Wind Tunnel Experiment Of Aeroelastic Flutter
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pitching oscillation of the wing is being observed to determine the dynamic instability point. The elastic axis will be manipulated in the experiment where the position of the elastic axis was varied at...
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| Format: | Monograph |
| Language: | English |
| Published: |
Universiti Sains Malaysia
2018
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| Online Access: | http://eprints.usm.my/52682/1/Wind%20Tunnel%20Experiment%20Of%20Aeroelastic%20Flutter_Mah%20Chuen%20Tak_A2_2018_MJMS.pdf http://eprints.usm.my/52682/ |
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