Atıf İçin Kopyala
Baufeld B., Bartsch M., Dalkilic S., Heinzelmann M.
SURFACE & COATINGS TECHNOLOGY, cilt.200, sa.5-6, ss.1282-1286, 2005 (SCI-Expanded)
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Yayın Türü:
Makale / Tam Makale
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Cilt numarası:
200
Sayı:
5-6
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Basım Tarihi:
2005
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Doi Numarası:
10.1016/j.surfcoat.2005.07.098
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Dergi Adı:
SURFACE & COATINGS TECHNOLOGY
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Derginin Tarandığı İndeksler:
Science Citation Index Expanded (SCI-EXPANDED), Scopus
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Sayfa Sayıları:
ss.1282-1286
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Anahtar Kelimeler:
interfaces, defects, nickel alloy, zirconium oxide, multilayer, thermal barrier coating, MECHANICAL FATIGUE
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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.