文献详情
Control of Corner Separation with Plasma Actuation in a High-Speed Compressor Cascade
文献类型期刊
作者Zhang, Haideng[1];Yu, Xianjun[2];Liu, Baojie[3];Wu, Yun[4];Li, Yinghong[5]
机构
通讯作者Yu, XJ (reprint author), Beihang Univ, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Sch Energy & Power Engn, Beijing 100191, Peoples R China.; Yu, XJ (reprint author), Beihang Univ, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China.; Yu, XJ (reprint author), Beihang Univ, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China.
来源信息年:2017  卷:7  期:5  
期刊信息APPLIED SCIENCES-BASEL影响因子和分区  ISSN:2076-3417
关键词plasma actuation; active flow control; compressor; corner separation
增刊正刊
摘要The performances of modern highly loaded compressors are limited by the corner separations. Plasma actuation is a typical active flow control methodology, which has been proven to be capable of controlling the corner separations in low-speed compressor cascades. The main purpose of this paper is to uncover the flow control law and the mechanism of high-speed compressor cascade corner separation control with plasma actuations. The control effects of the suction surface as well as the endwall plasma actuations in suppressing the high-speed compressor cascade flow separations are investigated with numerical methods. The main flow structures within the high-speed compressor cascade corner separation and the development of the corresponding flow loss are investigated firstly. Next, the performances of plasma actuations in suppressing the high-speed compressor cascade corner separation are studied. At last, the mechanisms behind the control effects of the suction surface and the endwall plasma actuations are discussed. Both the suction surface and the endwall plasma actuations can improve the high-speed compressor cascade static pressure rise coefficient, while reducing the corresponding total pressure loss and blockage coefficients. The suction surface plasma actuation can suppress not only the high-speed compressor cascade corner separation vortex but also the airfoil separation, so, compared to the endwall plasma actuation, the suction surface plasma actuation is more efficient in reducing the total pressure loss of the high-speed compressor cascade. However, through suppressing the development of the passage vortex, the endwall plasma actuation is more efficient in reducing the flow blockage and improving the static pressure rise of the high-speed compressor cascade.
收录情况SCIE(WOS:000404449000033)  
所属部门能源与动力工程学院
DOI10.3390/app7050465
百度学术Control of Corner Separation with Plasma Actuation in a High-Speed Compressor Cascade
语言外文
被引频次11
人气指数90
浏览次数90
基金National Natural Science Foundation of China [51336011, 51376014, 51476004]
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