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Flow Actuation by DC Surface Discharge Plasma Actuator in Different Discharge Modes
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 Title & Authors
Flow Actuation by DC Surface Discharge Plasma Actuator in Different Discharge Modes
Kim, Yeon-Sung; Shin, Jichul;
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 Abstract
Aerodynamic flow control phenomena were investigated with a low-current DC surface discharge plasma actuator. The plasma actuator was found to operate in three different discharge modes with similar discharge currents of about 1 mA or less. Stable continuous DC discharge without audible noise was obtained at higher ballast resistances and lower discharge currents. However, even with continuous DC power input, a low-frequency self-pulsed discharge was obtained at lower ballast resistances, and a high-frequency self-pulsed discharge was obtained at higher set-point currents and higher ballast resistances, both with audible noise. The Schlieren image reveals that the low-frequency self-pulsed mode produces a synthetic jet-like flow implying that a gas heating effect plays a role, even though the discharge current is small. The high-frequency self-pulsed mode produces pulsed jets in a tangent direction, and the continuous DC mode produces a steady straight pressure wave. Particle image velocimetry (PIV) images reveal that the induced flow field by the low-frequency self-pulsed mode has flow propagating in the radial direction and centered between the electrodes. The high-frequency self-pulsed mode and continuous DC mode produce flow from the anode to the cathode. The perturbed region downstream of the cathode is larger in the high-frequency self-pulsed mode with similar maximum speeds.
 Keywords
flow control;plasma actuator;self-Pulsed;DC discharge;
 Language
English
 Cited by
 References
1.
Yoo, D. W., Won, D. Y. and Tahk, M. J., "Optical flow based collision avoidance of multi-rotor UAVs in urban environments", International Journal of Aeronautical and Space Science, Vol.12, No. 3, 2011, pp.252-259. crossref(new window)

2.
Mueller, T. J., "Aerodynamic measurements at low Reynolds numbers for fixed wing micro-air vehicles", RTO AVT/VKI Special Course on Development and Operation of UAVs for Military and Civil Applications, 1999.

3.
Najafi, Y., Design of a High Altitude Long Endurance Solar Powered UAV, M.S. Thesis, San Jose State University, 2011.

4.
Santhanakrishnan, A., Pern, N. J., Ramakumar, K., Simpson, A. and Jacob, J. D., "Enabling flow control technology for low speed UAVs", AIAA Infotech(c)Aerospace, Arlington, Virginia, USA, 2005, AIAA 2005-6960.

5.
Selig, M. S., "Low Reynolds Number Airfoil Design", VKI Lecture Series - Low Reynolds Number Aerodynamics on Aircraft Including Applications in Emerging UAV Technology, 2003, RTO/AVT-VKI-104.

6.
Pelletier, A. and Mueller, T. J., "Low Reynolds number aerodynamics of low-aspect-ratio, thin/flat/cambered-plate wings", Journal of Aircraft, Vol. 37, No. 5, 2000, pp.825-832. crossref(new window)

7.
Sohn, M. H. and Chung, H. S., "Control of delta-wing vortex by apex strake", KSAS International Journal, Vol. 8, No. 2, 2007, pp.98-106.

8.
Blackwelder, R. F. and Gad-el-Hak M., "Method and apparatus for reducing turbulent skin friction", US Patent US 4932612 A, 1990.

9.
Godard, G. and Stanislas, M., "Control of a decelerating boundary layer Part 1: Optimization of passive vortex generators", Aerospace Science and Technology, Vol. 10, 2006, pp.181-191. crossref(new window)

10.
Ruffin, S. M., Gupta, A. and Marshall, D., "Supersonic Channel Airfoils for Reduced Drag", AIAA Journal, Vol. 38, No. 3, 2000, pp.480-486. crossref(new window)

11.
Saric, W. S. and Reed, H. L., "Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness", 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA, 2002, AIAA 2002-0147.

12.
Oruc, V., "Passive control of flow structures around a circular cylinder by using screen", Journal of Fluids and Structures, Vol. 33, 2012, pp.229-242. crossref(new window)

13.
Kral, L. D., "Active flow control technology", ASME Fluids Engineering Division Technical Brief, 2000.

14.
Jahanmiri M.. "Active flow control: A review", Research report, 2010, ISSN 1652-8549.

15.
Lee, K. Y., Chung, H. S. and Cho, D. H., "A PIV Study of Flow Patterns Over Stationary and Pitch-Oscillating Airfoils with Blowing Jet", KSAS International Journal, Vol. 9, No. 1, 2008, pp. 111-120.

16.
Sinha, S. K. and Ravande, S. V., "Drag Reduction of Natural Laminar Flow Airfoil with a Flexible Surface Deturbulator", 3rd AIAA Flow Control Conference, San Francisco, CA, USA, 2006, AIAA 2006-3030.

