Wind Tunnel Experiment Of Aeroelastic Flutter

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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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Bibliographic Details
Main Author:	Mah, Chuen Tak
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2018
Subjects:	T Technology TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.usm.my/52682/ http://eprints.usm.my/52682/1/Wind%20Tunnel%20Experiment%20Of%20Aeroelastic%20Flutter_Mah%20Chuen%20Tak_A2_2018_MJMS.pdf

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