The effect of pore structure on the erosion resistance of air plasma sprayed thermal barrier coatings on finite element simulation
Abstract Thermal barrier coatings (TBCs) applied to turbine blades in aviation engines and gas turbines often experience erosion damage from small solid particles. This damage is directly linked to the microscale pores randomly distributed within the TBCs, impacting their erosion resistance. The eff...
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| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Nature Portfolio
2025-07-01
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| Series: | Scientific Reports |
| Subjects: | |
| Online Access: | https://doi.org/10.1038/s41598-025-11612-8 |
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