Viscosity effects on weak irregular reflection of shock waves in steady flow

被引:20
作者
Ivanov, Mikhail S. [1 ]
Bondar, Yevgeniy A. [1 ]
Khotyanovsky, Dmitry V. [1 ]
Kudryavtsev, Alexey N. [1 ]
Shoev, Georgy V. [1 ]
机构
[1] Russian Acad Sci, Khristianovich Inst Theoret & Appl Mech, Computat Aerodynam Lab, Siberian Branch, Novosibirsk 630090, Russia
基金
俄罗斯基础研究基金会;
关键词
Von Neumann paradox; Irregular shock wave reflection; MACH REFLECTION; TRANSITION; HYSTERESIS; PARADOX;
D O I
10.1016/j.paerosci.2009.11.004
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The viscosity effects on weak shock wave reflection are investigated with the Navier-Stokes and DSMC flow solvers. It is shown that the viscosity plays a crucial role in the vicinity of three-shock intersection. Instead of a singular triple point, in viscous flow there is a smooth three shock transition zone, where one-dimensional shock jump relations cannot be applied. At the flow parameters corresponding to the von Neumann reflection, when no inviscid three-shock solution exists, the computations predict an irregular shock-wave configuration similar to that observed previously in experiments. The existence of a viscous zone in the region of shock-wave interaction allows a continuous transition from the parameters behind the Mach stem to the parameters behind the reflected shock, which is impossible in the inviscid three-shock theory. Results of numerical simulations agree qualitatively with the conclusions of the approximate viscous theory, which describes the flow in the vicinity of the three-shock intersection. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:89 / 105
页数:17
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