Research Article

High-Temperature Low-Cycle Fatigue Behaviour of MAR-M247 Coated with Newly Developed Thermal and Environmental Barrier Coating

Figure 5

Fracture surface of the specimen fatigued to failure, εa = 0.38%: (a) surface initiation site and crack growth path; (b) cleavage fracture of the upper layer splats; (c) cleavage fracture of the YSZ splats.