期刊论文：
[1].C. Li, Z. Chen*, J. Hao, Z. Wu，"Global stability of hypersonic flow over a spherically blunted double cone," Chinese Journal of Aeronautics, 2025, accepted
[2].G. Zhao, C. Wong, X. Li, X. Liu, Z. Chen, J. Hao,P. Guo,Z. Zhang*, C.-Y. Wen "Convective instabilities in hypersonic compression ramp flows," AIAA J, 2025, accepted
[3].Z. Jiang, Z. Chen, L. Shi, Z. Zhang*, J. Hao, C.-Y Wen，"Numerical study of oblique detonation initiation assisted by local energy deposition," Aerospace Science and Technology, vol. 168, 2025, https://doi.org/10.1016/j.ast.2025.111278
[4].Z. Chen, G. Zhao, L.Shen*, Z. Chen, Z. Zhang, Z. Li, and C.-Y. Wen, "Wake flow separation control on a notchback Ahmed body using sawtooth plasma actuators," Physics of Fluids, vol. 37, no. 11, 2025. https://doi.org/10.1063/5.0300615
[5].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
[6].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
[7].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
[8].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
[9].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
[10].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
[11].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
[12].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
会议文章（经评审）:
[1]. X.Li, Z. Chen, J. Hao, "Experimental Investigation on 25°-50° Double-cone Flow at Mach 6," The 35th International Symposium on Shock Waves, July 04-15, 2025, Queenland, Australia.
[2]. 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.
[3]. 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.
[4]. 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.
