个人简历
陈敏，男，海南省海口市人，博士，教授，博士生导师，硕士生导师，院长助理。1997年-2007年在北京航空航天大学动力学院分别获得工学学士、硕士和博士学位，2007-2009年在北航航空发动机数值仿真研究中心从事博士后研究，2009年-2014年在北航动力学院任讲师，2011年4月-10月在英国克兰菲尔德大学罗罗大学性能研究中心从事学术访问研究，2018年1月在新加坡南洋理工大学从事学术访问研究，2014年-2019年在北航动力学院任副教授,2019年任教授。2009获北航蓝天新秀称号，2013年入选北京高校青年英才计划。在新型及传统航空动力系统总体建模、总体优化设计、状态监视与故障诊断领域开展了多项具有显著学术及应用价值的研究工作，主持30项研究课题，含2项国家自然基金，4项国家级重点/重大项目专题，与中国航发、中航工业主机院所，中国上海商飞，航天科工31所，航天一院，航天二院207所等保持密切的技术合作关系。在国内外航空期刊及会议上发表中英文论文50篇（SCI论文17篇）；第一完成人获得中国航空学会2014年度科学技术奖二等奖；获2017年北航青年教师教学基本功大赛一等奖,2017年北京市青年教师基本功大赛最佳教案奖， 2017年北京市青年教师基本功大赛三等奖；第二完成人获2016年度北航教学成果一等奖，第五完成人获2018年北京市教学成果二等奖；曾指导学生获2017年美国AIAA本科生发动机设计大赛冠军。代表性研究成果发表于Aerospace Science and Technology,Applied Energy,Applied Thermal Engineering,P I MECH ENG G-J AER，ASME J. Gas Turbines Power，CHINESE J AERONAUT等国际航空学术期刊。代表性学术成果如下：
1）Min Chen*, Hai Long Tang, Zhi Li Zhu. "Goal Programming for Stable Mode Transition in Tandem Turbo-ramjet Engines." Chinese Journal of Aeronautics, 2009, 22(5):486-492.
2）Min Chen, Hai Long Tang*, Kun Zhang, Hui Ou Yang, Ya1）Min Chen, Hai Long Tang*, Kun Zhang, Hui Ou Yang, Yan Jun Wang. "Turbine-based combined cycle propulsion system integration concept design." Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2012, 227(7):1068-1089.
3）Hai Long Tang, Min Chen*, Dong Hai Jin, Zheng Ping Zou. "High altitude low Reynolds number effect on the matching performance of a turbofan engine." Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2012, 227(3):455-466.（SCI）
4）Min Chen, Kun Zhang, Hai Long Tang. "A Probabilistic Design Methodology for a Turboshaft Engine Overall Performance Analysis." Advances in Mechanical Engineering, 2014.2014(8):1-12.
5）Min Chen, Liang Quan Hu, Hai Long Tang. An Approach for Optimal Measurements Selection on Gas Turbine Engine Fault Diagnosis. Journal of Engineering for Gas Turbines & Power, 2015, 137(7):071203.
6）Ya Lv, Hailong Tang, Min Chen*, A Study on Combined Variable Geometries Regulation of Adaptive Cycle Engine during Throttling, Applied Sciences-Basel, 2016, Vol 6.
7）Junchao Zheng, Min Chen, Hailong Tang*, Matching mechanism analysis on an adaptive cycle engine. Chinese Journal of Aeronautics, 2017, Vol. 30. （SCI）
8）Junchao Zheng, Hailong Tang, Min Chen*. Equilibrium Running Principle Analysis on an Adaptive Cycle Engine[J]. Applied Thermal Engineering, 2018，132, 393-409.
9）Pengcheng Dong, Hailong Tang,Min Chen*. Overall performance design of paralleled heat release and compression system for hypersonic aero-engine [J]. Applied Energy, 2018,220: 36-46.
10）Pengcheng Dong, Hailong Tang,Min Chen*. Study on Multi-Cycle Coupling Mechanism of Hypersonic Precooled Combined Cycle Engine[J]. Applied Thermal Engineering, 2018, 131: 497-506.
11）Feijia Yin*, Arvind Gangoli Rao, Abhishek Bhat, Min Chen. Performance assessment of a multi-fuel hybrid engine for future aircraft[J]. Aerospace Science and Technology, 2018,208.77:217-227.
