Dielectric barrier discharge plasma actuators for flow control

Annual Review of Fluid Mechanics

Volumn 42, Issue , 2010, Pages 505-529

  Corke, Thomas C ^a   Enloe, C Lon ^b   Wilkinson, Stephen P ^c  

^a UNIVERSITY OF NOTRE DAME   (United States)

^b UNITED STATES AIR FORCE ACADEMY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Aerodynamic control; Body force; Ionized gasses

Indexed keywords

ACTUATOR DESIGN; AERODYNAMIC CONTROL; AUSTRALIA; BODY FORCES; DIELECTRIC BARRIER DISCHARGE PLASMAS; DIELECTRIC BARRIER DISCHARGES; ENGLAND; EXTERNAL FLOW; FIRST-PRINCIPLES; FLOW SOLVER; FORCE VECTORS; GERMANY; IONIZED GAS; LOW SPEED; NETHERLANDS; NEW APPLICATIONS; PLASMA ACTUATOR;

AERODYNAMICS; ATMOSPHERIC PRESSURE; DIELECTRIC DEVICES; ELECTRIC DISCHARGES; FLOW CONTROL; MACH NUMBER; OPTIMIZATION; PLASMAS;

ACTUATORS;

ACOUSTICS; AERODYNAMICS; ATMOSPHERIC PRESSURE; DIELECTRIC PROPERTY; FLOW REGULATION; FLUID DYNAMICS; GAS FLOW; PLASMA;

EID: 77952830330     PISSN: 00664189     EISSN: None     Source Type: Book Series    
DOI: 10.1146/annurev-fluid-121108-145550     Document Type: Review

References (106)

