Rotating stall stability theory of the transonic axial compressors/fans

被引：0
|
作者：
Yu, Wei-Wei [1 ]
Sun, Xiao-Feng [1 ]
机构：
[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2005年 / 20卷 / 06期
关键词：
Aerospace propulsion system - Rotating stall - Stability model - Winding number integral method;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1018 / 1027
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