Numerical modeling of DBD plasma actuators and the induced air flow

Collection of Technical Papers - 38th AIAA Plasmadynamics and Lasers Conference

Volumn 2, Issue , 2007, Pages 1060-1072

  Likhanskii, Alexandre V ^a,c,d   Shneider, Mikhail N ^a,c,d   Opaits, Dmitry F ^a,c,d   Miles, Richard B ^a,c,d   Macheret, Sergey O ^b,c,d  

^a PRINCETON UNIVERSITY   (United States)

^b Lockheed Martin Aeronautics Company   (United States)

^c Department of Mechanical and Aerospace Engineering ^*

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; BIAS VOLTAGE; COMPUTER SIMULATION; ELECTRIC DISCHARGES; MATHEMATICAL MODELS;

DBD PLASMA ACTUATORS; ELECTRODES DBD SYSTEMS;

PLASMA FLOW;

EID: 35648966588     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4533     Document Type: Conference Paper

References (52)

1. Macheret, S.O., Shneider, M.N., and Miles, R.B., " Magnetohydrodynamic and Electrohydrodynamic Control of Hypersonic Flows of Weakly Ionized Plasmas," AIAA Journal, Vol. 42, No. 11, November 2004, pp. 1378-1387.
2. Macheret, S.O., Shneider, M.N., Miles, R.B., and Lipinski, R.J., "Electron Beam Generated Plasmas in Hypersonic Magnetohydrodynamic Channels," AIAA Journal, Vol. 39, No. 6, 2001, pp. 1127-1136.
3. Macheret, S.O., Shneider, M.N., and Miles, R.B., " Magnetohydrodynamic Control of Hypersonic Flow and Scramjet Inlets Using Electron Beam Ionization," AIAA Journal, Vol. 40, No. 1, 2002, pp. 74-81.
4. Macheret, S.O., Shneider, M.N., and Miles, R.B., "MHD Power Extraction from Cold Hypersonic Air Flow with External Ionizers," Journal of Propulsion and Power, Vol. 18, No. 2, 2002, pp. 424-431.
5. Shneider, M.N., Macheret, S.O., and Miles, R.B., "Analysis of Magnetohydrodynamic Control of Scramjet Inlets," AIAA Journal, Vol. 42, No. 11, November 2004, pp. 2303-2310.
6. th AIAA Plasmadynamics and Lasers Conference, Orlando, FL, June 23-26, 2003.
7. nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 5-8, 2004.
8. nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 5-8, 2004.
9. th AIAA Plasmadynamics and Lasers Conference, Portland, OR, June 28-July 1, 2004.
10. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
11. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
12. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002.
13. rd AIAA Weakly Ionized Gases Workshop, Norfolk, VA, November 1-5, 1999.
14. Bityurin, V.A., Klimov, A.I., Leonov, S.B., Bocharov, A.N., and Lineberry, J.T., "Assessment of a Concept of Advanced Flow/Flight Control for Hypersonic Flights in Atmosphere," Paper AIAA 1999-4820, 3rd AIAA Weakly Ionized Gases Workshop, Norfolk, VA, November 1-5, 1999.
15. 15.Nishihara, M., Jiang, N., Rich, J.W., Lempert, W.R., Adamovich, I.V., and Gogineni, S., "LowTemperature Supersonic Boundary Layer Control Using Repetitively Pulsed MHD Forcing," Physics of Fluids, Vol. 17, 2005, pp. 106102-1 - 106102-12.
16. M. Nishihara, J.W. Rich, W.R. Lempert, I.V. Adamovich, and S. Gogineni, "Low-Temperature M=3 Flow Deceleration by Lorentz Force", Physics of Fluids, vol. 18, No. 8,2006, p. 086101
17. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
18. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
19. Surzhikov, S.T., and Shang, J.S., "Two-Component Plasma Model for Two-Dimensional Glow Discharge in Magnetic Field," Journal of Computational Physics, Vol. 199, 2004, pp. 437-464.
20. nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 5-8, 2004.
21. Surzhikov, S.T. and Shang, J.S., "Viscous interaction on a flat plate with a surface discharge in magnetic field", High Temperature, Vol. 43, No. 1, 2005, pp. 19-30.
22. nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 5-8, 2004.
23. Poggie, J., "Numerical Exploration of Flow Control with Glow Discharges," Paper AIAA 2004-2858, 35 AIAA Plasmadynamics and Lasers Conference, Portland, OR, 28 June - 1 July, 2004.
