High lift airfoil leading edge separation control with nanosecond pulse driven DBD plasma actuators

5th Flow Control Conference

Volumn , Issue , 2010, Pages

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

^a OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLES OF ATTACK; COHERENT STRUCTURE; COMPRESSION WAVES; DBD PLASMA; DIELECTRIC BARRIER DISCHARGE PLASMAS; FLOW INSTABILITIES; FLOW SEPARATION CONTROL; FREE-STREAM; HIGH AMPLITUDES; HIGH-LIFT AIRFOILS; LEADING EDGE; NANOSECOND PULSE; PLASMA ACTUATOR; SEPARATED FLOWS; SPANWISE VORTEX; SUCTION SURFACES;

ACTUATORS; AIRFOILS; ELECTRIC DISCHARGES; FLOW CONTROL; PLASMA DIAGNOSTICS; PLASMAS; VORTEX FLOW;

DIELECTRIC DEVICES;

EID: 78649505269     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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