介质阻挡放电等离子体流动控制研究进展

聂万胜; 程钰锋; 车学科

doi:10.6052/1000-0992-11-161

介质阻挡放电等离子体流动控制研究进展

doi: 10.6052/1000-0992-11-161

1 装备学院航天装备系, 北京 101416
2 装备学院研究生院, 北京 101416

基金项目: 国家自然科学基金项目(11205244, 51076168) 资助

详细信息

作者简介:
聂万胜, 1969 年生, 装备学院航天装备系教授、博士生导师, 推进理论与工程教研室主任, 航空宇航科学与技术一级学科负责人, 1998 年获国防科技大学工学博士学位, 中国空气动力学会理事, 中国宇航学会液体火箭推进专委会委员, 总装航天运载技术专家组专家, 总装航天运载技术专业组特邀专家, 总装"双百计划" 科技领军人才培养对象. 近期主要研究方向为航空宇航推进与流动控制技术.

通讯作者:
聂万胜

计量
- 文章访问数: 2839
- HTML全文浏览量: 363
- PDF下载量: 1986
- 被引次数: 0
出版历程
- 收稿日期: 2012-11-23
- 修回日期: 2012-07-10
- 刊出日期: 2012-11-25

A REVIEW ON DIELECTRIC BARRIER DISCHARGE PLASMA FLOW CONTROL

1 Department of Space Equipment, Academy of Equipment, Beijing 101416, China
2 Department of Postgraduate, Academy of Equipment, Beijing 101416, China

Funds: The project was supported by the National Natural Science Foundation of China (11205244, 51076168).

More Information

Corresponding author: NIE Wansheng

摘要

摘要: 介质阻挡放电(DBD) 等离子体流动控制技术适用于低速工况, 具有结构简单、动态响应快等优点, 受到了国内外学术界及工业界的高度重视. 近20 年来, 很多学者对DBD 等离子体流动控制进行了研究, 在机理和应用上都取得了很多有意义的结论. 本文首先分析了介质阻挡放电及其气动激励基本原理; 然后分别对近年来DBD 等离子体流动控制机理和应用研究进展进行了综述, 并总结提出3 个主要气动激励机理; 最后对该领域今后的工作提出了几点建议.
- 介质阻挡放电, 等离子体气动激励, 流动控制
Abstract: Dielectric barrier discharge (DBD) plasma flow control is suited to the low velocity condition. It has a simple structure without mechanical parts, and has thus attracted much attention in research and industry institutions all over the world. DBD plasma flow control has been researched by many scholars in the recent 20 years, and there were a wealth of significant results on both plasma aerodynamic actuation mechanism and applications. In this paper, the physical process of dielectric barrier discharge and the essential mechanism of plasma aerodynamic actuation have been analyzed. Then the DBD plasma flow control, both the aerodynamic actuation mechanism and its applications in recent years, have been reviewed, and the plasma aerodynamic actuation mechanism was generalized in 3 main items. And the paper ends with a discussion about future development of the DBD plasma flow control.
- dielectric barrier discharge, plasma aerodynamic actuation, flow control

HTML全文

参考文献(83)

1 张谷令, 敖玲, 胡建芳, 等. 应用等离子体物理学. 北京: 首都师范大学出版社, 2008

2 Chen F F 著. 等离子体物理导论. 林光海译. 北京: 人民教育出版社, 1980

3 菅井秀郞. 等离子体电子工程学. 北京: 科学出版社, 2002

4 胡希伟. 等离子体理论基础. 北京: 北京大学出版社, 2006

5 马腾才. 低温等离子体物理进展. 力学进展, 1990, 20(3):373-378

6 李刚, 聂超群, 朱俊强, 等. 介质阻挡放电等离子体流动控制技术的研究进展. 科技导报, 2008, 26(4): 87-92

7 程钰锋, 聂万胜, 车学科. 临近空间介质阻挡放电等离子体气动激励效果的数值分析. 高电压技术, 2011, 37(6): 1542-1547

8 程钰锋, 聂万胜, 李国强. 等离子体气动激励机理数值研究. 物理学报, 2012, 61(6): 060509

9 Porter C O, McLaughlin T E, Enloe C L, et al. Boundary layer control using a DBD plasma actuator. AIAA paper,2007-0786, 2007

