| Citation: | DAI Li-ping, ZHANG Hui, KANG Shun. Numerical simulation of the effect of blade tip blowing on a low speed axial compressor tip clearance flow[J]. Journal of Aerospace Power, 2010, 25(12): 2643-2649.
|
| [1] |
袁巍,周盛,陆亚钧.压气机间隙流与处理机匣作用的三维数值分析[J].北京航空航天大学学报,2004,30(9):885-888. YUAN Wei,ZHOU Sheng,LU Yajun.3D numerical analysis for the effect between tip clearance and casing treatment in turbomachinery[J].Journal of Beijing University of Aeronautics and Astronautics,2004,30(9):885-888.(in Chinese)
|
| [2] |
Denton J D.Loss mechanisms in turbomachines .ASME Paper 93-GT-435,1993.
|
| [3] |
楚武利,张皓光,吴艳辉,等.槽式处理机匣开槽数目对扩稳效果的影响[J].推进技术,2008,29(5):598-603. CHU Wuli,ZHANG Haoguang,WU Yanhui,et al.Effects of grooved number of grooved casing treatment on stall margin [J].Journal of Propulsion Technology,2008,29(5):598-603.(in Chinese)
|
| [4] |
LU Xingen,ZHU Junqiang,NIE Chaoqun,et al.The stability-limiting flow mechanisms in a subsonic axial-flow compressor and its passive control with casing treatment .ASME Paper 2008-GT-50006,2008.
|
| [5] |
陈海昕,黄旭东,符松.压气机机匣处理的数值研究[J].航空动力学报,2007,22(2):298-304. CHEN Haixin,HUANG Xudong,FU Song.CFD study on casing treatment in a transonic compressor[J].Journal of Aerospace Power,2007,22(2):298-304.(in Chinese)
|
| [6] |
张皓光,楚武利,吴艳辉,等.吹气型周向槽机匣处理扩稳机理的研究[J].航空动力学报,2007,22(6):961-966. ZHANG Haoguang,CHU Wuli,WU Yanhui,et al.Mechanism of stall margin improvement associated with the blowing circumferential grooved casing treatment[J].Journal of Aerospace Power,2007,22(6):961-966.(in Chinese)
|
| [7] |
孙大坤,刘小华,孙晓峰.非定常机匣处理扩稳实验研究[J].工程热物理学报,2008,29(12):2022-2026. SUN Dakun,LIU Xiaohua,SUN Xiaofeng.An experimental investigation of stall margin imporovment with unsteady casing treatment[J].Journal of Engineering Thermophysics,2008,29(12):2022-2026.(in Chinese)
|
| [8] |
马文生,顾春伟.轴流压气机跨声级转子叶顶喷气的流动特性[J].推进技术,2009,30(3):303-307. MA Wensheng,GU Chunwei.Tip injection in transonic axial compressor rotor[J].Journal of Propulsion Technology,2009,30(3):303-307.(in Chinese)
|
| [9] |
徐纲,聂超群,黄伟光,等.低速轴流压气机顶部微量喷气控制失速机理的数值模拟[J].工程热物理学报,2004,25(1):37-40. XU Gang,NIE Chaoqun,HUANG Weiguang,et al.Numerical simulation of micro injection in a low speed axial compressor[J].Journal of Engineering Thermophysics,2004,25(1):37-40.(in Chinese)
|
| [10] |
邓向阳.压气机叶顶间隙流的数值模拟研究 .北京:中国科学院工程热物理研究所,2006. DENG Xiangyang.Numerical investigation on tip clearance flow in compressor .Beijing:Institute of Engineering and Thermophysics,Chinese Academy of Sciences,2006.(in Chinese)
|
| [11] |
张辉,马宏伟,蒋浩康.压气机转子三维流场计算中叶尖间隙网格的影响[J].航空动力学报,2006,21(1):137-143. ZHANG Hui,MA Hongwei,JIANG Haokang.Effects of tip clearance grids on the simulations of three-dimensional flow fields in a low speed compressor rotor[J].Journal of Aerospace Power,2006,21(1):137-143.(in Chinese)
|
| [12] |
马宏伟,蒋浩康.单转子压气机设计和近失速状态出口三维紊流流场[J].工程热物理学报,1997,18(2):153-158. MA Hongwei,JIANG Haokang.Three-dimensional turbulent flow field at the exit of an axial compressor rotor passage in both design and near stall conditions[J].Journal of Engineering Thermophysics,1997,18(2):153-158.(in Chinese)
|
DownLoad: