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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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2013
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/53212 |
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| 機構: | Nanyang Technological University |
| 語言: | English |