Heat transfer for gas turbine internal cooling
High turbine inlet temperature is required for an efficient gas turbine engine. To maximise the turbine temperature, the internal channel of a turbine blade consists of rib-turbulators to enhance the heat transfer of the cooling air. This report focus on the effect of various rib configurations on c...
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| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2018
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| Online Access: | http://hdl.handle.net/10356/74952 |