摘要
The turbine blade works at high thermal loads, especially the trailing edge of the blade due to the hot gas leakage flow. Pin-fins are well recognized as a kind of effective device to augment the convective heat transfer and effectively cool the trailing edge. In this paper, the cooling effectiveness of chordwise outlet pin-fins distance and inner pin fin diameter is, respectively, studied on the heat transfer and flow friction of the trailing edge of the blade with software CFX. A 90 deg turn cooling wedge passage with cylindrical pin-fins is used to model the trailing edge. Results show that the pin-fins distance at the outlet and the arithmetic arrangement of the inner pin-fins diameter both are vital factors to influence the cooling effectiveness in the trailing edge of the blade.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 127078 |
| 期刊 | Advances in Mechanical Engineering |
| 卷 | 2013 |
| DOI | |
| 出版状态 | 已出版 - 2013 |
指纹
探究 'Computer-aided simulations of convective heat transfer in a wedged channel with pin-fins at various outlet arrangements and nonuniform diameters' 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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