winglet$92094$ - перевод на голландский
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winglet$92094$ - перевод на голландский

AIRCRAFT COMPONENT FIXED TO THE END OF THE WINGS TO IMPROVE PERFORMANCE
Winglets; Raked wingtip; Blended winglet; Wingtip fence; Blended winglets; Raked wingtips; Wingtip fences; Wing tip device; Wing-tip device; Winglet; Spiroid wingtip; Sharklet (wingtip device); Sharklets; Swept wingtips; Wingtip devices
  • Line drawing of [[wingtip vortices]] behind a conventional wingtip (on the left) and a blended winglet (on the right)
  • The [[Airbus A350]] wingtip
  • Ha 137]] prototype aircraft, fitted with vertical wing extensions, c.1935–1937
  • 737 MAX split-tip winglet
  • [[Heinkel He 162A]] with ''Lippisch-Ohren'' wingtip devices
  • Wingtip device on a [[NHIndustries NH90]]
  • A [[Learjet 28/29]], the first commercial aircraft with winglets
  • transonic wind tunnel]]
  • PSU-90-125 winglet [[airfoil]] profile
  • winch-launching]]
  • A Falcon 50 with a spiroid winglet
  • Tamarack Aerospace's active wingtip device
  • tufts]] showing airflow during [[NASA]] tests in 1979–1980

winglet      
n. vleugeltje

Определение

Winglet
·noun A bastard wing, or alula.
II. Winglet ·noun A little wing; a very small wing.

Википедия

Wingtip device

Wingtip devices are intended to improve the efficiency of fixed-wing aircraft by reducing drag. 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 by partial recovery of the tip vortex energy. 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, the winglet also reduces the lift-induced drag caused by wingtip vortices, and improves lift-to-drag ratio. This increases fuel efficiency in powered aircraft and increases cross-country speed in gliders, in both cases increasing range. 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.