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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| தலைமை எழà¯à®¤à¯à®¤à®¾à®³à®°à¯à®•à®³à¯: | , , , , |
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| வடிவமà¯: | Conference or Workshop Item |
| மொழி: | English English |
| வெளியீடபà¯à®ªà®Ÿà¯à®Ÿà®¤à¯: |
2009
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| பகà¯à®¤à®¿à®•à®³à¯: | |
| நிகழà¯à®¨à®¿à®²à¯ˆ அணà¯à®•à®²à¯: | http://irep.iium.edu.my/6029/ 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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