EFFECT OF SOLIDITY ON NON-AXISYMMETRIC ENDWALL CONTOURING PERFORMANCE IN COMPRESSOR LINEAR CASCADES

被引:0
|
作者
Liu Xiwu [1 ]
Jin Donghai [1 ,2 ]
Gui Xingmin [1 ,2 ]
Liu Xiaoheng [1 ]
Guo Hanwen [1 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing, Peoples R China
[2] Collaborat Innovat Ctr Adv Aeroengine, Beijing, Peoples R China
基金
中国国家自然科学基金; 北京市自然科学基金;
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents both the computational and experimental results to assess the effectiveness of non-axisymmetric endwall contouring in linear cascades under different solidities. Endwalls were designed by geometric scaling of a prior optimized endwall. The results show that the total pressure loss can be reduced by the contoured endwall (CEW) under different solidities. The mechanism of the improvement of CEW is that the adverse pressure gradient (APG) has been reduced mainly through the groove configuration near the leading edge of the suction surface. Besides, the cross-passage pressure gradient (CPG) has also been reduced, which has the benefits to further suppress the corner separation. Moreover, there is an optimum range of the solidity for the CEW. For a lower solidity, the performance of the CEW at +7 degree incidence presents a rapid deterioration, due to the risk of flow separation near the mid-span, for a higher solidity, the profile loss can be more dominant.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] NON-AXISYMMETRIC ENDWALL CONTOURING IN A LINEAR COMPRESSOR CASCADE
    Ma, Yuchen
    Teng, Jinfang
    Zhu, Mingmin
    Qiang, Xiaoqing
    PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY CONFERENCE AND EXPOSITION, VOL 2A, PT I, 2020,
  • [2] Effective strategy of non-axisymmetric endwall contouring in a linear compressor cascade
    Ma, Yuchen
    Teng, Jinfang
    Zhu, Mingmin
    Qiang, Xiaoqing
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (08) : 1473 - 1487
  • [3] Effect of Camber on Non-axisymmetric End-wall Contouring Performance in Compressor Linear Cascades
    Guo, Hanwen
    Jin, Donghai
    Liu, Xiwu
    Wang, Bing
    Gui, Xinming
    2019 5TH INTERNATIONAL CONFERENCE ON ENVIRONMENTAL SCIENCE AND MATERIAL APPLICATION, 2020, 440
  • [4] Investigation of non-axisymmetric endwall contouring in a compressor cascade
    Xiwu Liu
    Donghai Jin
    Xingmin Gui
    Journal of Thermal Science, 2017, 26 : 490 - 504
  • [5] Investigation of Non-Axisymmetric Endwall Contouring in a Compressor Cascade
    LIU Xiwu
    JIN Donghai
    GUI Xingmin
    Journal of Thermal Science, 2017, 26 (06) : 490 - 503
  • [6] Investigation of Non-Axisymmetric Endwall Contouring in a Compressor Cascade
    Liu Xiwu
    Jin Donghai
    Gui Xingmin
    JOURNAL OF THERMAL SCIENCE, 2017, 26 (06) : 490 - +
  • [7] NON-AXISYMMETRIC ENDWALL CONTOURING IN A COMPRESSOR CASCADE WITH TIP GAP
    Varpe, Mahesh K.
    Pradeep, A. M.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
  • [8] Design optimization of non-axisymmetric endwall contouring in compressor cascade
    Zhao, Wei-Guang
    Jin, Dong-Hai
    Gui, Xing-Min
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2013, 34 (06): : 1047 - 1050
  • [9] Influence of the inlet boundary layer on non-axisymmetric endwall contouring effects in a linear compressor cascade
    Ma, Yuchen
    Teng, Jinfang
    Zhu, Mingmin
    Qiang, Xiaoqing
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2022, 236 (12) : 6530 - 6542
  • [10] Optimization design for counter-rotating compressor with non-axisymmetric endwall contouring
    Zhang, Peng
    Liu, Bo
    Cao, Zhi-Yuan
    Na, Zhen-Zhe
    Shi, Lei
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2014, 29 (11): : 2570 - 2578