Hypersonic shockwave/turbulent boundary-layer interactions on a porous surface

被引:0
|
作者
Hanna, R.L. [1 ]
机构
[1] North Carolina State univ., Raleigh, United States
来源
AIAA journal | 1995年 / 33卷 / 10期
关键词
Boundary layers - Hypersonic flow - Turbulent flow;
D O I
暂无
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
The passive control of hypersonic shock/boundary-layer interactions is numerically studied. A previously developed Navier-Stokes code is applied, after modifications to the code to account for passive control have been implemented.
引用
收藏
页码:1977 / 1979
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