| 摘要 |
Described is a wing tip shape for a wing, in particular of aircraft, which wing comprises a profile that extends in the direction of the span of the wing (1), and across said direction of the span of the wing (1) extends from the wing leading edge (8, 6, 10) to the wing trailing edge (7), which profile is delimited by a first skin (11) and a second skin (12), with a winglet (3), arranged on the wing end, which winglet (3) is essentially planar, and with a transition region (2) arranged between the wing (1) and the winglet (3), which transition region (2) extends from a connection (4) on the wing (1) to a connection (5) on the winglet (3). The invention provides for the curvature of the local dihedral to increase in the transition region (2) from a low level or a level of zero at or near the wing intersection (4) in the outboard direction. |
