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
  • [31] A Combined Numerical and Experimental Study of the Effect of Non-Axisymmetric Contouring on Performance and Film Cooling Behavior of a Rotating Turbine Endwall
    Lu, K.
    Rezasoltani, M.
    Schobeiri, M. T.
    Han, J. C.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5B, 2014,
  • [32] Effects of inlet distortion and non-axisymmetric endwall modeling on performance of compact compressor intermediate duct
    Mao, Xiaochen
    Zhao, Lei
    Gao, Limin
    Liu, Tantao
    Wu, Yu
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (01):
  • [33] Investigation of non-axisymmetric endwall contouring in a high loaded turbine stator cascade
    Du, Zhengshuai
    Cai, Le
    Chen, Yingjie
    Wang, Songtao
    Tang, Hongfei
    Zeng, Jun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2024, 238 (05) : 818 - 837
  • [34] MEASUREMENTS OF SECONDARY LOSSES IN A TURBINE CASCADE WITH THE IMPLEMENTATION OF NON-AXISYMMETRIC ENDWALL CONTOURING
    Knezevici, D. C.
    Sjolander, S. A.
    Praisner, T. J.
    Allen-Bradley, E.
    Grover, E. A.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 1405 - 1417
  • [35] Application of 3D blading and non-axisymmetric endwall in a transonic compressor
    Zhang, Peng
    Liu, Bo
    Mao, Xiao-Chen
    Yang, Xi-Qiong
    Cheng, Hao
    Tuijin Jishu/Journal of Propulsion Technology, 2016, 37 (02): : 250 - 257
  • [36] Numerical investigation of the influence of non-axisymmetric hub contouring on the performance of a shrouded axial compressor stator
    F. Heinichen
    V. Gümmer
    A. Plas
    H.-P. Schiffer
    CEAS Aeronautical Journal, 2011, 2 (1-4) : 89 - 98
  • [37] Application of non-axisymmetric endwall contouring to conventional and high-lift turbine airfoils
    Praisner, T. J.
    Allen-Bradley, E.
    Grover, E. A.
    Knezevici, D. C.
    Sjolander, S. A.
    Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 653 - 661
  • [38] Numerical Investigation of the Effect of Purge Flow on Aerodynamic Performance and Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring
    Schobeiri, M. T.
    Lu, K.
    Han, J. C.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 413 - 423
  • [39] Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring
    Rezasoltani, M.
    Schobeiri, M. T.
    Han, J. C.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,
  • [40] ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART I: PRINCIPAL CASCADE DESIGN AND COMPRESSOR APPLICATION
    Dorfner, Christian
    Hergt, Alexander
    Nicke, Eberhard
    Moenig, Reinhard
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 113 - 120