10 孙宗祥. 等离子体减阻技术的研究进展. 力学进展, 2003,33(1): 87-94

11 Marchand K G. Computational model of one dimensional dielectric barrier discharges. ADA437735, 2005

12 Kantrowitz A. A survey of physical phenomena occurring in flight at extreme speeds. In: Proceedings of the Conference on High-Speed Aeronautics, New York, 1955. 335-339

13 Malik M, Weinstein L, Hussani M. Ion wind drag reduction. AIAA paper, 1983-0231, 1983

14 Roth J R, Barker R J. Investigation of a uniform glow discharge plasma in atmospheric air. ADA302641, 1995

15 Roth J R, Sherman D M. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma. AIAA paper, 1998-328, 1998

16 Roth J R. Industrial Plasma Engineering, volume II Applications to Non-thermal Plasma Processing. Bristol and Philadelphia: Institute of Physics Publishing, 2001

17 Roth J R, Rahel J, Dai X, et al. The physics and phenomenology of one atmosphere uniform glow discharge Plasma (OAUGD) reactors for surface tretment applications. J. Phys. D: Appl. Phys., 2005, 38: 555-567

18 Roth J R, Sin H J, Madhan R C M. Flow re-attachment and acceleration by paraelectric and peristaltic electrohydrodynamic (EHD) effects. AIAA paper, 2003-531, 2003

19 Roth J R, Madhan R C M, Yadav M, et al. Flow field measurements of paraelectric, peristaltic, and combined plasma actuators based on the one atmosphere uniform glow discharge plasma (OAUGDP). AIAA paper, 2004-845, 2004

20 郝江南, 蔡晋生, 李尹喆. 多级双极性等离子体激励器加速气流的实验研究. 中国科学G, 2012, 42(5): 538-546

21 Roth J R, Dai X. Optimization of the aerodynamic plasma actuator as an electrohydrodynamic(EHD) electrical device. AIAA paper, 2006-1203, 2006

22 Porter C O, Baughn J W, McLaughlin T E, et al. Temporal force measurements on an aerodynamic plasma actuator. AIAA paper, 2006-104, 2006

23 Sergey B L, Dmitry O, Richard M, et al. Time-resolved measurements of plasma-induced momentum of air and N2 under DBD actuation. AIAA paper, 2011-1141, 2011

24 Alan R H, Noah H. Comparisons of force measurement methods for DBD plasma actuators in quiescent air. AIAA paper, 2009-485, 2009

25 李益文, 李应红, 周章文, 等. 等离子体气动激励体积力的试验研究. 实验流体力学, 2009, 23(2): 82-86

26 Guo S, Simon T, Ernie D, et al. Separation control using DBD plasma actuators: Thrust enhancement studies. AIAA paper, 2010-1090, 2010

27 Post M, Corke T. Plasma actuators for separation control on stationary and oscillating airfoils. ADA424112, 2004

28 Estevadeordal J, Gogineni S. Low-speed flow control using dielectric barrier discharge (DBD). AFRL-VA-WPTR-2006-3211, 2006

29 Whalley R, Choi K S. Turbulent boundary layer control by DBD plasma: A spanwise travelling wave. AIAA paper,2010-4840, 2010

30 Abe T, Takagaki M. Momentum coupling and flow induction in a DBD plasma actuator. AIAA paper, 2009-4068,2009

31 Victor V G, Eduard E S, Andrii S S, et al. Investigation of vortex structure near the surface of DBD-actuator. AIAA paper, 2011-154, 2011

32 Forte M, Jolibois J, Morean E, et al. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity application to airflow control. AIAA paper, 2006-2863,2006

33 傅鑫. 一种基于低温等离子体的流动控制技术研究. [博士论文]. 南京: 南京理工大学, 2007

34 Joussot R, Hong D, Rabat H, et al. Thermal characterization of a DBD plasma actuator: Dielectric temperature measurements using infrared thermography. AIAA paper,2010-5102, 2010

