Finite Element Simulation on Thermal Fatigue of a Turbine Blade with Thermal Barrier Coatings
Yang L.1,2, Liu Q.X.1,2, Zhou Y.C.1,2,*, Mao W.G.1,2, Lu C.3
Fig. 11. Maximum principal stress contours and stress evolution of dangerous regions in top ceramic coat at the end of 100 thermal cycles. The top ceramic coat is separated from the model.