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：
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中图分类号：
学科分类号：
摘要：
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页码：2237 / 2242
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