Capacitance and power consumption quantification of dielectric barrier discharge (DBD) plasma actuators

Journal of Electrostatics

Volumn 69, Issue 4, 2011, Pages 302-312

  Kriegseis, Jochen ^a   Möller, Benjamin ^a   Grundmann, Sven ^a   Tropea, Cameron ^a  

^a DARMSTADT UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

DBD plasma actuator; Discharge capacitance; Flow control; Impedance matching; Lissajous figures; Surface discharge

Indexed keywords

ACTUATOR PERFORMANCE; DBD PLASMA; DIELECTRIC BARRIER DISCHARGE PLASMAS; ELECTRICAL CIRCUIT; LISSAJOUS FIGURES; OPERATING VOLTAGE; PLASMA ACTUATOR; TIME-RESOLVED;

ACTUATORS; CAPACITANCE; DIELECTRIC DEVICES; FLOW CONTROL; IMPEDANCE MATCHING (ELECTRIC); PLASMAS; SURFACE DISCHARGES;

ELECTRIC DISCHARGES;

EID: 79959512963     PISSN: 03043886     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.elstat.2011.04.007     Document Type: Article

References (56)

1. Abe T., Takizawa Y., Sato S. A parametric experimental study for momentum transfer by plasma actuator. AIAA 2007-185, 45th AIAA Aerospace Sciences Meeting and Exhibit 2007, Reno, Nevada.
2. Abe T., Takizawa Y., Sato S. Experimental study for momentum transfer in a dielectric barrier discharge plasma actuator. AIAA J. September 2008, 46(9).
3. Barckmann K., Kriegseis J., Grundmann S., Tropea C. Dielectric-barrier discharge plasmas for flow control at higher mach numbers. AIAA 2010-4258; 5th Flow Control Conference, 28 Jun 1-Jul 2010 2010, Chicago Illinois, USA.
4. Baughn J.W., Porter C.O., Peterson B.L., McLaughlin T.E., Enloe C.L., Font G.I., Baird C. Momentum transfer for an aerodynamic plasma actuator with an imposed boundary layer. AIAA 2006-166, 44th AIAA Aerospace Sciences Meeting and Exhibit 2006, Reno, Nevada.
5. Benard N., Moreau E., Griffin J., Cattafesta L.N. Plasma flow control autonomous lift improvement by slope-seeking. AIAA-2009-4182; 39th AIAA Fluid Dynamics Conference 2009, San Antonio, Texas, USA.
6. Borcia G., Anderson C.A., Brown N.M.D. Dielectric barrier discharge for surface treatment: application to selected polymers in film and fibre form. Plasma Sources Sci. Technol. 2003, 12(3):335-344.
7. Boucinha V., Joussot R., Magnier P., Weber R., Leroy-Chesneau A. Characterization of the ionic wind produced by a DBD actuator designed to control the laminar-to-turbulent transition. 14th Int Symp on Applications of Laser Techniques to Fluid Mechanics 2008.
8. Chen Z. Impedance matching for one atmosphere uniform glow discharge plasma (OAUGDP) reactors. IEEE Trans. Plasma Sci. 2002, 30(5):1922-1930.
9. Chen, Z., 2007. Impedance matching and Pspice simulation of one atmosphere uniform glow discharge plasma (OAUGDP) reactor/actuator systems. Ph.D. thesis, The University of Tennessee, Knoxville.
10. Corke T.C., Post M.L., Orlov D.M. SDBD plasma enhanced aerodynamics: concepts, optimization and applications. Prog. Aerosp. Sci. Oct. 2007, 43:193-217.
11. Corke T.C., Post M.L., Orlov D.M. Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications. Exp. Fluids Jan. 2009, 46:1-26.
12. Dong B., Bauchire J.M., Pouvesle J.M., Magnier P., Hong D. Experimental study of a DBD surface discharge for the active control of subsonic airflow. J. Phys. D: Appl. Phys. 2008, 41(15):155201. 9 pp.
13. Enloe C.L., Font G.I., McLaughlin T.E., Orlov D.M. Surface potential and longitudinal electric field measurements in the aerodynamic plasma actuator. AIAA J. 2008, 46:2730-2740.
14. Enloe C.L., McLaughlin T.E., Gregory J.W., Medina R.A., Miller W.S. Surface potential and electric field sturcture in the areodynamic plasma actuator. AIAA 2008-1103, 46th AIAA Aerospace Sciences Meeting and Exhibit 2008, Reno, Nevada.
15. Enloe C.L., McLaughlin T.E., VanDyken R.D., Fischer J.C. Plasma structure in the aerodynamic plasma actuator. AIAA-2004-0844; 42nd AIAA Aerospace Sciences Meeting and Exhibit 2004, Reno, Nevada, USA.
