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叶栅二次流旋涡结构与损失分析
引用本文:林奇燕,郑群,岳国强.叶栅二次流旋涡结构与损失分析[J].航空动力学报,2007,22(9):1518-1525.
作者姓名:林奇燕  郑群  岳国强
作者单位:哈尔滨工程大学,动力与能源工程学院,哈尔滨,150001
摘    要:采用三维粘性程序对某型动力涡轮的第一级进行了数值模拟,模拟结果捕捉到了该涡轮级叶栅的内部流的流动细节,展示了涡轮叶栅端壁和型面流动及叶栅通道内的三维流动结构.通过对叶栅中的二次流现象和流动损失机理的分析,揭示了该涡轮级叶栅通道内二次流旋涡结构(马蹄涡、通道涡、壁角涡、尾迹涡、泄漏涡等)的演变过程,以及旋涡结构对损失分布的影响.

关 键 词:航空、航天推进系统  二次流损失  涡系结构  尾迹涡  间隙流动  动力涡轮  数值模拟  叶栅二次流  旋涡结构  损失分析  turbine  losses  vortex  structure  secondary  flow  影响  损失分布  演变过程  泄漏涡  尾迹涡  角涡  通道涡  马蹄涡  损失机理  现象  三维流动结构  叶栅通道  涡轮叶栅端壁
文章编号:1000-8055(2007)09-1518-08
收稿时间:2006/8/24 0:00:00
修稿时间:2006年8月24日

Analysis of secondary flow vortex structure and losses in turbine cascades
LIN Qi-yan,ZHENG Qun and YUE Guo-qiang.Analysis of secondary flow vortex structure and losses in turbine cascades[J].Journal of Aerospace Power,2007,22(9):1518-1525.
Authors:LIN Qi-yan  ZHENG Qun and YUE Guo-qiang
Institution:College of Power and Energy Engineering, Harbin Engineering University, Harbin 150001, China;College of Power and Energy Engineering, Harbin Engineering University, Harbin 150001, China;College of Power and Energy Engineering, Harbin Engineering University, Harbin 150001, China
Abstract:Numerical simulation about the first stage of a power turbine was performed using 3D viscous code,showing that the details in this turbine stage were captured.And,the flow characteristics of endwalls and blade surfaces for these cascades and the structures of 3D flow field were also presented.After analysis of secondary flow phenomenon and loss mechanism,the evolution process of secondary flow vortex structures in cascade passage(horseshoe vortex,passage vortex,corner vortex,trailing vortex,tip leakage vortex,etc) were revealed,and the effects of vortex structures on loss distribution were also studied.
Keywords:aerospace propulsion system  secondary flows losses  vortex structures  trailing vortex  tip clearance flow  power turbine  numerical simulation
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