Serpentine inlet performance enhancement using vortex generator based flow control

被引：6
|
作者：
Sun, Shu [1 ,2 ]
Guo, Rong-Wei [1 ]
机构：
[1] Internal Flow Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
[2] Nanjing University of Aeronautical and Astronautics
来源：
Chinese Journal of Aeronautics | 2006年 / 19卷 / 01期
关键词：
15;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：10 / 17
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