摘要
Numerical method was used to analyze the characteristics of heat transfer and flow resistance in micro channels in the middle of turbine blades; and the effect of aspect ratio and the rib aspect ratio in the micro channels was also studied. The result shows: in the case of the inlet Re=11000, if the rib aspect ratio is invariable, and the aspect ratio of micro channel increases, the integrated effect of heat transfer will increase firstly and then decrease; if the aspect ratio is invariable, and the rib aspect ratio increases, the integrated effect of heat transfer also will increase firstly and then decrease.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1989-1993 |
| 页数 | 5 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 24 |
| 期 | 9 |
| 出版状态 | 已出版 - 9月 2009 |
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