Numerical simulation of the aerodynamics performance of swept and curved blade on the compressor stator

被引：0
|
作者：
Feng, Xiu-Lian [1 ]
Jin, Dong-Hai [1 ]
Gui, Xing-Min [1 ]
机构：
[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2009年 / 24卷 / 10期
关键词：
Compendex;
D O I：
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中图分类号：
学科分类号：
摘要：
Flow separation
引用
收藏
页码：2338 / 2343
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