1. Arad B, Gazit Y, Ludmirsky A. 1987. A sliding discharge device for producing cylindrical shock waves. J. Phys. D 77:360-367
2. Asghar A, Jumper EJ, Corke TC. 2006. On the use of Reynolds number as the scaling parameter for the performance of plasma actuator in a weakly compressible flow. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-21
3. Balcer BE, Franke ME, Rivir RB. 2006. Effects of plasma induced velocity on boundary layer flow. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-875
4. BenGadri R, Rabehi A, Massines F, Segur P. 1994. Numerical modelling of atmospheric pressure low-frequency glow discharge between insulated elecrodes. Proc. 12th ESCAMPIG, Netherlands, August 23-26, pp. 228-229
5. Boeuf JP, Pitchford LC. 2005. Electrohydrodynamic force and aerodynamic flow acceleration in surface dielectric barrier discharge. J. Appl. Phys. 97:103307
6. Boeuf JP, Lagmich Y, Unfer T, Callegari T, Pitchford L. 2007. Electrohydrodynamic force in dielectric barrier discharge plasma actuators. J. Phys. D 40:652-662 (Pubitemid 46485761)
7. Cavalieri D. 1995. On the experimental design for instability analysis on a cone at Mach 3. 5 and 6. 0 using a corona discharge perturbation method. PhD thesis, Illinois Inst. Technol.
8. Corke T, Cavalieri D, Matlis E. 2001. Boundary layer instability on a sharp cone at Mach 3. 5 with controlled input. AIAA J. 40:1015-1018
9. Corke TC, He C, Patel M. 2004. Plasma flaps and slats: an application of weakly-ionized plasma actuators. Presented at AIAA Flow Control Conf., 2nd, Portland, AIAA Pap. No. 2004-2127
10. Corke TC, Jumper EJ, Post ML, Orlov D, McLaughlin TE. 2002. Application of weakly-ionized plasmas as wing flow-control devices. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 40th, Reno, AIAA Pap. No. 2002-0350
11. Corke TC, Matlis E. 2000. Phased plasma arrays for unsteady flow control. Presented at Fluids 2000 Conf. Exhibit, Denver, AIAA Pap. No. 2000-2323
12. Corke TC, Mertz B, Patel MP. 2006. Plasma flow control optimized airfoil. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-1208
13. Davidson G, O'Neil R. 1964. Optical radiation from nitrogen and air at high pressure excited by energetic electrons. J. Chem. Phys. 41:3946-3949
14. Decomps Ph, Massines F, Mayoux C. 1994. Electrical and optical diagnosis of an atmospheric pressure glow discharge. Acta Phys. Univ. Com. 1994:47-53
15. Do H, Kim W, Mungal M, Capelli M. 2007. Bluff body flow control using surface dielectric barrier discharges. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0939
16. Douville T, Stephens J, Corke T, Morris S. 2006. Turbine blade tip leakage flow control by partial squealer tip and plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-20
17. Eliasson B, Kogelschatz U. 1991. Nonequilibrium volume plasma chemical processing. IEEE Trans. Plasma Sci. 19:1063-1077
18. Enloe C, Font G, McLaughlin T, Orlov D. 2008. Surface potential and longitudinal electricfield measurements in the aerodynamic plasma actuator. AIAA J. 46:2730-2740
19. Enloe C, McHarg M, Font G, McLaughlin T. 2009. Plasma-induced force and self-induced drag in the dielectric barrier discharge aerodynamic plasma actuator. Presented at AIAA Aerosp. Sci. Meet., 47th, Orlando, AIAA Pap. No. 2009-1622
20. Enloe C, McLaughlin T, Font G, Baughn J. 2006. Parameterization of temporal structure in the single-dielectric-barrier aerodynamic plasma actuator. AIAA J. 44:1127-1136
21. Enloe CL, McLaughlin TE, VanDyken RD, Kachner KD, Jumper EJ, Corke TC. 2004a. Mechanisms and responses of a single-dielectric barrier plasma actuator: plasma morphology. AIAA J. 42:589-594
22. Enloe CL, McLaughlin TE, VanDyken RD, Kachner KD, Jumper EJ, etal. 2004b. Mechanisms and responses of a single-dielectric barrier plasma actuator: geometric effects. AIAA J. 42:595-604
23. Falkenstein Z, Coogan J. 1997. Microdischarge behaviour in the silent discharge of nitrogen-oxygen and water-air mixtures. J. Phys. D 30:817-825
24. Font GI. 2004. Boundary layer control with atmospheric plasma discharges. Presented at AIAA/ASME/SAE/ASEE Joint Propul. Conf. Exhibit, 40th, Fort Lauderdale, AIAA Pap. No. 2004-3574
25. Font GI, Morgan WL. 2005. Plasma discharges in atmospheric pressure oxygen for boundary layer separation control. Presented at AIAA Fluid Dyn. Conf. Exhibit, 35th, Toronto, AIAA Pap. No. 2005-4632
