Experimental investigation on airfoil stall separation suppression by plasma actuation

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

Volumn 26, Issue 3, 2008, Pages 372-377

  Li, Ying Hong ^a   Wu, Yun ^a   Zhang, Pu ^a   Su, Chang Bing ^a   Song, Hui Min ^a  

^a AIR FORCE ENGINEERING UNIVERSITY   (China)

Author keywords

Aerospace propulsion system; Airfoil; Flow control; Plasma actuation; Stall separation

Indexed keywords

AERODYNAMICS; AIRCRAFT PROPULSION; ANGLE OF ATTACK; ELECTROLYSIS; EXPERIMENTS; FLOW OF FLUIDS; FLOW SEPARATION; ISOMERS; MIXED CONVECTION; PLASMA DIAGNOSTICS; PLASMA FLOW; PLASMAS; POLARIZATION; PROPULSION; REYNOLDS NUMBER; SEPARATION; THEOREM PROVING;

ACTUATION VOLTAGES; AEROSPACE PROPULSION SYSTEM; AIRFOIL STALLS; AIRFOIL SUCTIONS; ASYMMETRIC ELECTRODES; BEST POSITIONS; EXPERIMENTAL INVESTIGATIONS; INFLOW VELOCITIES; LEADING EDGES; PLASMA ACTUATION; PLASMA ACTUATIONS; PLASMA ACTUATORS; STALL SEPARATION; SUPPRESSION EFFECTS;

AIRFOILS;

EID: 55149092593     PISSN: 02581825     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (15)

1. GILARRANZ J L, REDINIOTIS O K. Compact high-power synthetic jet actuators for flow separation control[R]. AIAA 2001-0737, 2001.
2. JENKINS L N, KHORRAMI M R, CHOUDHARI M. Characterization of unsteady flow structures near leading-edge slat: Part I. PIV measurements[R]. AIAA 2004-2801, 2004.
3. ROTH J R, SIN H, MADHAN R C M. Flow re-attachment and acceleration by paraelectric and peristaltic electrohydrodynamic (EHD) effects[R]. AIAA 2003-0531, 2003.
4. POST M L, CORKE T C. Separation control on high angle of attack airfoil using plasma actuators[R]. AIAA 2003-1024, 2003.
5. POST M L, CORKET C. Separation control using plasmas actuators-stationary and oscillating airfoils[R]. AIAA 2004-0841, 2004.
6. SOSA R, MOREAU E, TOUCHARD G, et al. Stall control at high angle of attack with periodically excited EHD actuators[R]. AIAA 2004-2738, 2004.
7. CORKE T C, POST M L. Overview of plasma flow control concepts, optimization, and applications[R]. AIAA 2005-0563, 2005.
8. GAITONDE D V, VISBAL M R, Roy S. Control of flow past a wing section with plasma-based body forces[R]. AIAA 2005-5302, 2005.