Wind tunnel testing of a ducted-fan unmanned aerial vehicle
This report has investigated the effects of the aerodynamic parameters of lift, drag, moments and thrust and determined their relationships with different wingspans at different pitch and wing incidence angles on a ducted-fan Micro Air Vehicle (MAV) at a speed of approximately 15m/s. The experiments...
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2011
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/45901 |
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| 機構: | Nanyang Technological University |
| 語言: | English |