16. Enloe C.L., McLaughlin T.E., VanDyken R.D., Kachner K.D., Jumper E.J., Corke T.C. Mechanisms and responses of a single dielectric barrier plasma actuator: plasma morphology. AIAA J. March 2004, 42(3):589-594.
17. Enloe C.L., McLaughlin T.E., VanDyken R.D., Kachner K.D., Jumper E.J., Corke T.C., Post M., Haddad O. Mechanisms and responses of a single dielectric barrier plasma actuator: geometric effects. AIAA J. March 2004, 42(3):595-604.
18. Falkenstein Z., Coogan J.J. Microdischarge behaviour in the silent discharge of nitrogen-oxygen and water-air mixtures. J. Phys. D: Appl. Phys. 1997, 30(5):817-825.
19. Forte M., Jolibois J., Pons J., Moreau E., Touchard G., Cazalens M. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control. Exp. Fluids 2007, 43:917-928.
20. Gibalov V.I., Pietsch G.J. The development of dielectric barrier discharges in gas gaps and on surfaces. J. Phys. D: Appl. Phys. 2000, 33(20):2618.
21. Grundmann, S., 2008. Transition control using dielectric barrier discharge actuators. Ph.D. thesis, Technische Universität Darmstadt.
22. Grundmann S., Frey M., Tropea C. Unmanned aerial vehicle (UAV) with plasma actuators for separation control. AIAA-2009-698; 47th AIAA Aerospace Science Meeting 2009, Orlando, Florida, USA.
23. Grundmann S., Tropea C. Experimental transition delay using glow-discharge plasma actuators. Exp. Fluids April 2007, 42(4):653-657. 0723-4864.
24. Grundmann S., Tropea C. Experimental damping of boundary-layer oscillations using DBD plasma actuators. Int. J. Heat Fluid Flow 2009, 30:394-402.
25. Huang X., Zhang X., Li Y. Broadband flow-induced sound control using plasma actuators. J. Sound Vib. 2010, 329:2477-2489.
26. Jolibois J., Forte M., Moreau R. Application of an AC barrier discharge actuator to control airflow separation above a NACA 0015 airfoil: optimization of the actuation location along the chord. J. Electrostat. Sep. 2008, 66(9-10):496-503.
27. Kriegseis J., Dehler T., Gnirß M., Tropea C. Common-base proper orthogonal decomposition (CPOD) as a means of quantitative data comparison. Meas. Sci. Technol. 2010, 21:085403. 7 pp.
28. Kriegseis J., Dehler T., Grundmann S., Tropea C. Flowfield-characteristics generated by DBD plasma actuators. New Results in Numerical and Experimental Fluid Mechanics VII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design 2010, Springer-Verlag, Berlin Heidelberg. A. Dillmann (Ed.).
29. Kriegseis J., Dehler T., Pawlik M., Tropea C. Pattern-identification study of the flow in proximity of a plasma actuator. AIAA-2009-1001; 47th AIAA Aerospace Science Meeting 2009, Orlando, Florida, USA.
30. Lemire S., Vo H.D., Benner M.W. Performance improvement of axial compressors and fans with plasma actuation. Int. J. Rotating Mach. 2009, 2009:13.
31. Little J., Nishihara M., Adamovich I., Samimy M. High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator. Exp. Fluids Oct. 2010, 48:521-537.
32. Liu S., Neiger M. Excitation of dielectric barrier discharges by unipolar submicrosecond square pulses. J. Phys. D: Appl. Phys. 2001, 34:1632-1638.
33. Magnier P., Boucinha V., Dong B., Weber R., Leroy-Chesneau A., Hong D. Experimental study of the flow induced by a sinusoidal dielectric barrier discharge actuator and its effect on a flat plate natural boundary layer. J. Fluids Eng. January 2009, 131:011203.
34. Manley T.C. The electric characteristics of the ozonator discharge. J. Electrochem. Soc. 1943, 84(1):83-96.
35. Möller, B., 2010. Development and experimental investigation of valuation methods for the energetic efficiency of dbd plasma actuators. Master's thesis, Technische Universität Darmstadt.
36. Moreau E. Airflow control by non-thermal plasma actuators. J. Phys. D: Appl. Phys. 2007, 40:605-636.
