Drag reduction control of turbulent boundary layer based on plasma actuation
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摘要:
为了探究介质阻挡放电(dielectric barrier discharge, DBD)等离子体气动激励对平板湍流边界层的减阻情况,在控制来流速度为10.7 m/s的低速风洞中进行等离子体平板湍流边界层减阻控制实验。本实验重点研究了不同激励频率对湍流边界层的减阻控制效果,使用热线风速仪系统采集流向速度信号,获得边界层平均速度分布和脉动速度分布。对实验结果进行对比分析发现,在施加不同频率的等离子体激励之后,边界层内对数区速度明显减小;随着激励频率的增加,局部减阻率呈现出先增大后减小的趋势,在激励频率为200 Hz时,减阻率达到最大为7.4%。
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关键词:
- 介质阻挡放电(DBD) /
- 等离子体 /
- 平板 /
- 湍流边界层 /
- 减阻
Abstract:In order to further explore the drag reduction effect of the turbulent boundary layer by the dielectric barrier discharge (DBD) plasma actuation, an experimental study was performed to reduce the flat plate turbulent boundary layer drag in a low-speed wind tunnel with a freestream velocity of 10.7 m/s. This experiment focused on the drag reduction of different pulsing frequencies on the flat plate turbulent boundary layer. The hot wire anemometer system was used to collect the streamwise velocity signal, and acquire the mean velocity distribution and fluctuation velocity distribution within the turbulent boundary layer. A comparative analysis of the experimental results showed that the plasma significantly reduced the mean velocity in the logarithmic region of the boundary layer, and as the pulsing frequency increased, the local drag reduction showed a trend of first increased and then decreased. When the pulsing frequency of 200 Hz, the maximum local drag reduction rate was 7.4%.
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Key words:
- dielectric barrier discharge (DBD) /
- plasma /
- flat plate /
- turbulent boundary layer /
- drag reduction
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表 1 DBD等离子体激励器几何参数
Table 1. Geometric parameters of the DBD plasma actuator
激励器参数 数值 下电极尺寸(l×l )/(m×m) 80×80 有效放电长度l/mm 80 上电极宽度d/mm 2 电极间距s/mm 10 下电极厚度h1/mm 0.2 介电层厚度h2/mm 0.066(y+≈2<5) 表 2 不同频率下边界层相关参数变化
Table 2. Parameters variation of boundary layer with different frequencies
f/Hz uτ/(m/s) τw/Pa Cf η/% 0 0.4518 0.24189 0.00352 30 0.4352 0.22444 0.00331 5.97 100 0.4341 0.22330 0.00329 6.53 200 0.4322 0.22135 0.00326 7.39 500 0.4364 0.22568 0.00333 5.71 -
[1] 刘沛清,张雯,郭昊. 大型运输机的减阻技术[J]. 力学与实践,2018,40(2): 129-139. doi: 10.6052/1000-0879-17-295LIU Peiqing,ZHANG Wen,GUO Hao. Drag reduction technique for large transport aircraft[J]. Mechanics in Engineering,2018,40(2): 129-139. (in Chinese) doi: 10.6052/1000-0879-17-295 [2] ABBAS A,BUGEDA G,FERRER E,et al. Drag reduction via turbulent boundary layer flow control[J]. Science China (Technological Sciences),2017,60(9): 1281-1290. doi: 10.1007/s11431-016-9013-6 [3] KLINE S J,REYNOLDS W C,SCHRAUB F A,et al. The structure of turbulent boundary layers[J]. Journal of Fluid Mechanics,1967,30(4): 741-773. doi: 10.1017/S0022112067001740 [4] RAO K N,NARASIMHA R,NARAYANAN M A B. The ‘bursting’ phenomenon in a turbulent boundary layer[J]. Journal of Fluid Mechanics,1971,48(2): 339-352. doi: 10.1017/S0022112071001605 [5] ORLANDI P,JAVIER J. On the generation of turbulent wall friction[J]. Physics of Fluids,1994,6(2): 634-641. doi: 10.1063/1.868303 [6] ROBINSON S K. Coherent motions in the turbulent boundary layer[J]. Annual Review of Fluid Mechanics,1991,23(1): 601-639. doi: 10.1146/annurev.fl.23.010191.003125 [7] 李应红, 吴云, 宋慧敏, 等. 