Gas turbine internal cooling with 180 degree bend channel design
The primary method for maximising the efficiency of aircraft turbine engines is increasing the turbine inlet temperature, thereby prompting the adoption of rib-turbulated cooling techniques to manage the intense thermal loads on the internal walls. Past research into the two-channel turbine blade mo...
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| Format: | Final Year Project |
| Language: | English |
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Nanyang Technological University
2024
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| Online Access: | https://hdl.handle.net/10356/176887 |
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| Institution: | Nanyang Technological University |
| Language: | English |
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