On the vortex dynamic of airflow reattachment forced by a single non-thermal plasma discharge actuator

Flow, Turbulence and Combustion

Volumn 87, Issue 1, 2011, Pages 1-31

  Benard, Nicolas ^a   Moreau, Eric ^a  

^a UNIVERSITÉ DE POITIERS   (France)

Author keywords

Dielectric barrier discharge; Flow control; Plasma actuator; Separated airflow; Vortex dynamics

Indexed keywords

ACQUISITION SYSTEMS; AERIAL VEHICLE; CHORD LENGTHS; CONTROLLED FLOW; CROSS-CORRELATION FUNCTION; DIELECTRIC BARRIER DISCHARGES; FREE SHEAR LAYER; HIGH ANGLES OF ATTACK; HIGH-SPEED; LEADING EDGE; NATURAL FLOW; NON-THERMAL PLASMA DISCHARGES; PARTIAL FLOW; PLASMA ACTUATOR; PLASMA DISCHARGE; SEPARATED AIRFLOW; SEPARATED FLOWS; SPECIFIC FREQUENCIES; SUCTION SIDE; TEMPORAL ANALYSIS; TIME-RESOLVED ANALYSIS; TRAILING EDGES; VELOCITY FIELD; VORTEX DYNAMICS;

ACTUATORS; AIRFOILS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; DIELECTRIC DEVICES; ELECTRIC DISCHARGES; FLOW CONTROL; MILITARY VEHICLES; SHEAR FLOW; VELOCITY; VORTEX SHEDDING;

VORTEX FLOW;

EID: 79851514934     PISSN: 13866184     EISSN: 15731987     Source Type: Journal    
DOI: 10.1007/s10494-011-9325-4     Document Type: Article

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