Chinese Journal of Theoretical and Applied Mechanics ›› 2018, Vol. 50 ›› Issue (4): 776-786.DOI: 10.6052/0459-1879-17-392
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Zhang Xin1,*(), Huang Yong2, Yang Pengyu2, Tang Kun2, Li Huaxing1
Online:
2018-07-18
Published:
2018-08-17
Contact:
Zhang Xin
CLC Number:
Zhang Xin, Huang Yong, Yang Pengyu, Tang Kun, Li Huaxing. INVESTIGATION ON THE TURBULENT CHARACTERISTICS OF THE JET INDUCED BY A PLASMA ACTUATOR[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(4): 776-786.
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Fig.12 Distributions of the maximum streamwise r.m.s. velocity, the maximum vertical r.m.s. velocity, and the maximum Reynolds shear stress over the surface of flat plate (Up-p=9.8kV,fAC=3kHz) |||| (a) The maximum streamwise r.m.s. velocity ; (b) The maximum vertical r.m.s. velocity; (c) The maximum Reynolds shear stress
[1] | Corke TC, Enloe CL, Wilkinson SP.Dielectric barrier discharge plasma actuators for flow control.Annual Review of Fluid Mechanics, 2010, 42(1): 505-529 |
[2] | Li YH, Wu Y, Li J.Review of the investigation on plasma flow control in China.International Journal of Flow Control, 2013, 4(1): 1-18 |
[3] | 吴云, 李应红. 等离子体流动控制研究进展与展望. 航空学报, 2015, 36(2): 381-405 |
(Wu Yun, Li Yinghong.Progress and outlook of plasma flow control.Acta Aeronoutica et Astronautica Sinica, 2015, 36(2): 381-405 (in Chinese)) | |
[4] | Wang JJ, Choi KS, Feng LH, et al.Recent developments in DBD plasma flow control.Progress in Aerospace Sciences, 2013, 62: 52-78 |
[5] | Zhang PF, Liu AB, Wang JJ.Aerodynamic modification of a NACA 0012 aerofoil by trailing-edge plasma Gurney flap.AIAA Journal, 2009, 47(10): 2467-2474 |
[6] | 冯立好, 王晋军, Choi KS.等离子体环量控制翼型增升的实验研究. 力学学报, 2013, 45(6): 815-821 |
(Feng Lihao, Wang Jinjun, Choi Ks. Experimental investigation on lift increment of a plasma circulation control airfoil.Acta Mechanica Sinica, 2013, 45(6): 815-821 (in Chinese)) | |
[7] | 杜海, 史志伟, 程克明. 纳秒脉冲等离子体分离流控制频率优化及涡运动过程分析. 航空学报, 2016, 37(7): 2102-2111 |
(Du Hai, Shi Zhiwei, Cheng Keming.Frequency optimization and vortex dynamic process analysis of separated flow control by nanosecond pulsed plasma dischage.Acta Aeronoutica et Astronautica Sinica, 2016, 37(7): 2102-2111 (in Chinese)) | |
[8] | 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. 航空学报, 2015, 36(2): 441-448 |
(Che Xueke, Nie Wansheng, Hou Zhiyong, et al.High altitude plasma flow control simulation through ground experiment.Acta Aeronoutica et Astronautica Sinica, 2015, 36(2): 441-448 (in Chinese)) | |
[9] | Che XK, Shao T, Nie WS, et al.Numerical simulation on a nanosecond-pulse surface dielectric barrier discharge actuator in near space.Journal of Physics D: Applied Physics, 2012, 45: 145201 |
[10] | 孟宣市, 杨泽人, 陈琦等. 低雷诺数下层流分离的等离子体控制. 航空学报, 2016, 37(7): 2112-2122 |
(Meng Xuanshi, Yang Zeren, Chen Qi, et al.Laminar separation control at low Reynolds numbers using plasma actuator.Acta Aeronoutica et Astronautica Sinica, 2016, 37(7): 2112-2122 (in Chinese)) | |
[11] | 赵光银, 李应红, 梁华等. 纳秒脉冲表面介质阻挡等离子体激励唯象学仿真. 物理学报, 2015, 64(1): 015101-015112 |
(Zhao Guangyin, Li Yinghong, Liang Hua, et al.Phenomenological modeling of nanosecond pulsed surface dielectric barrier discharge plasma actuation for flow control.Acta Physica Sinica, 2015, 64(1): 015101-015112 (in Chinese)) | |
[12] | 林麒, 黄印阳, 潘波等. 新型等离子体主动流动控制器及其诱导流场研究. 空气动力学学报, 2012, 30(3): 146-150 |
