An experimental investigation of the geometric characteristics of flapping-wing propulsion for a micro-air vehicle
Approved for public release, distribution is unlimited === The geometric characteristics of flapping-wing propulsion are studied experimentally through the use of a force balance and a Micro Air Vehicle (MAV) system. The system used is built to duplicate the propulsion system currently on the flying...
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| Format: | Others |
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Monterey, California. Naval Postgraduate School
June
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| Online Access: | http://hdl.handle.net/10945/936 |