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. 4. Distribution and magnitude of U1, U2 and U3 displacements after deposition, heating, holding and cooling during the first thermal cycle in two aspect directions of a turbine blade.