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. 9. In-plane stress contours, σ 11 , in top ceramic coat during a whole thermal cycle from both pressure and suction sides of a turbine blade with TBCs.