冲击波
马赫反射
马赫数
高超音速
楔形(几何)
物理
休克(循环)
高超音速流动
机械
反射(计算机编程)
斜激波
流量(数学)
横截面
弓激波(空气动力学)
计算
马赫波
经典力学
光学
数学
计算机科学
工程类
内科学
算法
医学
结构工程
程序设计语言
作者
Zongmin Hu,R.S. Myong,M. S. Kim,T. H. Cho
标识
DOI:10.1017/s0022112008004837
摘要
In this paper, the regular reflection (RR) to Mach reflection (MR) transition of asymmetric shock waves is theoretically studied by employing the classical two- and three-shock theories. Computations are conducted to evaluate the effects of expansion fans, which are inherent flow structures in asymmetric reflection of shock waves, on the RR → MR transition. Comparison shows good agreement among the theoretical, numerical and experimental results. Some discrepancies between experiment and theory reported in previous studies are also explained based on the present theoretical analysis. The advanced RR → MR transition triggered by a transverse wave is also discussed for the interaction of a hypersonic flow and a double-wedge-like geometry.
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