High Mach number leading-edge flow separation control using AC DBD plasma actuators

50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2012, Pages

  Kelley, Christopher L ^a   Bowles, Patrick ^a   Cooney, John ^a   He, Chuan ^a   Corke, Thomas C ^a   Osborne, Bradley ^b   Silkey, Joseph ^b   Zehnle, Joseph ^b  

^a UNIVERSITY OF NOTRE DAME   (United States)

^b BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AC SIGNALS; ACTIVE FLOW CONTROL; AIRFOIL SURFACES; ALTERNATING CURRENT; ATMOSPHERIC CONDITIONS; CONTROL ACTUATORS; COPPER ELECTRODES; DBD PLASMA; DEEP STALL; DIELECTRIC BARRIER DISCHARGES; ENERGY EFFICIENT; FLOW REATTACHMENT; FLOW SEPARATION CONTROL; FREE-STREAM; HIGH MACH NUMBER; HIGH VOLTAGE; LEADING EDGE; LIFT AND DRAG; LOAD CELLS; MAXIMUM LIFT COEFFICIENT; PITCHING MOMENTS; PLASMA ACTUATOR; PRESSURE PEAKS; PRESSURE RECOVERY; PRESSURE TAPS; REDUCED FREQUENCY; SEPARATED FLOWS; SUCTION SURFACES; SUPERCRITICAL AIRFOILS; TIME-AVERAGED; TORQUE SENSORS; UNIVERSITY OF NOTRE DAME; WIND TUNNEL EXPERIMENT; WIND TUNNEL TESTS;

ACTUATORS; AEROSPACE ENGINEERING; AIRFOILS; DIELECTRIC FILMS; DRAG; ELECTRODES; ENERGY EFFICIENCY; EXHIBITIONS; EXPERIMENTS; FLOW CONTROL; LIFT; MACH NUMBER; NASA; PLASMAS; POLYIMIDES; REYNOLDS NUMBER; WIND TUNNELS;

DIELECTRIC DEVICES;

EID: 84873871956     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2012-906     Document Type: Conference Paper

References (13)

1. Corke, T. C., Enloe, C. L., and Wilkinson, S. P., "Dielectric barrier discharge plasma actuators for flow control." Ann. Rev. Fluid Mech., Vol. 42, 2010, pp. 505-529.
2. Corke, T. C., Post, M. L., and Orlov, D. M., "Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications." Exp. Fluids, Vol. 46, 2009, pp. 1-26.
3. Enloe, L., McLaughlin, T., VanDyken, Kachner, Jumper, E., and Corke, T., "Mechanisms and Responses of a Single-Dielectric Barrier Plasma Actuator: Plasma Morphology." AIAA, Vol. 42, 2004, pp. 589-594.
4. Enloe, L., McLaughlin, T., VanDyken, Kachner, Jumper, E., Corke, T., Post, M., and Haddad, O., "Mechanisms and Responses odf a Single-Dielectric Barrier Plasma Actuator: Geometric Effects." AIAA, Vol. 42, 2004, pp. 595-604.
5. Orlov, D. and Corke, T., "Numerical Simulation of Aerodynamic Plasma Actuator Effects." AIAA 2005-1083, 2005.
6. Orlov, D. M., Apker, T., He, C., Othman, H., and Corke, T. C., "Modeling and experiment of Leading-edge Separation Control Using Single-dielectric Barrier Discharge Plasma Actuators." AIAA, 2007.
7. Orlov, D. M., Modelling and Simulation of Single Dielectric Barrier Discharge Plasma Actuators., Ph.D. thesis, University of Notre Dame, 2006.
8. Mertz, B. E., Refinement, validation and implementation of lumped circuit element model for single dielectric barrier discharge plasma actuators., Ph.D. thesis, University of Notre Dame, 2010.
9. Post, M. and Corke, T., "Separation Control On High Angle Of Attack Airfoil Using Plasma Actuators," AIAA, Vol. 42, 2004, pp. 2177.
10. He, C., SDBD Plasma Actuator Separation Control., Ph.D. thesis, University of Notre Dame, 2008.
11. Post, M. and Corke, T., "Overview of Plasma Flow Control: Concepts, Optimization, and Application." AIAA Paper 2005-0563, 2005.
12. Huang, J., Documentation and control of flow separation on a linear cascade of Pak-B blades using plasma actuators., Ph.D. thesis, University of Notre Dame, 2005.
13. Huang, J., Corke, T. C., and Thomas, F. O., "Plasma actuators for separation control of low pressure turbine blades." AIAA Paper 2003-1027, 2003.