摘要
Local and average convection heat transfer coefficients were investigated inside the effusion hole in the impingement/effusion cooling schemes, which have the hole number ratio of 1:1, with different impingement wall and effusion wall pressure drop distribution. The benchmark is the cooling air mass flow rate per unit pressure and area of the high performance aeroengine. The results indicate that the pressure distribution has great influence on the heat transfer enhancement inside the effusion hole entrance (x/d<4). The mechanism of the enhanced heat transfer within the effusion hole entrance was explained using a CFD code. The correlation of the circumferential average heat transfer enhancement coefficients was fitted based on the experimental data, which plays an important role for the future heat transfer optimum of the impingement/effusion double skin wall.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 97-101 |
| 页数 | 5 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 24 |
| 期 | 2 |
| 出版状态 | 已出版 - 3月 2003 |
指纹
探究 'Influence of pressure drop distribution on the convection heat transfer inside the inclined hole of impingement/effusion cooling' 的科研主题。它们共同构成独一无二的指纹。引用此
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