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
收藏
页码：63 / 66
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