| Citation: | LIANG Zuozhao, SUN Peng, LI Xiaodong, et al. Effects of outlet position on corner separation of high speed compressor cascade with endwall self-adaptive injection[J]. Journal of Aerospace Power, 2025, 40（3）：20230325 doi: 10.13224/j.cnki.jasp.20230325
|
To explore the effects of endwall self-adaptive injection on corner separation and loss performance of high speed compressor cascade, the different outlet positions of endwall self-adaptive injection were studied by numerical simulation method. The results showed that the application of endwall self-adaptive injection can effectively control corner separation, reduce low-energy fluid accumulation, improve cascade pressure expansion ability and reduce total pressure loss of the cascade. The maximum relative reduction of the total pressure loss coefficient of 9.17% of the cascade at attack angle
| [1] |
刘永泉,刘太秋,季路成. 航空发动机风扇/压气机技术发展的若干问题与思考[J]. 航空学报,2015,36(8): 2563-2576. LIU Yongquan,LIU Taiqiu,JI Lucheng. Some problems and thoughts in the development of aero-engine fan/compressor[J]. Acta Aeronautica et Astronautica Sinica,2015,36(8): 2563-2576. (in Chinese
LIU Yongquan, LIU Taiqiu, JI Lucheng. Some problems and thoughts in the development of aero-engine fan/compressor[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(8): 2563-2576. (in Chinese)
|
| [2] |
张海灯,吴云,李应红,等. 高速压气机叶栅旋涡结构及其流动损失研究[J]. 航空学报,2014,35(9): 2438-2450. ZHANG Haideng,WU Yun,LI Yinghong,et al. Investigation of vortex structure and flow loss in a high-speed compressor cascade[J]. Acta Aeronautica et Astronautica Sinica,2014,35(9): 2438-2450. (in Chinese
ZHANG Haideng, WU Yun, LI Yinghong, et al. Investigation of vortex structure and flow loss in a high-speed compressor cascade[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(9): 2438-2450. (in Chinese)
|
| [3] |
刘华坪,陈焕龙,杨晓光,等. 基于耗散函数的低速扩压叶栅损失机理探讨[J]. 航空动力学报,2011,26(2): 289-296. LIU Huaping,CHEN Huanlong,YANG Xiaoguang,et al. Study of loss mechanism in low speed compressor cascade using dissipation function[J]. Journal of Aerospace Power,2011,26(2): 289-296. (in Chinese
LIU Huaping, CHEN Huanlong, YANG Xiaoguang, et al. Study of loss mechanism in low speed compressor cascade using dissipation function[J]. Journal of Aerospace Power, 2011, 26(2): 289-296. (in Chinese)
|
| [4] |
LI Z Y,DU J,JEMCOV A,et al. A study of loss mechanism in a linear compressor cascade at the corner stall condition[R]. ASME Paper GT2017-65192,2017.
|
| [5] |
田思濛,吴云,张海灯,等. 基于能量耗散率的低速扩压叶栅损失研究[J]. 航空学报,2015,36(10): 3249-3262. TIAN Simeng,WU Yun,ZHANG Haideng,et al. Energy loss in a low-speed compressor cascade with dissipation function[J]. Acta Aeronautica et Astronautica Sinica,2015,36(10): 3249-3262. (in Chinese
TIAN Simeng, WU Yun, ZHANG Haideng, et al. Energy loss in a low-speed compressor cascade with dissipation function[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(10): 3249-3262. (in Chinese)
|
| [6] |
CAMP T R,DAY I J. A study of spike and modal stall phenomena in a low-speed axial compressor[J]. Journal of Turbomachinery,1998,120(3): 393-401. doi: 10.1115/1.2841730
|
| [7] |
SINNETTE J T,COSTELLO G R. Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines[R]. NACA-TN-2371,1951.
|
| [8] |
STURM W,SCHEUGENPFLUG H,FOTTNER L. Performance improvements of compressor cascades by controlling the profile and sidewall boundary layers[J]. Journal of Turbomachinery,1992,114(3): 477-486. doi: 10.1115/1.2929168
|
| [9] |
GMELIN C,STEGER M,THIELE F,et al. Unsteady RANS simulations of a highly loaded low aspect ratio compressor stator cascade with active flow control[R]. ASME Paper GT2010-22516,2010.
|
| [10] |
HECKLAU M,WIEDERHOLD O,ZANDER V,et al. Active separation control with pulsed jets in a critically loaded compressor cascade[J]. AIAA Journal,2011,49(8): 1729-1739. doi: 10.2514/1.J050931
|
| [11] |
ZANDER V,NITSCHE W. Control of secondary flow structures on a highly loaded compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy,2013,227(6): 674-682.
