Wing and method for reducing effects of the propeller jet on the wing lift distribution

摘要

Wing (2) on which a drive unit (4) with a propeller (6) is arranged, for an aircraft, and wherein the for increasing an induced resistance, which is increased by a propeller jet flowing on the wing (2), a first region (8) having reduced local vane curvature and / or reduced local distortion, and a second region (12) having increased local vane curvature and / or increased local distortion, the first region (8) being defined as a wing surface downstream of the propeller jet viewed upstream, the blades of the propeller (6) move upwardly and wherein the second region (12) is defined as a propeller jet downstream wing surface, upstream of which the blades of the propeller (6) move downwardly.