A wing for an aircraft, comprising a main wing, a slat, and a connection assembly for movably connecting the slat to the main wing. The connection assembly comprises first and second link elements. The first link element has a first link end rotatably mounted to the slat via a first joint, and a second link end rotatably mounted to the main wing via a second joint. The second link element has a first element end rotatably mounted to the slat via a third joint, and a second element end rotatably mounted to the main wing via a fourth joint. The first joint, the second joint and the third joint are formed as spherical joints or as universal joints, while the fourth joint is formed as a hinged joint, wherein the hinge axis is inclined between a wing thickness direction and a wing span direction.