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跨音压气机转子叶尖间隙复杂流动观测
引用本文:桂幸民,聂超群,王同庆,于清,李运敏,史伟,NIE Chaoqun,WANG Tongqing,YU Qing.跨音压气机转子叶尖间隙复杂流动观测[J].工程热物理学报,2000,21(5):570-572.
作者姓名:桂幸民  聂超群  王同庆  于清  李运敏  史伟  NIE Chaoqun  WANG Tongqing  YU Qing
作者单位:1. 北京航空航天大学407教研室,北京 100083
2. 中国科学院工程热物理研究所,北京100080
3. Institute of Engineering Thermophysics, Academia Sinica,Beijing 100080, China
4. Group 407, Beijing University of Aeronautics andAstronautics, Beijing 100083, China
基金项目:航空基金!(NO.97Z51001),国家自然科学基金!(NO.59706005)
摘    要:本文利用高频响动态压力传感器,在文献[1]的基础上,对WP11压气机转子叶尖间隙 流场进行了流场测量。测试包括三个转速多个节流条件下的间隙流场。测试结果表明:激波总体位 置随节流加深而向上游移动,但吸力面最小压力点基本维持在40%或20%弦长处不变。当激波位 置在该点之后时,二次漏流直接冲击激波结构;当激波位置在该点之前时,激波结构基本只受前缘 漏流的影响。

关 键 词:叶轮机械  激波结构  激波—漏流干扰
文章编号:0253-231X(2000)05-0570-03
修稿时间:1999年5月18日

TIP CLEARANCE FLOW IN A TRANSONIC COMPRESSOR ROTOR
GUI Xingmin,NIE Chaoqun,WANG Tongqing,YU Qing,LI Yunmin,SHI Wei,NIE Chaoqun,WANG Tongqing,YU Qing.TIP CLEARANCE FLOW IN A TRANSONIC COMPRESSOR ROTOR[J].Journal of Engineering Thermophysics,2000,21(5):570-572.
Authors:GUI Xingmin  NIE Chaoqun  WANG Tongqing  YU Qing  LI Yunmin  SHI Wei  NIE Chaoqun  WANG Tongqing  YU Qing
Abstract:High frequency response unsteady pressure transducers were used to investigate tip clearance flow structures in a transonic compressor rotor. Shock structures and their interactions with tip clearance leakage flow are studied in the present paper from open throttle operating condition to stall for three corrected rotating speeds. The position of minimum static pressure locates at 40% or 20% chord length, and keeps the position for the different operating conditions, although the passage shock moves upstream with closing outlet throttle. When the impacting point of shock on suction surface locates behind the minimum pressure, secondary leakage flow distorts the passage shock directly, otherwise, leading edge leakage flow effects much upon the passage shock wave.
Keywords:turbomachinery  shock structure  shock-leakage flow interaction  
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