Text this: Effects of plasma actuator on flow over an airfoil

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|      \\  |  ___||  | \| ||  |  ___||  /_   _// 
|  --  //  | ||__    |  ' ||  | ||__      | ||   
|  --  \\  | ||__    | .  ||  | ||__     _| ||   
|______//  |_____||  |_|\_||  |_____||  /__//    
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