Dynamic stall control over an airfoil by NS-DBD actuation

doi:10.1088/1674-1056/abb227

中国物理B ›› 2020, Vol. 29 ›› Issue (10): 105203-.doi: 10.1088/1674-1056/abb227

He-Sen Yang(杨鹤森)¹, Guang-Yin Zhao(赵光银)²^,†(), Hua Liang(梁华)¹^,‡(), Biao Wei(魏彪)¹

收稿日期:2020-07-03 修回日期:2020-08-06 接受日期:2020-08-25 出版日期:2020-10-05 发布日期:2020-10-05
通讯作者: Guang-Yin Zhao(赵光银), Hua Liang(梁华)

Dynamic stall control over an airfoil by NS-DBD actuation

He-Sen Yang(杨鹤森)¹, Guang-Yin Zhao(赵光银)^2,†, Hua Liang(梁华)^1,‡, and Biao Wei(魏彪)¹

¹ Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China
² State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China

Received:2020-07-03 Revised:2020-08-06 Accepted:2020-08-25 Online:2020-10-05 Published:2020-10-05
Contact: ^†Corresponding author. E-mail: zym19860615@163.com ^‡Corresponding author. E-mail: lianghua82702@126.com
About author:
†Corresponding author. E-mail: zym19860615@163.com
‡Corresponding author. E-mail: lianghua82702@126.com
* Project supported by the National Natural Science Foundation of China (Grant No. 11802341) and the Open Fund from State Key Laboratory of Aerodynamics of China (Grant No. SKLA20180207).

摘要/Abstract

Abstract:

The wind tunnel test was conducted with an NACA 0012 airfoil to explore the flow control effects on airfoil dynamic stall by NS-DBD plasma actuation. Firstly, light and deep dynamic stall states were set, based on the static stall characteristics of airfoil at a Reynolds number of 5.8 × 10⁵. Then, the flow control effect of NS-DBD on dynamic stall was studied and the influence law of three typical reduced frequencies (k = 0.05, k = 0.05, and k = 0.15) was examined at various dimensionless actuation frequencies (F⁺ = 1, F⁺ = 2, and F⁺ = 3). For both light and deep dynamic stall states, NS-DBD had almost no effect on upstroke. However, the lift coefficients on downstroke were increased significantly and the flow control effect at F⁺ = 1 is the best. The flow control effect of the light stall state is more obvious than that of deep stall state under the same actuation conditions. For the same stall state, with the reduced frequency increasing, the control effect became worse. Based on the in being principles of flow separation control by NS-DBD, the mechanism of dynamic stall control was discussed and the influence of reduced frequency on the dynamic flow control was analyzed. Different from the static airfoil flow separation control, the separated angle of leading-edge shear layer for the airfoil in dynamic stall state is larger and flow control with dynamic oscillation is more difficult. The separated angle is closely related to the effective angle of attack, so the effect of dynamic stall control is greatly dependent on the history of angles of attack.

Key words: flow control, dynamic stall, dielectric barrier discharge (DBD), nanosecond pulse, reduced frequency

中图分类号: (Plasma dynamics and flow)

52.30.-q

47.85.ld (Boundary layer control) 47.20.Ib (Instability of boundary layers; separation) 47.32.Ff (Separated flows)

He-Sen Yang(杨鹤森), Guang-Yin Zhao(赵光银), Hua Liang(梁华), Biao Wei(魏彪). [J]. 中国物理B, 2020, 29(10): 105203-.

He-Sen Yang(杨鹤森), Guang-Yin Zhao(赵光银)†, Hua Liang(梁华)‡, and Biao Wei(魏彪). Dynamic stall control over an airfoil by NS-DBD actuation[J]. Chin. Phys. B, 2020, 29(10): 105203-.

