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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| Main Authors: | , , , , |
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| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
2009
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| Subjects: | |
| Online Access: | 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 http://irep.iium.edu.my/6029/ http://www.aiaa.org/agenda.cfm?lumeetingid=1811&viewcon=agenda&pageview=2&programSeeview=1&formatview=2 |
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Internet
http://irep.iium.edu.my/6029/1/Experimental_Investigation_of_Wing_Tip_Vortex.pdfhttp://irep.iium.edu.my/6029/4/Experimental_investigation_of_wing_tip_vortex.pdf
http://irep.iium.edu.my/6029/
http://www.aiaa.org/agenda.cfm?lumeetingid=1811&viewcon=agenda&pageview=2&programSeeview=1&formatview=2