[1] Daiwen Jiang, Hui Zhang, Baochun Fan, Zijie Zhao, Mingyue Gui, Zhihua Chen “Vortex structures and drag reduction in turbulent channel flow with theeffect of space-dependent electromagnetic force”, Ocean Engineering 176 (2019) 74–83
[2] Jiang D.W., Zhang H., Fan B.C., Zhao Z.J., Li J., Gui M.Y., “Numerical study of the turbulent channel flow under space-dependent electromagnetic force control at different Reynolds numbers”, Applied Mathematics and Mechanics, 2019, 40(4), 435-448.
[3] Zijie Zhao, Y. D. Cui, Jiun-Ming Li, Jian-Guo Zheng, and B. C. Khoo, “On the boundary flow using pulsed nanosecond DBD plasma actuators”, Modern Physics Letters B, May 2018, Vol. 32, No. 12n13
[4] Zijie Zhao，Hui Zhang，Y. D. Cui, Jiun-Ming Li, Jian-Guo Zhengand B. C. Khoo,Flow “Separation Control by NS-DBD Plasma Actuator on NACA0015 Airfoil at Low Reynolds Number”, China Mechanics Conference 2017.8
[5] Zijie Zhao, Jiun-Ming Li, Jianguo Zheng, Y. D. Cui, B. C. Khoo, “Study of Shock and Induced Flow Dynamics by Nanosecond Dielectric-Barrier-Discharge Plasma Actuators”,, AIAA Journal, Vol. 53, No. 5 (2015), pp. 1336-1348.
[6] Zijie Zhao, Chao Gao, Feng Liu, Shijun Luo, “Plasma Flow control over Forebody at High Angle of Attack,” Modern Physics Letters B Vol.24,No.13(2010)1405-1408.
[7] 赵子杰，高超，张正科，“涡破裂诱导的垂尾抖振气动弹性分析”，航空学报，2015.7
[8] 赵子杰，高超，张正科，“新型人工转捩技术及风洞试验验证”，航空学报，2015, 36(6) , pp.1830-1838.
[9] Zijie Zhao, Jiun-Ming Li, Jianguo Zheng, Y. D. Cui, B. C. Khoo, “Study of shock and induced flow dynamics by pulsed nanosecond DBD plasma actuators”, AIAA 2014-0402, 52nd Aerospace Sciences Meeting, 2014,13-17 Jan, National Harbor, Maryland.
[10] Zijie Zhao, Xudong Ren, C. Gao, Juntao Xiong, Feng Liu, Shijun Luo, “Experimental Study of Shock Wave Oscillation on SC(2)-0714 Airfoil,” 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013-0537.
[11] Zijie Zhao, Chao Gao, Feng Liu, Shijun Luo, “Influence of Plasma Actuations on Forebody Side Forces and Wakes” 48 AIAA Aerospace Sciences Meeting, Orlando, Florida, 4-7 Jan 2010, 2010–1041.
[12] Zijie Zhao, Huaxing Li, Feng Liu, Shijun Luo, “Forward-Blowing Plasma Actuation over Forebody Asymmetric Vortex,” 47th AIAA Aerospace Sciences Meeting, Orland, , Florida, 5-8 Jan 2009, 2009-0752.
[13] Zijie Zhao, Chao Gao, Feng Liu, Shijun Luo “Study on the Characteristics of Separate Flow under the influence of Plasma Actuations on Forebody,” 2010Asia –Pacific International Symposium on Aerospace Technology(Vol1.1).
[14] Zijie Zhao, Jiun-Ming Li, Jianguo Zheng, Y. D. Cui, B. C. Khoo, "On the boundary flow using pulsed nanosecond DBD plasma actuators". International Journal of Modern Physics: Conference Series, (2015). (Singapore).
