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Numerical Simulation of Plasma Actuator Using OpenFOAM

Authors: H. Yazdani, K. Ghorbanian

Abstract:

This paper deals with modeling and simulation of the plasma actuator with OpenFOAM. Plasma actuator is one of the newest devices in flow control techniques which can delay separation by inducing external momentum to the boundary layer of the flow. The effects of the plasma actuators on the external flow are incorporated into Navier-Stokes computations as a body force vector which is obtained as a product of the net charge density and the electric field. In order to compute this body force vector, the model solves two equations: One for the electric field due to the applied AC voltage at the electrodes and the other for the charge density representing the ionized air. The simulation result is compared to the experimental and typical values which confirms the validity of the modeling.

Keywords: Active flow control, flow field, OpenFOAM, plasma actuator.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1127272

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References:


[1] U. Kogelschatz, B. Eliasson, W. Egli, “From ozone generators to flat television screens: history and future potential of dielectric-barrier discharges,” Pure and Applied Chemistry, pp.1819-1828, 1999.
[2] T.C. Corke, C.E. Enloe, and S.P. Wilkinson, “Dielectric Barrier Discharge Plasma Actuators for Flow Control,” Annual Review of Fluid Mechanics, 2009.
[3] B. Jayaraman B., Y.C. Cho, and W. Shyy, “Modeling of dielectric barrier discharge plasma actuator,” Journal Appl. Phys. 2008.
[4] W.K. Lord, D.G. MacMartin, and T.G. Tillman, “Flow Control Opportunities in Gas Turbine engines,” AIAA 2000-2234, 2000.
[5] R. Rivir, R. Sondergaard, J.P. Bons, and J.P. Lake, “Passive and Active control of separation in Gas Turbines,” AIAA 200-2235, 2000.
[6] T.C. Corke, M.L. Post, and D.M. Orlov, “Single Dielectric Barrier Discharge Plasma Enhanced Aerodynamics: Physics, Modeling and Applications,” Review Article: Experiments in Fluids, v. 46, n. 1, pp.1-26, 2008.
[7] B. Jayarama, Y. Cho, W. Shyy, “Modeling of Dielectric Barrier Discharge Plasma Actuator,” 38th AIAA Plasma Dynamics and Lasers Conferences, 2007.
[8] T.C. Corke, M. Post, “Overview of Plasma Flow Control: Concepts, Optimization and Applications,” AIAA paper, 2005.
[9] J.R. Roth, D.M. Sherman, and S.P. Wilkinson, “Boundary Layer Flow Control with A one Atmosphere Uniform Glow Discharge Plasma,” 36th AIAA Aerospace Sciences Meeting and Exhibits, Reno, 1998.
[10] M.L. Post, T. Corke, “Separation Control on High Angle of Attack Airfoil Using Plasma Actuators,” 2003-1024, 2003.
[11] D. Orlov, T. Corke, M. Post, “DNS Modeling of Plasma Array Flow Actuators,” Bulletin of the American Physical Society Fluid Dynamics Division, Annual Meeting, 2002.
[12] J. Huang, T.C. Corke, and F.O. Thomas, “Plasma Actuators for Separation Control of Low Pressure Turbine Blades,” AIAA- 2003-1027, AIAA 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.
[13] S.C. Morris, T.C. Corke, D. Van Ness, J. Stephens, and T. Douville, “Tip Clearance Control Using Plasma Actuators,” AIAA- 2005-0782, January 2005.
[14] H.D. Vo, “Control of short length-scale rotating stall inception on A high-speed axial compressor with plasma actuator,” ASME Turbo Expo 2008, GT2008-50967, 2008.
[15] H.D. Vo, J.D. Cameron, and S.C. Morris, “Control of short length-scale rotating stall inception on a high-speed axial compressor with plasma actuation,” ASME Turbo Expo 2008, GT2008-50967, 2008.
[16] F. Afshari, M. Michaud, and H.D. Vo, “Delay of Rotating Stall in Compressors using Plasma Actuator,” International Gas Turbine Institute, 2015.
[17] S. Lemire, H.D. Vo, and M.W. Banner, “Performance Improvement of Axial Compressors and Fans with Plasma Actuation,” International Journal of Rotary Machinery, 2009.
[18] W. Shyy, B. Jayarman, and A. Anderson, “Modeling of Glow Discharge-Induced Fluid Dynamics,” Journal of Applied Physics, v.92, n.11, PP. 6434-6443.
[19] Y.B. Suzen, P.G. Huang, J.D. Jacob, and D.E. Ashpis, “Numerical Simulations of Plasma Based Flow Control Applications,” AIAA Paper 2005.
[20] J.R. Roth, D.M. Sherman, and S.R. Wilkinson, “Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma,” AIAA Journal, v.38, n.7, 2000.
[21] C.L. Enloe, T.E. McLaughlin, R.D. Van Dyken, K.D. Kachner, E.J. Jamper, T.C. Corke, M. Post, and O. Haddad, “Mechanism and Response of a single Dielectric Barrier Plasma Actuator: Geometric Effects,” AIAA Journal, v.42, n.3, 2004.
[22] J.D. Jacob, K. Ramakumar, R. Anthony, and R.B. Rivir,“Control of Laminar and Turbulent Shear Flows Using Plasma Actuators,” Fourth International Symposium on Turbulence and Shear Flow Phenomena, TSFP-4, Williamsburg, VA, June 2005.
[23] C.L. Enloe, T.E. McLaughlin, G.I. Font, J.W. Baughn, “Parameterization of Temporal Structure in a Single Dielectric Barrier Aerodynamic Plasma Actuator,” AIAA Journal, v.44, n.6, 2006.