张子健_北京理工大学宇航学院

力学系

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正高级职称（按拼音排序）

张子健

所在学科：力学

联系电话：

通讯地址：北京理工大学空天科学与技术学院

职称：准聘教授，博导

邮箱：zjzhang@bit.edu.cn

邮编：100081

教育经历

2015年09月-2020年07月，在中国科学院大学获得流体力学博士学位
2011年09月-2015年07月，在中国科学技术大学获得理论与应用力学学士学位

工作经历

2025年03月-至今，北京理工大学，空天科学与技术学院，准聘教授
2022年06月-2025年03月，香港理工大学，航空及民航工程学系，研究助理教授
2020年12月-2022年05月，香港理工大学，航空及民航工程学系，博士后研究员

主要研究领域

1、高温气体动力学
2、激波与爆轰现象
3、爆轰发动机流动机理与控制

获奖情况

1、2024年获得国家自然科学基金委优秀青年科学基金（海外）
2、2020年获得中国科学院院长优秀奖

社会兼职

1、流体力学、燃烧学、航空航天领域重要SCI期刊审稿人：Journal of Fluid Mechanics, Physics of Fluids, Combustion and Flame, Combustion Science and Technology, AIAA Journal, Chinese Journal of Aeronautics, Aerospace Science and Technology等
2、国际期刊Aerospace客座编辑

近年来主要发表论文

[1] X. Shao, Z. Zhang, L. Shi, H. Huang, C. Y. Wen. Effects of swirling inflow on the stability and combustion mode of rotating detonations. Physics of Fluids, 2024, 36: 026116.

[2] W. Zhang, Z. Zhang, X. Han, C. Yuan, Y. Liu, L. Ma, W. Ren. On the determination of the standing oblique detonation wave in an engine combustor using laser absorption spectroscopy of hydroxyl radical. Aerospace Science and Technology, 2024, 152: 109344.

[3] G. Zhao, T. Ma, Z. Chen, Z. Zhang, J. Hao, C. Y. Wen. Investigation of streamwise streak characteristics over a compression ramp at Mach 4. Physics of Fluids, 2024, 36: 104121.

[4] Y. Liu, X. Han, Z. Zhang. Study on the propulsive performance of oblique detonation engine. Energy, 2024, 292: 130519.

[5] X. Han, Y. Liu, Z. Zhang, W. Zhang, C. Yuan, G. Han, Z. Jiang. Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model. Combustion and Flame, 2023, 258: 113102.

[6] Z. Zhang, Z. Jiang. Numerical Investigation of transverse-jet-assisted initiation of oblique detonation waves in a combustor. Aerospace, 2023, 10: 1033.

[7] Z. Zhang, Y. Liu, C. Wen. Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner. Journal of Fluid Mechanics, 2022, 940: A29.

[8] Z. Zhang, C. Wen, C. Yuan, Y. Liu, G. Han, C. Wang, Z. Jiang. An experimental study of formation of stabilized oblique detonation waves in a combustor. Combustion and Flame, 2022, 237: 111868.

[9] Z. Zhang, C. Wen, W. Zhang, Y. Liu, Z. Jiang. A theoretical method for solving shock relations coupled with chemical equilibrium and its applications. Chinese Journal of Aeronautics, 2022, 35(6): 47–62.

[10] Z. Zhang, C. Wen, W. Zhang, Y. Liu., Z. Jiang. Formation of stabilized oblique detonation waves in a combustor. Combustion and Flame, 2021, 223: 423–436.

[11] Z. Jiang. Z. Zhang, Y. Liu, C. Wang, C. Luo. Criteria for hypersonic airbreathing propulsion and its experimental verification. Chinese Journal of Aeronautics, 2021, 34(3): 94–104.

[12] W. Zhang, Z. Zhang, Z. Jiang, X. Han, Y. Liu, C. Wang. Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition. AIP Advances, 2021, 11: 125119.

[13] Z. J. Zhang, C. Y. Wen, Y. F. Liu, D. L. Zhang, Z. L. Jiang. Effects of different particle size distributions on aluminum particle–air detonation. AIAA Journal, 2020, 58(7): 3115–3128.

[14] Z. Zhang, K. Ma, W. Zhang, X. Han, Y. Liu, Z. Jiang. Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection. Aerospace Science and Technology, 105, 106054, 2020.

[15] H. Teng, S. Liu, Z. Zhang. Unsteady combustion mode with a super-high frequency induced by a curved shock. Physics of Fluids, 2020, 32: 116101.

[16] K. Wang, Z. Zhang, P. Yang, H. Teng. Numerical study on reflection of an oblique detonation wave on an outward turning wall. Physics of Fluids, 2020, 32: 046101.

[17] K. Ma, Z. Zhang, Y. Liu, Z. Jiang. Aerodynamic principles of shock-induced combustion ramjet engines. Aerospace Science and Technology, 2020, 103: 105901.

[18] Z. Zhang, C. Wen, Y. Liu, D. Zhang, Z. Jiang. Application of CE/SE method to gas-particle two-phase detonations under a Eulerian-Lagrangian framework. Journal of Computational Physics, 2019, 394: 18–40.

[19] Y. Fang, Z. Zhang, Z. Hu. Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures. International Journal of Hydrogen Energy, 2019, 44: 23429–23435.

[20] Y. Fang, Z. Zhang, Z. Hu, X. Deng. Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures. Aerospace Science and Technology, 2019, 92: 676–684.

[21] J. Peng, Z. Zhang, Z. Hu, Z. Jiang. A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections. Aerospace Science and Technology, 2019, 89: 299–306.