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Wingtip device information


The Airbus A350 wingtip device
Line drawing of wingtip vortices behind a conventional wingtip (on the left) and a blended winglet (on the right)

Wingtip devices are intended to improve the efficiency of fixed-wing aircraft by reducing drag.[1] Although there are several types of wing tip devices which function in different manners, their intended effect is always to reduce an aircraft's drag. Wingtip devices can also improve aircraft handling characteristics and enhance safety for following aircraft. Such devices increase the effective aspect ratio of a wing without greatly increasing the wingspan. Extending the span would lower lift-induced drag, but would increase parasitic drag and would require boosting the strength and weight of the wing. At some point, there is no net benefit from further increased span. There may also be operational considerations that limit the allowable wingspan (e.g., available width at airport gates).

Wingtip devices help prevent the flow around the wingtip of higher pressure air under the wing flowing to the lower pressure surface on top at the wingtip, which results in a vortex caused by the forward motion of the aircraft. Winglets also reduce the lift-induced drag caused by wingtip vortices and improve lift-to-drag ratio. This increases fuel efficiency in powered aircraft and increases cross-country speed in gliders, in both cases increasing range.[1] U.S. Air Force studies indicate that a given improvement in fuel efficiency correlates directly with the causal increase in the aircraft's lift-to-drag ratio.[2]

  1. ^ a b Robert Faye, Robert Laprete, Michael Winter (January 2002). "Blended winglets for improved airplane performance" (PDF). Aero magazine. No. 17. Boeing.{{cite magazine}}: CS1 maint: multiple names: authors list (link)
  2. ^ Committee on Assessment of Aircraft Winglets for Large Aircraft Fuel Efficiency (2007). Assessment of Wingtip Modifications to Increase the Fuel Efficiency of Air Force Aircraft. National Academies Press. p. 33. ISBN 978-0-309-38382-0. {{cite book}}: |work= ignored (help)[permanent dead link]

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