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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