Aeroelastic Flutter of Subsonic Aircraft Wing Section with Control Surface

Aeroelastic flutter in aircraft mechanisms is unavoidable, essentially in the wing and control surface. In this work a three degree-of-freedom aeroelastic wing section with trailing edge flap is modeled numerically and theoretically. FLUENT code based on the steady finite volume is used for the pred...

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Bibliographic Details
Published in:	Journal of Engineering
Main Authors:	Hatem Rahim Wasmi, Ass. Prof. Dr., Ali Abdul Mohsin Hasan, Ass. Prof. Dr., Waleed Jasim Mhaimeed, Ass. Lect.
Format:	Article
Language:	English
Published:	University of Baghdad 2015-12-01
Subjects:	aeroelastic, wing, control surface, aerodynamic
Online Access:	http://joe.uobaghdad.edu.iq/index.php/main/article/view/292

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