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Reduced detonation kinetics and detonation structure in one- and multi-fuel gaseous mixtures

机译:在单燃料气体混合物中减少爆轰动力学和爆轰结构

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Two-step approximate models of chemical kinetics of detonation combustion of (i) one-fuel (CH_4/air) and (ii) multi-fuel gaseous mixtures (CH_4/H_2/air and CH_4/CO/air) are developed for the first time. The models for multi-fuel mixtures are proposed for the first time. Owing to the simplicity and high accuracy, the models can be used in multi-dimensional numerical calculations of detonation waves in corresponding gaseous mixtures. The models are in consistent with the second law of thermodynamics and Le Chatelier's principle. Constants of the models have a clear physical meaning. Advantages of the kinetic model for detonation combustion of methane has been demonstrated via numerical calculations of a two-dimensional structure of the detonation wave in a stoichiometric and fuel-rich methane-air mixtures and stoichiometric methane-oxygen mixture. The dominant size of the detonation cell, determines in calculations, is in good agreement with all known experimental data.
机译:(i)单燃料(CH_4 /空气)和(ii)多燃料气态混合物(CH_4 / h_2 /空气和CH_4 / CO /空气)的两步近似模型时间。第一次提出了多燃料混合物的模型。由于简单性和高精度,该模型可用于相应气态混合物中的爆轰波的多维数值计算。该模型与第二热力学和Le Chatelier原则一致。模型的常数具有明显的物理意义。通过在化学计量和富含燃料的甲烷 - 空气混合物和化学计量甲烷 - 氧混合物中的爆轰波的二维结构的二维结构的数值计算证明了甲烷的动力学模型的优点。爆轰细胞的主要大小在计算中确定,与所有已知的实验数据吻合良好。

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