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    何小民

    • 教授
    • 招生学科专业:
      动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
    • 毕业院校:南京航空航天大学
    • 学历:南京航空航天大学
    • 学位:工学博士学位
    • 所在单位:能源与动力学院
    • 联系方式:hxm@nuaa.edu.cn
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    Effect of strut length on combustion performance of a trapped vortex combustor

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    所属单位:能源与动力学院

    发表刊物:AEROSPACE SCIENCE AND TECHNOLOGY

    关键字:Strut length Flow field Combustion performance Trapped vortex combustor

    摘要:Experimental studies with four different strut setups are conducted to investigate the effect of strut length on combustion performance of a trapped vortex combustor (TVC). The experimental results indicate that ignition, lean blowout (LBO) and combustion efficiency depend to a great extent upon the length of the strut. The longer struts show prominent advantages in terms of ignition and LBO, whereas the shorter ones perform rather poorly. Interestingly, the combustion efficiency achieved by the shorter struts is higher than the longer ones. Furthermore, RANS based simulations are also performed to explain the experimental results. From the detailed numerical simulations, it can be inferred that the poor ignition performance and LBO limits of the shorter struts are mainly caused by the great amount of mainstream air entrained into the cavity. And the higher combustion efficiency achieved by the shorter struts is mainly attributed to much more wake regions formed behind the struts. (C) 2018 Elsevier Masson SAS. All rights reserved.

    ISSN号:1270-9638

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    发表时间:2018-05-01

    合写作者:Li, Mingyu,Zhao, Yuling,金义,Ge, Zhenghao,Huang, Weidong

    通讯作者:何小民