Failure mechanism of YSZ coatings prepared by EB-PVD under partial penetration of CMAS attacking
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OpenAlex topics: High-Temperature Coating Behaviors · Nuclear Materials and Properties · Advanced ceramic materials synthesis
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References (24)
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1. Gas turbine coatings–an overview10.1016/j.engfailanal.2012.07.007 ↗
2. Thermal barrier coatings for aircraft engines: history and directions10.1007/BF02646310 ↗
3. Thermal barrier coatings for gas-turbine engine applications10.1126/science.1068609 ↗
4. The hotter the engine, the better10.1126/science.1179327 ↗
5. Mechanisms governing the performance of thermal barrier coatings10.1016/S1359-0286(99)00024-8 ↗
6. Materials design for the next generation thermal barrier coatings10.1146/annurev.matsci.33.011403.113718 ↗
7. Mechanisms of cracking and delamination within thick thermal barrier systems in aero-engines subject to calcium-magnesium-alumino-silicate (CMAS) penetration
8. Ceramic materials for thermal barrier coatings10.1016/S0955-2219(03)00129-8 ↗
9. Microstructure and texture of EB-PVD TBCs grown under different rotation modes10.1016/S0921-5093(03)00470-2 ↗
10. Effect of morphology on thermal conductivity of EB-PVD PYSZ TBCs10.1016/j.surfcoat.2006.05.003 ↗
11. In situ Raman spectroscopy studies of high-temperature degradation of thermal barrier coatings by molten silicate deposits10.1016/j.scriptamat.2013.12.008 ↗
12. Stott F.H., Wet D., Taylor R. , The effects of molten silicate deposits on the stability of thermal barrier coatings for turbine applications at very high temperatures, in: Proceedings of the Twenty Fourth International SAMPE Technical Conference, 1992.
13. Smialek · 1991
14. Deposition of volcanic materials in the hot sections of two gas turbine engines
15. Role of environmental deposits and operating surface temperature in spallation of air plasma sprayed thermal barrier coatings10.1016/S0257-8972(96)02994-5 ↗
16. Calcium–magnesium–alumino-silicate (CMAS) degradation of EB-PVD thermal barrier coatings: characterization of CMAS damage on ex-service high pressure blade TBCs10.1016/j.surfcoat.2012.07.074 ↗
17. Mechanisms of cracking and delamination within thick thermal barrier systems in aero-engines subject to calcium-magnesium-alumino-silicate (CMAS) penetration10.1016/j.msea.2008.01.006 ↗
18. Thermochemical interaction of thermal barrier coatings with molten CaO–MgO–Al2O3–SiO2 (CMAS) deposits10.1111/j.1551-2916.2006.01209.x ↗
19. The spreading behavior of CMAS melt on YSZ single crystal with low index orientation10.1016/j.apsusc.2020.146846 ↗
20. On the mechanical behavior of brittle coatings and layers10.1007/BF00656841 ↗
21. A delamination mechanism for thermal barrier coatings subject to calcium–magnesium–alumino-silicate (CMAS) infiltration10.1016/j.actamat.2004.11.028 ↗
22. Crack channelling and spalling in a plate due to thermal shock loading10.1016/S0022-5096(99)00064-2 ↗
23. Study on deflection energy release rate of matrix crack in ceramic
24. Ceramic materials for thermal barrier coatings10.1016/S0955-2219(03)00129-8 ↗