Study on rotational effects of modern turbine blade on coolant injecting nozzle position with film cooling and vortex composite performance
The flow structure of the vortex cooling is asymmetrical compared to the traditional gas turbine leading edge cooling, such as the impingement cooling and the axial f low cooling. This asymmetrical property will affect the cooling performance in the blade leading edge, whereas such effects are not f...
Saved in:
| Main Authors: | , , , , , |
|---|---|
| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2024
|
| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/173182 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|