26. Forte M, Jolibois J, Moreau F, Touchard G, Cazalens M. 2006. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to flow control. Presented at AIAA Flow Control Conf., 3rd, San Francisco, AIAA Pap. No. 2006-2863
27. Gibalov V, Pietsch G. 2000a. The development of dielectric barrier discharges in gas gaps and surfaces. J. Phys. D 33:2618-2636
28. Goeksel B, Rechenberg I. 2004. Active separation flow control experiments in weakly ionized air. Presented at EUROMECH Eur. Turbul. Conf., 10th, Barcelona
29. Goeksel B, Rechenberg I, Greenblatt D, Paschereit C. 2006. Steady and unsteady plasma wall jets for separation and circulation control. Presented at AIAA Flow Control Conf., 3rd, San Francisco, AIAA Pap. No. 2006-3686
30. Golubovskii YuB, Maiorov VA, Behnke J, Behnke JF. 2002. Influence of interaction between charged particles and dielectric surface over a homogeneous barrier discharge in nitrogen. J. Phys. D 35:751-761
31. Hoskinson A, Oksuz L, Hershkowitz N. 2008. Microdischarge propogation and expansion in a surface dielectric barrier discharge. Appl. Phys. Lett. 93:221501
32. Huang J. 2005. Documentation and control of flow separation on a linear cascade of Pak-B blades using plasma actuators. PhD thesis, Univ. Notre Dame
33. Huang J, Corke TC, Thomas FO. 2006a. Plasma actuators for separation control of low pressure turbine blades. AIAA J. 44:51-57
34. Huang J, Corke TC, Thomas FO. 2006b. Unsteady plasma actuators for separation control of low-pressure turbine blades. AIAA J. 44:1477-1487
35. Hultgren LS, Ashpis DE. 2003. Demonstration of separation delay with glow-discharge plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 41st, Reno, AIAA Pap. No. 2003-1025
36. Kanzawa S, Kogoma M, Kanazawa S, Moriwaki T, Okazaki SJ. 1990. The improvement of atmospheric-pressure glow plasma method and the deposition of organic films. J. Phys. D. 23:374-377
37. Kanazawa S, Kogoma M, Moriwaki T, Okazaki SJ. 1988. Stable glow plasma at atmospheric pressure. J. Phys. D 21:838-840
38. Kanazawa S, Kogoma M, Okazaki SJ, Moriwaki T. 1989. Glow plasma treatment at atmospheric pressure for surface modification and film deposition. Nucl. Inst. Methods Phys. Res. B 37:842-845
39. Kim W, Do H, Mungal M, Cappelli M. 2007. On the role of oxygen in dielectric barrier discharge actuation of aerodynamic flows. Appl. Phys. Lett. 91:181501
40. Kline M, Miller N, Walhout M. 2001. Time-resolved imaging of spatiotemporal patterns in a one-dimensional dielectric-barrier discharge system. Phys. Rev. E 64:026402
41. Kogelschatz U. 2002. Filamentary, patterned and diffuse barrier discharges. IEEE Trans. Plasma Sci. 30:1400-1408
42. Kogelschatz U, Eliasson B, Egli W. 1997. Dielectric-barrier discharges: principles and applications. J. Phys. IV (France) 7:C4-47-66
43. Kogoma M, Okazaki SJ. 1994. Raising of ozone formation efficiency in a homogeneous glow discharge plasma at atmospheric pressure. J. Phys. D 27:1985-1987
44. Kosinov A, Maslov A, Shevelkov S. 1990. Experiments on the stability of supersonic laminar boundary layers. J. Fluid Mech. 219:621-633
45. Kozlov KV, Wagner H-E, Brandenburg R, Michel P. 2001. Spatio-temporally resolved spectroscopic diagnostics of the barrier discharge in air at atmosperic pressure. J. Phys. D 34:3164-3176
46. Kunhardt E. 2000. Generation of large volume atmospheric pressure nonequilibrium plasmas. IEEE Trans. Plasma Sci. 28:189-199
47. Kunhardt EE. 1980. Electrical breakdown of gases: the pre-breakdown stage. IEEE Trans. Plasma Sci. PS-8:130-138
48. Kunhardt EE, Luessen L. 1981. Electrical Breakdown and Discharges. New York: Plenum
49. Landau LD, Lifshitz EM. 1984. Electrodynamics of Continuous Media. Oxford: Pergamon
50. Langmuir I. 1928. Oscillations in ionized gases. Proc. Natl. Acad. Sci. USA 14:627-637
51. Likhanskii AV, Shneider MN, Macheret SO, Miles RB. 2006. Modeling of interaction between weakly ionized near-surface plasmas and gas flow. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-1204
52. List J, Byerley AR, McLaughlin TE, VanDyken RD. 2003. Using a plasma actuator to control laminar separation on a linear cascade turbine blade. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 41st, Reno, AIAA Pap. No. 2003-1026
53. LLewellyn-Jones F. 1966. The Glow Discharge and an Introduction to Plasma Physics. New York: Methuen
54. Louste C, Artana G, Moreau E, Touchard G. 2005. Sliding discharge in air at atmospheric pressure: electrical properties. J. Electrost. 63:615-620
