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. 7. Evolution of strain components at location A as shown in Fig. 6 developed from a heating and b cooling with the number of cycles, respectively.