Interaction of shock/boundary layers in a scramjet inlet

被引：0
|
作者：
Wang, Ge [1 ]
Jiang, Xu-Xu [1 ]
Tang, Qiang [1 ]
机构：
[1] Department of Aerospace Engineering, Harbin Engineering University, Harbin 150001, China
来源：
Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University | 2007年 / 28卷 / 11期
关键词：
16;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：1206 / 1212
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