(Lin Qi, Huang Yinyang, Pan Bo, et al.Investigation on new-style plasma active flow controllers and its induced flow field.Acta Aerodynamica Sinica, 2011, 32(1): 312-317 (in Chinese)) | |
[13] | 史志伟, 杜海, 李铮等. 等离子体流动控制技术原理及典型应用. 高压电器, 2017, 53(4): 72-78 |
(Shi Zhiwei, Du Hai, Li Zheng, et al.Mechanism and applications of plasma flow control technology.High Voltage Apparatus, 2017, 53(4): 72-78 (in Chinese)) | |
[14] | Feng LH, Shi TY, Liu YG.Lift enhancement of an airfoil and an unmanned aerial vehicle by plasma Gurney flaps.AIAA Journal, 2017, 55(5): 1622-1632 |
[15] | Xu SY, Cai JS, Li J.Modeling and simulation of plasma gas flow driven by a single nanosecond-pulsed dielectric barrier discharge.Physics of Plasma, 2016, 23(10): 505-529 |
[16] | Wu Z, Wong CW, Wang L, et al.A rapidly settled closed-loop control for airfoil aerodynamics based on plasma actuation.Experiments in Fluids, 2015, 56: 1-15 |
[17] | 吴云, 张海灯, 于贤君等. 轴流压气机等离子体流动控制. 工程热物理学报, 2017, 38(7): 1396-1414 |
(Wu Yun, Zhang Haideng, Yu Xianjun, et al.Plasma flow control of axial compressor.Journal of Engineering Thermophysics, 2017, 38(7): 1396-1414 (in Chinese)) | |
[18] | 李应红, 吴云, 张海灯等. 等离子体激励式压气机. 推进技术, 2017, 38(10): 2164-2171 |
(Li Yinghong, Wu Yun, Zhang Haideng, et al.Plasma actuated compressor.Journal of Propulsion Technology, 2017, 38(10): 2164-2171 (in Chinese)) | |
[19] | 魏彪, 梁华, 牛中国等. 三角翼微秒脉冲等离子体流动控制的试验研究. 高电压技术, 2016, 42(3): 782-789 |
(Wei Biao, Liang Hua, Niu Zhongguo, et al.Experimental investigation of delta-wing flow control by microsecond pulse plasma actuator.High Voltage Engineering, 2016, 42(3): 782-789 (in Chinese)) | |
[20] | 吴阳阳, 贾敏, 王蔚龙等. 新型介质阻挡放电等离子体激励器的放电与诱导流动特性实验. 电工技术学报, 2016, 31(24): 45-53 |
(Wu Yangyang, Jia Min, Wang Weilong, et al.Experimental research on the discharge and induced flow characteristics of a new dielectric barrier discharge plasma actuator.Transaction of China Electrotechnical Society, 2016, 31(24): 45-53 (in Chinese)) | |
[21] | 陈庆亚, 田希晖, 车学科. 平流层表面介质阻挡放电等离子体流动控制相似准则验证. 高电压技术, 2016, 42(3): 821-827 |
(Chen Qingya, Tian Xihui, Che Xueke.Verification on similarity of SDBD plasma actuator induced jet for stratospheric flow control.High Voltage Engineering, 2016, 42(3): 821-827 (in Chinese)) | |
[22] | Yan HJ, Yang L, Qi XH, et al.Improving thrust by pulse induced breakdown enhancement in AC surface dielectric barrier discharge actuators for airflow control.Journal of Physics D: Applied Physics, 2016, 42(1): 505-529 |
[23] | 于金革, 牛中国, 梁华等. 等离子体用于三角翼模型流动控制试验研究. 空气动力学学报, 2017, 35(2): 305-309 |
(Yu Jinge, Niu Zhongguo, Liang Hua, et al.Experimental investigation on delta wing flow control by plasma.Acta Aerodynamica Sinica, 2017, 35(2): 305-309 (in Chinese)) | |
[24] | 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. 航空学报, 2012, 33(10): 1781-1790 |
(Du Hai, Shi Zhiwei, Geng Xi.Experimental study of directional-lateral aerodynamic moment control of micro air vehicle by plasma actuator.Acta Aeronoutica et Astronautica Sinica, 2012, 33(10): 1781-1790 (in Chinese)) | |
[25] | 车学科, 聂万胜, 周朋辉等. 亚微秒脉冲表面介质阻挡放电等离子体诱导连续漩涡的研究. 物理学报, 2013, 62(22): 279-288 |
(Che Xueke, Nie Wansheng, Zhou Penghui, et al.Study on continuous vortices induced by sub-microsecond pulsed surface dielectric barrier discharge plasma.Acta Physica Sinica, 2013, 62(22): 279-288 (in Chinese)) | |
[26] | Wu Y, Li YH, Jia M, et al.Experimental investigation into characteristics of plasma aerodynamic actuation generated by dielectric barrier discharge.Chinese Journal of Aeronautics, 2010, 23(1): 39-45 |
