Defect evolution in thermal barrier coating systems under multi-axial thermomechanical loading
SURFACE & COATINGS TECHNOLOGY, vol.200, no.5-6, pp.1282-1286, 2005 (SCI-Expanded, Scopus)
- Publication Type: Article / Article
- Volume: 200 Issue: 5-6
- Publication Date: 2005
- Doi Number: 10.1016/j.surfcoat.2005.07.098
- Journal Name: SURFACE & COATINGS TECHNOLOGY
- Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
- Page Numbers: pp.1282-1286
- Keywords: interfaces, defects, nickel alloy, zirconium oxide, multilayer, thermal barrier coating, MECHANICAL FATIGUE
- Anadolu University Affiliated: No
Abstract
In service, gas turbine components with thermal barrier coatings experience high cyclic mechanical and thermal loading. Important, but not yet considered sufficiently, are the multi-axial stresses arising from thermal gradients.