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  2. Wingtip vortices - Wikipedia

    en.wikipedia.org/wiki/Wingtip_vortices

    Wingtip vortices are circular patterns of rotating air left behind a wing as it generates lift. [1]: 5.14 The name is a misnomer because the cores of the vortices are slightly inboard of the wing tips. [2]: 369 Wingtip vortices are sometimes named trailing or lift-induced vortices because they also occur at points other than at the wing tips.

  3. Wingtip device - Wikipedia

    en.wikipedia.org/wiki/Wingtip_device

    The wingtip vortex, which rotates around from below the wing, strikes the cambered surface of the winglet, generating a force that angles inward and slightly forward, analogous to a sailboat sailing close hauled. The winglet converts some of the otherwise-wasted energy in the wingtip vortex to an apparent thrust. This small contribution can be ...

  4. Vortex lift - Wikipedia

    en.wikipedia.org/wiki/Vortex_lift

    Image showing formation of vortices behind the leading edge of a delta wing at high angle of attack A cloud of smoke shows the roll-up of the vortex sheet shed from the whole trailing edge of a wing producing lift from attached flow, with its core aligned with the wing tip. Vortex lift has an additional vortex close to the body when shed by a ...

  5. Wing tip - Wikipedia

    en.wikipedia.org/wiki/Wing_tip

    The winglet and red navigation light on the wing tip of a South African Airways Boeing 747-400 Many aircraft types, such as the Lockheed Super Constellation shown here, have fuel tanks mounted on the wing tips, commonly called tip tanks The wing tip of a Quad City Challenger II, formed with an aluminum bow The wing tip of a Grumman American AA-1, showing its Hoerner style design A Piper PA-28 ...

  6. Closed wing - Wikipedia

    en.wikipedia.org/wiki/Closed_wing

    Wingtip vortices form a major component of wake turbulence and are associated with induced drag, which is a significant contributor to total drag in most regimes. A closed wing avoids the need for wingtips and thus might be expected to reduce wingtip drag effects.

  7. Forward-swept wing - Wikipedia

    en.wikipedia.org/wiki/Forward-swept_wing

    With the air flowing inwards, wingtip vortices and the accompanying drag are reduced. Instead, the fuselage acts as a very large wing fence and, since wings are generally larger at the root, this raises the maximum lift coefficient allowing a smaller wing. As a result, maneuverability is improved, especially at high angles of attack.

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