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
  • [41] THE AERODYNAMIC INTERACTION OF SEAL LEAKAGE AND MAINSTREAM FLOWS IN A COMPRESSOR CASCADE WITH NON-AXISYMMETRIC ENDWALL
    Li, Jian
    Qiang, Xiaoqing
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12A, 2024,
  • [42] INFLUENCE OF PURGE FLOW INJECTION ON THE PERFORMANCE OF AN AXIAL TURBINE WITH THREE-DIMENSIONAL AIRFOILS AND NON-AXISYMMETRIC ENDWALL CONTOURING
    Schaeflein, Lukas
    Janssen, Johannes
    Brandies, Henri
    Jeschke, Peter
    Behre, Stephan
    PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 10B, 2022,
  • [43] On- and off-design performance of a model rotating turbine with non-axisymmetric endwall contouring and a comparison to cascade data
    Snedden, G.
    Dunn, D.
    Ingram, G.
    AERONAUTICAL JOURNAL, 2018, 122 (1250): : 646 - 665
  • [44] Flow physics of highly loaded tandem compressor cascade with non-axisymmetric endwall profiling
    Cao, Zhiyuan
    Guo, Wei
    Song, Cheng
    Liu, Bo
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2021, 235 (05) : 931 - 943
  • [45] Influence of Purge Flow Injection on the Performance of an Axial Turbine With Three-Dimensional Airfoils and Non-Axisymmetric Endwall Contouring
    Schaeflein, Lukas
    Janssen, Johannes
    Brandies, Henri
    Jeschke, Peter
    Behre, Stephan
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (06):
  • [46] Effect of non-axisymmetric contouring on performance and film cooling of a rotating turbine endwall subjected to the secondary air purge: A combined numerical and experimental study
    Schobeiri, M. T.
    Lu, K.
    Rezasoltani, M.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2015, 229 (08) : 813 - 831
  • [47] Effect of three non-axisymmetric stator schemes on compressor performance with distorted inlet
    Fu, Wenguang
    Sun, Peng
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (10) : 2044 - 2056
  • [48] Aero-thermal optimization of a gas turbine blade endwall with non-axisymmetric contouring and purge flow
    Tao, Zhi
    Guo, Zhendong
    Yu, Boyang
    Song, Liming
    Li, Jun
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2021, 178
  • [49] COMPUTATIONAL PREDICTIONS OF HEAT TRANSFER AND FILM-COOLING FOR A TURBINE BLADE WITH NON-AXISYMMETRIC ENDWALL CONTOURING
    Lynch, Stephen P.
    Thole, Karen A.
    Kohli, Atul
    Lehane, Christopher
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 4, PTS A AND B, 2010, : 1641 - 1653
  • [50] INVESTIGATION OF 3D BLADING AND NON-AXISYMMETRIC HUB ENDWALL CONTOURING TO A DUAL-STAGE COUNTER-ROTATING COMPRESSOR IN MULTISTAGE ENVIRONMENT
    Zhang, Peng
    Liu, Bo
    Zhang, Guochen
    Na, Zhenzhe
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,