本科生课程：系统建模与仿真

研究生课程：无

社会/学术兼职：美国机械工程师协会(ASME)会员、Energies期刊客座主编

教育经历：

2007.09－2011.07　北京理工大学，热能与动力工程专业，获学士学位

2011.09－2014.03　北京理工大学，动力工程及工程热物理专业，获硕士学位

2014.04－2014.12　上海交通大学，动力工程及工程热物理专业，博士学习

2015.09－2019.07　清华大学，动力工程及工程热物理专业，获博士学位

工作经历：

2019.08-2021.07　航天五院，五O二所，工程师

2021.09-2024.03　北京大学，工学院，博士后/助理研究员

2024.04-至今　　 新葡的京集团35222vip，新葡的京集团35222vip，讲师

代表性论著：

[1] Meijie Zhang, Yi Cao, Chao Zhou. Flow physics and loss mechanisms of tip leakage flow in variable-blade-pitch-angle ducted fans. Aerospace Science and Technology, 2023, 142: 108588.

[2] Meijie Zhang, Wangxia Wu, Chao Zhou. Numerical model of predicting surge boundaries in high-speed centrifugal compressors. Aerospace Science and Technology, 2023, 141: 108518.

[3] Meijie Zhang, Wangxia Wu. Role of the inducer in flow instability of a high-speed centrifugal compressor impeller. Proceedings of ASME Turbo Expo, 2023: 1-10.

[4] Meijie Zhang, Mingxu Qi, Hong Zhang. Influence of uneven blade tip clearances on aeroacoustic characteristics of centrifugal compressors. Journal of the Global Power and Propulsion Society, 2022, 6: 254–265.

[5] Meijie Zhang, Xinqian Zheng, Zhenzhong Sun. Experimental investigation of the flow instability of a compression system with an upstream plenum. Experimental Thermal and Fluid Science, 2019, 102: 406–420.

[6] Meijie Zhang, Xinqian Zheng, Qiangqiang Huang, Zhenzhong Sun. A novel one-dimensional- three-dimensional coupled method to predict surge boundary of centrifugal compressors. Journal of Engineering for Gas Turbines and Power-ASME Transaction, 2019, 141(7): 071012.

[7] Qiangqiang Huang, Meijie Zhang, Xinqian Zheng. Compressor surge based on a 1D-3D coupled method–Part 1: Method establishment. Aerospace Science and Technology, 2019, 90: 342–356.

[8] Qiangqiang Huang, Meijie Zhang, Xinqian Zheng. Compressor surge based on a 1D-3D coupled method–Part 2: Surge investigation. Aerospace Science and Technology, 2019, 90: 289–298.

[9] Changbin Guan, Yan Shen, Zhaopu Yao, Zhaoli Wang, Meijie Zhang, et al. Design, simulation, and experiment of an LTCC-based Xenon micro flow control device for an electric propulsion system. Processes, 2019, 7(11): 862.

[10] Meijie Zhang, Xinqian Zheng. Criteria for the matching of inlet and outlet distortions in centrifugal compressors. Applied Thermal Engineering, 2018, 131: 933–946.

[11] 祁明旭, 张美杰, 马朝臣. 间隙非谐对离心压气机散噪声的影响. 北京理工大学报, 2016, 36(5): 475-479.

[12] Mingxu Qi, Meijie Zhang, Chaochen Ma. Influences of dis-tuned tip clearance on the discrete aerodynamic noise in centrifugal compressor. 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Hawaii, US, 2016: 1-10.

[13] 荆磊, 杨策, 张美杰, 等. 非对称进气双面压气机大小叶轮拓稳特性研究. 工程热物理学报, 2015, 10: 2127-2131.

[14] 张美杰, 祁明旭, 马朝臣. 间隙非谐对离心压气机动噪声的影响. 柴油机, 2013, 35(250): 367-371.

代表性专利：

[1] 官长斌, 张美杰, 等, “一种基于弹簧管位移放大的小型化高压电比例阀”, 2021，授权专利号：ZL202010301348.X

[2] 郑新前, 孙振中, 张美杰，等, “采用周向可变叶片安装角非对称有扩压器的离心气机”,  2019，授权专利号：ZL201710154445.9

[3] 郑新前, 孙振中, 张美杰，等，“采用周向可变叶片高度非对称有扩压器的离心气机”,  2018，授权专利号：ZL201710154921.7

[4] 郑新前, 孙振中, 张美杰，等, “采用周向可变叶片稠度非对称有扩压器的离心气机”,  2018，授权专利号：ZL201710154466.0

[5] 郑新前, 孙振中, 张美杰，等, “采用安装角和稠度耦合可变的非对称有叶扩压器气机”,  2018，授权专利号：ZL201710154444.4

代表性项目：

[1] 中国航空工业集团项目，XFX20220502，2022-2024，主持

[2] 江西省科技厅重点研发项目，20223BBE51003，2022-2025，参与

[3] 航空发动机/燃气轮机国家两机重大专项，2017-Ⅱ-0004，2018-2022，参与

[4] 国家自然科学基金，面上项目，51876097, 2019-2022，参与

成果与荣誉：

2021 北京大学博雅博士后