期刊
AEROSPACE SCIENCE AND TECHNOLOGY
卷 15, 期 1, 页码 45-52出版社
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2010.06.001
关键词
Shock wave; Boundary layer; Separation control; Streamwise vortices; Air-jet vortex generator
Control of shock wave and boundary layer interaction continues to attract a lot of attention. In recent decades several methods of interaction control have been investigated in particular. The research has mostly concerned solid (vane type) vortex generators and transpiration methods of suction and blowing. In our investigations it is proposed to use air jets to generate streamwise vortices (AJVG) for interaction control. The effectiveness of air-jet vortex generators in controlling separation has been proved in our previous research. The present paper focuses on the influence of AJVGs of various parameters on the separation region. The results presented here concern experimental investigations and provide new guidelines for the design of AJVGs to obtain more effective separation control. (C) 2010 Elsevier Masson SAS. All rights reserved.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据