Experimental investigation on the suction surface boundary layer separation of a low-speed compressor cascade

被引：0
|
作者：
Lei, Zhi-Jun [1 ,2 ]
Wang, Ming-Jie [1 ,2 ]
Zhu, Jun-Qiang [1 ]
机构：
[1] Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
[2] Graduate University, Chinese Academy of Sciences, Beijing 100190, China
来源：
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics | 2008年 / 29卷 / 11期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1839 / 1843
相关论文
共 50 条
  • [31] NON-SYMMETRICAL BOUNDARY LAYER SUCTION IN A COMPRESSOR CASCADE
    Liesner, Karsten
    Meyer, Robert
    Schulz, Sebastian
    JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2012, 50 (02) : 455 - 472
  • [32] BOUNDARY LAYER CONTROL IN A COMPRESSOR CASCADE USING DISTRIBUTED SUCTION
    Chakraborthy, Utpal
    Pradeep, A. M.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 149 - 155
  • [33] Energy loss in a low-speed compressor cascade with dissipation function
    Tian, Simeng
    Wu, Yun
    Zhang, Haideng
    Li, Yinghong
    Li, Jun
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2015, 36 (10): : 3249 - 3262
  • [34] ENDWALL BOUNDARY LAYER DEVELOPMENT IN A MULTISTAGE LOW-SPEED COMPRESSOR WITH TANDEM STATOR VANES
    Hopfinger, Michael
    Guemmer, Volker
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2A, 2021,
  • [35] Experimental Investigation of Effects of Distributed Riblets on Aerodynamic Performance of a Low-speed Compressor
    Ma Hongwei
    Wei Wei
    JOURNAL OF THERMAL SCIENCE, 2013, 22 (06) : 592 - 599
  • [36] Experimental Investigation of Effects of Distributed Riblets on Aerodynamic Performance of a Low-speed Compressor
    MA Hongwei
    WEI Wei
    JournalofThermalScience, 2013, 22 (06) : 592 - 599
  • [37] Experimental investigation of the tip leakage flow in a low-speed multistage axial compressor
    Li, Jun
    Hu, Jun
    Zhang, Chenkai
    SCIENCE PROGRESS, 2020, 103 (03)
  • [38] Experimental investigation of effects of distributed riblets on aerodynamic performance of a low-speed compressor
    Hongwei Ma
    Wei Wei
    Journal of Thermal Science, 2013, 22 : 592 - 599
  • [39] Investigation of improving the aerodynamic performance in highly-loaded compressor cascade by boundary layer suction holes
    Ding, Jun
    Chen, Shao-Wen
    Xu, Hao
    Han, Dong
    Wang, Song-Tao
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2013, 34 (12): : 2237 - 2242
  • [40] Experimental investigation on evolution characteristics of high- and low-speed streaks in supersonic turbulent boundary layer
    Han, Junhao
    He, Lin
    Wu, Zhengbang
    AIP ADVANCES, 2022, 12 (11)
12345