12) Min Chen, Jiyuan Zhang, Hailong Tang*, Interval Analysis of the Standard of Adaptive Cycle Engine Component Performance Deviation, Aerospace Science and Technology, 2018, Vol.81: 179-191
13）Min Chen, Jiyuan Zhang, Hailong Tang*, Performance Analysis of a Three-Stream Adaptive Cycle Engine during Throttling. International Journal of Aerospace Engineering, 2018: 1-16
14）Min Chen, Zihao Jia, Hailong Tang*, Yi Xiao, Yonghang Yang, Feijia Yin, Research on Simulation and Performance Optimization of Mach 4 Civil Aircraft Propulsion Concept. International Journal of Aerospace Engineering, 2019: 1-19
15）Yi Hao Xu, Hai Long Tang, Min Chen*, Fei Duan. "Optimization and Design of Heat Recovery System for Aviation," Applied Thermal Engineering, 2019.
16）Shanxuan Tang, Hailong Tang, Min Chen*, Transfer-learning based gas path analysis method for gas turbines. Applied Thermal Engineering, 2019, Vol.155: 1-13.
17）Jiyuan Zhang, Hailong Tang, Min Chen*, Linear substitute model-based uncertainty analysis of complicated non-linear energy system performance (case study of an adaptive cycle engine). Applied Energy, 2019, Vol.249: 87-108.
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论文
39）Min Chen, Hai Long Tang, Zhi Li Zhu. "Turbofan Engine Transient Performance Simulation Based on Cooling Effectiveness" Chinese Society of Aeronautics and Astronautics Propulsion Aero-thermodynamic Subject Exchange Communication Forum, Taiyuan, 2005. (in Chinese)
38）Min Chen, Jin Zhang, Hai Long Tang, Zhi Li Zhu, Da Ming Zhu. "Assessment on the hypersonic combined cycle augmented engine concepts with the tandem layout." Aeronautics & Astronautics Propulsion & Power Engineering Branch Forum, 2006..(in Chinese )
37）Hui Ou Yang, Zhi Li Zhu, Min Chen. "Size and Weight Estimation of Turbine Based Combined Cycle Turbofan Engine." Chinese Society of Aeronautics and Astronautics Propulsion Aero-thermodynamic Subject Exchange Communication Forum, JiLin,2007. (in Chinese )
36）Min Chen, Hai Long Tang, Jin Zhang. "Real-Time Performance Simulation of a Mixed-Flow Two-Spool Augmented Turbofan Engine." Journal of Aerospace Power, 2005, 20.1:13-17. (in Chinese ) （EI）
35）Da Ming Zhu, Min Chen, Hai Long Tang, Jin Zhang. ""Over-under" concept hypersonic turbo-ramjet combined propulsion system." Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(3):263-266. (in Chinese ) （EI）
34）Min Chen, Zhi Li Zhu, Da Ming Zhu, Hai Long Tang. "Performance Analysis Tool for Turbine Based Combined Cycle Engine Concept." Journal of Astronautics, 2006, 27(5):854-859. (in Chinese ) （EI）
33）Min Chen, Hai Long Tang, Da Ming Zhu, Zhi Li Zhu. "Hypersonic combined cycle engine concept with tandem layout." Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(3):265-268. (in Chinese ) （EI）
32）Bo Wang, Hai Long Tang, Ru Hao Zhong, Min Chen. "Visualize framework for aero-engine performance simulation." Journal of Aerospace Power, 2009, 24(3). ( in Chinese ) （EI）
31）Min Chen, Hai Long Tang, Da Xiang Liu, Jie Jin. "Conceptual design of Mach number 3.5 air-breathing propulsion system." Journal of Aerospace Power, 2009, 24(7). (in Chinese ) （EI）
30）Bin Li, Min Chen*, Zhi Li Zhu, Kun Zhang. "Steady Performance Investigation on Various Modes of an Adaptive Cycle Aero-Engine." Journal of Propulsion Technology, 2013, 34(8):1009-1015. (in Chinese ) （EI）
29）Min Chen, Hai Long Tang, Kun Zhang. "Some Critical Issues in the Development of Chinese High-Speed Rail: Challenges and Coping Strategies." Journal of Transportation Technologies, 2014, 04(2):164-174.
28）Jie Jin, Min Chen*. "Brief Introduction on Technology Development of Turbine Based Combined Cycle Engine." Aeronautical Manufacturing Technology, 2014(9):32-35. (in Chinese )
27）Hai Long Tang, Kun Zhang, Kun Guo, Min Chen*. "Quantification Method of Effects of Uncertainty on Component Performance for Turbo-Shaft Engine Performance." Journal of Propulsion Technology, 2015, 36(8):1143-1150. (in Chinese ) （EI）
26）Liang Quan Hu, Min Chen*, Hai Long Tang, Kun Guo. "Measurement parameters selection method for gas path fault diagnosis of two-shaft split flow turbofan engine." Journal of Aerospace Power, 2015, 30(8):1853-1861. (in Chinese ) （EI）
25）Wang Gang Tong, Hai Long Tang, Min Chen. “Investigation on Axial Compressor Flow Path Design Methods." Aeroengine, 2015, 41(5):53-57. (in Chinese )

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