An experimental study of a turbulent wing-body junction and wake flow
</p> <p>Extensive hot-wire measurements were conducted in an incompressible turbulent flow around a wing-body junction. The measurements were performed adjacent to the body and up to 11.56 chord lengths downstream of the body. The junction wake flow entered an adverse pressure gradient r...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/44377 http://scholar.lib.vt.edu/theses/available/etd-08222009-040300/ |