Wing for an aircraft

A wing for an aircraft, comprising

• a main wing, and
• a leading edge high lift assembly comprising
• a high lift body, and
• a connection assembly connecting the high lift body to the main wing in such a way that the high lift body is movable relative to the main wing between a stowed position and a deployed position,
• wherein a wing profile has a greater curvature in the deployed position than the stowed position,
• wherein the connection assembly comprises at least one rotation element that is mounted to the high lift body and that is mounted to the main wing rotatably about an axis of rotation,
• wherein the main wing comprises an upper skin panel and a lower skin panel, wherein the upper skin panel has a leading edge portion,
• wherein the high lift body extends between a leading edge and a trailing edge, wherein the trailing edge of the high lift body is configured to move along the leading edge portion of the upper skin panel of the main wing, when the high lift body is moved between the stowed position and the deployed position,
• wherein the leading edge portion of the upper skin panel is configured to be elastically deformed when the high lift body is moved from the stowed position to the deployed position,
• wherein the wing further comprises:
• a rotating actuator for driving the rotation element about the axis of rotation, and the rotating actuator comprising:
• a first rotating arm, and
• a second rotating arm, the first rotating arm and the second rotating arm configured to rotate in opposite directions about a common axis,
• wherein the first rotating arm is rotatably mounted to the main wing, and the second rotating arm is rotatably mounted to the rotation element or to the high lift body.