Language : English
戴健
  • Personal Information

    Associate Professor


    Supervisor of Doctorate Candidates


    Supervisor of Master's Candidates

    School/Department:Research Institute of Aerospace Technology

    Education Level:PhD Graduate

    Business Address:校本部升华楼后栋705室

    Sex:Male

    Degree:Doctoral degree

    Status:Employed

    Alma Mater:北京航空航天大学

    Discipline:Aerospace Science and Technology

  • Profile

    戴健,博士,博士生导师,特聘副教授。长期从事高超声速组合动力技术、液体火箭发动机气气喷注器燃烧数值仿真、地面试验技术研究。先后主持参与了多项国家级课题,具有充足科研经费保障学生培养质量,助力学生成长成才。近五年来,与本课题组优秀研究生共同合作,已在Physcis of Fluids, Aerospace Science and Technology, Acta Astronautica,推进技术等航空航天领域权威期刊上公开发表学术论文10余篇,其中在当季期刊发表封面文章,得到业内权威认可,并助力其获得一等学业奖学金及企业奖学金。欢迎各位有志于从事空天组合先进动力、爆震发动机等基础研究的研究生报考,一起携手共进为祖国航天事业添砖加瓦!!!


    论文列表

    1. Peng Linyuan, Dai Jian*, Effects of staggered opposed hot jets on the initiation and propagation of gaseous detonation in a supersonic combustible inflow, Physics of Fluids, 35, 014102(2023). 

    2. Qiuru Zuo, Huanli Yu, Jian Dai*, Yude Yan, Long Chen, Numerical study of injection strategy based on cavity combustor under oblique shock wave interference, International Journal of Hydrogen Energy, 47(2022), 36693-36702.

    3. Dai Jian*, Zuo Qiuru, Numerical investigation on mixing enhancement of the cavity with pulsed jets under oblique shock wave interference, Aerospace Science and Technology, 123(2022), 107454. 

    4. Jian Dai*, Linyuan Peng, Numerical investigation on detonation initiation and propagation with a symmetric-jet in supersonic combustible gas, Aerospace, 9, 9(2022):501. 

    5. Zuo Qiuru, Yu Huanli, Dai Jian*, Effects of cavity-induced mixing enhancement under oblique shock wave interference: numerical study, International Journal of Hydrogen Energy, 46(2021), 35706-35717.

    6. Jian Dai, Fei Xu, Xiaodong Cai*, Yasser Mahmoudi, Effects of velocity shear layer on detonation propagation in a supersonic expanding combustor, Physics of Fluids, 33, 105110(2021).

    7. Dai Jian*, Huang Chao, Xu Fei, Zuo Qiuru, Peng Linyuan, Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine, Aerospace Science and   Technology, 118(2021), 107068. 

    8. Jian Dai*, Chao Huang, Secondary fuel jet stategies on mixing enhancement performance of rocket-based combined cycle engine, Acta Astronautica, 178(2021), 285-295. 

    9. Dai Jian*, Zuo Qiuru, Huang Chao, Numerical investigation of cavity-induced enhanced supersonic mixing with inclined injection strategies, Acta Astronautica, 180(2021), 630-638. 

    10. Dai Jian*, Huang Chao, Zuo Qiuru, Xufei, A numerical study on flow structure and combustion mechanism of supersonic mixed inflow with transverse jet, Aerospace Science and Technology, 116(2021), 106865. 

    11. 戴健,许菲*,陈琪锋, 多无人机协同搜索区域划分与路径规划研究,航空学报, 2020,41(S1):723770. 

    12. Dai Jian*, Yu Huanli, Numerical and experimental investigations of geometrical parameters on gh2/go2 injector, Aerospace Science And Technology, 106(2020), 106187. 

    13. Dai Jian*, Zuo Qiuru, Key technologies for thermodynamic cycle of precooled engines: A review, Acta Astronautica, 177(2020), 299-312. 

    14. Huang Chao, Yu Huanli, Dai Jian*, Mixing and combustion augmentation of the RBCC with different mixer configurations in ejector mode, Acta Astronautica, 174(2020), 281-293.


    专著

    1. 戴健,黄超,左秋儒,闫雨德,高超声速受限通道混合增强技术研究,中南大学出版社,2022.11.1,20万字。


    联系方式

    daijian@csu.edu.cn

  • Research Field

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  • Education Background

    [1]  2008.9- 2012.7
    北京航空航天大学 | University graduated | Bachelor's Degree in Engineering
    [2]  2012.9- 2018.7
    北京航空航天大学 | 航空宇航推进理论与工程 | PhD Graduate | Doctoral degree
  • Work Experience

    [1]  2018.9- Now
    中南大学 | 航空航天学院 | 在职
  • Research Group

    Name of Research Group:先进空天动力团队

    Description of Research Group:研究生发展动态
    黄超(2018级硕士研究生):格林美创新奖学金,一等奖学金,发表4篇SCI高水平航空航天类期刊论文,研究方向为RBCC燃烧室混合增强机理研究,毕业前往贵州航天十院十部;
    左秋儒(2019级硕士研究生):国家奖学金,一等奖学金,主持省级研究生创新创业课题,现已发表3篇SCI高水平航空航天类期刊论文,研究方向为斜激波诱导混合增强机理研究;
    许菲(2019级硕士研究生):格林美创新奖学金,一等奖学金,现已发表1篇高水平流体力学顶刊论文(Physics of Fluids),并获得当期封面文章,研究方向为非均匀来流条件下爆震发动机起爆机理研究。
    彭琳媛(2020级硕士研究生):研究方向为热射流凹腔诱导爆震起爆机理研究。
    闫雨德(2022级博士研究生):研究方向为高超声速宽速域混合增强机理研究。
    刘津典(2021级硕士研究生):研究方向为高超声速边界层效应爆震起爆机理研究。

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