24. Shang, J.S., Kimmel, R., Hayes, J., Tyler, C, and Menart, J., "Hypersonic Experimental Facility for Magnetoaerodynamic Interactions," Journal of Spacecraft and Rockets, Vol. 42, No. 5, 2005, pp. 780789.
25. Shang, J.S., and Surzhikov, S.T., "Magnetoaerodynamic Actuator for Hypersonic Flow Control," AIAA Journal, Vol. 43, No. 8, 2005, pp. 1633-1652.
26. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 10-13, 2005.
27. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
28. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 2006.
29. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 2006.
30. 30.Enloe, C.L., McLaughlin, T.E., VanDyken, R.D., Kachner, K.D., Jumper, E.J., and Corke, T.C., "Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology," AIAA Journal, Vol. 42, No. 3, 2004, pp. 589-594.
31. 31.Enloe, CL., McLaughlin, T.E., VanDyken, R.D., Kachner, K.D., Jumper, E.J., Corke, T.C, Post, M., and Haddad, O., "Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Geometric Effects," AIAA Journal, Vol.42, No. 3, 2004, pp. 595-604.
32. th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Ontario, June 6-9, 2005.
33. th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, January 14-17, 2002.
34. Post, M.L., and Corke T.C., "Separation Control on High Angle of Attack Airfoil Using Plasma Actuators," AIAA Journal, Vol. 42, No. 11, 2004, pp. 2177-2184.
35. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
36. D. Opaits, A. Likhanskii, M. Shneider, G. Neretti, S. Zaidi, S. Macheret and R. Miles, Paper AIAA-2007-4532, 38th AIAA Plasmadynamics and Lasers Conference, Miami, Florida, June 25-28, 2007
37. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
38. Roy, S., "Flow actuation using radio frequency in partially ionized collisional plasmas," Applied Physics Letters, Vol. 86, 2005, pp. 1001502-1 - 101502-3
39. Singh, K.P. and Roy, S., "Simulation of an asymmetric single dielectric barrier plasma actuator," Journal of Applied Physics, Vol. 98, 2005, 083303-1 - 083303-7
40. Boeuf, J.P., and Pitchford, L.C., "Electrohydrodynamic force and aerodynamic flow acceleration in surface dielectric barrier discharge," Journal of Applied Physics, Vol. 97, 2005, 103307-1 - 103307-10
41. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2005.
42. A. Likhanskii, M. Shneider, S. Macheret and R. Miles, Paper AIAA-2006-1204,44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006
43. A. Likhanskii, M. Shneider, S. Macheret and R. Miles, Paper AIAA-2007-633, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan, 10-13, 2007
44. A. Likhanskii, M. Shneider., S. Macheret and R. Miles, Physics of Plasmas, Volume 14, Issue 6, 2007
45. C. O. Porter, J. W. Baughn, T. E. McLaughlin, C. L. Enloe, G. I. Font, "Temporal Force Measurements on an Aerodynamic Plasma Actuator", Paper AIAA 2006-104, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006
46. S.O. Macheret, M.N. Shneider, and R.B. Miles, IEEE Transactions On Plasma Science, Vol.30, No.3 (2002)
47. I.S. Grigoriev, and E.Z. Meilikhov, Handbook of physical quantities, (CRC Press, Boca Raton, 1997), chapter 20
48. H.K. Gummel, IEEE Trans. Electron Dev. 11,10,455-465 (1964)
49. D.L. Scharfetter, H.K. Gummel, IEEE Trans. Electron Dev. 16, 1, 64-77 (1969)
50. J.C Butcher, The numerical analysis of ordinary differential equations: Runge-Kutta and general linear methods, (Wiley, New York, 1987)
51. D.A. Anderson, J.C. Tannehill, and R.H. Pletcher, Computational Fluid Mechanics and Heat Transfer (Hemisphere, New York, 1984)
52. M. Visbal, D. Gaitonde, and S. Gogineni "Direct Numerical Simulation of a Forced Transitional Plane Wall Jet," Paper AIAA 98-2643, 29th AIAA Fluid Dynamics Conference, Albuquerque, NM, June 1998