Three-dimensional flow measurements induced from serpentine plasma actuators in quiescent air

Journal of Physics D: Applied Physics

Volumn 45, Issue 3, 2012, Pages

  Durscher, R J ^a   Roy, S ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPLIED VOLTAGES; CIRCULAR ARC; DIELECTRIC BARRIER DISCHARGES; INDUCED FLOW FIELD; PLASMA ACTUATOR; RAPID MIXING; SERPENTINE CONFIGURATION; SPATIALLY RESOLVED; STEREO PARTICLE IMAGE VELOCIMETRY; THREE COMPONENT; THREE-DIMENSIONAL FLOW MEASUREMENTS; TIME-AVERAGED; VELOCITY VECTORS;

ACTUATORS; DIELECTRIC DEVICES; ELECTRIC DISCHARGES; FLOW FIELDS; SERPENTINE; THREE DIMENSIONAL; VELOCITY MEASUREMENT;

FLOW MEASUREMENT;

EID: 84855905981     PISSN: 00223727     EISSN: 13616463     Source Type: Journal    
DOI: 10.1088/0022-3727/45/3/035202     Document Type: Article

References (14)

1. Benard N, Braud P, Jolibois J and Moreau E 2008 Airflow reattachment along a NACA 0015 airfoil by surfaces dielectric barrier discharge actuator-time resolved particle image velocimetry investigation 4th Flow Control Conf. (Seattle, WA,) AIAA 2008-4202
2. Huang J, Corke T C and Thomas F O 2006 Plasma actuators for separation control of low-pressure turbine blades AIAA J. 44 517
3. Sung Y, Kim W, Mungal M G and Cappeli M 2006 Aerodynamic modification of flow over bluff objects by plasma actuation Exp. Fluids 41 47986 (Pubitemid 44290903)
4. Santhanakrishnan A and Jacob J 2007 Flow control with plasma synthetic jet actuators J. Phys. D: Appl. Phys. 40 63751 (Pubitemid 46485760)
5. Schatzman D M and Thomas F O 2008 Turbulent boundary layer separation control with plasma actuators 4th Flow Control Conf. (Seattle, WA,) AIAA 2008-4199
6. He C 2008 Plasma slats and flaps: an application of plasma actuators for hingeless aerodynamic control PhD Thesis Notre Dame
7. Porter C, Abbas A, Cohen K, McLaughlin T and Enloe C 2009 Spatially distributed forcing and jet vectoring with a plasma actuator AIAA J. 47 136878
8. Roy S and Wang C 2009 Bulk flow modification with horseshoe and serpentine plasma actuators J. Phys. D: Appl. Phys. 42 032004
9. Rizzetta D P and Visbal M R 2011 Effect of plasma-based control on low-Reynolds number flapping airfoil performance 49th AIAA Aerospace Sciences Meeting. (Orlando, FL,) AIAA 2011-735
10. Rizzetta D P and Visbal M R 2011 Numerical investigation of plasma-based control for low-Reynolds-number airfoil flows AIAA J. 49 41125
11. Poggie J, Tilmann C P, Flick P M, Silkey J S, Osborne B A, Ervin G, Maric D, Mangalam S and Mangalam A 2010 Closed-loop stall control system J. Aircraft 47 174755
12. TSI 2000 Model 9302 Atomizer, Instruction Manual
13. 2007 DaVis 7.2, Instruction Manual
14. Forte M, Jolibois J, Pons J, Moreau E, Touchard G and Cazalens M 2007 Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control Exp. Fluids 43 91728 (Pubitemid 350165582)