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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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2018
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/74952 |
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| 機構: | Nanyang Technological University |
| 語言: | English |