首页 | 官方网站   微博 | 高级检索  
     

扩压叶栅端壁区旋涡流动显示研究
引用本文:马宏伟,蒋浩康.扩压叶栅端壁区旋涡流动显示研究[J].航空动力学报,1997,12(3):258-262,330.
作者姓名:马宏伟  蒋浩康
作者单位:北京航空航天大学
摘    要:通过氢气泡流动显示,获取不同攻角、不同径向间隙下扩压叶栅端壁区内各种旋涡的发生、发展、涡-涡、涡-附面层干涉的流动图画。

关 键 词:叶栅  端部效应  旋涡  流动显示
收稿时间:8/1/1996 12:00:00 AM
修稿时间:1996/10/1 0:00:00

FLOW VISUALIZATIONS OF FLOW FIELD IN ENDWALL REGION OF A COMPRESSOR CASCADE
Ma Hongwei and Jiang Haokang.FLOW VISUALIZATIONS OF FLOW FIELD IN ENDWALL REGION OF A COMPRESSOR CASCADE[J].Journal of Aerospace Power,1997,12(3):258-262,330.
Authors:Ma Hongwei and Jiang Haokang
Affiliation:4th Dept.Beijing University of Aeronautics and Astronautics, Beijing 100083;4th Dept.Beijing University of Aeronautics and Astronautics, Beijing 100083
Abstract:This paper describes flow visualizations of the flow field in the endwall region of a compressor cascade. Within the cascade passage without radial clearance,it was found that many low-energy fluids exit in the corner between the suction surface and the endwall, and some vorticities of the corner vortex come from the leading edge horse shoe vortex.Tangential migration of the pressure-side horse-shoe vortex leads to flow mixing among the endwall boundary layer, suction surface boundary layer and the horse-shoe vortex.Small radial clearance leads to a weak leakage vortex that is far away from the suction surface,while large radial clearance leads to a strong one closer to the suction surface.The corner vortex is not obvious due to blowing of the leakage flow.In the endwall region, reaction among the vortexes and the boundary layers result in much more flow mixing and unsteadiness.
Keywords:Cascades  End effects  Vortex  Flow visualization
本文献已被 CNKI 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-23

京公网安备 11010802026262号