Investigation of improving the aerodynamic performance in highly-loaded compressor cascade by boundary layer suction holes

被引：0
|
作者：
Ding, Jun [1 ]
Chen, Shao-Wen [1 ]
Xu, Hao [1 ]
Han, Dong [1 ]
Wang, Song-Tao [1 ]
机构：
[1] Engine Aerodynamics Research Center, Harbin Institute of Technology, Harbin 150001, China
来源：
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics | 2013年 / 34卷 / 12期
关键词：
Aero-dynamic performance - Aerodynamic parameters - Boundary layer suction - Compressor cascade - Experimental investigations - Numerical results - Suction hole - Suction surfaces;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2237 / 2242
相关论文
共 50 条
  • [21] Effects of Boundary Layer Suction on Aerodynamic Performance in a High-load Compressor Cascade
    Guo Shuang
    Chen Shaowen
    Song Yanping
    Song Yufei
    Chen Fu
    CHINESE JOURNAL OF AERONAUTICS, 2010, 23 (02) : 179 - 186
  • [22] EFFECT OF BOUNDARY LAYER SUCTION ON AERODYNAMIC PERFORMANCE OF HIGH-TURNING COMPRESSOR CASCADE
    Zhang, Longxin
    Chen, Shaowen
    Xu, Hao
    Ding, Jun
    Wang, Songtao
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 6A, 2013,
  • [23] Aerodynamic performance of high-turning curved compressor cascade with boundary layer suction
    School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
    J. Harbin Inst. Technol., 2007, 3 (341-348):
  • [24] Study of Shock Wave Control by Suction & Blowing on a Highly-loaded Transonic Compressor Cascade
    Wang, Yangang
    Rao, Arvind G.
    Eitelberg, Georg
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2013, 30 (01) : 79 - 90
  • [25] EXPERIMENTAL AND NUMERICAL INVESTIGATION OF CORNER STALL IN A HIGHLY-LOADED COMPRESSOR CASCADE
    Zhang, Yanfeng
    Mahallati, Ali
    Benner, Michael
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
  • [26] Numerical investigation of endwall boundary layer removal on highly-loaded axial compressor blade rows
    Guemmer, V.
    Goller, M.
    Swoboda, M.
    Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 281 - 290
  • [27] Numerical and Experimental Study of Separation Control by Boundary Layer Aspiration in a Highly-Loaded Axial Compressor Cascade
    Mao, X.
    Liu, B.
    Yuan, F.
    JOURNAL OF APPLIED FLUID MECHANICS, 2018, 11 (02) : 433 - 446
  • [28] Corner Separation Control by Boundary Layer Suction Applied to a Highly Loaded Axial Compressor Cascade
    Liu, Yangwei
    Sun, Jinjing
    Lu, Lipeng
    ENERGIES, 2014, 7 (12): : 7994 - 8007
  • [29] Effect of combined boundary layer suction on the separation control in a highly loaded transonic compressor cascade
    Li, Bai
    Mu, Guangyuan
    Luo, Lei
    Du, Wei
    Zhou, Xun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2024, 238 (02) : 217 - 231
  • [30] CONTROL OF FLOW SEPARATIONS IN COMPRESSOR CASCADE BY BOUNDARY LAYER SUCTION HOLES IN SUCTION SURFACE
    Ding, Jun
    Chen, Shaowen
    Xu, Hao
    Sun, Shijun
    Wang, Songtao
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 6A, 2013,
12345