姓名:陈宗南 职称:助理教授 导师类型:硕导 团队名称:先进空天动力与能源团队 邮箱:chenzongnan@bitzh.edu.cn
|
主要研究领域为:1.主动流动控制、2.等离子体激励器设计及应用、3.激波/边界层干扰及不稳定性、4.实验、计算流体力学
2019年1月–2023年1月:香港理工大学大学 机械工程专业 博士学位
2015年9月–2016年6月:香港理工大学大学 机械工程专业 硕士学位
2010年9月–2014年6月:南京航空航天大学 飞行器设计与工程专业 学士学位
2025年1月– 至今 :北京理工大学(珠海) 空天信息学域 助理教授
2023年2月–2024年12月 : 香港理工大学 航空及民航工程学系 博士后
2017年4月–2018年12月 : 香港理工大学大学 机械工程学院 研究助理
近年来主要发表论文:
[1] G. Zhao, T. Ma, Z. Chen*, Z. Zhang, J. Hao, and C.-Y. Wen, "Investigation of streamwise streak characteristics over a compression ramp at Mach 4, " Physics of Fluids, vol. 36, no. 10, 2024. doi.org/10.1063/5.0224568 (Q1, 4.6)
[2] Z. Chen, J. Hao, and C.-Y. Wen*, "Numerical study on the periodic control of supersonic compression corner flow using a nanosecond pulsed plasma actuator,” International Journal of Heat and Mass Transfer, vol. 214, no. 124868, 2024. doi.org/10.1016/j.ijheatmasstransfer.2023.124868 (Q1, 5.2)
[3] Z. Chen, C. Wong, and C.-Y. Wen*, "Thermal Effects on the Performance of a Nanosecond Dielectric Barrier Discharge Plasma Actuator in Low Air Pressure," Physics of Fluids, No.35, pp. 017110, 2023. doi.org/10.1063/5.0127251 (Q1, 4.6)
[4] Z. Chen, J. Hao, and C.-Y. Wen*, "Control of Supersonic Compression Corner Flow Using a Plasma Actuator," Physics of Fluids, vol. 34, no. 7, 2022. doi.org/10.1063/5.0096511 (Q1, 4.6)
[5] Z. Chen and C.-Y. Wen*, "Flow Control of a D-Shaped Bluff Body Using Different DBD Plasma Actuators," Journal of Fluids and Structures, vol. 103, no. 103292, 2021. doi.org/10.1016/j.jfluidstructs.2021.103292 (Q2, 3.6)
[6] L. Shen, Z. Chen, and C.-Y. Wen*, "Thermal Effect on the Performance of an Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator," AIAA Journal, vol. 58, no. 8, pp. 3368-3377, 2020. doi.org/10.2514/1.J059264 (Q2, 2.5)
[7] Z. Chen, L. Shen, and C.-Y. Wen*, "Flow Control on a Bluff Body Using Dielectric Barrier Discharge Plasma Actuators," AIAA Journal, vol. 57, no. 7, pp. 2670-2674, 2019. doi.org/10.2514/1.J058196 (Q2, 2.5)
[8] L. Shen, Z. Chen, and C.-Y. Wen*, "Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods," J Vis Exp, no. 134, Apr 23, 2018. doi: 10.3791/57244 (Q3, 1.4)
[9] Z. Chen and C.-Y. Wen, "Flow Control of a D-Shaped Bluff Body Using Plasma Streamwise Vortex Generators," The 24th Annual Conference of HKSTAM 2020 in conjunction with The 16th Shanghai–Hong Kong Forum on Mechanics and Its Application, December 5, 2020, HK.
[10] Z. Chen, J. Hao, and C.-Y. Wen, "Flow Control on a Supersonic Compression Corner with the Nanosecond Surface Dielectric Barrier Discharge Plasma Actuators," The 7th International Conference on Jets, Wakes and Separated Flows, March 15-17, 2022, Nihon Univ., Tokyo, Japan.
[11] Z. Chen, J. Hao, and C.-Y. Wen, "Flow Control on a Supersonic Compression Corner with the Periodic Activations of Nanosecond Surface Dielectric Barrier Discharge Plasma Actuators," The 34th International Symposium on Shock Waves, July 16-21, 2023, Daegu, Korea
1. 主讲研究生课程《高等空气动力学/Advanced Aerodynamics》(全英文)
2. 主讲研究生课程《高等实验空气动力学/Advanced Experimental Aerodynamics》(全英文)
1. 担任 AIAA Journal,Journal of Physics D: Applied Physics,Physics of Fluids等航空航天领域、流体力学领域权威期刊审稿人。