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dc.contributor.authorSeliquini, Sky
dc.contributor.authorAzelis, Augustus
dc.contributor.authorAl-Sulaiti, Mohammed
dc.contributor.authorKasyanju, Ambonisye
dc.contributor.authorLopez, Vanessa
dc.contributor.authorAl Metwali, Mohammed
dc.contributor.authorVogel, Noah
dc.contributor.authorFry, John
dc.date2015-04
dc.date.accessioned2015-05-15T19:09:38Z
dc.date.available2015-05-15T19:09:38Z
dc.identifier.citationAzelis, A., Al Metwali, M., Al-Sulaiti, M., Fry, J., Kasyanju, A., Lopez, V., Seliquini, S., & Vogel, N. (2015, April). Wing tip vortex reduction. Poster presented at the Northrop Grumman Engineering & Science Student Design Showcase, Florida Institute of Technology, Melbourne, FL.en_US
dc.identifier.urihttp://hdl.handle.net/11141/660
dc.description.abstractWinglets are used vastly in commercial jets. The main purpose of a winglet is to minimize the vortex effect forming at the tip of the wing in result to the transition between higher pressure and lower pressure. The main purpose of this project is to research, design, and test a new wing tip device that will improve the wing's aerodynamic efficiency.en_US
dc.language.isoen_USen_US
dc.titleWing Tip Vortex Reductionen_US
dc.typeposteren_US


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