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. 2. A typical thermal cycle for a turbine blade with TBCs, which contains three steps: heating, holding and cooling.