|
| [12] |
NERGER D,SAATHOFF H,RADESPIEL R,et al. Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade[J]. Journal of Turbomachinery,2012,134(2): 021010. doi: 10.1115/1.4003254
|
| [13] |
弓志强,陆亚钧,葛敬东. 环形扩压叶栅流动非定常控制方法的PIV研究[J]. 航空动力学报,2006,21(3): 455-460. GONG Zhiqiang,LU Yajun,GE Jingdong. Investigation of unsteady flow control in an annular compressor cascade using PIV[J]. Journal of Aerospace Power,2006,21(3): 455-460. (in Chinese
GONG Zhiqiang, LU Yajun, GE Jingdong. Investigation of unsteady flow control in an annular compressor cascade using PIV[J]. Journal of Aerospace Power, 2006, 21(3): 455-460. (in Chinese)
|
| [14] |
ZHENG Xinqian,ZHOU Sheng,LU Yajun,et al. Flow control of annular compressor cascade by synthetic jets[J]. Journal of Turbomachinery,2008,130(2): 021018.
|
| [15] |
茅晓晨,刘波,曹志远,等. 端壁射流对压气机叶栅角区分离控制的研究[J]. 推进技术,2014,35(12): 1615-1622. MAO Xiaochen,LIU Bo,CAO Zhiyuan,et al. Research on corner separation control for compressor cascade with end-wall jet flow[J]. Journal of Propulsion Technology,2014,35(12): 1615-1622. (in Chinese
MAO Xiaochen, LIU Bo, CAO Zhiyuan, et al. Research on corner separation control for compressor cascade with end-wall jet flow[J]. Journal of Propulsion Technology, 2014, 35(12): 1615-1622. (in Chinese)
|
| [16] |
陈萍萍. 轴流压气机角区分离流动损失机理及流动控制策略研究[D]. 西安: 西北工业大学,2015. CHEN Pingping. Investigations of corner separated flow loss mechanism and its flow control techniques for axial-compressors[D]. Xi’an: Northwestern Polytechnical University,2015. (in Chinese
CHEN Pingping. Investigations of corner separated flow loss mechanism and its flow control techniques for axial-compressors[D]. Xi’an: Northwestern Polytechnical University, 2015. (in Chinese)
|
| [17] |
TIAN Simeng,WU Yangyang,ZHANG Zhibo,et al. Experimental study and vortex analysis in a linear compressor cascade with active flow control[R]. ASME Paper GT2016-57276,2016.
|
| [18] |
刘华坪,张东飞,陈焕龙. 端壁射流对高速扩压叶栅性能的影响[J]. 工程热物理学报,2017,38(12): 2569-2575. LIU Huaping,ZHANG Dongfei,CHEN Huanlong. The performance of corner endwall jet in a high speed compressor cascade[J]. Journal of Engineering Thermophysics,2017,38(12): 2569-2575. (in Chinese
LIU Huaping, ZHANG Dongfei, CHEN Huanlong. The performance of corner endwall jet in a high speed compressor cascade[J]. Journal of Engineering Thermophysics, 2017, 38(12): 2569-2575. (in Chinese)
|
| [19] |
ZHANG Hongxin,CHEN Shaowen,GONG Yun,et al. A comparison of different unsteady flow control techniques in a highly loaded compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering,2019,233(6): 2051-2065.
|
| [20] |
ZHANG Hongxin,CHEN Shaowen. A comparative experimental analysis of two unsteady flow control methods in a highly loaded compressor cascade[J]. Experiments in Fluids,2020,61(6): 132. doi: 10.1007/s00348-020-02976-w
|
| [21] |
HERGT A,MEYER R,LIESNER K,et al. A new approach for compressor endwall contouring [R]. ASME Paper GT2011-45858,2011.
|
| [22] |
李晓东,孙鹏,傅文广. 端壁凹槽控制扩压叶栅角区分离的数值研究[J]. 工程热物理学报,2022,43(2): 316-323. LI Xiaodong,SUN Peng,FU Wenguang. Numerical study of corner separation control on compressor cascade with endwall groove[J]. Journal of Engineering Thermophysics,2022,43(2): 316-323. (in Chinese
LI Xiaodong, SUN Peng, FU Wenguang. Numerical study of corner separation control on compressor cascade with endwall groove[J]. Journal of Engineering Thermophysics, 2022, 43(2): 316-323. (in Chinese)
|
| [23] |
KÖLLER U,MÖNIG R,KÜSTERS B,et al. Development of advanced compressor airfoils for heavy-duty gas turbines: Part I design and optimization[J]. Journal of turbomachinery,2000,122(3): 397-405. doi: 10.1115/1.1302296
|
| [24] |
DE HALLER P. Das verhalten von tragflügelgittern in axialverdichtern und im windkanal[J]. Brennst-Waerme-Kraft,1953,5(10): 333-337.
|
DownLoad:
