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Volumn 513-514, Issue C, 2009, Pages 302-310
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Modelling the high temperature behaviour of TBCs using sequentially coupled microstructural-mechanical FE analyses
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Author keywords
Creep; Eshelby; Finite element analysis; Oxidation; Stress accumulation; Thermal barrier coating
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Indexed keywords
ALUMINA;
ALUMINUM OXIDE;
GAS TURBINES;
THERMAL BARRIER COATINGS;
THERMAL INSULATION;
ELEVATED TEMPERATURE;
ESHELBY;
EXPOSED TO;
FINITE ELEMENT ANALYSE;
GAS TURBINE COMPONENTS;
HIGH TEMPERATURE BEHAVIOR;
MECHANICAL;
MICRO-STRUCTURAL;
MICROSTRUCTURAL CHANGES;
STRESS ACCUMULATION;
FINITE ELEMENT METHOD;
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EID: 65349087278
PISSN: 09215093
EISSN: None
Source Type: Journal
DOI: 10.1016/j.msea.2009.02.006 Document Type: Article |
Times cited : (25)
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References (48)
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