图/表 18

参考文献 37

[1]	Xing S L, Xu H Y, Ye Z Y, Ma M S, Xu Y 2020 Int. J. Mod. Phys. B 34 2040108
[2]	Raghav V, Komerath N 2014 Experiments in Fluids 55 1669
[3]	Wang R, Xia P Q 2013 Sci. China Technol. Sci. 1 175
[4]	Wen G, Gross A 2019 AIAA J. 57 1434
[5]	Visbal M R, Benton S I 2018 AIAA J. 56 2974
[6]	Ye Z L, Wang X D, Chen Z W, Wang L Y 2020 Acta Mech. Sin. 36 320
[7]	Fu L, Yang C, Zhang H, Bao W R 2020 Proceedings of the Institution of Mechanical Engineers Part D Journal of Automobile Engineering 095440702091656
[8]	Veerakumar R, Raul V, Liu Y, Wang X D, Leifsson L, Hu H 2020 Acta Mech. Sin. 36 260
[9]	Messanelli F, Frigerio E, Tescaroli E, Belan M 2019 Experimental Thermal & Fluid Science 105 123
[10]	Walker S, Segawa T 2012 Renewable Energy 42 105
[11]	Henne S, Parikh A, Deparday J, Mulleners K 2018 International Symposium on the Applications of Laser & Imaging Techniques to Fluid Mechanics
[12]	Post M L, Corke T C 2006 AIAA Journal 44 3125
[13]	Jiang J, Yang A M, Weng P F 2008 Journal of Shanghai University (Natural Science) 14 405
[14]	Mai H, Dietz G, Geissler W, Richter K 2008 Journal of the American Helicopter Society 53 26
[15]	Ben-Harav A, Greenblatt D 2016 Wind Energy 19 3
[16]	Castañeda D, Whiting N, Webb N J, Samimy M 2019 AIAA Aviation 2019 Forum 3212
[17]	Rethmel C, Little J, Takashima K, Sinha A 2011 Int. J. Flow Control 3 213
[18]	Cattafesta L N, Sheplak M 2011 Ann. Rev. Fluid Mech. 43 247
[19]	Corke T C, Enloe C L, Wilkinson S P 2010 Ann. Rev. Fluid Mech. 42 505
[20]	Wang J J, Choi K S, Feng L H, Timothy N J, Whalley R D 2013 Progress in Aerospace Sciences 62 52
[21]	Roupassov D, Zavialov I, Starikovskii A 2006 44th AIAA Aerospace Sciences Meeting and Exhibit AIAA-2006-373
[22]	Frankhouser M, Hird K, Naigle S, Gregory J W, Bons J P 2015 46th AIAA Plasmadynamics and Lasers Conference American Institute of Aeronautics and Astronautics
[23]	Starikovskiy A, Meehan K, Miles R B 2018 AIAA Aerospace Sciences Meeting 0681
[24]	Singhal A, Castañeda D, Webb N J, Samimy M 2018 AIAA Journal 56 78
[25]	Chen W X 2008 Helicopter Technique 155 4
[26]	Mulleners K, Raffel M 2012 Experiments in Fluids 52 779
[27]	Chandrasekhara M, Carr L 1995 AGARD FDP Symposium CP-552
[28]	Chen Z L, Hao L Z, Zhang B Q 2013 Sci. China-Series A-Math. Phys. Astron. & Technol. Sci. 56 1055
[29]	Ullmer D, Peschke P, Terzis A, Ott P 2015 J. Phys. D: Appl. Phys. 48 365203
[30]	Zhao G Y, Li Y H, Liang H, Hua W Z, Han M H 2015 Acta Phys. Sin. 64 015101 in Chinese
[31]	Wei B, Wu Y, Liang H, Su Z, Li Y H 2019 Aerospace Science and Technology 96 105584
[32]	Mitsuo K, Watanabe S, Atobe T, Kato H 2013 AIAA Aerospace Sciences Meeting Including the New Horizons Forum & Aerospace Exposition
[33]	Fukumoto H, Aono H, Nonomura T, Oyama A 2016 AIAA Flow Control Conference
[34]	Wang F, Cui J Q 2015 Flight dynamics modeling of coaxial rotorcraft UAVs Berlin Springer 1217 1256
[35]	Zhao G Q 2015 CFD Simulation of unsteady dynamic stall of helicopter rotor and active flow control Nanjing Nanjing University of Aeronautics and Astronautics 58 63 in Chinese
[36]	Zhang R M, Zhao J B, Guo S J 2016 Aeronautical Computing Technique 46 75
[37]	Wang Q 2017 Research on dynamic stall mechanics mechanism and aerodynamic shape optimization of rotor Nanjing Nanjing University of Aeronautics and Astronautics 61 72 in Chinese

