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...
Main Author: | Liong, Sun Loon. |
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Other Authors: | Jorg Uwe Schluter |
Format: | Thesis |
Language: | English |
Published: |
2013
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Subjects: | |
Online Access: | http://hdl.handle.net/10356/53212 |
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