High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator

Experiments in Fluids

Volumn 48, Issue 3, 2010, Pages 521-537

  Little, Jesse ^a   Nishihara, Munetake ^a   Adamovich, Igor ^a   Samimy, Mo ^a  

^a Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DBD PLASMA; DIELECTRIC BARRIER DISCHARGE PLASMAS; DUTY CYCLES; FREE-STREAM; HIGH-FREQUENCY ACTUATION; HIGH-LIFT AIRFOILS; MODULATION FREQUENCIES; MODULATION WAVEFORMS; NATURAL OSCILLATION FREQUENCY; PLASMA DISCHARGE; POWER REQUIREMENT; PRIMARY CONTROL MECHANISM; QUASI-STEADY; QUIESCENT CONDITIONS; SEPARATED REGION; SINUSOIDAL MODULATION; TIME-AVERAGED; TRAILING EDGES; VELOCITY PERTURBATION;

ACTUATORS; AIRFOILS; DIELECTRIC DEVICES; FLOW CONTROL; MODULATION; OSCILLATING FLOW; PLASMAS; REYNOLDS NUMBER; VORTEX SHEDDING;

ELECTRIC DISCHARGES;

EID: 77952095125     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-009-0755-x     Document Type: Article

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