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.