A computational technique for high enthalpy shock tube and shock tunnel flow simulation

被引：0

作者：

Y. Sheng

J.P. Sislian

J.J. Liu

机构：

[1] Department of Mechanical Engineering,

[2] McMaster University,undefined

[3] Hamilton,undefined

[4] Ontario,undefined

[5] Canada ,undefined

[6] Institute for Aerospace Studies ,undefined

[7] University of Toronto,undefined

[8] Downsview,undefined

[9] Ontario,undefined

[10] Canada ,undefined

[11] Department of Engineering Science,undefined

[12] National Cheng-Kung University,undefined

[13] Tainan,undefined

[14] Taiwan ROC ,undefined

来源：

Shock Waves | 1998年 / 8卷

关键词：

Key words:Shock tube, Shock tunnel, Riemann solver;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

A contact discontinuity tracking method with a specially designed moving grid is developed to eliminate the interface smearing completely. In order to precisely locate the contact surface, an updated Riemann solver for unsteady one-dimensional inviscid flows is also developed to allow consideration of the specific heat ratio change across the shock wave. These two new computational techniques are illustrated in a high Mach number shock tube flow field computation.

引用

页码：203 / 214

页数：11

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