Effect of squealer tip geometry on rotor blade aerodynamic performance

被引：14
|
作者：
Gao, Jie [1 ]
Zheng, Qun [1 ]
机构：
[1] College of Power and Energy Engineering, Harbin Engineering University, Harbin 150001, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2013年 / 34卷 / 02期
关键词：
Angle of attack;
D O I：
10.7527/S1000-6893.2013.0025
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：218 / 226
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