55. Madani M, Bogaerts A, Gijbels R, Vangeneugden D. 2003. Modelling of a dielectric barrier glow discharge at atmospheric pressure in nitrogen. In Int. Conf. Phenom. Ionized Gases, ed. J Meichsner, D Loffhagen, HE Wagner. Greifswald: ICPIG
56. Massines F, Ghadri RB, Decomps Ph, Rabehi A, Segur P, Mayoux C. 1996. Atmospheric pressure dielectric controlled glow discharges: diagnostics and modelling. Proc. Int. Conf. Phenom. Ionized Gases, ICPIG, 22nd, Hoboken, New Jersey, 363:306-315
57. Massines F, Rabehi A, Decomps P, Gadri RB, Segur P, Mayoux C. 1998. Experimental and theoretical study of a glow discharge at atmospheric pressure controlled by dielectric barrier. J. Appl. Phys. 83:2950-2957
58. Matlis E, Corke T. 2005. AC plasma anemometer for hypersonic Mach number experiments. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 43rd, Reno, AIAA Pap. No. 2005-0952
59. Matlis E, Corke T, Cameron J, Morris S. 2008. A. C. plasma anemometer for axial compressor stall warning. Presented at 12th Int. Symp. Transp. Phenom. Dyn. Rotat. Mach., February 17-22, Honolulu
60. Matlis EH. 2004. Controlled experiments on instabilities and transition to turbulence on a sharp cone at Mach 3. 5. PhD thesis, Univ. Notre Dame
61. Meek JM, Craggs JD, eds. 1978. Electrical Breakdown of Gases. Chichester, UK: Wiley
62. Mertz B, Corke T. 2009. Time-dependent dielectric barrier discharge plasma actuator modeling. Presented at AIAA Aerosp. Sci. Meet., 47th, Orlando, AIAA Pap. No. 2009-1083
63. Morris SC, Corke TC, VanNess D, Stephens J, Douville T. 2005. Tip clearance control using plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, Reno, AIAA Pap. No. 2005-0782
64. Nasser E. 1971. Fundamentals of Gaseous Ionization and Plasma Electronics. New York: Wiley-Interscience
65. Naude N, Cambronne J-P, Gherardi N, Massines F. 2004. Electrical model of an atmospheric pressure Townsend-like discharge (APTD). Eur. Phys. J. Appl. Phys. 29:173-180
66. Nelson CC, Cain AB, Patel MP, Corke TC. 2006. Simulation of plasma actuators using the wind-US code. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-634
67. Nelson R, Corke T, Patel M, Ng T. 2007. Modification of the flow structure over a UAV wing for roll control. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0884
68. Okazaki SJ, Kogoma M, Uehara M, Kimura Y. 1993. Appearance of stable glow discharge in air, argon oxygen, and nitrogen at atmospheric pressure using 50 hz source. J. Phys. D 26:889-892
69. Opaits D, Zaidi S, Schneider M, Miles R, Likhanskii A, Macheret S. 2009. Improving thrust by suppressing charge build-up in pulsed DBD plasma actuators. Presented at AIAA Aerosp. Sci. Meet., 47th, Orlando, AIAA Pap. No. 2009-487
70. Orlov DM. 2006. Modelling and simulation of single dielectric barrier discharge plasma actuators. PhD thesis, Univ. Notre Dame
71. Orlov D, Corke T. 2005. Numerical simulation of aerodynamic plasma actuator effects. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 43rd, Reno, AIAA Paper 2005-11083
72. Orlov D, Corke T, Haddad O. 2003. DNS modeling of plasma array flow actuators. Am. Phys. Soc. Div. Fluid Dyn., 48:JA. 004 (Abstract)
73. Orlov D, Corke T, Patel M. 2006. Electric circuit model for aerodynamic plasma actuator. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-1206
74. Pai ST, Guo XM, Zhou TD. 1996. Closed form analytic solution describing glow discharge plasma. Phys. Plasmas 3:3842-3852
75. Patel MP, Sowle ZH, Corke TC, He C. 2006. Autonomous sensing and control of wing stall using a smart plasma slat. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-1207
76. Paulus M, Stals L, Rude U, Rauschenbach B. 1999. Two-dimensional simulation of plasma-based ion implantation. J. Appl. Phys. 85:761-766
77. Porter C, McLaughlin T, Enloe L, Font G. 2007. Boundary layer control using DBD plasma actuator. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0786
78. Post ML. 2001. Phased plasma actuators for unsteady flow control. Master's thesis, Univ. Notre Dame
79. Post ML. 2004. Plasma actuators for separation control on stationary and unstationary airfoils. PhD thesis, Univ. Notre Dame
80. Post ML, Corke TC. 2003. Separation control on high angle of attack airfoil using plasma actuator. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 41st, Reno, AIAA Pap. No. 2003-1024
