Wind Tunnel and Flight Testing of Active Flow Control on a UAV
Active flow control has been extensively explored in wind tunnel studies but successful in-flight implementation of an active flow control technology still remains a challenge. This thesis presents implementation of active flow control technology onboard a 33% scale Extra 330S ARF aircraft, wind tun...
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| Format: | Others |
| Language: | en_US |
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2011
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| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8003 |