Stall state	α₀/(°)	α_m/(°)	Range of α/(°)	k
Light stall	13.1	7.9	5.2–21	0.05, 0.1, 0.15
Deep stall	14.85	9.45	5.4–24.3	0.05, 0.1, 0.15

Dynamic stall control over an airfoil by NS-DBD actuation

RichHTML

PDF (PC)

赞

可视化

摘要/Abstract

引用本文

使用本文

图/表 18

参考文献 37

相关文章 15

Metrics

本文评价

推荐阅读 0

[1]	Meryem Grari, CifAllah Zoheir, Yasser Yousfi, and Abdelhak Benbrik. Effect of pressure and space between electrodes on the deposition of SiN_xH_y films in a capacitively coupled plasma reactor[J]. 中国物理B, 2021, 30(5): 55205-055205.
[2]	. [J]. 中国物理B, 2020, 29(12): 125201-.
[3]	Bing-Liang Tang(唐冰亮), Shan-Guang Guo(郭善广), Hua Liang(梁华), Meng-Xiao Tang(唐孟潇). [J]. 中国物理B, 2020, 29(10): 105204-.
[4]	贺启坤, 梁华, 郑博睿. Discharge and flow characterizations of the double-side sliding discharge plasma actuator[J]. 中国物理B, 2020, 29(6): 64702-064702.
[5]	林启富, 赵彦君, 段文学, 倪国华, 靳兴月, 隋思源, 谢洪兵, 孟月东. Characteristics of non-thermal AC arcs in multi-arc generator[J]. 中国物理B, 2019, 28(12): 125205-125205.
[6]	李子圣, 王焕宇, 高新亮. Formation of electron depletion layer and parallel electric field in the separatrix region of anti-parallel magnetic reconnection[J]. 中国物理B, 2019, 28(7): 75203-075203.
[7]	刘维媛, 罗文, 袁韬, 余继晔, 陈民. Dense pair plasma generation and its modulation dynamics in counter-propagating laser field[J]. 中国物理B, 2018, 27(10): 105202-105202.
[8]	苏志, 李军, 梁华, 郑博睿, 魏彪, 陈杰, 谢理科. UAV flight test of plasma slats and ailerons with microsecond dielectric barrier discharge[J]. 中国物理B, 2018, 27(10): 105205-105205.
[9]	李鸿, 夏国俊, 毛威, 刘金文, 丁永杰, 于达仁, 王晓钢. Experimental and numerical investigation of a Hall thruster with a chamfered channel wall[J]. 中国物理B, 2018, 27(10): 105209-105209.
[10]	赵璐璐, 刘悦. Numerical study on discharge characteristics influenced by secondary electron emission in capacitive RF argon glow discharges by fluid modeling[J]. 中国物理B, 2018, 27(2): 25201-025201.
[11]	尹相辉, 陈俊, 胡睿佶, 李颖颖, 王福地, 符佳, 丁伯江, 王茂, 刘甫坤, 臧庆, 石跃江, 吕波, 万宝年. Toroidal rotation induced by 4.6 GHz lower hybrid current drive on EAST tokamak[J]. 中国物理B, 2017, 26(11): 115203-115203.
[12]	张志波, 吴云, 贾敏, 宋慧敏, 孙正中, 李应红. Modeling and optimization of the multichannel spark discharge[J]. 中国物理B, 2017, 26(6): 65204-065204.
[13]	刘慧, 董全力, 袁大伟, 刘勋, 华能, 乔战峰, 朱宝强, 朱健强, 蒋柏彬, 杜凯, 唐永健, 赵刚, 远晓辉, 盛政明, 张杰. Filamentation instability in two counter-streaming laser plasmas[J]. 中国物理B, 2016, 25(12): 125201-125201.
[14]	刘阳, 崔翔, 卢铁兵, 李学宝, 王振国, 向宇, 王小波. A novel simulation method for positive corona current pulses[J]. 中国物理B, 2015, 24(6): 65201-065201.
[15]	Emad K. El-Shewy, Abeer A. Mahmoud, Ashraf M. Tawfik, Essam M. Abulwafa, Ahmed Elgarayhi. Space–time fractional KdV–Burgers equation for dust acoustic shock waves in dusty plasma with non-thermal ions[J]. , 2014, 23(7): 70505-070505.