Numerical simulation on supersonic combustion of methane

被引：0

作者：

Liu, Hong ^{[1
]}

Du, Xin ^{[1
]}

Shen, Yue-Yang ^{[1
]}

Lei, Mai-Fang ^{[1
]}

Wang, Fa-Min ^{[1
]}

机构：

[1] Inst. of Mech., China Acad. Sinica, Beijing 100080, China

来源：

Tuijin Jishu/Journal of Propulsion Technology | 2002年 / 23卷 / 01期

关键词：

Combustion - Computer simulation - Methane - Navier Stokes equations - Supersonic aerodynamics;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

A flow field with a sonic methane jet injected transversely into a supersonic hot air flow was simulated. The model of six elementary reactions of the methane-oxygen system was verified by solving N-S equations using the Harten-Yee implicit TVD scheme. The effects of different boundary conditions and inlet conditions were studied and a contrast was made with the model of single-reaction of the methane-oxygen system.

引用

页码：63 / 66