Non-symmetrical boundary layer suction in a compressor cascade

被引：0
|
作者：
Problem zasysania w niesymetrycznej warstwie przyściennej kaskady sprężarki
机构：
[1] Liesner, Karsten
[2] Meyer, Robert
[3] Schulz, Sebastian
来源：
Liesner, K. (karsten.liesner@dlr.de) | 2012年 / Polish Society of Theoretical and Allied Mechanics卷 / 50期
关键词：
Boundary layers;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] 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
  • [2] 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
  • [3] 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,
  • [4] Control of Corner Separation in a Linear Highly Loaded Compressor Cascade by Boundary Layer Suction
    Liu, Yangwei
    Sun, Jinjing
    Lu, Lipeng
    FLUID-STRUCTURE-SOUND INTERACTIONS AND CONTROL, 2016, : 307 - 311
  • [5] Effect of Boundary Layer Suction on the Corner Separation in a Highly Loaded Axial Compressor Cascade
    Liang, Tian
    Liu, Bo
    Spence, Stephen
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 143 (06):
  • [6] 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,
  • [7] EFFECT OF BOUNDARY LAYER SUCTION ON THE CORNER SEPARATION IN A HIGHLY LOADED AXIAL COMPRESSOR CASCADE
    Liang, Tian
    Liu, Bo
    Spence, Stephen
    PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY CONFERENCE AND EXPOSITION, VOL 2A, PT I, 2020,
  • [8] Effects of boundary layer suction on the flow and load of highly-loaded compressor cascade
    Energy Science and Engineering School, Harbin Institute of Technology, Harbin 150001, China
    Kung Cheng Je Wu Li Hsueh Pao, 2009, 9 (1479-1481):
  • [9] 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
  • [10] Control of Corner Separation to Enhance Stability in a Linear Compressor Cascade by Boundary Layer Suction
    Sun Jinjing
    Liu Yangwei
    Lu Lipeng
    Wang Qiuhui
    3RD INTERNATIONAL SYMPOSIUM ON AIRCRAFT AIRWORTHINESS (ISAA 2013), 2014, 80 : 380 - 391
12345