Combustion Simulation in Afterburner Using Flamelet Model Based on OpenFOAM

被引：0
|
作者：
Xiao, Yin-li [1 ]
Chen, Ke-fei [1 ]
Wang, Zu-peng [1 ]
Lai, Zheng-xin [1 ]
机构：
[1] Northwestern Polytech Univ, Sch Engine & Energy, Xian, Shaanxi, Peoples R China
来源：
INTERNATIONAL CONFERENCE ON OPTICS, ELECTRONICS AND COMMUNICATIONS TECHNOLOGY (OECT) | 2017年 / 175卷
基金：
中国国家自然科学基金;
关键词：
Steady Laminar Flamelet Model; OpenFOAM; Afterburner;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Simulation of combustion in the afterburner of solid ducted rocket is still a big challenge due to the interaction of turbulent and combustion. In the current study, a steady laminar flamelet model has been conducted to model the flow field of the afterburning chamber of solid ducted rocket based on OpenFOAM. The predicted main flow features in different transverse and longitudinal planes are analyzed. The performance parameter of the afterburning chamber is analyzed.
引用
收藏
页码：193 / 198
页数：6
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