Volume 33 Issue 4
Apr.  2018
Turn off MathJax
Article Contents
Effects of moving endwall on tip leakage flowin compressor cascade[J]. Journal of Aerospace Power, 2018, 33(4): 803-811. doi: 10.13224/j.cnki.jasp.2018.04.005
Citation: Effects of moving endwall on tip leakage flowin compressor cascade[J]. Journal of Aerospace Power, 2018, 33(4): 803-811. doi: 10.13224/j.cnki.jasp.2018.04.005

Effects of moving endwall on tip leakage flowin compressor cascade

doi: 10.13224/j.cnki.jasp.2018.04.005
  • Received Date: 2016-11-02
  • Publish Date: 2018-04-28
  • A numerical simulation was carried out to investigate the effect of the moving endwall on the tip leakage flow structure in a compressor cascade with different tip clearances. A detailed comparison of leakage flows loss, trajectory, size and mass flow rate, as well as the tip leakage flow features and its interaction with the mainstream, was conducted. Results showed that the moving endwall led to more leakage mass flow through the gap. The region of the tip leakage vortex was flattened away from the blade suction side. The interaction between the mainstream and the tip leakage flow was weakened. The structure of the vortexes inside the passage was altered. In the small clearance cases, the main effects of the moving endwall were focused on the near wall region. While in the large clearance cases, the moving endwall clearly suppressed the tip separation vortex, thus influencing the velocity distribution of the whole clearance, and further impacting the shear between the mainstream and the tip leakage flow.

     

  • loading
  • [1]
    DENTON J D.Loss mechanisms in turbomachines[J].Journal of Turbomachinery,1993,115(4):621-656.
    [2]
    DAY I J.Stall,surge,and 75 years of research[J].Journal of Turbomachinery,2016,138(1):1-9.
    [3]
    INOUE M,KUROUMARU M.Structure of tip clearance flow in an isolated axial compressor rotor[J].Journal of Turbomachinery,1989,111(3):250-256.
    [4]
    STORER J A,CUMPSTY N A.Tip leakage flow in axial compressors[J].Journal of Turbomachinery,1991,113(2):252-259.
    [5]
    KANG S,HIRSCH C.Experimental study on the three-dimensional flow within a compressor cascade with tip clearance:Part Ⅰ velocity and pressure fields[J].Journal of Turbomachinery,1993,115(3):435-443.
    [6]
    于宏军,刘宝杰,刘火星,等.近失速状态下压气机转子叶尖旋涡流动研究[J].航空学报,2004,25(1):9-15.YU Hongjun,LIU Baojie,LIU Huoxing,et al.Investigation of tip vortex in compressor at near stall condition[J].Acta Aeronautica et Astronautica Sinica,2004,25(1):9-15.(in Chinese)
    [7]
    LIU Yangwei,YU Xianjun,LIU Baojie.Turbulence models assessment for large-scale tip vortices in an axial compressor rotor[J].Journal of Propulsion and Power,2008,24(1):15-25.
    [8]
    KOCH C C.Stalling pressure rise capability of axial flow compressor stages[J].Journal of Engineering for Gas Turbines and Power,1981,103(4):645-656.
    [9]
    WISLER D C.Core compressor exit stage study:Volume 4 data and performance report for the best stage configuration[R].NASA-CR-165357,1981.
    [10]
    BAGHDADI S.Modeling tip clearance effects in multi-stage axial compressors[J].Journal of Turbomachinery,1996,118(4):697-705.
    [11]
    KANG S,HIRSCH C.Numerical simulation of three-dimensional viscous flow in a linear compressor cascade with tip clearance[J].Journal of Turbomachinery,1996,118(3):492-502.
    [12]
    邓向阳,张宏武,陈乃兴,等.叶顶间隙大小和壁面相对运动对低速轴流压气机孤立转子性能的影响[J].工程热物理学报,2004,25(5):773-775.DENG Xiangyang,ZHANG Hongwu,CHEN Naixing,et al.The effect of tip clearance gap size and wall rotation on the performance of a low-speed axial compressor rotor [J].Journal of Engineering Thermophysics,2004,25(5):773-775.(in Chinese)
    [13]
    吴艳辉,楚武利,刘志伟.移动壁对压气机叶栅间隙流动的影响[J].航空动力学报,2006,21(1):112-118.WU Yanhui,CHU Wuli,LIU Zhiwei.Influence of moving end-wall on tip clearance flow in an axial-flow compressor cascade[J].Journal of Aerospace Power,2006,21(1):112-118.(in Chinese)
    [14]
    韩少冰,钟兢军,严红明.端壁相对运动对压气机叶栅间隙流场影响的数值模拟[J].动力工程学报,2011,31(4):257-262.HAN Saobing,ZHONG Jingjun,YAN Hongming.Influence of endwall relative movement on tip clearance flow in a compressor cascade[J].Journal of Chinese Society of Power Engineering,2011,31(4):257-262.(in Chinese)
    [15]
    MUTHANNA C.Flowfield downstream of a compressor cascade with tip leakage[D].Virginia:Virginia Polytechnic Institute and State University,1998.
    [16]
    WANG Y.Tip leakage flow downstream of a compressor cascade with moving end wall[D].Virginia:Virginia Virginia Polytechnic Institute and State University,2000.
    [17]
    HOU Jiexuan,LIU Yangwei,ZHONG Luyang,et al.Turbulence models assessment for tip leakage flow through a linear compressor cascade[C]∥Proceedings of 2015 Asian-Pacific.Jeju Island,Korea:the Society for Aerospace System Engineering,2015:500-504.
    [18]
    HUNT J C R.Eddies stream,and convergence zones in turbulent flows[R].California:Center for Turbulence Research,1988:193-208.
    [19]
    SAKULKAEW S.Effects of rotor tip clearance on an embedded compressor stage performance[D].Massachusetts:Massachusetts Institute of Technology,2012.
    [20]
    LAKSHMINARAYANA B.Fluid dynamics and heat transfer of turbomachinery[M].New York:Wiley,1996.
    [21]
    TALLMAN J,LAKSHMINARAYANA B.Numerical simulation of tip leakage flows in axial flow turbines,with emphasis on flow physics:Part Ⅰ effect of tip clearance height[J].Journal of Turbomachinery,2001,123(2):314-323.
    [22]
    TALLMAN J,LAKSHMINARAYANA B.Numerical simulation of tip leakage flows in axial flow turbines,with emphasis on flow physics:Part Ⅱ effect of outer casing relative motion[J].Journal of Turbomachinery,2001,123(2):817-824.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1181) PDF downloads(956) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return