37. Nersisyan G., Graham W.G. Characterization of a dielectric barrier discharge operating in an open reactor with flowing helium. Plasma Sources Sci. Technol. Nov. 2004, 13:582-587.
38. Opaits D.F., Likhanskii A.V., Neretti G., Zaidi S., Shneider M.N., Miles R.B., Macheret S.O. Experimental investigation of dielectric barrier discharge plasma actuators driven by repetitive high-voltage nanosecond pulses with dc or low frequency sinusoidal bias. J. Appl. Phys. 2008, 104:043304.
39. Opaits D.F., Neretti G., Likhanskii A.V., Zaidi S., Shneider M.N., Miles R.B. Experimental investigation of DBD plasma actuators driven by repetitive high voltage nanosecond pulses with dc or low-frequency sinusoidal bias. AIAA 2007-4532, 38th AIAA Plasmadynamics and Lasers Conference 2007, Miami, FL.
40. Orlov D., 2006. Modelling and simulation of single dielectric barrier discharge plasma actuators. Ph.D. thesis, University of Notre Dame, USA.
41. Orlov D., Apker T., He C., Othman H., Corke T. Modeling and experiment of leading edge separation control using SDBD plasma actuators. AIAA 2007-0877; 45th Aerospace Sciences Meeting, 8-11 January 2007 2007, Reno, Nevada.
42. Orlov D., Corke T., Patel M. Electric circuit model for aerodynamic plasma actuator. AIAA-2006-1206; 44th AIAA Aerospace Science Meeting and Exhibit 2006, Reno, Nevada, USA.
43. Orlov D., Corke T.C. Numerical simulation of aerodynamic plasma actuator effects. AIAA 2005-1083, AIAA 43rd Aerospace Sciences Meeting 2005, Reno, Nevada.
44. Orlov D.M., Font G.I., Edelstein D. Characterization of discharge modes of plasma actuators. AIAA J. 2008, 46(12):3142-3148.
45. Pavon, S., 2008. Interaction between a surface dielectric barrier discharge and transonic airflows. Ph.D. thesis, Lausanne.
46. Pavon S., Dorier J.-L., Hollenstein C., Ott P., Leyland P. Effects of high-speed airflows on a surface dielectric barrier discharge. J. Phys. D: Appl. Phys. 2007, 40:1733-1741.
47. Pons J., Moreau E., Touchard G. Asymmetric surface dielectric barrier discharge in air at atmospheric pressure: electrical properties and induced airflow characteristics. J. Phys. D: Appl. Phys. 2005, 38(19):3635.
48. Porter C.O., Baughn J.W., McLaughlin T.E., Enloe C.L., Font G.I. Plasma actuator force measurements. AIAA J. Jul. 2007, 45:1562-1570.
49. Porter C.O., McLaughlin T.E., Enloe C.L., Font G.I., Roney J., Baughn J.W. Boundary layer control using a DBD plasma actuator. AIAA 2007-786, 45th AIAA Aerospace Sciences Meeting and Exhibit 2007, Reno, Nevada.
50. Porter C.O., Baughn J.W., McLaughlin T.E., Enloe C.L., Font G.I. temporal force measurements on an aerodynamic plasma actuator. AIAA-2006-1206; 44th AIAA Aerospace Science Meeting and Exhibit 2006, Reno, Nevada, USA.
51. Roth R.J., Dai X. Optimization of the aerodynamic plasma actuator as an electrohydrodynamic (EHD) electrical device. AIAA 2006-1203, 44th AIAA Aerospace Sciences Meeting and Exhibit 2006, Reno, Nevada.
52. Roth R.J., Rahel J., Dai X., Sherman D.M. The physics and phenomenology of one atmosphere uniform glow discharge plasma reactors for surface treatment applications. J. Phys. D: Appl. Phys. 2005, 38:555-567.
53. Savitzky A., Golay M.J.E. Smoothing and differentiation of data by simplified least squares procedures. Anal. Chem. July 1964, 36(8):1627-1639.
54. Singh K.P., Roy S. Impedance matching for an asymmetric dielectric barrier discharge plasma actuator. Appl. Phys. Lett. 2007, 91(8):081504.
55. Van Dyken R., McLaughlin T.E., Enloe C.L. Parametric investigations of a single dielectric barrier plasma actuator. AIAA 2004-0846 2004.
56. Wagner H.E., Brandenburg R., Kozlov K.V., Sonnenfeld A., Michel P., Behnke J.F. The barrier discharge: basic properties and applications to surface treatment. Vac. 2003, 71(3):417-436.