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碳氢燃料超声速燃烧的化学动力学研究 (Ⅰ)甲烷超声速燃烧的简化化学动力学模型
引用本文:唐亚林,张德良,王琳琳,袁生学,王发民.碳氢燃料超声速燃烧的化学动力学研究 (Ⅰ)甲烷超声速燃烧的简化化学动力学模型[J].推进技术,1999,20(5):91-94.
作者姓名:唐亚林  张德良  王琳琳  袁生学  王发民
作者单位:中国科学院力学研究所,北京,100080
摘    要:采用雷诺平均N-S方程对碳氢燃料甲烷(CH4) 在超声速流动中混合燃烧过程进行了数值研究, 提出了简化的甲烷燃烧的反应机理及反应动力学模型, 建立了Baldw in-Lom ax 代数涡粘性湍流模型, 采用了高精度的TVD隐式格式和化学源项隐式解法, 计算结果和氢气/空气超燃的计算结果进行了比较, 表明所采用的反应机理及计算模型合理, 算法可行, 就算例结果而言,碳氢化合物作为一种超燃燃料有其独特的优势, 值得进一步深入研究

关 键 词:烃类燃料  甲烷  超音速燃烧  数值仿真
修稿时间::1998-09-1

NUMERICAL SIMULATION FOR COMBUSTION OF METHANE FUEL IN SUPERSONIC FLOW
Tang Yalin,Zhang Deliang,Wang Linlin,Yuan Shengxue and Wang Famin.NUMERICAL SIMULATION FOR COMBUSTION OF METHANE FUEL IN SUPERSONIC FLOW[J].Journal of Propulsion Technology,1999,20(5):91-94.
Authors:Tang Yalin  Zhang Deliang  Wang Linlin  Yuan Shengxue and Wang Famin
Institution:Inst.of Mechanics,Academia Sinica,Beijing,100080;Inst.of Mechanics,Academia Sinica,Beijing,100080;Inst.of Mechanics,Academia Sinica,Beijing,100080;Inst.of Mechanics,Academia Sinica,Beijing,100080;Inst.of Mechanics,Academia Sinica,Beijing,100080
Abstract:The mixing and combustion of hydrocarbon(methane) in supersonic flow were investigated numerically by using Reynolds average equations. The turbulent model of Baldwin Lomax algebraic eddy viscosity and the chemical models of implicit treatment of chemical source term were adopted. Numerical results were analysed and compared with one of hydrogen fuel.The results show that the chemical model established is reasonable and the numerical method is reliable. The hydrocarbon fuel is a prospective fuel in supersonic combustion flow.
Keywords:Hydrocarbon fuel  Methane  Supersonic combustion  Numerical simulation
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