摘要
Numerical simulations are performed to investigate the effects of super-elliptic film holes on adiabatic film cooling effectiveness under three blowing ratios (M = 0.5, 1.0, 1.5). The results show that compared with the basic circular model, super-elliptic model I with length-to-width ratio of 2 provides the better film cooling effectiveness in the range of x/D < 5 at M = 0.5 while at M = 1.0 the better film cooling effectiveness is observed in the range of x/D <17.35 and at M = 1.5 the higher film cooling performance is shown along the mainstream direction. However, due to the large laterally coverage of the film, super-elliptic model II with length-to-width ratio of 4 exhibits the best film cooling effectiveness at three different blowing ratios among all models. Such advantages become more significant with the increase of the blowing ratio.
| 投稿的翻译标题 | Effect of Super-Elliptic Film Holes on Adiabatic Film Cooling Effectiveness |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 427-434 |
| 页数 | 8 |
| 期刊 | Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics |
| 卷 | 50 |
| 期 | 4 |
| DOI | |
| 出版状态 | 已出版 - 1 8月 2018 |
关键词
- Adiabatic cooling effectiveness
- Blowing ratio
- Film cooling
- Super-elliptic hole
- Vortex
学术指纹
探究 '超椭圆孔型对气膜绝热冷却效率的影响' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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