On the use of single dielectric barrier discharge plasma actuators for improving the performance of airfoils

Collection of Technical Papers - 37th AIAA Fluid Dynamics Conference

Volumn 1, Issue , 2007, Pages 293-309

  Mabe, James H ^a,c   Calkins, Frederick T ^a,c   Wesley, B ^b,c,d   Woszidlo, R ^b,c,d   Taubert, L ^b,c,d   Wygnanski, I ^b,c,e  

^a BOEING COMPANY   (United States)

^b University of Arizona   (United States)

^c AIAA   (United States)

^d UNIVERSITY OF ARIZONA   (United States)

^e MS 67 ML ^*

Author keywords

[No Author keywords available]

Indexed keywords

DIELECTRIC BARRIER DISCHARGE; INPUT MOMENTUM; MICRO-AIR-VEHICLES; PLASMA ACTUATORS;

AIRFOILS; APPROXIMATION THEORY; DIELECTRIC DEVICES; FLOW CONTROL; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; ROTORS; WIND TUNNELS;

ACTUATORS;

EID: 35648969982     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. 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 589-594. Also AIAA 2003-1021.
2. 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 585-604.
3. B. Göksel, D. Greenblatt, I. Rechenberg, Y. Singh, C.N. Nayeri, C.O. Paschereit, "Pulsed Plasma Actuators for Separation Flow Control", Conference on Turbulence and Interactions TI2006, May 29 - June 2, 2006, Porquerolles, France
4. B. Göksel, D. Greenblatt, I. Rechenberg, C.N. Nayeri, C.O. Paschereit, "Steady and Unsteady Plasma Wall Jets for Separation and Circulation Control", 3rd AIAA Flow Control Conference, 5-8 June 2006, San Francisco, California