Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings

被引：0
|
作者：
Ogawa, H. [1 ,3 ,4 ]
Babinsky, H. [1 ,4 ,5 ]
M. Patzold [2 ,6 ]
T. Lutz [2 ,4 ,6 ]
机构：
[1] University of Cambridge, Cambridge, CB2 1PZ, United Kingdom
[2] University of Stuttgart, D-70550 Stuttgart, Germany
[3] Aerodynamics Laboratory, Department of Engineering, Trumpington Street, United Kingdom
[4] AIAA
[5] Department of Engineering, Trumpington, United Kingdom
[6] Aerodynamics Group, Department of Aerodynamics and Gas Dynamics
来源：
AIAA Journal | 2008年 / 46卷 / 06期
关键词：
Drag reduction;
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：1442 / 1452
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