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

改进的Qiu滑移因子模型用于离心压气机叶轮的参数研究
引用本文:孟斐,田晓沛,单鹏.改进的Qiu滑移因子模型用于离心压气机叶轮的参数研究[J].航空动力学报,2014,29(4):944-952.
作者姓名:孟斐  田晓沛  单鹏
作者单位:北京航空航天大学 能源与动力工程学院, 北京 100191;北京航空航天大学 能源与动力工程学院, 北京 100191;北京航空航天大学 能源与动力工程学院, 北京 100191
摘    要:为适用于微型离心压气机叶轮的通流设计,对Qiu滑移因子模型加入了3个经验参数.首先对经验参数的求解方法及参数对于设计精度的影响进行了分析研究,发现其中经验参数cr对于设计精度影响较大.其次在通流设计中应用改进的Qiu滑移因子模型辅助生成叶片,用计算流体动力学(CFD)研究了cr所影响的模型滑移因子,与数值流场的出口平均滑移因子对比,得到了多种叶轮总体参数下cr的最佳取值.发现虽然微型、大型离心压气机叶轮总体参数变化范围很大,但cr的取值均以0.7左右为其最佳值.

关 键 词:离心压气机  大小叶片  通流设计  流线曲率法  滑移因子模型
收稿时间:2013/1/16 0:00:00

Parametric research on improved Qiu slip factor modelfor centrifugal compressor impellers
MENG Fei,TIAN Xiao-pei and SHAN Peng.Parametric research on improved Qiu slip factor modelfor centrifugal compressor impellers[J].Journal of Aerospace Power,2014,29(4):944-952.
Authors:MENG Fei  TIAN Xiao-pei and SHAN Peng
Institution:School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:To adapt the slip factor model proposed by Qiu to the through-flow design of micro-centrifugal impellers, three empirical parameters were introduced to reduce the system error. Firstly, the solving method of these empirical parameters and the impact on the design accuracy were researched. It is seen that empirical parameter cr influences the design accuracy greatly. Secondly, with employment of the improved Qiu slip factor model, a micro-centrifugal impeller was designed. The predicted slip factors impacted by cr in the model were compared with the impeller-outlet-averaged slip factors resulted from the CFD flow field simulation. The most suitable values of cr were found at different prescribed design overall parameters. It is found that cr nearby 0.7 has a best estimation, though the overall parameters of micro- or large-centrifugal compressor impeller vary widely.
Keywords:centrifugal compressor  splitter blade  through-flow design  streamline curvature method  slip factor model
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