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

页码：1018 / 1027

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