张悦，1986年生，工学博士，教授，博导，国家级青年人才。
主要从事先进进气道流动机理和设计方法研究， 目前主持相关科研项目十余项。 其中，JKW××特区重点项目1项、 国防科技基础加强基金项目1项、 国家自然科学基金项目2项、 JKW重大基础加强项目2项、 “两机”基础科学中心国际合作项目1项，作为专题负责人负责“ 民机” 专项、 “ 两机” 专项专题各1项， 还承担了业内主机单位的多项委托课题。以第一作者或通讯作者在国际航空航天领域期刊AIAA Journal、Acta Astronautica、Journal of Fluid Mechanics等发表论文近40篇，申请发明专利50余项，其中获授权38项。
入选国家重大人才工程青年项目，江苏省“333高层次人次培养工程”第三层次，江苏省“青年托举”人才工程，南京航空航天大学“长空之星”人才培养计划。获“航空强国中国心”教育基金“突出贡献奖”一等奖、陕西省科技进步一等奖、航空宇航科学技术学科全国优秀博士学位论文、江苏省优秀博士学位论文、南京航空航天大学青年创新奖。
近五年发表主要论文如下：
1. Yue Zhang, Liang Chen, Hui-jun Tan, Chao Wang, Fei Cheng and Chao Li. Visualization of Curved Swept Shock Wave/Turbulent Boundary Interaction in Supersonic Flow, Journal of Visualization, Vol.24, No.2, pp:1-7, 2021.
2.Yi Jin, Yue Zhang, Hui-Jun Tan, Xin Li, Shu Sun, and De-peng Wang. Oscillations in Rectangular Supersonic Inlets with Large Internal Contraction Ratio. AIAA Journal,vol.60, No.8, pp: 4628-4638, 2022.8.
3. Xin Li, Yue Zhang, Huijun Tan, Yi Jin and Chao Li. Comparative Study on Single-Incident and Dual-Incident Shock Wave/Turbulent Boundary Layer Interactions with Identical Total Deflection Angle. Journal of Fluid Mechanics, 2022.4.5, vol.940, A7
4. Xin Li, Yue Zhang, Hang Yu, Zheng-Kang Lin, Hui-Jun Tan and Shu Sun. Görtler Vortices Behavior and Prediction in Dual-Incident Shock-Wave/Turbulent Boundary-Layer Interactions. Physics of Fluids, vol.34, 106103, 2022.
5. Yi Jin, Yue Zhang, Xin Li, Huijun Tan, Shu Sun. Suppression of Flow Response Hysteresis in the Throttling/Unthrottling Process for Supersonic Inlet. Acta Astronautica, 2022.9.30, 202 (2023) 34–47.
6. Yi Jin, Yue Zhang, Hui-jun Tan, Hang Yu. Unstart/Restart Boundary Broadening Method for a Two-Dimensional Supersonic Variable Inlet Based on a Distributed Bleed System. Journal of Aerospace Engineering, (ASCE)，Vol. 36，No.1, 2023, 36(1): 04022115.
7. Li, Xin; Zhang, Yue; Tan, Hui-jun; Sun, Shu; Yu, Hang; Jin, Yi; Zhou, Jie. Separation length scaling for dual-incident shock wave/turbulent boundary layer interactions with different shock wave distances. Journal of Fluid Mechanics，(2023), vol. 960, A9.
8. Mengge Wang, Ziyun Wang, Yue Zhang, Daishu Cheng, Huijun Tan, Kun Wang and Simin Gao. Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator. Aerospace 2023,10,729.
9. Liang Chen, Yue Zhang, Hong-chao Xue, Hui-jun Tan, Zi-yun Wang, Hang Yu. Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp. Aerospace Science and Technology, 142 (2023) 108639.
10. Hang Yu, Yue Zhang, Liang Chen, and Huijun Tan, Juanjuan Wang and Jie Zhou. Characteristics of Combined-Cycle Inlet During Mode Transition in Off-Design State. AIAA Journal, Vol.61, No.6, June 2023, 2601-2611.
11. Yu Hang, Tan Hui-Jun, Li Xin, Li Fang-Bo, Zhang Yue, Wang Zi-Yun, Analysis of shock train leading shock structure under oscillatory backpressure. Physics of Fluids, 35, 061706(2023).
12. Liang Chen, Yue Zhang* , Juanjuan Wang, Hongchao Xue, Yixuan Xu, Ziyun Wang and Huijun Tan, Görtler Vortices in the Shock Wave/Boundary-Layer Interaction Induced by Curved Swept Compression Ramp. Aerospace, 11090760, 2024
13. Liang Chen, Yue Zhang, Hao Zhang, Huijun Tan,Ziyun Wang, Hang Yu, Hongchao Xue, Unsteady flow Characteristics in an over-under TBCC inlet during mode transition under unthrotted and throttled conditions. Chinese Journal of Aeronautics, 2024.7.30, 3152.
14. Liang Chen, Yue Zhang, Yi-Xuan Xu, Hui-Jun Tan, Hong-Chao Xue, Zi-Yun Wang, Investigation of the impact of splitter rotation speed on mode transition characteristics of an over-under turbinebased combined cycle inlet. Physics of Fluids, 2024, 8,21, 36, 086126 (2024).
15. Yunjie Guo, Huijun Tan, Yue Zhang, Xin Li, Hongchao Xue, Ziqi Luo and Hexia Huang. On incident shock wave/boundary layer interactions under the influence of expansion corner. Journal of Fluid Mechanics,vol.988, A28.(2024)
16. L. Chen, Y. Zhang, Y.X. Xu, Z.Y. Wang, H. J. Tan and H. C. Xue. Analysis of the impact of key similarity criteria numbers of TBCC inlet during the mode transition, The Aeronautical Journal (2025), 129, pp. 395–410.
17. Liang Chen, Yue Zhang, Yi xuan Xu, Hui jun Tan, Hong chao Xue, Ziyun Wang, Oscillation and Hysteresis Characteristics of High-Speed Duct During TBCC Inlet Mode Transition Under the Mildly Throttled Condition, Chinese Journal of Aeronautics
18. 张悦. 进气道内激波/边界层干扰及控制研究进展，推进技术，Vol.41, No.2, pp: 241-259, 2020.
19. 张悦. 弯曲后掠压缩拐角激波/湍流边界层干扰特性研究，推进技术，Vol.42, No.2, pp:309-318, 2021。
20. 张悦. 超声速条件下等离子体合成射流对鼓包诱导流场的影响，推进技术，Vol.42, No.5, pp:532-539, 2021.
21. 张悦. 内并联型进气道模态转换过程中流道间干扰特性研究，推进技术，vol. 43, No.7, pp:200764-1~200764-10, 2022.
22. 张悦. 预冷器对高超声速轴对称进气道设计状态气动性能影响, 推进技术，2022.8。
目前指导博士生5名，研究生10名，已毕业研究生3名
Professor
Supervisor of Doctorate Candidates
Gender:Male
Alma Mater:南京航空航天大学
Education Level:南京航空航天大学
Degree:Doctoral Degree in Engineering
School/Department:College of Energy and Power Engineering
Discipline:Aerospace Propulsion Theory and Engineering
Business Address:南京航空航天大学能源与动力学院A10
Contact Information:邮箱：y.zhang@nuaa.edu.cn
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