Experimental investigation of wing tip vortex

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Experimental investigation of wing tip vortex

Particle image velocimetery was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a SWIM model was used as a vortex generator in two different configurations, (i) plain wing and (ii) flapped wing with trailing edge flap extended at 2...

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Bibliographic Details
Main Authors:	Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung, Jung, Hyejin
Format:	Proceeding Paper
Language:	English English
Published:	2009
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/6029/ http://irep.iium.edu.my/6029/1/Experimental_Investigation_of_Wing_Tip_Vortex.pdf http://irep.iium.edu.my/6029/4/Experimental_investigation_of_wing_tip_vortex.pdf

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