[27] | Roth JR, Sherman DM, Wilkinson SP.Boundary layer flow control with a one atmosphere uniform glow discharge plasma//36th Aerospace Sciences Meeting and Exhibit, Reno, 1998: 1-28 |
[28] | Forte M, Jolibois J, Pons J, et al.Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control.Experiments in Fluids, 2007, 43(6): 917-928 |
[29] | Kelley CL, Bowles PO, Cooney J.Leading edge separation control using alternating-current and nanosecond pulse plasma actuator.AIAA Journal, 2014, 52(9): 1871-1884 |
[30] | Zhang X, Huang Y, Wang XN.Turbulent boundary layer separation control using plasma actuator at Reynolds number 2 000 000.Chinese Journal of Aeronautics, 2016, 29(5): 1237-1246 |
[31] | Sekimoto S, Nonomura T, Fujii K.Burst-mode frequency effects of dielectric barrier discharge plasma actuator for separation control.AIAA Journal, 2017, 55(4): 1385-1392 |
[32] | Zhang X, Li HX, Huang Y.Wing flow separation control using asymmetrical and symmetrical plasma actuator.Journal of Aircraft, 2017, 54(1): 301-309 |
[33] | Zhang X, Huang Y, Wang WB.Unmanned air vehicle flow separation control using dielectric barrier discharge plasma at high wind speed.Science China: Physics, Mechanics & Astronomy, 2014, 57(6): 1160-1168 |
[34] | Jukes TN, Choi K-S, Johnson GA, et al.Turbulent boundary-layer control for drag reduction using surface plasma//2nd AIAA Flow Control Conference, Portland, 2004: 1-11 |
[35] | 梁华, 李应红, 宋慧敏等. 等离子体气动激励诱导空气流动的PIV研究. 实验流体力学, 2011, 25(4): 22-25 |
(Liang Hua, Li Yinghong, Song Huimin, et al.PIV investigation on flow induced by plasma aerodynamic actuation.Journal of Experimental in Fluids Mechanics, 2011, 25(4): 22-25 (in Chinese)) | |
[36] | 梁华, 吴云, 李军等. 等离子体气动激励改善增升装置气动性能的试验. 航空学报, 2016, 37(8): 2603-2613 |
(Liang Hua, Wu Yun, Li Jun, et al.Test of high lift system flow control by plasma aerodynamic actuation.Acta Aeronoutica et Astronautica Sinica, 2016, 37(8): 2603-2613 (in Chinese)) | |
[37] | Chun DH, Schwarz WH.Stability of the plane incompressible viscous wall jet subjected to small disturbances.Physics of Fluids, 1967, 10: 911-915 |
[38] | Whalley RD, Choi KS.The starting vortex in quiescent air induced by dielectric-barrier-discharge plasma.Journal of Fluid Mechanics, 2013, 703: 192-203 |
[39] | 刘沛清. 自由紊动射流理论. 北京: 北京航空航天大学出版社, 2008 |
(Liu Peiqing.The Theory of Free Turbulent Jet. Beijing: Beihang University Press, 2008 (in Chinese)) | |
[40] | Zhou J, Adrian RJ, Balachandar S.Mechanisms for generating coherent packets of hairpin vortices in channel flow.Journal of Fluid Mechanics, 1999, 387: 353-396 |
[41] | Yarusevych S, Sullivan P, Kawall JG.On vortex shedding from an airfoil in low Reynolds number flow.Journal of Fluid Mechanics, 2009, 632: 245-271 |
[42] | Feng LH, Choi KS, Wang JJ.Flow control over an airfoil using virtual Gurney flaps.Journal of Fluid Mechanics, 2015, 767: 595-626. |
[43] | Boutilier MSH, Yarusevych S.Separated shear layer transition over an airfoil at a low Reynolds number.Physics of Fluids, 2012, 24: 084105 |
[44] | Burgmann S, Schroder W.Investigation of the vortex induced unsteadiness of a separation bubble via time-resolved and scanning PIV measurements.Experiments in Fluids, 2008, 45(4): 675-691 |
[45] | Hatman A, Wang T.A prediction model for separated flow transition.Journal of Turbomachinery, 1998, 121(3): 594-602 |
[46] | Spalart P R.Airplane trailing vortices.Annual Review of Fluid Mechanics, 1998, 30: 107-138 |
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