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Why do some aircraft have winglets?
Tip devices have become a popular technique to increase the aerodynamic performances of lifting wings, short and slender alike. The idea behind all wingtip devices is to diffuse the strong vortices released at the tip and optimise the span-wise lift distribution, while maintaining the additional moments on the wing within certain limits. Investigations and experiments, indicated that the use of vertical lifting surfaces placed at the wing tips produce a beneficial effect on both lift and drag characteristics. This is found at the cost of increased bending moment. The increase in root bending moment is found to be lower than for an equivalent tip extension. Winglet sections can be airfoils with their own design.
At the tip, due to the pressure differential between the upper and lower surfaces, there is a significant span wise component to the airflow. On the lower surface, the span wise component of flow is outwards, away from the wing root, and on the upper surface, the span wise component tends to be towards the root. Lift is defined as acting perpendicularly to the flow local of the airfoil and the surface plan form, then with a bit of cunning engineering, the lift on a vertical surface at the wing tip, in a flow with a span wise component toward the root such as occurs on the upper wing surface, could be directed "forward" - in the direction of flight, - and "inward" - toward the wing root. The forward component of lift manifests itself as a reduction in total aircraft drag. Of course, the benefit is reduced somewhat by the component of winglet drag acting aft, but nonetheless, the net result is a reduction in total aircraft drag. And as mentioned elsewhere, winglets will indeed reduce the strength of the shed vortices in the tip region, but only as a consequence of the generation of a lift force on the winglet. For a given angle of attack, installation of winglets can also increase lift, but since aircraft mass is approximately unchanged, the aircraft would have to fly at a decreased angle of attack to maintain the same lift as in the pre-winglet case - which further decreases drag.
Winglets can be used to produce extra lift, besides lower drag. The winglets must be mounted on the rear part of the wing (region of lowest pressure), to minimize interference effects. Drag reduction rates are of the order of 5 %.
Winglets are applied in the latest generation of Boeing 747, MD 11, Airbus, and most executive jets and many sailplanes. Data available for the Boeing 747-400 indicate that without winglets the aircraft. suffers about 2.5 % drag losses, which corresponds to +9.5 tons at take-off.