[15] Zijie Zhao, Y. D. Cui, "Aeroelastic Analysis of Vertical Tail Buffeting Induced by Vortex Breakdown". International Journal of Modern Physics (2015). Singapore: World Scientific. (Plenary paper) (Sixth International Symposium on Physics of Fluids, 6 - 9 Jul 2015, San Want Hotel Xining, Xining, China)
[16] Jianguo Zheng, Zijie Zhao, Jiun-Ming Li, Y. D. Cui and B. C. Khoo, “Numerical simulation of nanosecond pulsed dielectric barrier discharge actuator in a quiescent flow,” Phys. Fluids, Vol. 26, 2014, pp. 036102.
[17] Bo Li, Zijie Zhao,” Electromechanical deformation of dielectric elastomer in two types of pre-stretch”, EPL (Europhysics Letters) Vol. 106 No. 6, 2014.6
[18] Y. D. Cui, Zijie Zhao, Li Jiun-Ming, Zheng Jianguo and B C Khoo, "Flow separation control over a ramp with nanosecond pulsed plasma actuators". 30th International Symposium on Shock Waves (2015). Tel-Aviv: Springer. (30th International Symposium on Shock Waves, 19 - 24 Jul 2015, Dan Panorama Convention Center, Tel-Aviv, Israel)
[19] Y. D. Cui, Zijie Zhao, Bouremel Yann, Li Jiun-Ming, Zheng Jianguo, Hu Fu-Gang, Khoo Boo Cheong,” Studies on the configurations of nanosecond DBD pulse plasma actuators”, 19th Australasian Fluid Mechanics Conference (01 Dec 2014), RMIT, Melbourne, Australia
[20] Xudong Ren, Zijie Zhao, C. Gao, Juntao Xiong, Feng Liu, Shijun Luo, “Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel,” 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013-0791, 10.2514/6.2013-791
[21] Huarui Tang, Zijie Zhao, Huaxing Li, Feng Liu, Shijun Luo “Flow Asymmetry over a Conical Forebody under Plasma Actuation,” 5th AIAA Flow Control Conference, Chicago, Illinois, 28 Jun - 1 Jul 2010
[22] Jianguo Zheng, B. C. Khoo, Y. D. Cui, Zijie Zhao and Jiun-Ming Li, "Numerical study of control of flow separation over a ramp with nanosecond plasma actuator". International Journal of Modern Physics: Conference Series, (2015). (Singapore).
[23] Ujjaval Gupta, Hareesh Godaba, Zijie Zhao, Chee Kong Chui, Jian Zhu,” Tunable force/displacement of a vibration shaker driven by a dielectric elastomer actuator”, Extreme Mechanics Letters 2 (2015) 72–77
[24] Zhenbo Lu, Y. D. Cui, Debiasi Marco and Zijie Zhao, "A Tunable Dielectric Elastomer Acoustic Absorber". Acta Acustica united with Acustica, 101, no. 4 (2015).
[25] Li bo, Lu Zhenbo, Zhao Zijie, Cui Yongdong, Zhu Jian,” Vibration of Dielectric Elastomer Actuators”, The Third international conference on Electromechanically Active Polymer (EAP) transducers & artificial muscles (02 Jun 2013), Switzerland
[26] Lu Zhenbo, Cui Yongdong, Zhu Jian, Zhao Zijie, Debiasi Marco,’” Acoustic characteristics of a dielectric elastomer absorber”, The 166th Meeting of the Acoustical Society of America (01 Dec 2013), San Francisco, California
[27] Xudong Ren, C. Gao, Zijie Zhao, Juntao Xiong, Feng Liu, Shijun Luo, “Boundary-Layer Transition Effects on Aerodynamic Characteristics of AGARD-B Mode,” 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012, 10.2514/6.2012-1217
[28] Juntao Xiong, Ya Liu, Feng Liu, Shijun Luo, Zijie Zhao, Xudong Ren, Chao Gao, “Multiple Solutions and Buffet of Transonic Flow over the NACA0012 Airfoil,” 31st AIAA Applied Aerodynamics Conference, 2013-3026
[29] Meng Xuanshi, Wang Jianglei, Zijie Zhao, Feng Liu, Shijun Luo “Flow Control Mechanism Study over Conical Forebody Using Plasma Duty Cycle,” 2010Asia –Pacific International Symposium on Aerospace Technology(Vol1.1)