17.
Cho, Y. C. and Shyy, W., "Adaptive flow control of low-Reynolds number aerodynamics using dielectric barrier discharge actuator", Progress in Aerospace Sciences, Vol. 47, 2011, pp.495-521. crossref(new window)

18.
Moreau, E., "Airflow control by non-thermal plasma actuators", Journal of Physics D: Applied Physics, Vol. 40, No. 3, 2007, pp. 605-636.

19.
Benard, N., Jolibois. J., Mizuno, A. and Moreau, E., "Innovative Three-Electrode Design for Definition of Multiple Dielectric Barrier Discharge Actuators", ESA/IEEEIAS/ IEJ/SFE Joint Conference on Electrostatic, Boson, USA, 2009.

20.
Huang, J., Corke, T. C. and Thomas, F. O., "Plasma Actuators for Separation Control of Low-Pressure Turbine Blades", AIAA Journal, Vol. 44, No. 1, 2006, pp. 51-57. crossref(new window)

21.
Jukes, T., Segawa, T. and Walker, S., "Active Separation Control over a NACA0024 by DBD Plasma Actuator and FBG Sensor", Journal of Fluid Science and Technology, Vol. 7, No. 1, 2012, pp. 39-52. crossref(new window)

22.
Vorobiev, A., Rennie, R. M. and Jumper, E. J., "Lift Enhancement by Plasma Actuators at Low Reynolds Numbers", 5th AIAA Flow Control Conference, AIAA 2010-483.

23.
Rethmel, C., Little, J., Takashima, K. Sinha, A., Adamovich, I. and Samimy, M., "Flow Separation Control over an Airfoil with Nanosecond Pulse Driven DBD Plasma Actuators", AIAA Journal, AIAA 2011-487.

24.
Menghu, Han, Jun, L., Zhongguo, N., Hua, L., Huangyin, Z. and Weizhuo, H., "Aerodynamic performance enhancement of a flying wing using nanosecond pulsed DBD plasma actuator", Chinese Journal of Aeronautics, Vol. 28, 2015.

25.
Tabatabaeian, S., Mirzaei, M., Sadighzadeh, A., Damideh, V. and Shadaram, A., "Experimental investigation of the effects of various plasma actuator configuration on lift and drag coefficients of a circular cylinder including the effects of electrodes", Chinese Journal of Aeronautics, Vol. 25, 2012, pp.311-324. crossref(new window)

26.
Klimov, A., Moralev, I., Bityurin, V.A., Kazansky, P.N., Chertov, D.A. and Borisov I.A, "Flow Around Wing Model with a Surface HF Discharge", 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA, 2001, AIAA 2011-1146.

27.
Porter, C. O., Baughn, J. W., McLaughlin, T. E., Enloe, C. L. and Font, G. I., "Temporal Force Measurements on an Aerodynamic Plasma Actuator", 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2006-104.

28.
Moreau, E., Sosa, R., and Artana, G., "Electric wind produced by surface plasma actuators: a new dielectric barrier discharge based on a three-electrode geometry", Journal of Physics D: Applied Physics, Vol. 41, No. 11, 2008, 115204 (12 pp).

29.
Ye, Q., Wu, Y., Li, X., Chen, T. and Shao, G., "Uniformity of dielectric barrier discharges using mesh electrodes", Plasma Sources Science and Technology, Vol. 21, No. 6, 2012, 065008 (7 pp). crossref(new window)

30.
Grange, F., Soulem, N., Loiseau. J. F. and Spyrou, N., "Numerical and experimental determination of ionizing front velocity in a DC point-to-plane corona discharge," Journal of Physics D: Applied Physics, Vol. 28, No. 8, 1995, pp. 1619-1629.

31.
Shin, J. and Raja, L. L., "Cathode-sheath driven lowspeed aerodynamic flow actuation using direct-current surface glow discharges", Journal of Electrostatics, Vol. 68, No. 5, 2010, pp. 453-457. crossref(new window)

32.
Sosa, R. and Artana, G., "Steady control of laminar separation over airfoils with plasma sheet actuators", Journal of Electrostatics, Vol. 68, No. 7-9, 2006, pp. 604-610.

33.
Roth, J. R., "Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a one atmosphere uniform glow discharge plasma", Physics of Plasmas, Vol. 10, No. 5, 2003, pp. 2116-2126.

34.
Stark, R. H. and Schoenbach, K. H., "Direct current high-pressure glow discharges", Journal of Applied Physics, Vol. 85, No. 4, 1999, pp. 2075-2080. crossref(new window)

35.
Raizer, Yu. P., Gas Discharge Physics, Springer, New York, 1991.

36.
Roupassov, D. V., Nikipelov, A. A., Nudnova, M. M. and Starikovskii, A. Yu., "Flow separation control by plasma actuator with nanosecond pulsed-periodic discharge," AIAA Journal, Vol. 47, No. 1, 2009, pp. 168-185. crossref(new window)