Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a M∞ =  9 hypersonic flow

被引：0
作者：
Z. M. Hu
R. S. Myong
Y. R. Yang
T. H. Cho
机构：
[1] Gyeongsang National University,Department of Mechanical and Aerospace Engineering, Research Center for Aircraft Parts Technology
来源：
Theoretical and Computational Fluid Dynamics | 2010年 / 24卷
关键词：
Shock/shock interaction; Hypersonic; Double wedge; Hysteresis; Oscillation;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Shock polar analysis as well as 2-D numerical computation technique are used to illustrate a diverse flow topology induced by shock/shock interaction in a M∞ = 9 hypersonic flow. New flow features associated with inviscid shock wave interaction on double-wedge-like geometries are reported in this study. Transition of shock interaction, unsteady oscillation, and hysteresis phenomena in the RR ↔ MR transition, and the physical mechanisms behind these phenomena are numerically studied and analyzed.
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页码：551 / 564
页数：13
相关论文
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