Volume 35 Issue 11
Nov.  2020
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ZHANG Botao, LIU Bo, WANG Hejian. Impact of incidence angle on tip leakage flow control ,by endwall suction in a compressor cascade[J]. Journal of Aerospace Power, 2020, 35(11): 2400-2412. doi: 10.13224/j.cnki.jasp.2020.11.017
Citation: ZHANG Botao, LIU Bo, WANG Hejian. Impact of incidence angle on tip leakage flow control ,by endwall suction in a compressor cascade[J]. Journal of Aerospace Power, 2020, 35(11): 2400-2412. doi: 10.13224/j.cnki.jasp.2020.11.017

Impact of incidence angle on tip leakage flow control ,by endwall suction in a compressor cascade

doi: 10.13224/j.cnki.jasp.2020.11.017
  • Received Date: 2020-04-22
  • Publish Date: 2020-11-28
  • In order to reduce the tip leakage loss and improve the tip passage blockage caused by the tip leakage vortex, numerical simulation was conducted to investigate the flow control effect of suction scheme with endwall slot in flow direction on the tip leakage flow in a diffuser cascade. The impact of incidence angle on flow control effect was analysed emphatically. Results showed that the leakage vortex intensity and the leakage loss were reduced by the endwall suction scheme by directly controlling the development of the tip leakage flow. The influence of endwall suction on the cascade flow field at the design and negative incidence angles was limited to the vicinity of the blade tip. However, at a large incidence angle, suction can advance the boundary layer separation in the low span region, and the position of the vortex shedding on the suction surface of blade raised to about 70% span. Therefore, the overall impact of the endwall suction scheme on the cascade at a large incidence angle was determined by both the reduction of leakage loss and the increase of separation loss. With the suction flow rate of 07%, the overall total pressure loss coefficient of aspirated cascade decreased by about 90%, 108% and 68%, respectively, at the incidence angles of -8°, 0°and +4°, and increased by about 57% at the incidence angles of +8°.

     

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  • [1]
    MOORE R D.Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage[R].NASA-TP-2049,1982.
    [2]
    INOUE M,KUROUMARU M.Structure of tip clearance flow in an isolated axial compressor rotor[J].Journal of Turbomachinery,1989,111(3):250-256.
    [3]
    LANGE M,ROLFES M,MAILACH R,et al.Periodic unsteady tip clearance vortex development in a low-speed axial research compressor at different tip clearances[J].Journal of Turbomachinery,2018,140(3):0310051-03100510.
    [4]
    BESELT C,ECK M,PEITSCH D.Three-dimensional flow field in highly loaded compressor cascade[J].Journal of Turbomachinery,2014,136(10):1010071-10100710.
    [5]
    茅晓晨.轴流压气机内部流动分离和叶尖泄漏流抽吸控制策略及机理的研究[D].西安:西北工业大学,2018. MAO Xiaochen.Investigation on control strategies and mechanisms of aspiration in controlling the flow separation and tip leakage flow for axial flow compressors[D].Xian:Northwestern Polytechnical University,2018.(in Chinese)
    [6]
    DENTON J D.Loss mechanisms in turbomachines[J].Journal of Turbomachinery,1993,115(4):621-656.
    [7]
    SUDER K L.Blockage development in a transonic,axial compressor rotor[J].Journal of Turbomachinery,1998,120(3):465-476.
    [8]
    韩少冰,钟兢军.叶尖小翼对跨声速压气机转子变工况性能的影响[J].航空动力学报,2016,31(3):647-658. HAN Shaobing,ZHONG Jingjun.Influence of blade tip winglet on the off-design performance of a transonic compressor rotor[J].Journal of Aerospace Power,2016,31(3):647-658.(in Chinese)
    [9]
    吕从鹏,姜斌,张寅豹,等.跨声速轴流压气机转子弯掠控制机理[J].航空动力学报,2017,32(4):1001-1011. Lv Congpeng,JIANG Bin,ZHANG Yanbao,et al.Controlling mechanisms of bowed and swept of rotor in transonic axial compressor[J].Journal of Aerospace Power,2017,32(4):1001-1011.(in Chinese)
    [10]
    HORN J R A,LOUGHERY R J,TRAMM P C.Single stage experimental evaluation of boundary layer blowing and bleed techniques for high lift stator blades[R].NASA-CR-54573,1971.
    [11]
    郭爽,陆华伟,宋彦萍,等.吸力面附面层抽吸在三维高负荷扩压叶栅中的作用机制[J].航空动力学报,2014,29(11):2529-2536. GUO Shuang,LU Huawei,SONG Yanping,et al.Mechanism of suction surface boundary layer suction in three-dimensional high loaded diffuser cascades[J].Journal of Aerospace Power,2014,29(11):2529-2536.(in Chinese)
    [12]
    赵振国,周正贵,陶胜.吸附式压气机转子叶片气动优化设计[J].航空动力学报,2015,30(3):726-735. ZHAO Zhenguo,ZHOU Zhenggui,TAO Sheng.Aerodynamic optimization design of an aspirated compressor rotor blade[J].Journal of Aerospace Power,2015,30(3):726-735.(in Chinese)
    [13]
    SACHDEVA A,LEBOEUF F.Topological studies of three-dimensional flows in a high pressure compressor stator blade row without and with boundary layer aspiration[J].Chinese Journal of Aeronautics,2011,24(5):541-549.
    [14]
    张博涛,刘波,赵航.叶顶抽吸对叶栅间隙泄漏流动的控制研究[J].推进技术,2020,41(8):1701-1709. ZHANG Botao,LIU Bo,ZHAO Hang.Effects of blade tip suction on cascade gap leakage flow[J].Journal of Propulsion Technology,2020,41(8):1701-1709.(in Chinese)
    [15]
    陆华伟,韩兴伟,张永超,等.机匣周向槽抽吸影响跨声速压气机转子性能的数值研究[J].工程热物理学报,2017,38(6):1191-1195. LU Huawei,HAN Xingwei,ZHANG Yongchao,et al.Numerical simulation of transonic compressor rotor performance affected by the casing circumferential groove suction[J].Journal of Engineering Thermophysics,2017,38(6):1191-1195.(in Chinese)
    [16]
    MAO Xiaochen,LIU Bo,ABDUL R,et al.Numerical investigation into the effects of casing aspiration on the overall performance and flow unsteadiness in a counter-rotating axial flow compressor[J].Aerospace Science and Technology,2018,78:671-681.
    [17]
    ZHANG Botao,LIU Bo,HAN Changfu,et al.Control and entropy analysis of tip leakage flow for compressor cascade under different clearance sizes with endwall suction[J].Entropy,2020,22(2):128.1-128.17.
    [18]
    MAO Xiaochen,LIU Bo,TANG Tianquan.Effect of casing aspiration on the tip leakage flow in the axial flow compressor cascade[J].Journal of Power and Energy,2018,232(3):225-239.
    [19]
    MAO Xiaochen,LIU Bo,TANG Tianquan.Control of tip leakage flow in axial flow compressor cascade by suction on the blade tip[J].Journal of Applied Fluid Mechanics,2018,11(1):137-149.
    [20]
    EVANS S,HODSON H,HYNES T,et al.Flow control in a compressor cascade at high incidence[J].Journal of Propulsion and Power,2010,26(4):828-836.
    [21]
    STORER J A,CUMPSTY N A.Tip leakage flow in axial compressors[J].Journal of Turbomachinery,1991,113(2):252-259.
    [22]
    HUNT J C R,WRAY A A,MOIN P.Eddies,streams,and convergence zones in turbulent flows[R].NASA-N89-24555,1988.
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