Derivation of ODEs and Bifurcation Analysis of a Two-DOF Airfoil Subjected to Unsteady Incompressible Flow

An airfoil subjected to two-dimensional incompressible inviscid flow is considered. The airfoil is supported via a translational and a torsional springs. The aeroelastic integro-differential equations of motion for the airfoil are reformulated into a system of six first-order autonomous ordinary dif...

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Bibliographic Details
Main Authors: H. Alighanbari, S. M. Hashemi
Format: Article
Language:English
Published: Hindawi Limited 2009-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2009/248930

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