81. Post ML, Corke TC. 2004. Separation control using plasma actuators: stationary and oscillatory airfoils. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 42nd, Reno, AIAA Pap. No. 2004-0841
82. Rabehi A, BenGadri R, Segur P, Massines F, Decomps Ph. 1994. Numerical modelling of high pressure glow discharges controlled by dielectric barrier. Proc. Conf. Electr. Insul. Dielectr. Phenom., Arlington, TX, October 23-26, pp. 840-845 New York: IEEE
83. Raizer YP. 1991. Gas Discharge Physics. Berlin: Springer-Verlag
84. Rizzetta D, Visbal M. 2007. Numerical investigation of plasma-based flow control for a transitional highly-loaded low-pressure turbine. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0938
85. Roth JR. 1995. Industrial Plasma Engineering. Philadelphia, PA: Inst. Phys.
86. Roth JR, Dai X. 2006. Optimization of the aerodynamic plasma actuator as an EHD electrical device. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-1203
87. Roth JR, Sherman D, Wilkinson S. 1998. Boundary layer flow control with one atmosphere uniform glow discharge surface plasma. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 36th, Reno, AIAA Pap. No. 1998-0328
88. Roth JR, Sherman DM, Wilkinson SP. 2000. Electrohydrodynamic flow control with a glow-discharge surface plasma. AIAA J. 38:1166-1172
89. Shyy W, Jayaraman B, Andersson A. 2002. Modeling of glow discharge-induced fluid dynamics. J. Appl. Phys. 92:6434-6443
90. Singh K, Roy S. 2008. Force approximation for a plasma actuator operating in atmospheric air. J. App. Phys. 103:013305
91. Suzen Y, Huang G, Ashpis D. 2007. Numerical simulations of flow separation control in low-pressure turbines using plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0937
92. Suzen YB, Huang PG. 2006. Simulation of flow separation control using plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-877
93. Suzen YB, Huang PG, Jacob JD, Ashpis DE. 2005. Numerical simulations of plasma based flow control applications. Presented at AIAA Fluid Dyn. Conf. Exhibit, 35th, Toronto, AIAA Pap. No. 2005-4633
94. Thomas F, Corke T, Iqbal M, Kozlov A, Shatzman D. 2009. Optimization of SDBD plasma actuators for active aerodynamic flow control. AIAA J. In Press
95. Thomas F, Corke T, Wang M. 2008a. Experimental aircraft noise control using dielectric barrier discharge plasma actuators: benchmark experiments and LES simulations. NASA Progr. Rep. NNX07AO09A
96. Thomas FO, Kozlov A, Corke TC. 2006. Plasma actuators for bluff body flow control. Presented at AIAA Flow Control Conf., 3rd, San Francisco, AIAA Pap. No. 2006-2845
97. Thomas F, Kozlov A, Corke T. 2008b. Plasma actuators for bluff body flow control. AIAA J. 46:1921-1931
98. Trunec D, Brablec A, Stastny F. 1998. Experimental study of atmospheric pressure glow discharge. Contrib. Plasma Phys. 38:435-445 (Pubitemid 128397728)
99. Van Ness DK, Corke TC, Morris SC. 2006. Turbine tip clearance flow control using plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-21
100. Vidmar RJ, Stalder KR. 2003. Air chemistry and power to generate and sustain plasma: plasma lifetime calculations. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 41st, Reno, AIAA Pap. No. 2003-1189
101. Visbal MR, Gaitonde DV. 2006. Control of vortical flows using simulated plasma actuators. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 44th, Reno, AIAA Pap. No. 2006-505
102. Voikov V, Corke T, Haddad O. 2004. Numerical simulation offlow control over airfoils using plasma actuators. Am. Phys. Soc. Div. Fluid Dyn. 49:FG. 008 (Abstract)
103. Wall JD, Boxx IC, Rivir RB, Franke ME. 2007. Effects of pulsed DC discharge plasma actuators in a separated LPT boundary layer. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 45th, Reno, AIAA Pap. No. 2007-0942
104. Wilkinson SP. 2003. Investigation of an oscillating surface plasma for turbulent drag reduction. Presented at AIAA Aerosp. Sci. Meet. Exhibit, 41st, Reno, AIAA Pap. No. 2003-1023
105. Yokoyama T, Kogoma M, Moriwaki T, Okazaki SJ. 1990. The mechanism of the stabilization of glow plasma at atmospheric pressure. J. Phys. D 23:1125-1128
106. Zouzou N, Takashima K, Moreau E, Mizuno A, Touchard G. 2007. Sliding discharge study in axisymmetric configuration. In 28th ICPIG, Prague, Czech Republic, ed. J Schmidt, M Simek, S Pekarek, V Prukner, Art. No. 1007-10. London: Int. Union Pure Appl. Phys.