Aerodynamic design principle and verification for subsonic axial-flow compressor with low reaction based on enhanced axial velocity at rotor outlet

被引：0
|
作者：
Hu, Ying-Jiao [1 ]
Wang, Song-Tao [1 ]
机构：
[1] School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2014年 / 29卷 / 03期
关键词：
Axial-flow compressors;
D O I：
10.13224/j.cnki.jasp.2014.03.032
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：708 / 718
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