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