期刊文献+

基于HyChem方法的正丙基环己烷反应动力学模型

Reaction kinetic model of n-propylcyclohexane based on HyChem method
原文传递
导出
摘要 采用Hybrid Chemistry(HyChem)建模方法对正丙基环己烷开展模型研究,以七步集总反应对大分子燃料热解形成小分子产物这一过程进行建模,小分子产物氧化过程则以小分子详细机理USC MechⅡ进行描述。将两个子机理结合构建了正丙基环己烷的HyChem反应动力学模型(包括112个组分和791个基元反应),并通过流动管热解、点火延迟时间以及层流火焰速度的实验数据进行了模型验证。验证结果表明,正丙基环己烷HyChem反应动力学模型可以很好的预测正丙基环己烷热解过程中主要组分分布情况,在宏观燃烧参数的预测方面也有很好的表现,对点火延迟时间的计算相对误差为29.7%,对火焰传播速度的计算相对误差为11.1%。 The kinetic model of n-propylcyclohexane was studied by using the Hybrid Chemistry(HyChem)modeling method.The pyrolysis of the large fuel molecule to form small products was modeled by the seven-step lumped reaction,while the oxidation of the small products was described by the detailed reaction model USC MechⅡ.The HyChem kinetic model of n-propylcyclohexane consisting of 112 species and 791 elementary reactions was constructed by coupling the two sub-mechanisms,and the experimental data of the flow reactor pyrolysis,ignition delay time and laminar flame speed were used to conduct the model validation.The results showed that this reaction mechanism can accurately predict the product distribution during the pyrolysis of n-propylcyclohexane,and it also had good performance in the prediction of the global combustion parameters,the calculation relative error of ignition delay time was 29.7%,and the calculation relative error of laminar flame speed was 11.1%.
作者 王光彩 王乾鹏 丁梦缘 王娟 WANG Guangcai;WANG Qianpeng;DING Mengyuan;WANG Juan(National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2021年第7期1452-1461,共10页 Journal of Aerospace Power
基金 国家自然科学基金(U2032119,71690245)。
关键词 正丙基环己烷 反应动力学模型 HyChem方法 热解 点火延迟时间 层流火焰速度 n-propylcyclohexane reaction kinetic model HyChem method pyrolysis ignition delay time laminar flame speed
  • 相关文献

参考文献4

二级参考文献36

  • 1侯宽新,刘勇,赵坚行.详细反应机理的航空发动机二维燃烧流场计算[J].航空动力学报,2009,24(12):2655-2660. 被引量:3
  • 2范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-192. 被引量:112
  • 3朱玉红,余彩香,李子木,米镇涛,张香文.航空燃料超临界热裂解过程中焦炭的形成[J].石油化工,2006,35(12):1151-1155. 被引量:16
  • 4王俊清.BP神经网络及其改进[J].重庆工学院学报,2007,21(5):75-77. 被引量:23
  • 5杨晔,张镇西,蒋大宗.微粒直径及直径分布的激光测量技术[J].激光技术,1997,21(2):124-127. 被引量:14
  • 6Edwards T,Maurice L Q. Surrogate mixtures to represent complex aviation and rocket fuels[J]. Journal of Propul sion and Power,2001,17(2) :461 -466.
  • 7Riesmeir E, Honnet S,Peters N. Fiamelet modeling of pol lutant formation in a gas turbine combustion chamber using detailed chemistry for a kerosene model fuel [J]. Journal of Engineering for Gas Turbines and Power, 2004, 126(4) :899-905.
  • 8Luche J, Reuillon M, Boettner J C, et al. Reduction of large detailed kinetic mechanisms: application to kerosene/air combustion [J]. Combustion Science and Technology, 2004,176 (3) : 1935-1963.
  • 9Violi A, Yah S,Eddings E G, et al. Experimental formula- tion and kinetic model for JP-8 surrogate mixture [J]. Combustion Science and Technology, 2002,174 (11/12) : 399-417.
  • 10Agosta A, Cernansky N P, Miller D L, et al. Reference components of jet fuels: kinetic modeling and experimental results[J]. Experimental Thermal and Fluid Science, 2004, 28(7) : 701-708.

共引文献37

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部