首页 | 本学科首页   官方微博 | 高级检索  
     检索      

有无叶顶间隙条件下斜流风机叶轮内部三维流动的数值研究
引用本文:赖焕新,康顺,谭春青,吴克启.有无叶顶间隙条件下斜流风机叶轮内部三维流动的数值研究[J].航空动力学报,2000,15(1):17-21.
作者姓名:赖焕新  康顺  谭春青  吴克启
作者单位:1.中国科学院工程热物理研究所,北京100080
基金项目:国家自然科学基金!资助项目(59876042)
摘    要:本文使用NUMECA 的商业软件Fine/Turbo,对一种斜流风机叶轮在有无叶顶间隙条件下的三维粘性流场进行数值研究。在与测量数据比较的基础上,对两种流场的极限流线和二次流图谱及速度分布等进行了分析。揭示了流道中低速流体的输运,“射流—尾迹”流型和叶顶间隙泄漏涡等的形成过程。研究结果表明:二次流和涡运动导致叶道出口流动尾迹发生于外端壁/压力面角域。 

关 键 词:斜流叶轮    内部流动    间隙    数值模拟
收稿时间:1999/1/25 0:00:00
修稿时间:1999-0125-

Numerical Study of 3-D Flow in a Diagonal Fan Impeller
Lai Huanxin,Kang Shun,Tan Chunqing and Wu Keqi.Numerical Study of 3-D Flow in a Diagonal Fan Impeller[J].Journal of Aerospace Power,2000,15(1):17-21.
Authors:Lai Huanxin  Kang Shun  Tan Chunqing and Wu Keqi
Institution:1.Institute of Engineering Thermophysics, Chinese Academy of Sciences,Beijing 100080,China2.Dept.Power Engineering,Huazhong University of Science and Technology,Wuhan 430074,China
Abstract:The NUMECA software Fine/Turbo is employed to investigate the three dimensional viscous flow in a diagonal fan impeller at the operating conditions with and without blade tip clearance respectively.The limiting streamlines,secondary flow patterns and velocity distributions of the two flow fields are analyzed by comparison between their numerical and experimental results.The transportation of low energy fluid in the flow passage,"jet/wake" structure and the formation of tip leakage vortex are revealed.The results show that the non-uniform flow wake induced by secondary motion and vortex always appear in the corner region of casing wall and pressure surface;and the effects of the tip clearance are to reduce the efficiency of the impeller and to enlarge the non-uniform level of the outflow field in the impeller.
Keywords:diagonal impeller  internal flow  clearance  numerical  simulation
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
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号