Heat transfer for gas turbine internal cooling with channel design
With the greater need for higher inlet temperature operations of the turbine blade, enhanced cooling mechanisms have become imperative to prevent temperatures from exceeding turbine blade material limits. Achieving these elevated temperatures necessitates greater heat transfer capabilities, and one...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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Nanyang Technological University
2023
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| Online Access: | https://hdl.handle.net/10356/172829 |