Wing Tip Devices and Aerodynamic Efficiency

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Wing tip devices are simply designed airfoils that improve a wing’s lift-to-drag ratio. Through this combination of increased lift and reduced drag, an aircraft can fly more efficiently with the net result being more economical fuel burn. Wing tip devices were first created in 1897, a British engineer named Frederick Lancaster created wing tip devices called wing end plates to improve the aerodynamic characteristics of the airfoils he designed (Air force Studies Board, 2007). Through the years, designers created wing tip devices in many different shapes and sizes; each design has its own advantages, with some providing the most benefit in cruise, while others optimize takeoff and climb performance. In the United States, winglets have been extensively researched and tested by the National Aeronautics and Space Administration (NASA), the United States Air force (USAF), the U.S. Navy, and many large aircraft manufacturers. Just about every large commercial passenger and cargo aircraft have some type of wing tip device, and it is expected that most future aircraft will also incorporate wing tip devices. The term wing tip device encompasses a whole family of devices that includes standard winglets, blended winglets/Sharklets, raked wing tips, Hoerner wing tips, non-planar wing tips, wing tip fences, and hybrid wing tips/Split Scimitar winglets, (see appendix A for picture descriptions). Wing Tip Devices and Aerodynamic Efficiency Since man’s first powered flight was accomplished by the Wright brothers, on 17 December 1903 at Kill Devil Hills, North Carolina, the quest from that day forward was to design aircraft that were capable of flying higher, faster, and further. Through the years, designers have created aircraft and airfoil... ... middle of paper ... ...ufacturers incorporate these simple devices on the wings of their aircraft. Wing tip devices… so simple, yet so complex, have and will continue to make positive contributions to the aerospace industry. Works Cited 1. Air force Studies Board. (2007). Assessment of Wing tip Modifications to Increase Fuel Efficiency of Air force Aircraft, National Academic Press, 18-27 2. Bargsten, C. J. (2011). Innovation in Aeronautics: Winglets Striving for Wing tip Efficiency, NASA, 12-22 3. Hoerner, S. Dr. (1952). Aerodynamic Shape of Wing tips, USAF Air Materiel Command, ii, 1-4 4. Wenz, R. (2009). http://www.ilavhalloffame.org/Newsletters/5Newsletter.pdf, edition 5 5. Curry, M. & Dunbar B. (2008). http://www.nasa.gov/centers/dryden/about/Organizations/Technology/Facts/TF-2004-15-DFRC.html 6. Dunbar, B. (2013). http://www.nasa.gov/topics/people/features/richard_whitcomb.html

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