Finite element simulations on erosion and crack propagation in thermal barrier coatings
Erosion of thermal barrier coatings occurs when atmospheric or carbon particles from the combustion chamber are ingested into aviation turbine engines. To understand the influence of erosion on the service life of thermal barrier coatings, we introduce the erosion and crack propagation models, and t...
| Main Authors: | , , , , |
|---|---|
| Format: | Journal Article |
| Published: |
Walter de Gruyter, Berlin/Boston
2014
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/20.500.11937/40991 |