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高速离心叶轮叶片开缝的数值研究
引用本文:韩伟,高丽敏,白莹,李晓军,高杰. 高速离心叶轮叶片开缝的数值研究[J]. 流体机械, 2011, 39(11). DOI: 10.3969/j.issn.1005-0329.2011.11.004
作者姓名:韩伟  高丽敏  白莹  李晓军  高杰
作者单位:西北工业大学,陕西西安,710072
摘    要:提出在离心叶轮吸力面尾部开缝抽吸的方法,在叶片吸力面尾部对低速流体区域进行抽吸,以减弱由叶轮内二次流所导致的射流—尾迹结构。以Krain高速离心叶轮为例,建立抽吸模型,并进行了数值计算。数值仿真结果表明,在压气机流量范围内,叶轮尾部开缝抽吸可以减少叶片表面的分离区域,改善叶轮内部流场的流动状况,有效地提高离心叶轮性能。

关 键 词:离心叶轮  叶片开缝  射流-尾迹结构  边界层控制  

Numerical Study of Centrifugal Compressor with Slots in Blade Surface
HAN Wei,GAO Li-min,BAI Ying,LI Xiao-jun,GAO Jie. Numerical Study of Centrifugal Compressor with Slots in Blade Surface[J]. Fluid Machinery, 2011, 39(11). DOI: 10.3969/j.issn.1005-0329.2011.11.004
Authors:HAN Wei  GAO Li-min  BAI Ying  LI Xiao-jun  GAO Jie
Abstract:A new method of drilling through-slots in blade suction surfaces near the shroud of a centrifugal impeller is proposed,where low velocity area or separation area is sucked,as a result,the jet-wake flow caused by secondary flows in the impeller is weakened.The numerical model of Krain centrifugal impeller is built and computed.The result show that the seperation area near blade suction surfaces is reduced,the flow field inside centrifugal impeller is improved and better performance of the centrifugal impelle...
Keywords:centrifugal impeller  slots in blade  jet-wake flows  boundary layer control  
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