Simulation of flapping wing
This research’s objective is to present the application of Reynolds Stress Model (RSM) for evaluating the performance of flapping wing aerodynamic using Fluent. It also made a detail investigation on the parameters that influence the airfoil during the oscillating movement. The investigation begins...
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| Format: | Theses and Dissertations |
| Language: | English |
| Published: |
2013
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| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/53212 |
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| Institution: | Nanyang Technological University |
| Language: | English |