Design gas turbine vane with ceramics matrix composites
To improve the efficiency of a gas turbine engine (GTE), there is a need to develop new technologies to increase the turbine inlet temperature. One promising technology is to replace the current Ni-based superalloys material with Ceramic Matrix Composite (CMC). The CMC material can operate 200℃ hott...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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Nanyang Technological University
2020
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| Online Access: | https://hdl.handle.net/10356/141271 |