Masoud Roudneshin
Université de Montréal
Simulated annealingCreepComposite materialThermal barrier coatingMaterials scienceStochastic optimizationTurbinePlane stressThermal fatigueParticle swarm optimization
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Turbine entry temperature of turbo-engines has been increased to improve proficiency. Consequently, protecting the hot section elements experiencing aggressive service conditions necessitates the applying of thermal barrier coatings (TBC). Developing TBC systems and improving performance is an ongoing endeavour to prolong the lifetime. Thus, various studies have been conducted to find the optimum properties and dimensions. In this paper, the optimum thickness of intermediate bond coat (BC) and t...
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