甲烷超声速燃烧过程的数值模拟

推进技术 ›› 2002, Vol. 23 ›› Issue (1): 63-66.

甲烷超声速燃烧过程的数值模拟

刘宏,杜新,沈月阳,雷麦芳,王发民

中国科学院力学研究所北京100080;中国科学院力学研究所北京100080;中国科学院力学研究所北京100080;中国科学院力学研究所北京100080;中国科学院力学研究所北京100080

发布日期:2021-08-15
基金资助:
国家自然科学基金资助项目 (1980 2 0 19)

Numerical simulation on supersonic combustion of methane

Inst. of Mechanics,Academia Sinica, Beijing, 100080,China;Inst. of Mechanics,Academia Sinica, Beijing, 100080,China;Inst. of Mechanics,Academia Sinica, Beijing, 100080,China;Inst. of Mechanics,Academia Sinica, Beijing, 100080,China;Inst. of Mechanics,Academia Sinica, Beijing, 100080,China

Published:2021-08-15

摘要/Abstract

摘要： 提出了一种CH4 O2 在超声速气流中燃烧的 6方程化学反应模型 ,并且用在超声速高温空气中横向喷射的二维流场进行了数值模拟验证。特别模拟了不同来流条件和壁面条件对燃烧效率的影响及CH4 和空气中的氧气混合燃烧的过程。数值方法采用二阶精度的Harten Yee隐式TVD格式 ,计算结果表明 6方程反应模型能较好地反映CH4 O2 的燃烧过程

关键词: 超音速冲压喷气发动机;超音速燃烧;甲烷;数值仿真

Abstract: 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.

Key words: Supersonic combustion ramjet engine;Supersonic convbustion;Methane;Numerical simulation

刘宏,杜新,沈月阳,雷麦芳,王发民. 甲烷超声速燃烧过程的数值模拟[J]. 推进技术, 2002, 23(1): 63-66.