35 李刚, 聂超群, 朱俊强, 等. 介质阻挡放电等离子体热效应对流场影响的研究. 科技导报, 2008, 26(8): 40-44

36 李应红, 梁华, 吴云, 等. 等离子体气动激励建模仿真终述. 空军工程大学学报, 2008, 9(5): 1-5

37 Shyy W, Jayaraman B A. Modeling of glow-discharge induced fluid dynamics. Appl. Phys., 2002, 92(11): 6434-6443

38 毛枚良, 邓小刚, 向大平, 等. 辉光放电等离子体对边界层流动控制的机理研究. 空气动力学报, 2006, 24(3): 269-274

39 王江南, 钟诚文, 高超, 等. 基于等离子体简化模型的流动分离控制. 航空计算技术, 2007, 37(2): 30-34

40 Suzen Y B, Huang P G, Jacob J D, et al. Numerical simulations of plasma based flow control applications. AIAA paper, 2005-4633, 2005

41 李刚. 等离子体流动控制机理及其应用研究. [博士论文]. 北京: 中国科学院, 2008

42 梁华, 李应红, 吴云, 等. 等离子体气动激励的数值仿真. 高电压技术, 2009, 35(9): 1071-1076

43 William M H, Benjamin J C. Preliminary development of a computational model of a dielectric barrier discharge. ADA437435, 2005

44 车学科.等离子体流动控制机理研究. [博士论文]. 北京: 装备指挥技术学院, 2010

45 Nishida H, Abe T. Validation study of numerical simulation of discharge plasma on DBD plasma actuator. AIAA paper, 2011-3913, 2011

46 Jayaraman B, Cho Y C, Shyy W. Modeling of dielectric barrier discharge plasma actuator. AIAA paper, 2007-4531, 2007

47 Orlov D M, Corke T C.Numerical simulation of aerodynamic plasma actuator effects. AIAA paper, 2005-1083,2005

48 宋慧敏, 李应红, 魏沣亭, 等. 等离子体电流体动力激励器的建模与仿真. 高电压技术, 2006, 32(3): 72-74

49 安治永, 李应红, 吴云, 等.对称等离子体激励器系统电场仿真研究. 物理学报, 2007, 56(8): 4778-4784

50 Font G I, Morgan W L. Plasma discharges in atmospheric pressure oxygen for boundary layer separation control. AIAA paper, 2005-4632, 2005

51 Font G I, Jung S, Enloe C L, et al. Simulation of the effects of force and heat produced by a plasma actuator on neutral flow evolution. AIAA paper, 2006-167, 2006

52 Ebato S, Oginoy Y, Ohnishi N, et al. Numerical analysis of momentum transfer process in DBD plasma actuator. AIAA paper, 2010-4635, 2010

53 Ebato S, Oginoy Y, Ohnishi N, et al. Computational study of flow generation by charged particles in DBD plasma actuators. AIAA paper, 2011-1142, 2011

54 William B J Z. 有限元法多物理场建模与分析. 北京: 人民交通出版社, 2007. 220-244

55 Corke T C, Jumper E J, Post M L, et al. Application of weakly-ionized plasmas as wing flow-control devices. AIAA paper, 2002-350, 2002

56 Patel M P, Ng T T, Vasudevan S, et al. Plasma actuators for hingeless aerodynamic control of an unmanned air vehicle. AIAA paper, 2006-3495, 2006

57 Jayaraman B, Lian Y S, Shyy W. Low-reynolds number flow control using dielectric barrier discharge actuators. AIAA paper, 2007-3974, 2007

58 Kwak D Y, Nelson R C. Vortical flow control over delta wings with different sweep back angles using DBD plasma actuators. AIAA paper, 2010-4837, 2010

59 Riherd M, Roy S, Visbal M, et al. Numerical investigation of serpentine plasma actuators for separation control at low reynolds number. AIAA paper, 2011-3990, 2011

60 Little J, Samimy M. Control of separation from the flap of a high-lift airfoil with DBD plasma actuation. AIAA paper, 2010-1088, 2010

