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Thermal barrier coatings (TBCs) have been essential technologies to improve the performance and efficiency of advanced gas turbines, which are in service at extremely high temperatures. Interfacial strength is one of the important properties in TBCs, and it has been often evaluated by tensile method, e.g. the ASTM standard; ASTM C633. However, the applicability of tensile method is limited, due to its size dependence. To overcome this problem, a new method has been proposed in the previousdoi:10.1016/j.proeng.2011.04.139 fatcat:a6i3e3tpezalfdrbjgqc5osjzq