等离子体流动控制的研究进展与机理探讨[C]// 中国航空学会第6届动力年会论文集. 北京: 中国航空学会动力专业分会, 2006: 790-799. [8] 赵小虎,李应红,李益文,等. 介质阻挡放电等离子体气动激励的动量特性[J]. 航空动力学报,2010,25(8): 1791-1798.ZHAO Xiaohu,LI Yinghong,LI Yiwen,et al. Momentum characteristic of dielectric barrier discharge plasma aerodynamic actuation[J]. Journal of Aerospace Power,2010,25(8): 1791-1798. (in Chinese) [9] 聂万胜,程钰锋,车学科. 介质阻挡放电等离子体流动控制研究进展[J]. 力学进展,2012,42(6): 722-734. doi: 10.6052/1000-0992-11-161NIE Wansheng,CHENG Yufeng,CHE Xueke. A review on dielectric barrier discharge plasma flow controI[J]. Advances in Mechanics,2012,42(6): 722-734. (in Chinese) doi: 10.6052/1000-0992-11-161 [10] CORKE T C, ENLOE C L, WILKINSON S P, Dielectric barrier discharge plasma actuators for flow control[J]. Annual Review of Fluid Mechanics, 2010, 42(1): 505-529. [11] 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.WU Yun,LI Yinghong. Progress and outlook of plasma flow control[J]. Acta Aeronautica et Astronautica Sinica,2015,36(2): 381-405. (in Chinese) [12] JUKES T,CHOI K S,JOHNSON G A,et al. Characterization of surface plasma-induced wall flows through velocity and temperature measurements[J]. AIAA Journal,2006,44(4): 764-771. doi: 10.2514/1.17321 [13] JUKES T, CHOI K S, JOHNSON G, et al. Turbulent drag reduction by surface plasma through spanwise flow oscillation[R]. AIAA-2006-3693, 2006. [14] WHALLEY R, CHOI K S. Turbulent boundary layer control by DBD plasma: a spanwise travelling wave[R]. AIAA-2010-4840, 2010. [15] CHOI K S,JUKES T,WHALLEY R. Turbulent boundary layer control with plasma actuators[J]. Philosophical Transactions of The Royal Society of London A: Mathematical Physical and Engineering Sciences,2011,369(1940): 1443-1458. doi: 10.1098/rsta.2010.0362 [16] CORKE T C,THOMAS F O. Active and passive turbulent boundary layer drag reduction[J]. AIAA Journal,2018,56(10): 3835-3847. doi: 10.2514/1.J056949 [17] DUONG A H, CORKE T C, THOMAS F O. Characteristics of drag reduced turbulent boundary layers through pulsed-DC actuation[R]. AIAA-2020-0098, 2020. [18] WU B,GAO C,LIU F,et al. Reduction of turbulent boundary layer drag through dielectric-barrier-discharge plasma actuation based on the Spalding formula[J]. Plasma Science and Technology,2019,21(4): 111-118. [19] WONG C W, CHENG X Q, PENG Q, et al. Effects of plasma-actuator-generated vortices on a turbulent boundary layer[R]. Chicago, US: the 10th International Symposium on Turbulence and Shear Flow Phenomena, 2017. [20] CHENG X Q, WONG C W, LI Y Z, et al. Friction drag reduction mechanism under DBD plasma control[C]// Proceedings of the 4th Symposium on Fluid-Structure-Sound Interactions and Control. Singapore City: Springer Nature Singapore, 2019: 105-110. [21] 陆连山,李栋,郑杰,等. 基于狭缝合成射流的湍流边界层流动控制实验研究[J]. 航空工程进展,2020,11(5): 618-628.LU Lianshan,LI Dong,ZHENG Jie,et al. An experimental study of turbulent boundary layer flow control by synthetic jet through spanwise slot[J]. Advances in Aeronautical Science and Engineering,2020,11(5): 618-628. (in Chinese) [22] VILA C S,VINUESA R,DISCETTI A,et al. On the identification of well-behaved turbulent boundary layers[J]. Journal of Fluid Mechanics,2017,822: 109-138. doi: 10.1017/jfm.2017.258 [23] 许春晓. 壁湍流相干结构和减阻控制机理[J]. 力学进展, 2015, 45: 111-140.XU Chunxiao. Coherent structures and drag-reduction mechanism in wall turbulence[J]. Advances in Mechanics, 2015, 45: 111-140. (in Chinese)