Numerical investigation of interaction between asymmetric crossing shock waves/turbulence boundary layer

被引：0

作者：

Zhao, Hui-Yong ^{[1
,2
]}

Lei, Bo ^{[1
]}

Le, Jia-Ling ^{[2
]}

机构：

[1] Traction Power State Key Laboratory, Southwest Jiaotong University, Chengdu 610031, China

[2] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China

来源：

Hangkong Dongli Xuebao/Journal of Aerospace Power | 2009年 / 24卷 / 10期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：2183 / 2188

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