Modelling of TBC system failure: Stress distribution as a function of TGO thickness and thermal expansion mismatch

Engineering Failure Analysis

Volumn 13, Issue 3 SPEC. ISS., 2006, Pages 409-426

  Martena, Manuela ^a   Botto, D ^a   Fino, P ^a   Sabbadini, S ^b   Gola, M M ^a   Badini, C ^a  

^a POLITECNICO DI TORINO   (Italy)

^b AVIO S P A   (Italy)

Author keywords

Failure; Oxidation; Stress analysis; Surface coatings; Turbine blade

Indexed keywords

ADHESION; GAS TURBINES; NICKEL ALLOYS; OXIDATION; PLASMA SPRAYING; STRESS ANALYSIS; STRESS CONCENTRATION; SUPERALLOYS; THERMAL BARRIER COATINGS; THERMAL EXPANSION; TURBOMACHINE BLADES; ZIRCONIA;

SURFACE COATINGS; THERMALLY GROWN OXIDE (TGO); TURBINE BLADE;

FAILURE ANALYSIS;

FAILURE ANALYSIS;

EID: 28344441724     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2004.12.027     Document Type: Article

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