Plasma flow control optimized airfoil

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 19, Issue , 2006, Pages 14707-14719

  Corke, Thomas C ^a,c   Mertz, Benjamin ^a   Patel, Mehul P ^b,c  

^a UNIVERSITY OF NOTRE DAME   (United States)

^b Orbital Research Inc   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT CONTROL; NAVIER STOKES SIMULATION; PLASMA ACTUATOR; SINGLE-DIELECTRIC BARRIER DISCHARGE (SDBD);

AIRFOILS; COMPUTER SIMULATION; ELECTRIC DISCHARGES; FLOW CONTROL; NAVIER STOKES EQUATIONS; PLASMA DEVICES;

PLASMA FLOW;

EID: 34250746866     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Post, M. and T. Corke. 2003. Separation control on high angle of attack airfoil using plasma actuators. AIAA Paper 2003-1024,
2. also AIAA J., 42, 11, p. 2177.
3. Post, M. and Corke, T. 2004. Separation control using plasma actuators - stationary and oscillating airfoils. AIAA Paper 2004-0841. Also AIAA J.
4. Huang, J., Corke, T. and Thomas, F. 2003. Plasma actuators for separation control of low pressure turbine blades. AIAA Paper 2003-1027. To appear AIAA J.
5. Corke, T. C. and Post, M. L., 2005. Overview of plasma flow control: concepts, opimization, and applications. AIAA Paper 2005-0563.
6. Enloe, L, T. McLaughlin, VanDyken, Kachner, E. Jumper, and T. Corke. 2004. Mechanisms and Response of a single dielectric barrier plasma actuator: Plasma morphology. AIAA J., 42, 3, p. 589.
7. Also AIAA 2003-1021.
8. Enloe, L, T. McLaughlin, VanDyken, Kachner, E. Jumper, T. Corke.. M. Post, O. Haddad. 2004. Mechanisms and Response of a single dielectric barrier plasma actuator: Geometric effects. AIAA J., 42, 3, p 585.
9. Orlov, D., E. Erturk, M. Post, and T. Corke. 2001. DNS Modeling of Plasma Array Flow Actuators. Bulletin of the American Physical Society Fluid Dynamics Division, Annual Meeting.
10. Orlov, D., T. Corke, and M. Post, 2002. DNS Modeling of plasma array flow actuators. Bulletin of the American Physical Society Fluid Dynamics Division, Annual Meeting.
11. Orlov, D., T. Corke, and Haddad, O., 2003. DNS Modeling of plasma actuators. Bulletin of the American Physical Society Fluid Dynamics Division, Annual Meeting.
12. Post, M. 2004. Plasma actuators for separation control on stationary and oscillating wings. Ph.D Dissertation, University of Notre Dame.
13. Corke, T., He, C. and Patel, M., 2004. Plasma flaps and slats: an application of weakly-ionized plasma actuators. AIAA Paper 2004-2127.
14. Corke, T., E. Jumper, M. Post, D. Orlov, and T. McLaughlin. 2002. Application of weakly-ionized plasmas as wing flow-control devices. AIAA Paper 2002-0350.
15. Hall, K. D. 2004. Potential flow model for plasma actuation as a lift enhancement device. M.S Thesis, University of Notre Dame.
16. Hall, K., Jumper, E., Corke, T. and McLaughlin, T. 2005. Potential flow model of a plasma actuator as a lift enhancement device. AIAA Paper 2005-0783.
17. Corke, T., Design of Aircraft, Prentice-Hall Publishers, New York, 2002.
18. Sewall, W., McGhee, R., Viken, J., Waggoner, E. Walker, B., and Millard, B. 1985. Wind tunnel results for a high-speed, natural laminar-flow airfoil designed for general aviation aircraft. NASA TM 87602.
19. Orlov, D. and Corke, T. 2005. Numerical simulation of aerodynamic plasma actuator effects. AIAA Paper 2005-1083.
20. Orlov, D., Corke, T. and Patel. M. 2005. Electric circuit model for aerodynamic plasma actuator. AIAA Paper 2006-1206.
21. Huang, J. 2005. Documentation and control of flow separation on a linear cascade of Pak-B blades using plasma actuators. Ph.D., University of Notre Dame, Notre Dame, Indiana.
22. Huang, J., Corke, T. and Thomas, F., 2005. Unsteady Plasmpa actuators for separation control of low pressure turbine blades. To appear AIAA J..
23. Jeong, J. and Hussain, F. 1995. On the identification of a vortex. J. Fluid Mech., 285, p. 69-94.
24. Shiokawa, M., Matsushima, K., and Nakahashi, K. 2005. Design and aerodynamics of lift enhancement control for a single element airfoil. AIAA Paper 2005-0853.