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Topological Studies of Three-dimensional Flows in a High Pressure Compressor Stator Blade Row without and with Boundary Layer Aspiration 被引量:3

Topological Studies of Three-dimensional Flows in a High Pressure Compressor Stator Blade Row without and with Boundary Layer Aspiration
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摘要 This paper presents a numerical study of the flow topologies of three-dimensional (3D) flows in a high pressure compressor stator blade row without and with boundary layer aspiration on the hub wall. The stator blade is representative of the first stage operating under transonic inlet conditions and the blade design encourages development of highly complex 3D flows. The blade has a small tip clearance. The computational fluid dynamics (CFD) studies show progressive increase of hub corner stall with the increase in incidence. Aspiration is implemented on the hub wall via a slot in the comer between the hub wall and the suction surface. The CFD studies show aspiration to be sensitive to the suction flow rate; lower rate leads to very complex flow struc- tures and increased level of losses whereas higher rate renders aspiration effective for control of hub comer separation. The flow topologies are studied by trace of skin friction lines on the walls. The nature of flow can be explained by the topological rules of closed separation. Furthermore, a deeper analysis is done for a particular case with advanced criterion to test the non-degeneracy of critical points in the flow field. This paper presents a numerical study of the flow topologies of three-dimensional (3D) flows in a high pressure compressor stator blade row without and with boundary layer aspiration on the hub wall. The stator blade is representative of the first stage operating under transonic inlet conditions and the blade design encourages development of highly complex 3D flows. The blade has a small tip clearance. The computational fluid dynamics (CFD) studies show progressive increase of hub corner stall with the increase in incidence. Aspiration is implemented on the hub wall via a slot in the comer between the hub wall and the suction surface. The CFD studies show aspiration to be sensitive to the suction flow rate; lower rate leads to very complex flow struc- tures and increased level of losses whereas higher rate renders aspiration effective for control of hub comer separation. The flow topologies are studied by trace of skin friction lines on the walls. The nature of flow can be explained by the topological rules of closed separation. Furthermore, a deeper analysis is done for a particular case with advanced criterion to test the non-degeneracy of critical points in the flow field.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第5期541-549,共9页 中国航空学报(英文版)
关键词 high pressure compressor flow topologies three-dimensional flows boundary layer aspiration tip clearance high pressure compressor flow topologies three-dimensional flows boundary layer aspiration tip clearance
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参考文献10

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同被引文献29

  • 1周海,李秋实,陆亚钧.跨音风扇转子叶片抽吸气数值实验探索[J].航空动力学报,2004,19(3):408-412. 被引量:34
  • 2韩万今,吕红卫,芦文才,王仲奇.进口附面层厚度对大转角弯叶片损失的影响[J].工程热物理学报,1994,15(4):391-394. 被引量:10
  • 3南向谊,刘波,靳军,陈云永,侯为民.超声速压气机转子叶片吸力面抽气抑制附面层分离的机理[J].航空动力学报,2007,22(7):1093-1099. 被引量:16
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  • 8Reijnen D P. Experimental study of boundary layer suction in a transonic compressor[D]. Cambridge, Massachusetts: Massachusetts Institute of Technology, 1997.
  • 9SONG Yanping, CHEN Fu, YANG Jun, et al. A numericalinvestigation of boundary layer suction in compound lean compressor cascades[J]. Journal of Turbomachinery, 2006, 128(2) :357-366.
  • 10Gbadebo S A,Cumpsty N A, Hynes T P. Control of three- dimensional separations in axial compressors by tailored boundary layer suction [J]. Journal of Turbomachinery, 2008,130(1) :1-8.

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