反旋腰圆形鼓筒孔腔体内旋涡破碎机制与压损特性  

Research on the vortex breakdown and pressure loss characteristics in the cavity with anti-swirling waist circular drum hole

作　　者：沈文杰 王锁芳[1] 张馨丹 SHEN Wenjie;WANG Suofang;ZHANG Xindan(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)

机构地区：[1]南京航空航天大学能源与动力学院,南京210016

出　　处：《航空动力学报》2024年第8期60-68,共9页Journal of Aerospace Power

基　　金：国家科技重大专项(2017-Ⅲ-0011-0037)。

摘　　要：为降低压气机径向引气过程中的压损,本文设计了反旋腰圆形鼓筒孔结构,采用大涡模拟(LES)和经验证的RNG k-ε模型分别探究了腔体内的旋涡演化规律和压损特性,揭示了反旋腰圆形鼓筒孔的旋涡破碎机制与减阻机理。结果表明:反旋腰圆形鼓筒孔可降低腔体内压损。高速旋涡在腰圆形鼓筒孔腔体的低径位区域内快速强化,旋涡尺度呈快速增大趋势,致使压损系数随径向高度降低而快速升高。与腰圆形鼓筒孔相比,反旋腰圆形鼓筒孔可有效抑制旋涡尺度增大,相对可降低腔体内15.6%的压损。反旋腰圆形鼓筒孔结构简单且引气过程呈线性状态,具有较高工程应用价值。To reduce the pressure loss in a compressor disk cavity,an anti-swirling waist circular drum hole structure was designed.Large Eddy simulation(LES) and the RNG k-ε model were used to investigate the vortex evolution and pressure loss characteristics in the cavity,respectively,revealing the vortex breakdown mechanism and drag reduction mechanism of the anti-swirling waist circular drum hole.The results showed that the anti-swirling waist circular drum hole can reduce the pressure loss in the cavity.The high-speed vortex was intensified rapidly in the low region of the cavity with waist circular drum,and the vortex scale increased rapidly,resulting in the rapid increase of pressure loss coefficient with the radial height decrease.Compared with the waist circular drum hole,the anti-swirling waist circular drum hole can effectively restrain the vortex scale increase and reduce the pressure loss in the cavity by 15.6%.With simple structure and linear airflow characteristic,the anti-swirling waist circular drum hole has high engineering application value.

关 键 词：共转腔体 鼓筒孔 相干涡 旋涡尺度 压损 

分 类 号：V231.1[航空宇航科学与技术—航空宇航推进理论与工程]