61 Asada K, Ninomiya Y, Oyama A, et al. Airfoil flow experiment on the duty cycle of DBD plasma actuator. AIAA paper, 2009-531, 2009

62 Joussot R, Hong D, Rozenbaum R W, et al. Modification of the laminar-to-turbulent transition on a flat plate using a DBD plasma actuator. AIAA paper, 2010-4708, 2010

63 Jörg L, Aaron R B, Thomas E M, et al. Using a plasma actuator to control laminar separation on a linear cascade turbine blade. AIAA paper, 2003-1206, 2003

64 Huang J H, Thomas C, Thomas F, et al. Plasma actuators for separation control of low pressure turbine blades. AIAA paper, 2003-1027, 2003

65 Huang J H, Thomas C, Flint O T, et al. Plasma actuators for separation control of low-pressure turbine blades. AIAA J. 2006, 44(1): 51-57

66 Travis D, Julia S, Thomas C, et al. Turbine blade tip leakage flow control by partial squealer tip and plasma actuators. AIAA paper, 2006-20, 2006

67 Julia S, Thomas C, Scott M. Control of a turbine tip leakage vortex using casing vortex generators. AIAA paper,2009-299, 2009

68 Daniel K V N, Thomas C C, Scott C M. Tip clearance flow control in a linear turbine cascade using plasma actuation. AIAA paper, 2009-300, 2009

69 Huang J H, Thomas C, Corkey C, et al. Unsteady plasma actuators for separation control of low-pressure turbine blades. AIAA J., 2006, 44(7): 1477-1486

70 Huu D V. Journal of propulsion and power rotating stall suppression in axial compressors with casing plasma actuation. Journal of Propulsion and Power, 2010, 26(4):808-818

71 吴云, 李应红, 朱俊强, 等. 等离子体气动激励扩大低速轴流式压气机稳定性的实验. 航空动力学学报, 2007, 22(12):2024-2030

72 吴云, 李应红, 朱俊强, 等. 等离子体气动激励抑制压气机叶素角区流动分离的仿真与实验. 航空动力学学报, 2009,24(4): 831-835

73 Wang J L, Li H X, Liu F, et al. Forebody asymmetric load manipulated by a horseshoe shaped plasma actuator. AIAA paper, 2009-0904, 2009

74 孟宣市, 王健磊, 蔡晋生, 等. 不同形式等离子体激励对细长体分离涡的控制特性研究. 见:中国力学大会-- 2011 暨钱学森诞辰100 周年纪念大会, 2011, E03-1009

75 Munska M D, McLaughlin T E. Circular cylinder flow control using plasma actuators. AIAA paper, 2005-141, 2005

76 苏长兵, 宋慧敏, 李应红, 等. 基于等离子体激励的圆柱绕流控制实验研究. 实验流体力学, 2006, 20(4): 45-48

77 Santhanakrishnan A, Jacob J D. Flow control with plasma synthetic jet actuators. Journal of Physics D: Applied Physics, 2007, 40(3): 637-651

78 Benard N, Balcon N, Touchard G, et al. Control of diffuser jet flow turbulent kinetic energy and jet spreading enhancements assisted by a non-thermal plasma discharge. Exp.Fluids, 2008, 45: 333-355

79 Robert C N, Thomas C C, Hesham O. A smart wind turbine blade using distributed plasma actuators for improved performance. AIAA paper, 2008-1312, 2008

80 Kopiev V, Ostrikov N, Zaitsev M, et al. Jet noise control by nozzle surface HF DBD actuators. AIAA paper,2011-911, 2011

81 Axel V R, Serge L, Philippe M, et al. Plasma assisted combustion: effect of a coaxial DBD on a methane diffusion flame. Plasma Sources Sci. Technol., 2007, 16:149-160

82 汤洁, 段忆翔, 赵卫, 等. 介质阻挡放电等离子体增强引擎燃烧技术的初步研究. 高电压技术, 2010, 36(3): 733-738

83 李刚, 徐燕骥, 聂超群, 等. 等离子体旋流器调控燃烧的机理分析. 高电压技术, 2011, 37(6): 1479-1485

施引文献

资源附件(0)

访问统计