The circulation of a high-lift airfoil is enhanced using a spanwise array of fluidically oscillating wall jets to engender a Coanda-like effect on the suction surface near the cove between the flap and the main element. The actuation jets manipulate the interaction between the main element boundary layer and the cove jet to overcome flow separation over the flap and yield high-lift performance that is comparable to or better than conventional high-lift airfoils. The fluidic actuation enables effective operation at larger flap deflections while diminishing the sensitivity to cove characteristics. The performance of the actuator array varies with both the jet momentum coefficient and the spanwise periodic jet spacing. It is shown that the lift increment per jet, which for a sufficiently sparse jet array is invariant with jet spacing, diminishes as jet spacing is reduced due to spanwise jet interactions. Accordingly, the overall lift increment scales with the number of active jets and jet density, and a characteristic spanwise jet spacing is identified for optimal performance.
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