US 1 14 2012
- Tuegel , E.J. , Ingraffea , A.R. , Eason , T.G. , and Michael Spottswood , S. Reengineering Aircraft Structural Life Prediction Using a Digital Twin International Journal of Aerospace Engineering 2011 2011
- Mars , William V. , Matthew Castanier , David Ostberg , and William Bradford Digital Twin for Tank Track Elastomers: Predicting Self-Heating And Durability 2017 NDIA Ground Vehicle Systems Engineering and Technology Symposium 2017 Novi, Michigan
- Barbash , K.P. and Mars , W.V. Critical Plane Analysis of Rubber Bushing Durability under Road Loads SAE Technical Paper 2016 10.4271/2016-01-0393
- Gent , A.N. , Lindley , P.B. , and Thomas , A.G. Cut Growth and Fatigue of Rubbers. I. The Relationship between Cut Growth and Fatigue Journal of Applied Polymer Science 8 455 1964
- Mars , W.V. Computed Dependence of Rubber's Fatigue Behavior on Strain Crystallization Rubber Chemistry and Technology 82 1 51 61 2009
- Mars , W.V. Cracking Energy Density as a Predictor of Fatigue Life under Multiaxial Conditions Rubber Chemistry and Technology 75 1 1 17 2002
- Gent A.N. , Mars W.V. Chapter 10 - Strength of Elastomers Mark E. , Burak Erman , Mike Roland The Science and Technology of Rubber Fourth Edition Academic Press Boston 2013 473 516 9780123945846 10.1016/B978-0-12-394584-6.00010-8
- Aït-Bachir , M. , Mars , W.V. , and Verron , E. Energy Release Rate of Small Cracks in Hyperelastic Materials International Journal of Non-Linear Mechanics 47 4 22 29 2012
- Li , F. , Liu , J. , Mars , W.V. , Chan , T.W. et al. Crack Precursor Size for Natural Rubber Inferred from Relaxing and Non-relaxing Fatigue Experiments International Journal of Fatigue 80 50 57 2015
- Mars , W.V. Analysis of Stiffness Variations in Context of Strain-, Stress-, and Energy-Controlled Processes Rubber Chemistry and Technology 84 2 178 186 2011
- Sun , C. , Gent , A. , and Marteny , P. Effect of Fatigue Step Loading Sequence on Residual Strength Tire Science and Technology 28 3 196 208 2000
- Mars , W.V. and Fatemi , A. Analysis of Fatigue Life under Complex Loading: Revisiting Cadwell, Merrill, Sloman, and Yost Rubber Chemistry and Technology 79 4 589 601 2006
- Zarrin-Ghalami , T. , Fatemi , A. , and Lee , Y. Fatigue Life Prediction of an Automobile Cradle Mount SAE Int. J. Passeng. Cars - Mech. Syst. 6 1 351 359 2013 10.4271/2013-01-1009
- Harbour , R.J. , Fatemi , A. , and Mars , W.V. Fatigue Crack Growth of Filled Rubber under Constant and Variable Amplitude Loading Conditions Fatigue & Fracture of Engineering Materials & Structures 30 7 640 652 2007b
- Harbour , R.J. , Fatemi , A. , and Mars , W.V. Fatigue Life Analysis and Predictions for NR and SBR under Variable Amplitude and Multiaxial Loading Conditions International Journal of Fatigue 30 7 1231 1247 2008b
- Poisson , J.-L. , Méo , S. , Lacroix , F. , Berton , G. et al. Comparison of Fatigue Criteria under Proportional and Non-Proportional Multiaxial Loading Rubber Chemistry and Technology 2017