摘要
To match the rotor blade of real engine operating condition, the Reynolds and rotation number range of current experiment were expanded from 10 000 to 70 000 and 0 to 2.08 by increasing the pressure of the air in the U-shaped channel to 500 kPa. Experiments were conducted to investigate the heat transfer characteristics in a square U-shaped channel with inclined 45 deg ribs. Results indicated that, in the first passage of the U-shaped channel, heat transfer coefficient of leading wall firstly decreased with the increase of the rotation number, then increased with the rotation number after reaching a critical value; in the second passage of the U-shaped channel, the difference of heat transfer coefficient between leading and trailing walls was not obvious at low rotation number, but kept increasing with the rotation number to a higher level; the heat transfer of leading wall behaved better than trailing wall, which was totally different from that of a smooth channel.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 360-368 |
| 页数 | 9 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 31 |
| 期 | 2 |
| DOI | |
| 出版状态 | 已出版 - 1 2月 2016 |
指纹
探究 'Heat transfer characteristics in U-shaped rib-roughened channel at high rotation numbers' 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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