赵国庆，南京航空航天大学副研究员，硕士生导师，磁悬浮技术与振动控制学会专业委员会、中国空气动力学会测控专业委员会委员，中国航空学会流动控制与热管理分会青年委员，《南京航空航天大学学报》中英文版青年编委。研究方向为直升机空气动力学、计算流体力学、主动流动控制、高性能旋翼设计等。获国防科技进步一等奖、二等奖各一项（均排4），航空学会科技进步二等奖1项（排5）。出版《先进旋翼设计空气动力学》专著（排2），在《Journal of Aircraft》、《Aerospace Science and Technology》、《航空学报》中/英文版等航空领域著名期刊和学术会议发表论文100余篇，其中SCI收录论文35篇，EI收录论文28篇。作为负责人承担173重点项目课题/专题、预研专项、国家自然科学基金面上项目、重点实验室基金等项目10余项，授权发明专利38项（含3项国际专利）。

Scopus个人网址链接，代表性论文：

[1]    Zhao Guoqing, Jing Simeng, Chen Xi, Zhao Qijun, Wang Bo. Analysis of virtual profiles of rotor sections and loss of angle of attack in hovering state. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2024. DOI:10.1177/09544100251321961.(SCI)

[2]    Zhao Guoqing, Cui ZhuangZhuang, Zhao Qijun, Chen Xi. Investigations on trimming strategy and unsteady aerodynamic characteristics of tiltrotor in conversion procedure. Aerospace, 2024, 11: 632. (SCI)

[3]    Zhao Guoqing, Zhao Qijun, Chen Xi. Wind‑tunnel tests of synthetic jet control effects on airfoil flow separation. Scientific Reports, 2023, 12:21994. (SCI)

[4]    Zhao Guoqing, Zhao Qijun, Li Peng, Wang Bo. Parametric analyses for effects of rpm and diameter on tiltrotor aerodynamic performances in hovering and cruise mode. International Journal of Aeronautical and Space Sciences, 2021, 22(3):479-488. (SCI)

[5]    Zhao Guoqing, Zhao Qijun, Li Peng, Wang Bo. Numerical investigations for passive and active flow control on tiltrotor-wing aerodynamic interactions. Journal of Aerospace Engineering, 2021, 34(6):04021094. (SCI)

[6]    Zhao Guoqing, Zhao Qijun, Gu Yunsong, Chen Xi. Experimental investigations for parametric effects of dual synthetic jets on delaying stall of a thick airfoil. Chinese Journal of Aeronautics, 2016, 29(2): 346-357. (SCI)

[7]    Zhao Guoqing, Zhao Qijun, Chen Xi. New 3-D ice accretion method of hovering rotor including effects of centrifugal force. Aerospace Science and Technology, 2016, 48:122-130. (SCI)

[8]    Zhao Guoqing, Zhao Qijun. Dynamic stall control optimization of rotor airfoil via variable droop leading edge. Aerospace Science and Technology, 2015, 43:406-414. (SCI)

[9]    Zhao Guoqing, Zhao Qijun. Parametric analyses for synthetic jet control on separation and stall over rotor airfoil. Chinese Journal of Aeronautics, 2014, 27(5):1051-1061. (SCI)

[10] Yuan Xin, Bian Wei, Zhao Qijun, Zhao Guoqing. Numerical investigation of aerodynamic interactions for the coaxial rotor system in low-speed forward flight. Aerospace Science and Technology, 2024, 149: 109148.(通讯作者, SCI)

[11] Jing Simeng, Zhao Guoqing, Gao Yuan, Zhao Qijun. Effects of leading edge radius on stall characteristics of rotor airfoil. Aerospace, 2024, 11(6): 470.( 通讯作者, SCI)

[12] Yang Tao, Chen Xi, Wang Bo, Zhao Qijun, Zhao Guoqin. Perturbed polynomial with multiple free-parameters reconstructed WENO schemes. International Journal for Numerical Methods in Fluid, 2024. https://doi.org/10.1002/fld.5370.(通讯作者, SCI)

[13] Yang Tao, Zhao Guoqing, Zhao Qijun. Novel TENO Schemes with Improved Accuracy Order Based on Perturbed Polynomial Reconstruction. Journal of Computational Physics, 2023, 488: 112219. (SCI)

[14] Zhu Zhijie, Zhao Guoqing, Zhao Qijun. Fast and high-precision compressible flowfield inference method of transonic airfoils based on Attention Unet. Physics of Fluids, 2024, 36: 036111. (SCI)

[15] Zhao Qijun, Zhao Guoqing, Wang Bo, Wang Qing, et al. Robust Navier-Stokes method for predicting unsteady flowfield and aerodynamic characteristics of helicopter rotor. Chinese Journal of Aeronautics, 2018, 31(2): 214-224. (SCI)

[16] Bian Wei, Zhao Guoqing, Chen Xi, Wang Bo, Zhao Qijun. High-fidelity simulation of blade vortex interaction of helicopter rotor based upon TENO scheme. Chinese Journal of Aeronautics, 2023, 36(10): 275-292. (SCI)

[17] Jing Simeng, Zhao Qijun, Zhao Guoqing. Multi-objective airfoil optimization under unsteady-freestream dynamic stall conditions. Journal of Aircraft, 2023, 60(2): 293-309. (SCI)

[18] Zhang Hang, Zhao Guoqing, Zhao Qijun, Wang Bo, Bian Wei. Influence of Mach numbers and telescoping positions on aerodynamic performance of variable diameter-and-speed tilt-rotors. International Journal of Aeronautical and Space Sciences, 2024, 26:539-561. (SCI)

[19] 赵国庆, 招启军, 顾蕴松等. 合成射流对失速状态下翼型大分离流动控制的试验研究. 力学学报, 2015, 47(2):351-355.(EI)

[20] 赵国庆, 招启军．基于目标压力分布的旋翼先进气动外形反设计分析方法．航空学报, 2014, 35(3):744-755. (EI)