Numerical simulation of damage and inelastic deformation of porous thermal barrier coatings system
Thermal barrier coating (TBC) is widely applied to gas turbine blade surface to protect the metallic substrate from high-temperature combustion gas flow. Porous TBC system has been developed by our research group in order to further increase the turbine inlet temperature. In this study, in order to...
| Main Authors: | , , |
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| Format: | Article |
| Language: | Japanese |
| Published: |
The Japan Society of Mechanical Engineers
2021-08-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
| Subjects: | |
| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/87/901/87_21-00086/_pdf/-char/en |