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In this study, dielectric barrier discharge plasma actuators (DBD-PA) were used to actively control flow separation over a NACA0024 airfoil. Experiments were conducted at a free stream velocity up to U ≈ 10m/s (Re ≈ 1.3 × 10 5 ) in an open-circuit blower type wind tunnel with a test section measuring 200 mm × 200 mm × 600mm. The airfoil model was designed specifically to incorporate minimum...
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