In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements
One of the last remaining challenges preventing the laminarization of sweptwings is the control of unstable crossflow vortices. In low-disturbance environments the transition from laminar to turbulent flow on the swept-wing initially takes the path of receptivity, where surface roughness or disturba...
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| Format: | Others |
| Language: | en_US |
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2010
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| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728 http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728 |