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. 10. Stress evolution with thermal cycles in region A as shown in Fig. 9 , at which stress components at the end of heating a and cooling b stages are shown, respectively.