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  • 博士生导师
  • 招生学科专业:
    力学 -- 【招收博士、硕士研究生】 -- 航空学院
    航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
    机械 -- 【招收硕士研究生】 -- 航空学院
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  • 所在单位:航空学院
  • 学历:法国巴黎第六大学
  • 办公地点:本部流体楼(C12)- 301室
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  • 联系方式:wangjf@nuaa.edu.cn
  • 学位:工学博士学位
  • 职称:教授
  • 毕业院校:南京航空航天大学; Université Pierre et Marie Curie
论文成果
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Reduced kinetic model for supersonic combustion of vaporized kerosene
  • 点击次数:
  • 所属单位:航空学院
  • 发表刊物:Guofang Keji Daxue Xuebao
  • 摘要:In order to explore the chemical kinetics process of kerosene combustion in scramjet combustor, a detailed chemical reaction model for the combustion of RP-3 surrogate fuel was simplified to obtain a new reduced model (26 species and 89 reactions) based on the sensitivity analysis and reaction path analysis, and the combustion characteristics of supersonic reacting flow field were depicted. The ignition and combustion characteristics of this surrogate fuel under various conditions were simulated by using the reduced reaction model,and the simulation results were compared with the experimental data and the calculated results by the detailed reaction model. Furthermore, numerical simulations were implemented by using a coupled nonequilibrium reaction solver with the proposed reduced model, and the combustion characteristic of a scramjet combustor with single-side cavity was analyzed in detail. The results indicate that the reduced model can represent the ignition and combustion characteristic of the detailed model to some extent. And the proposed reduced chemical kinetic model predicts the myriad details of the reacting flow field accurately, including the distributions of major species, such as alkenes and cycloalkanes. At the same time, the number of species involved in the reduced model is much fewer, and the reduced model can improve the combustion simulation efficiency. © 2019, NUDT Press. All right reserved.
  • ISSN号:1001-2486
  • 是否译文:
  • 发表时间:2019-02-28
  • 合写作者:Fan, Xiaofeng,Zhao, Faming,Yang, Tianpeng
  • 通讯作者:王江峰
  • 发表时间:2019-02-28