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. 6. Simulation results of strain, ɛ 11 , as a typical component of the strain field, at the end of each cycling stage.