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
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页码：2183 / 2188
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