The reflection of asymmetric shock waves in steady flows: a numerical investigation

被引:39
作者
Ivanov, MS [1 ]
Ben-Dor, G
Elperin, T
Kudryavtsev, AN
Khotyanovsky, DV
机构
[1] Russian Acad Sci, Inst Theoret & Appl Mech, Computat Aerodynam Lab, Siberian Div, Novosibirsk 630090, Russia
[2] Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, IL-84105 Beer Sheva, Israel
关键词
D O I
10.1017/S0022112002001799
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The theoretical study and experimental investigation of the reflection of asymmetric shock waves in steady flows reported by Li et al. (1999) are complemented by a numerical simulation. All the findings reported in both the theoretical study and the experimental investigation were also evident in the numerical simulation. In addition to weak regular reflection and Mach reflection wave configurations, strong regular reflection and inverse-Mach reflection wave configurations were recorded numerically. The hysteresis phenomenon, which was hypothesized in the course of the theoretical study and then verified in the experimental investigation, was also observed in the numerical simulation.
引用
收藏
页码:71 / 87
页数:17
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