Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design
A parametric study of low altitude small Unmanned Autonomous Vehicle (UAV) conceptual design was performed. The purpose was to estimate constraint diagram propulsive efficiency of propeller-Brushless Direct Current (BLDC) motor propulsion system at two different flight conditions with the considerat...
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| Format: | Thesis |
| Language: | English |
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2012
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| Online Access: | http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf |