Experimental investigation of pulsed dielectric barrier discharge actuators in sub- and transonic flow

44th AIAA Plasmadynamics and Lasers Conference

Volumn , Issue , 2013, Pages

  Peschke, P ^a   Goekce, S ^a   Leyland, P ^a   Ott, P ^a   Hollenstein, Ch ^a  

^a EPFL   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY-LAYER SEPARATION; COMPRESSOR BLADES; CONTROL AUTHORITIES; DIFFERENT VOLTAGES; EXPERIMENTAL INVESTIGATIONS; PULSED DIELECTRIC BARRIER DISCHARGES; SCHLIEREN FLOW VISUALIZATION; SURFACE PRESSURE DISTRIBUTION;

BOUNDARY LAYERS; DIELECTRIC DEVICES; EXPERIMENTS; FLOW CONTROL; MAGNETOHYDRODYNAMICS; SHOCK WAVES; TRANSONIC FLOW;

ACTUATORS;

EID: 84883479675     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2013-2885     Document Type: Conference Paper

References (22)

1. 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.
2. Post, M. L. and Corke, T. C., "Separation control on high angle of attack airfoil using plasma actuators, " AIAA 2003-1024, 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, 2003.
3. Grundmann, S. and Tropea, C., "Experimental transition delay using glow-discharge plasma actuators, " Experiments in Fluids, Vol. 42, No. 4, 2007.
4. Jukes, T. N. and Choi, K. S., "Long lasting modifications to vortex shedding using a short plasma excitation, " physical review letters, Vol. 102, No. 25, 2009.
5. Benard, N., Bonnet, J. P., Touchard, G., and Moreau, E., "Flow control by dielectric barrier discharge actuators: jet mixing enhancement, " AIAA Journal, Vol. 46, No. 9, 2008.
6. Moreau, E., "Airflow control by non-thermal plasma actuators, " Journal of Physics D: Applied Physics, Vol. 40, No. 3, 2007.
7. Corke, T. C., Enloe, C. L., and Wilkinson, S. P., "Dielectric Barrier Discharge Plasma Actuators for Flow Control, " Annual Review of Fluid Mechanics, Vol. 42, No. 1, 2010, pp. 505-529.
8. Roupassov, D. V., Nikipelov, A. A., Nudnova, M. M., and Starikovskii, A. Y., "Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge, " AIAA Journal, Vol. 47, No. 1, 2009.
9. Little, J., Takashima, K., Nishihara, M., Adamovich, I., and Samimy, M., "Separtion Control with Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators, " AIAA Journal, Vol. 50, No. 2, 2012, pp. 350-365.
10. Nishihara, M., Takashima, K., Rich, J. W., and Adamovich, I. V., "Mach 5 bow shock control by a nanosecond pulse surface dielectric barrier discharge, " Physics of Fluids, Vol. 23, No. 6, 2011, pp. 066101.
11. Biollo, R. and Benini, E., "Recent advances in transonic axial compressor aerodynamics, " Progress in Aerospace Sciences, Vol. 56, No. 0, 2013, pp. 1-18.
12. Lehr, A. and Blcs, A., "Experimental Investigation of the Periodic Unsteady Transonic Flow Field Around a Compressor Blade by Means of Particle Image Velocimetry, " The 9th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, 2002.
13. Bell, R. M. and Fottner, L., "Investigations of Shock/Boundary-Layer Interaction in a Highly Loaded Compressor Cas-cade, " ASME Paper 95-GT-84, 1995.
14. Schulz, K., Dalbert, P., and Blcs, A., "Experimental Investigation in Annular Compressor Cascades at Transonic Flow Conditions, " ASME Paper 95-GT-83, 1995.
15. Hennings, H. and Belz, J., "Experimental investigation of the aerodynamic stability of an annular compressor cascade performing tuned pitching oscillations in transonic flow, " ASME Paper 99-GT-407, 1999.
16. Carstens, V. and Belz, J., "Numerical Investigation of Nonlinear Fluid-Structure Interaction in Vibrating Compressor Blades, " Journal of Turbomachinery, Vol. 123, No. 2, 2000.
17. Pavon, S., Dorier, J. L., Hollenstein, C., Ott, P., and Leyland, P., "Effects of high-speed airflows on a surface dielectric discharge, " Journal of Physics D: Applied Physics, Vol. 40, No. 6, 2007.
18. Pavon, S., Ott, P., Leyland, P., Dorier, J. L., and Hollenstein, C., "Effects of a surface dielectric barrier discharge on transonic flows around an airfoil, " AIAA 2009-649, 47th AIAA Aerospace Sciences Meeting, Orlando, 2009.
19. Correale, G., Popov, I., Rakitin, A., Starikovskii, A., Hulshoff, S., and Veldhuis, L., "Flow Separation Control on Airfoil With Pulsed Nanosecond Discharge Actuator, " AIAA 2011-1079, 49th AIAA Aerospace Sciences Meeting, Orlando, Florida, 2011.
20. Benard, N., Zouzou, N., Claverie, A., Sotton, J., and Moreau, E., "Optical visualization and electrical characterization of fast-rising pulsed dielectric barrier discharge for airflow control applications, " Journal of Applied Physics, Vol. 111, 2012.
21. Peschke, P., Goekce, S., Hollenstein, C., Leyland, P., and Ott, P., "Interaction Between Nanosecond Pulse DBD Actuators and Transonic Flow, " AIAA 2011-3734, 42nd AIAA Plasmadynamics and Lasers Conference, Honolulu, 2011.
22. Little, J., Takashima, K., Nishihara, M., Adamovich, I., and Samimy, M., "High lift airfoil leading edge separation control with nanosecond pulse driven DBD plasma actuators, " AIAA 2010-4256, 5th AIAA Flow Control Conference, Chicago, 2010.