Experimental investigation of tip vortex control using a half delta shaped tip strake
The effectiveness of using a half delta wing tip strake for static wing tip vortex control and performance enhancement was investigated. The flowfield over the wingtip and in the near-field was studied over a low aspect ratio NACA 0012 wing fitted with a half delta wing with a leading-edge sweep of...
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| Format: | Others |
| Language: | en |
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McGill University
2012
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| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=107592 |