Efficient wing tip devices and methods for incorporating...

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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C244S091000

Reexamination Certificate

active

06886778

ABSTRACT:
Efficient wing tip devices for use with aircraft wings. In one embodiment, an aircraft wing/winglet combination includes a wing having a wing root portion and a wing tip portion spaced apart from the wing root portion. The wing tip portion can have a wash-out twist relative to the wing root portion. The aircraft wing/winglet combination can further include a winglet extending from the wing tip portion of the wing. The winglet can be swept at least generally forward relative to the wing to favorably change the lift distribution on the wing and in turn reduce the induced drag on the wing.

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www.boeing.com/commercial/aeromagazine/aero_17/wingtip_devices.html.*
Whitcomb, Richard T, NASA Technical Note, NASA TN D-8260, “A Design Approach and Selected Wind-Tunnel Results at High Subsonic Speeds for Wing-Tip Mounted Winglets,” National Aeronautics and Space Administration, Washington, D.C., Jul. 1976 (33 pages).*
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