Defect evolution in thermal barrier coating systems under multi-axial thermomechanical loading
SURFACE & COATINGS TECHNOLOGY, cilt.200, sa.5-6, ss.1282-1286, 2005 (SCI-Expanded, Scopus)
- Yayın Türü: Makale / Tam Makale
- Cilt numarası: 200 Sayı: 5-6
- Basım Tarihi: 2005
- Doi Numarası: 10.1016/j.surfcoat.2005.07.098
- Dergi Adı: SURFACE & COATINGS TECHNOLOGY
- Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
- Sayfa Sayıları: ss.1282-1286
- Anahtar Kelimeler: interfaces, defects, nickel alloy, zirconium oxide, multilayer, thermal barrier coating, MECHANICAL FATIGUE
- Anadolu Üniversitesi Adresli: Hayır
Özet
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.