Micro air vehicles : flapping wing propulsion
This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. The wing used was a straight wing of airfoil NACA 0012. Two different methods were us...
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| Format: | Final Year Project |
| Language: | English |
| Published: |
2011
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| Online Access: | http://hdl.handle.net/10356/45669 |
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| Institution: | Nanyang Technological University |
| Language: | English |