Turbulent boundary layer control with spanwise DBD plasma actuators
-
摘要:
文章研究展向介质阻挡放电(dielectric barrier discharge,DBD)等离子体激励控制平板湍流边界层(
Re τ=1140 ),采用热线技术测量减阻效果和边界层速度型。在相邻上电极中心的下游位置,等离子体控制使得摩阻减小,随着占空比的增加,减阻率先增加后减小,在占空比为0.5时达到最大,边界层内层区域(y + < 200)的速度减小;在上电极正下游位置,等离子体控制使得摩阻增加,减阻率随占空比的增加而几乎线性地减小,边界层内层区域(y + < 100)的速度增大;随着远离激励器,控制效果逐渐减弱,在激励器下游1.27δ 附近,控制效果基本消失。Abstract:The flat plate turbulent boundary layer control by spanwise dielectric barrier discharge (DBD) plasma at
Re τ = 1 140 was investigated, and the drag reduction and boundary layer profiles were measured using hot-wire technology. Result showed that, the skin fraction drag with plasma control decreased downstream of the center of two adjacent upper electrodes, and with the increase of duty cycle, the drag reduction increased first and then decreased, reaching a maximum as the duty cycle was 0.5. Meanwhile, the velocity in the inner region of the boundary layer (y +<200) decreased. In the downstream position of the upper electrode, the drag increased with plasma control, the drag reduction decreased almost linearly with the increase of duty cycle, and the velocity in the inner region of the boundary layer (y +<100) increased. The control effect gradually weakened as it moved away from the actuators, and the control effect basically disappeared around 1.27δ downstream of the actuators.-
Key words:
- DBD plasma /
- flat plate /
- turbulent boundary layer /
- drag reduction /
- hot wire
-
表 1 未控制下的湍流边界层特征参数
Table 1. Characteristic parameters of the uncontrolled turbulent boundary layer
参数 数值 U∞/(m/s) 7.5 δ/mm 55 δ*/mm 8.46 θ/mm 6.15 uτ/(m/s) 0.31 δν/mm 0.048 H 1.37 Reτ 1140 Reδ* 4262 -
[1] SPALART P R, DOUGLAS MCLEAN J. Drag reduction: enticing turbulence, and then an industry[J]. Philosophical Transactions Series A, Mathematical, Physical, and Engineering Sciences, 2011, 369(1940): 1556-1569. [2] 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 [3] ROTH J, SHERMAN D, WILKINSON S. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma[R]. AIAA-1998-0328, 1998. [4] ROTH J R, SHERMAN D M, WILKINSON S P. Electrohydrodynamic flow control with a glow-discharge surface plasma[J]. AIAA Journal, 2000, 38(7): 1166-1172. doi: 10.2514/2.1110 [5] JUKES T, CHOI K S, JOHNSON G, et al. Turbulent drag reduction by surface plasma through spanwise flow oscillation[R]. AIAA-2006-3693, 2006. [6] 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. [7] DUONG A H, CORKE T C, THOMAS F O. Characteristics of drag-reduced turbulent boundary layers with pulsed-direct-current plasma actuation[J]. Journal of Fluid Mechanics, 2021, 915: A113. doi: 10.1017/jfm.2021.167 [8] WONG C W, ZHOU Y, LI Y Z, et al. Skin friction drag reduction based on plasma-induced streamwise vortices[M]//Fluid-Structure-Sound Interactions and Control. Berlin: Springer Berlin Heidelberg, 2015: 139-144. [9] CHENG X Q, WONG C W, LI Y Z, et al. Friction drag reduction mechanism under DBD plasma control[M]//Fluid-Structure-Sound Interactions and Control. Singapore: Springer Singapore, 2018: 105-110. [10] CHENG X Q, WONG C W, HUSSAIN F, et al. Flat plate drag reduction using plasma-generated streamwise vortices[J]. Journal of Fluid Mechanics, 2021, 918: A24. doi: 10.1017/jfm.2021.311 [11] WONG C W, CHENG Xiaoqi, FAN Dewei, et al. Friction drag reduction based on a proportional-derivative control scheme[J]. Physics of Fluids, 2021, 33(7): 075115. doi: 10.1063/5.0056169 [12] MAHFOZE O, LAIZET S. Skin-friction drag reduction in a channel flow with streamwise-aligned plasma actuators[J]. International Journal of Heat and Fluid Flow, 2017, 66: 83-94. doi: 10.1016/j.ijheatfluidflow.2017.05.013 [13] ALTıNTAŞ A, DAVIDSON L, PENG S H. Direct numerical simulation of drag reduction by spanwise oscillating dielectric barrier discharge plasma force[J]. Physics of Fluids, 2020, 32(7): 075101. doi: 10.1063/5.0007103 [14] WU Bin, GAO Chao, LIU Feng, 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): 045501. doi: 10.1088/2058-6272/aaf2e2 [15] CLAUSER F H. The turbulent boundary layer[M]//Advances in Applied Mechanics Volume 4. Amsterdam: Elsevier, 1956: 1-51. [16] BRUUN H H. Hot-wire anemometry: principles and signal analysis[M]. Oxford: Oxford University Press, 1995. [17] LI Yueqiang, WU Bin, GAO Chao, et al. Turbulent boundary layer control with DBD plasma actuators[J]. Plasma Science and Technology, 2023, 25(4): 045508. doi: 10.1088/2058-6272/aca503 [18] HUTCHINS N, CHOI K S. Accurate measurements of local skin friction coefficient using hot-wire anemometry[J]. Progress in Aerospace Sciences, 2002, 38(4/5): 421-446. [19] XUE Ming, GAO Chao, XI Hengdong, et al. Vortices induced by a dielectric barrier discharge plasma actuator under burst-mode actuation[J]. AIAA Journal, 2020, 58(6): 2428-2441. doi: 10.2514/1.J057764 -

下载: