Subsonic compressor plane cascade experiment at low Reynolds number

被引：0
|
作者：
机构：
[1] Ling, Dai-Jun
[2] Wang, Hui
[3] Ma, Chang-You
来源：
Ling, D.-J. | 2013年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 28期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Wakes
引用
收藏
相关论文
共 50 条
  • [1] INVESTIGATION OF LOW REYNOLDS NUMBER EXPERIMENT AND NUMERICAL SIMULATION ON COMPRESSOR CASCADE
    Hou, Anping
    Shan, Shujun
    Wu, Yu
    Ling, Daijun
    Jiang, Zhengli
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2011, VOL 6, PTS A AND B, 2012, : 57 - 68
  • [2] Aerodynamic Optimization and Flow Mechanism for a Compressor Cascade at Low Reynolds Number
    Li, Lin
    Zhang, Jianshe
    Chen, Caiyan
    Tan, Wei
    Zhang, Yanfeng
    JOURNAL OF THERMAL SCIENCE, 2025, 34 (01) : 92 - 109
  • [3] Influence of Incidence Angle on Compressor Cascade Performance at Low Reynolds Number
    Du, W.
    Peng, M.
    Zhu, J.
    Lorenzini, G.
    JOURNAL OF ENGINEERING THERMOPHYSICS, 2022, 31 (01) : 50 - 63
  • [4] Influence of Incidence Angle on Compressor Cascade Performance at Low Reynolds Number
    W. Du
    M. Peng
    J. Zhu
    G. Lorenzini
    Journal of Engineering Thermophysics, 2022, 31 : 50 - 63
  • [5] Aerodynamic Optimization and Flow Mechanism for a Compressor Cascade at Low Reynolds Number
    LI Lin
    ZHANG Jianshe
    CHEN Caiyan
    TAN Wei
    ZHANG Yanfeng
    Journal of Thermal Science, 2025, 34 (01) : 92 - 109
  • [6] EXPERIMENTAL CASCADE PERFORMANCE OF NACA COMPRESSOR PROFILES AT LOW REYNOLDS-NUMBER
    ROBERTS, WB
    JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1975, 97 (03): : 454 - 459
  • [7] Flow and Loss Mechanism of High Subsonic Compressor Airfoil under Low Reynolds Number Conditions
    Wang M.-Y.
    Zhao S.-F.
    Li Z.-L.
    Lu X.-G.
    Zhang Y.-F.
    Zhu J.-Q.
    Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (05): : 1046 - 1054
  • [8] Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number
    Mingyang WANG
    Chengwu YANG
    Ziliang LI
    Shengfeng ZHAO
    Yanfeng ZHANG
    Xin'gen LU
    Chinese Journal of Aeronautics, 2021, 34 (03) : 71 - 81
  • [9] Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number
    Mingyang WANG
    Chengwu YANG
    Ziliang LI
    Shengfeng ZHAO
    Yanfeng ZHANG
    Xingen LU
    Chinese Journal of Aeronautics, 2021, (03) : 71 - 81
  • [10] Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number
    WANG, Mingyang
    YANG, Chengwu
    LI, Ziliang
    ZHAO, Shengfeng
    ZHANG, Yanfeng
    LU, Xin'gen
    Chinese Journal of Aeronautics, 2021, 34 (03): : 71 - 81
12345