飞行器设计系
黄志伟

黄志伟

职务:长聘教轨副教授

电子邮件:zhiwei@sjtu.edu.cn

办公地址:上海交通大学航空航天学院A202

 

工作经历

时间 任职单位 职务

2022.07 – 今

上海交通大学 长聘教轨副教授

2018.10 – 2022.01

National University of Singapore (NUS)

Postdoctoral Research Fellow

教育背景

时间 毕业院校 学历

2013.09 – 2018.09

西北工业大学

博士

2012.09 – 2015.03

西北工业大学

硕士

2008.09 – 2012.07

西北工业大学

本科

研究方向

(1) 吸气式高超声速先进空天动力技术

(2) 超声速湍流燃烧理论、实验与计算

(3) 气相及气-液两相爆轰高精度数值模拟

主要科研项目

(1) Prediction of soot formation from turbulent flames under gas turbine combustion condition, Ministry of Education (MOE), Singapore. 2019.03 – 2022.02, 参与

(2) Modelling extinction dynamics in turbulent flames, Ministry of Education (MOE), Singapore. 2017.09 – 2021.08, 参与

(3) Numerical simulations of rotating detonation engines for next-generation aero-propulsion systems, Ministry of Education (MOE), Singapore. 2019.04 – 2021.03, 参与

(4) Large eddy simulation of high-speed turbulent flows, Ministry of Defence (MINDEF), Singapore. 2019.01 – 2019.12, 参与

代表性论文专著

(1) ZW Huang, HW Zhang. Ignition and deflagration-to-detonation transition modes in ethylene/air mixtures behind a reflected shock. Physics of Fluids, 34 (8): 086105, 2022.

(2) ZW Huang, MJ Cleary, ZY Ren, HW Zhang. Large eddy simulation of a supersonic lifted hydrogen flame with sparse-Lagrangian multiple mapping conditioning approach. Combustion and Flame, 238: 111756, 2022.

(3) ZW Huang, MJ Zhao, Y Xu, GZ Li, HW Zhang. Eulerian-Lagrangian modelling of detonative combustion in two-phase gas-droplet mixtures with OpenFOAM: Validations and verifications. Fuel, 286: 119402, 2021.

(4) ZW Huang, HW Zhang. On the interactions between a propagating shock wave and evaporating water droplets. Physics of Fluids, 32 (12): 123315, 2020. (Editor’s Pick)

(5) ZW Huang, MJ Cleary, HW Zhang. Application of the sparse-Lagrangian multiple mapping conditioning approach to a model supersonic combustor. Physics of Fluids, 32 (10): 105120, 2020.

(6) ZW Huang, HW Zhang. Investigations of autoignition and propagation of supersonic ethylene flames stabilized by a cavity. Applied Energy, 265: 114795, 2020.

(7) ZW Huang, MJ Zhao, HW Zhang. Modelling n-heptane dilute spray flames in a model supersonic combustor fueled by hydrogen. Fuel, 264: 116809, 2020.

(8) ZW Huang, HW Zhang. Numerical investigations of mixed supersonic and subsonic combustion modes in a model combustor. International Journal of Hydrogen Energy, 45 (1): 1045‒1060, 2020.

(9) ZW Huang, GQ He, S Wang, F Qin, XG Wei, L Shi. Simulations of combustion oscillation and flame dynamics in a strut-based supersonic combustor. International Journal of Hydrogen Energy, 42 (12): 8278‒8287, 2017.

(10) ZW Huang, GQ He, F Qin, R Xue, XG Wei, L Shi. Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor. Acta Astronautica, 129: 260‒270, 2016.

(11) ZW Huang, GQ He, F Qin, DG Cao, XG Wei, L Shi. Large eddy simulation of combustion characteristics in a kerosene fueled rocket-based combined-cycle engine combustor. Acta Astronautica, 127: 326‒334, 2016. (ESI hot paper)

(12) ZW Huang, GQ He, F Qin, XG Wei. Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor. International Journal of Hydrogen Energy, 40 (31): 9815‒9824, 2015.

(13) 黄志伟, 何国强, 秦飞, 魏祥庚. 支板增强混合超声速燃烧的大涡模拟. 固体火箭技术, 38 (5): 664‒670 & 678, 2015.

(14) F Qin, ZW Huang, GQ He, S Wang, XG Wei, B Liu. Flame stabilization mechanism study in a hydrogen-fueled model supersonic combustor under different air inflow conditions. International Journal of Hydrogen Energy, 42 (33): 21360‒21370, 2017.

(15) ZW Huang, HW Zhang. Two-phase interactions between propagating shock waves and evaporating water droplets. 15th Triennial International Conference on Liquid Atomization and Spray Systems, 2021.

(16) ZW Huang, MJ Zhao, HW Zhang. Simulation of spray combustion of n-heptane in a model supersonic combustor with pilot hydrogen. 27th International Colloquium on the Dynamics of Explosions and Reactive Systems, 2019.

(17) ZW Huang, HW Zhang, GQ He. Large eddy simulation of shock-induced ignition in an ethylene-fueled model supersonic combustor. 32nd International Symposium on Shock Waves, 2019.

(18) ZW Huang, GQ He, F Qin, S Wang, B Liu. Combustion characteristics of transverse hydrogen jet in a supersonic compact inlet/combustor model. 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, 2017.

(19) ZW Huang, GQ He, F Qin, XG Wei, DG Cao. Large eddy simulation of effects of primary rocket jet on low frequency combustion instability in a RBCC combustor. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA paper 2015-3623.

(20) ZW Huang, GQ He, F Qin, XG Wei, L Shi. Supersonic turbulent combustion characteristics of a rocket-based combined-cycle engine combustor. 10th Asia-Pacific Conference on Combustion, 2015.

(21) GQ He, ZW Huang, F Qin, YJ Wang, XG Wei. Effects of primary rocket nozzle expansion ratio on combustion oscillating characteristics in a RBCC engine combustor. 66th International Astronautical Congress, 2015.

(22) F Qin, ZW Huang, B Liu, XG Wei. Large eddy simulation of combustion characteristics in a hydrogen fueled model scramjet combustor. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA paper 2015-3619.

(23) F Qin, ZW Huang, XG Wei, XS Bai. Large eddy simulation of supersonic turbulent mixing and combustion. 9th Mediterranean Combustion Symposium, 2015.

 

学术兼职

(1) Defence Technology青年编委

(2) Combustion Institute (CI)、American Institute of Aeronautics and Astronautics (AIAA)、American Physical Society (APS)会员

(3) Proceedings of the Combustion Institute, Applied Energy, Physics of Fluids, Aerospace Science and Technology, Energy Conversion and Management, International Journal of Hydrogen Energy, Sustainable Energy Technologies and Assessments, Journal of Zhejiang University – Science A, Acta Astronautica等国际期刊常任审稿人

 

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