[1] Li Y H, Liang H, Ma Q Y, et al. Experimental investigation on airfoil suction side flow separation by pulse plasma aerodynamic actuation[J]. Acta Aeronoutica et Astronautica Sinica, 2008, 29(6): 1429-1435(in Chinese).
李应红，梁华，马清源，等. 脉冲等离子体气动激励抑制翼型吸力面流动分离的实验研究[J]. 航空学报, 2008, 29(6): 1429-1435.
[2] Wu Y, Li Y H. Progress and outlook of plasma flow con-trol[J]. Acta Aeronoutica et Astronautica Sinica, 2015, 36(2): 381-405(in Chinese).
吴云，李应红. 等离子体流动控制研究进展与展望 [J]. 航空学报, 2015, 36(2): 381-405.
[3] Wang J J, Choi K S, Feng L H, Jukes T N, Whalley R D. Recent developments in DBD plasma flow control[J]. Progress in Aerospace Sciences, 2013, 62:52-78.
[4] Zhang P F, Liu A B, Wang J J. Aerodynamic modification of a NACA 0012 aerofoil by trailing-edge plasma Gurney flap[J]. AIAA Journal, 2009, 47(10):2467-2474.
[5] Che X K, Nie W S, Hou Z Y, et al. High altitude plasma flow control simulation through ground experiment[J]. Acta Aeronoutica et Astronautica Sinica, 2015, 36(2): 441-448(in Chinese).
车学科，聂万胜，侯志勇，等. 地面实验模拟高空等离子体流动控制效果[J]. 航空学报, 2015, 36(2): 441-448.
[6] Che X K, Shao T, Nie W S, Yan P. Numerical simulation on a nanosecond-pulse surface dielectric barrier discharge actuator in near space[J]. Journal of physics D: applied physics, 2012, 45:145201.
[7] Shi Z W, Fan B G. Experimental study on flow control characteristics of different plasma actuator[J]. Acta Aero-noutica et Astronautica Sinica, 2011, 32(9): 1583-1589(in Chinese).
史志伟，范本根. 不同结构等离子体激励器的流场特性实验研究[J]. 航空学报, 2011, 32(9): 1583-1589.
[8] Du H, Shi Z W, GENG X. Experimental study of direc-tional-lateral aerodynamic moment control of micro air vehicle by plasma actuator[J]. Acta Aeronoutica et Astro-nautica Sinica, 2012, 33(10): 1781-1790(in Chinese).
杜海，史志伟，耿玺. 等离子体激励器对微型飞行器横航向气动力矩控制的实验研究[J]. 航空学报, 2012, 33(10): 1781-1790.
[9] Feng L H, Jukes T N, Choi K S. Flow control over a NACA 0012 aerofoil using dielectric barrier discharge plasma actuator with a Gurney flap[J]. Experimental in Fluids, 2012, 52:1533-1546.
[10] Meng X S, Li H X, TANG H R, et al. Exploring flow features of conical forebody versus angle of attack under plasma actuation[J]. Journal of Northwestern Polytech-nical University, 2012, 30(3): 402-406(in Chinese).
孟宣市，李华星，唐花蕊，等. 不同迎角下前体涡流动的等离子体控制特性[J]. 西北工业大学学报, 2012, 30(3): 402-406.
[11] Meng X S, GUO Z X, LUO S J, et al. Control of asym-metric vortices over a slender conical forebody using plasma actuator[J]. Acta Aeronoutica et Astronautica Sinica, 2010, 3(3): 500-505(in Chinese).
孟宣市，郭志鑫，罗时钧，等. 细长圆锥前体非对称涡流场的等离子体控制[J]. 航空学报, 2010, 3(3): 500-505.
[12] Lin Q, Huang Y Y, Pan B, Niu Z G. Investigation on new-style plasma active flow controllers and its induced flow field[J]. Acta Aerodynamica Sinica, 2011, 32(1): 312-317(in Chinese).
林麒，黄印阳，潘波, 牛中国. 新型等离子体主动流动控制器及其诱导流场研究[J]. 空气动力学学报, 2012, 30(3): 146-150.
[13] Pan B, Shen J M, Lin Q. Experiment on flow field and thrust induced by plasma actuator[J]. Journal of Propul-sion technology, 2011, 32(1): 146-150(in Chinese).
潘波，沈锦明，林麒. 等离子体激励器流场测量及诱导推力实验 [J]. 推进技术, 2011, 32(1): 146-150.
[14] Wu Y, Li Y H, Jia M. Experimental investigation into characteristics of plasma aerodynamic actuation generated by dielectric barrier discharge[J]. Chinese Journal of Aeronautics, 2010, 23(1): 39-45.
[15] Wang L, Luo Z B, Xia Z X. Energy efficiency and per-formance characteristics of plasma synthetic jet[J]. Acta Physica Sinica, 2013, 62(12): 1-10(in Chinese).
王林，罗振兵，夏智勋. 等离子体合成射流能量效率及工作特性研究[J]. 物理学报, 2013, 62(12): 1-10.
[16] Zhu Y F, Wu Y, Cui W, et al. Numerical simulation and experimental validation of pulsed nanosecond plasma aerodynamic actuation in air under atmospheric pressure[J]. Acta Aeronoutica et Astronautica Sinica, 2013, 34(9): 2081-2091(in Chinese).
朱益飞，吴云，崔巍等. 大气压空气纳秒脉冲等离子体气动激励特性数值模拟与实验验证[J]. 航空学报, 2013, 34(9): 2081-2091.
[17] Wang L, Xia Z X, Luo Z B, Zhou Y, Zhang Y. Experi-mental study on the characteristics of a two-electrode plasma synthetic jet actuator[J]. Acta Physica Sinica, 2014, 63(19): 194702(in Chinese).
王林，夏智勋，罗振兵，周岩，张宇. 两电极等离子体合成射流激励器工作特性研究[J]. 物理学报, 2014, 63(19): 194702.
[18] Liu Z F, Wang L Z, Fu S. Study of flow induced by sine wave and saw tooth plasma actuators[J]. SCIENCE CHINA Physics, Mechanics & Astronomy, 2011, 54(11): 2033–2039.
[19] Nie C Q, Li G, Zhu J Q. Investigation of dielectric barrier discharge plasma flow control[J]. SCIENCE CHINA Physics, Mechanics & Astronomy, 2008, 51(7): 1064–1072
[20] Zhang X, Huang Y, Wang W B, et al. Unmanned air vehicle flow separation control using dielectric barrier discharge plasma at high wind speed[J]. SCIENCE CHINA Physics, Mechanics & Astronomy, 2014, 57(6): 1160-1168.
[21] Roth J R, Sherman D M, Wilkinson S P. Boundary layer flow control with a one atmosphere uniform glow dis-charge plasma[C] // 36th Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 1998: 1-28.
[22] Sidorenko A A, Budovsky A D, Pushkarev A V. Flight testing of DBD plasma separation control system[C] // 46th Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2008: 1-9.
[23] Friedrichs W. Unmanned Aerial Vehicle for flow control experiments with dielectric barrier discharge plasma ac-tuators[D]. Darmstadt: Technical University of Darmstadt, 2014.
[24] Zhang X, Li H X, Huang Y. Wing Flow Separation Con-trol Using Asymmetrical and Symmetrical Plasma Actua-tor[J]. Journal of Aircraft, 2017, 54(1): 301-309.
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