Design of a ducted fan for an unmanned aerial vehicle
The development of ducted fan propulsion systems in the model and full scale light aircraft has shown steady increase in the recent years due to its advantages under static and low speed thrust. This work is focused on the conceptual design, fabrication and testing of the ducted fan blades in an...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2009
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| Online Access: | http://hdl.handle.net/10356/16233 |