Aerodynamic control using windward-surface plasma actuators on a separation ramp

Journal of Aircraft

Volumn 44, Issue 6, 2007, Pages 1889-1895

  Lopera, Javier ^a,d,e   Ng, T Terry ^a,d,e   Patel, Mehul P ^b,e,f   Vasudevan, Srikanth ^b,e   Santavicca, Ed ^b   Corke, Thomas C ^c,e,g  

^a UNIVERSITY OF TOLEDO   (United States)

^b Orbital Research Inc   (United States)

^c UNIVERSITY OF NOTRE DAME   (United States)

^d Industrial and Manufacturing Engineering

^e AIAA ^*

^f Aerodynamics Group

^g Aerospace and Mechanical Engineering Department

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CONTROL SYSTEMS; STEADY FLOW; UNMANNED AERIAL VEHICLES (UAV);

AERODYNAMIC CONTROL; MODULATION FREQUENCY; SURFACE PLASMA ACTUATORS;

AERODYNAMICS;

EID: 38149005559     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.30741     Document Type: Article

References (15)

1. Patel, M. P., Ng, T. T., Vasudevan, S., Corke, T. C., and He, C., "Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle," AIAA Paper 2006-3495, June 2006.
2. Corke, T. C., Cavalieri, D., and Maths, E., "Boundary Layer Instability on a Sharp Cone at Mach 3.5 with Controlled Input," AIAA Journal, Vol. 40, No. 5, 2002, pp. 1015-1018.
3. Roth, J. R., Sherman, D. M., and Wilkinson, S. R., "Electro- hydrodynamic Flow Control with a Glow-Discharge Surface Plasma," AIAA Journal, Vol. 38, No. 7, 2000, pp. 1166-1172.
4. Corke, T., Jumper, E., Post, M., Orlov, D., and McLaughlin, T., "Application of Weakly Ionized Plasmas as Wing Flow Control Devices," AIAA Paper 2002-0350, Jan. 2002.
5. 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;
6. also AIAA Paper 2003-1024, Jan. 2003.
7. Post, M. L., and Corke, T., "Separation Control Using Plasma Actuators: Stationary & Oscillating Airfoils," AIAA Paper 2004-0841, Jan. 2004.
8. Corke, T. C., He, C., and Patel, M. P., "Plasma Flaps and Slats: An Application of Weakly-Ionized Plasma Actuators," AIAA Journal (to be published); also AIAA Paper 2004-2127, 2004.
9. Jacob, J., Rivir, R., Campbell, C., and Estevedoreal, J., "Boundary Layer Flow Control Using AC Discharge Plasma Actuators," AIAA Paper 2004-2128, June 2004.
10. Patel, M. P., Sowie, Z. H., Corke, T. C., and He, C., "Autonomous Sensing and Control of Wing Stall Using a Smart Plasma Slat," AIAA Paper 2006-1207, Jan. 2006.
11. Corke, T. C., Mertz, B., and Patel, M. P., "Plasma Flow Control Optimized Airfoil," AIAA Paper 2006-1208, Jan. 2006.
12. Enloe, L., McLaughlin, T., VanDyken, R., Kachner, Jumper, E., and Corke, T. C., "Mechanisms and Response of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology," AIAA Journal, Vol. 42, No. 3, 2004, pp. 589-594.
13. Enloe, L., McLaughlin, T., VanDyken, R., Kachner, Jumper, E., Corke, T. C., Post, M., and Haddad., O., "Mechanisms and Response of a Single Dielectric Barrier Plasma Actuator: Geometric Effects," AIAA Journal, Vol. 42, No. 3, 2004, pp. 595-604.
14. Corke, T. C., and Post, M., "Overview of Plasma Flow Control: Concepts, Optimization, and Applications," AIAA Paper 2005-0563, Jan. 2005.
15. Patel, M. P., Ng, T. T., Vasudevan, S., Corke, T. C., Post, M. L., McLaughlin, T. E., and Suchomel, C. F., "Scaling Effects of an Aerodynamic Plasma Actuator," AIAA Paper 2007-0635, Jan. 2007.