A reduced two-stage model of detonation combustion of methane in oxygen and air for equimolar and fuel-lean mixtures is proposed. One-dimensional structures of the detonation wave are calculated for different ratios of the fuel and oxidizer corresponding to the overdriven and Chapman-Jouguet regimes. A comparison of the calculated dependences of the detonation velocity on the methane concentration in the methane-air mixture with available published data reveals their reasonable agreement.
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Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R ChinaHarbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R China
Guo, Hongbo
Zhao, Ningbo
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Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R ChinaHarbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R China
Zhao, Ningbo
Yang, Honglei
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Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R ChinaHarbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R China
Yang, Honglei
Li, Shuying
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Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R ChinaHarbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R China
Li, Shuying
Zheng, Hongtao
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Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R ChinaHarbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Peoples R China