Low reynolds number effects in a mach 3 shock/turbulent-boundary-layer interaction

被引：0
|
作者：
Ringuette, M. [1 ,2 ,3 ]
Wu, M. [1 ,2 ,3 ]
Martín, M.P. [1 ,2 ,3 ]
机构：
[1] Princeton University, Princeton, NJ 08544, United States
[2] Mechanical and Aerospace Engineering Department
[3] AIAA
来源：
AIAA Journal | 2008年 / 46卷 / 07期
关键词：
11;
D O I：
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学科分类号：
摘要：
Journal article (JA)
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页码：1884 / 1887
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