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CH_4-O_2 混合气中爆燃爆震转捩的数值模拟 被引量:15
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作者 高泰荫 黄军涛 +2 位作者 李元明 高越 信一兵 《爆炸与冲击》 EI CAS CSCD 北大核心 1998年第4期323-330,共8页
运用化学流体力学基本理论和两步燃烧反应模型原理,建立了一维封闭体系可燃气爆燃爆震转变现象的数学模型,利用拉格朗日质量坐标变换下的Lax-Wendrof和Mecormic气动差分与Adams化学差分格式,求解基本方程,... 运用化学流体力学基本理论和两步燃烧反应模型原理,建立了一维封闭体系可燃气爆燃爆震转变现象的数学模型,利用拉格朗日质量坐标变换下的Lax-Wendrof和Mecormic气动差分与Adams化学差分格式,求解基本方程,成功地完成了过程的数值模拟,清楚地说明了可燃气中DDT现象由压缩波到激波达到稳态爆震的发生机制和火焰带引生爆震波的过程行为。 展开更多
关键词 可燃气 爆燃爆震转捩 DDT 数值模拟
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焦炭粉-氧气混合物爆燃向爆震转捩的数值模拟 被引量:1
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作者 高泰荫 高越 +3 位作者 栗自彬 李元明 张明新 张殿杰 《东北大学学报(自然科学版)》 EI CAS CSCD 北大核心 2000年第3期290-293,共4页
根据化学反应和两相反应流体动力学理论 ,建立了焦炭粉 氧气混合物燃烧波在一维封闭空间内的爆燃爆震转捩现象的数学模型 ,运用坐标变换和MacCormack两步显式差分格式 ,成功地完成了过程的数值模拟·清楚地诠释了气固两相混合物中... 根据化学反应和两相反应流体动力学理论 ,建立了焦炭粉 氧气混合物燃烧波在一维封闭空间内的爆燃爆震转捩现象的数学模型 ,运用坐标变换和MacCormack两步显式差分格式 ,成功地完成了过程的数值模拟·清楚地诠释了气固两相混合物中DDT现象的转变机制 :激波诱导、激波生成、激波加强及至稳态爆震·转变过程受初始温度场、压力场。 展开更多
关键词 两相可燃混合物 爆燃爆震转捩 数值模拟
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Investigation of Detonative Combustion Characteristics 被引量:2
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作者 HAN Qi-xiang WANG Jia-hua WANG Bo 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第2期72-76,共5页
The pressure and deflagration to detonation transition(DDT)characteristics of acetylene and oxygen flame were studied in a detonation tube.The pressure history and the flame velocity along the tube were measured with ... The pressure and deflagration to detonation transition(DDT)characteristics of acetylene and oxygen flame were studied in a detonation tube.The pressure history and the flame velocity along the tube were measured with high frequency pressure transducers and ion probes.By analyzing the data recorded in the experiment,the detonation wave pressure,post wave pressure and DDT distance were obtained,together with the effects of the initial pressure varying from 2×10^(4)Pa to 10^(5)Pa,equivalence ration from 0.3 to 1.0,and mixture concentration from 60%to 100%.It was found that the detonation pressure was decreased respectively with the decrease of initial pressure,equivalence ratio and mixture concentration,but the DDT distance was enlarged.The DDT distance was found particularly sensitive to mixture concentration. 展开更多
关键词 DETONATION COMBUSTION deflagration to detonation transition pulse detonation engine
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Single-step chemistry model and transport coefficient model for hydrogen combustion 被引量:3
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作者 WEN Jennifer WANG ChangJian +1 位作者 LU ShouXiang GUO Jin 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第8期2163-2168,共6页
To satisfy the needs of large-scale hydrogen combustion and explosion simulation,a method is presented to establish single-step chemistry model and transport model for fuel-air mixture.If the reaction formula for hydr... To satisfy the needs of large-scale hydrogen combustion and explosion simulation,a method is presented to establish single-step chemistry model and transport model for fuel-air mixture.If the reaction formula for hydrogen-air mixture is H2+0.5O2→H2O,the reaction rate model is ?? =1.13×10?5[H2][O2]exp(?46.37T0/T) mol(cm3 s)?1,and the transport coefficient model is ?=K/CP=ρD=7.0×10?5T 0.7 g(cm s)?1.By using current models and the reference model to simulate steady Zeldovich-von Neumann-Doering(ZND) wave and free-propagating laminar flame,it is found that the results are well agreeable.Additionally,deflagration-to-detonation transition in an obstructed channel was also simulated.The numerical results are also well consistent with the experimental results.These provide a reasonable proof for current method and new models. 展开更多
关键词 hydrogen combustion singe-step chemistry model transport coefficient model
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