| 不同长度吸力面小翼对压气机叶栅间隙影响的数值研究 |
| |
| 引用本文： | 韩少冰,钟兢军,严红明.不同长度吸力面小翼对压气机叶栅间隙影响的数值研究[J].航空动力学报,2011,26(3):656-661. |
| |
| 作者姓名： | 韩少冰 钟兢军 严红明 |
| |
| 作者单位： | 1. 大连海事大学,轮机工程学院,大连,116026
2. 哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001 |
| |
| 摘 要： | 对常规直叶栅和三种具有不同长度和起始位置的吸力面小翼叶栅内的三维黏性流场进行了数值模拟.结果表明,不同长度吸力面小翼都不同程度上改善了叶栅顶部的气流流动状况;在叶顶吸力面侧加装与其型线等长度的小翼可以较好地削弱泄漏涡的强度,随着叶顶间隙的增大,泄漏流动增强,其作用效果逐渐降低.
|
| 关 键 词： | 压气机叶栅 吸力面小翼 叶顶间隙 数值模拟 泄漏流 |
| 收稿时间： | 3/9/2010 12:00:00 AM |
| 修稿时间： | 2010/6/30 0:00:00 |
Influence of suction-side winglet length on tip leakage flow in compressor cascade |
| |
| HAN Shao-bing,ZHONG Jing-jun and YAN Hong-ming.Influence of suction-side winglet length on tip leakage flow in compressor cascade[J].Journal of Aerospace Power,2011,26(3):656-661. |
| |
| Authors: | HAN Shao-bing ZHONG Jing-jun and YAN Hong-ming |
| |
| Institution: | Marine Engineering College,Dalian Maritime University,Dalian 116026,China;Marine Engineering College,Dalian Maritime University,Dalian 116026,China;School of Energy Science and Engineering, Harbin Institute of Technology,Harbin 150001,China |
| |
| Abstract: | The numerical simulation was performed to investigate the influence of the suction-side winglet with different lengthes on the tip leakage flow in compressor cascade.The simulation results show that the suction-side winglets can improve the tip clearance flow condition.It is found that the winglet is most effective to weaken the intensity of the leakage vortices if their length is the same with that of the blade tip.With increasing clearance and stronger intensity leakage flow,the winglet's effect is gradually decreased. |
| |
| Keywords: | compressor cascade suction-side winglet tip clearance |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
| 点击此处可从《航空动力学报》下载免费的PDF全文 |
|
