Experimental investigation on airfoil suction side flow separation by pulse plasma aerodynamic actuation

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 29, Issue 6, 2008, Pages 1429-1435

  Li, Yinghong ^a   Liang, Hua ^a   Ma, Qingyuan ^a   Wu, Yun ^a   Song, Huimin ^a   Wu, Wei ^a  

^a AIR FORCE ENGINEERING UNIVERSITY   (China)

Author keywords

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

Indexed keywords

AERODYNAMICS; AIR; AIRCRAFT PROPULSION; EXPERIMENTS; FLOW CONTROL; FLOW OF FLUIDS; FLOW SEPARATION; GAS DYNAMICS; PLASMA DIAGNOSTICS; PLASMAS; POLARIZATION; PROPULSION; SEPARATION;

AEROSPACE PROPULSION SYSTEM; AIRFOIL STALLS; AIRFOIL SUCTIONS; BEST POSITIONS; CONTROL CAPABILITIES; DUTY CYCLES; EQUIVALENT CONTROL EFFECTS; EXPERIMENTAL INVESTIGATIONS; INFLOW VELOCITIES; LEADING EDGES; PLASMA ACTUATIONS; POWER CONSUMPTIONS; PULSE FREQUENCIES; PULSE PLASMAS; SUCTION SIDES; SUPPRESSION EFFECTS;

AIRFOILS;

EID: 57649103103     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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