Effects of rotating inlet distortion on aerodynamic stability and stall inception of axial-flow compressor

被引：0
|
作者：
Zhang, Huan [1 ]
Hu, Jun [1 ]
Tu, Bao-Feng [1 ]
Wang, Zhi-Qiang [1 ]
Zhao, Yong [1 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2008年 / 23卷 / 11期
关键词：
Aerodynamic stability;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2095 / 2100
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