Design and analysis for the flutter behaviour of different selected wing plan forms computationally

The objective behind this work is to analyse different aerofoils and study their flutter behaviour and the trying to understand the influence the aerofoil parameters has on the dynamic aero-elastic behaviour of the wing that is constructed by that aerofoil. In an attempt to understand this, wings of same span and chord dimensions are constructed using different aerofoil sections which have different camber locations. One way FSI analysis was performed and the mode frequencies were extracted to observe the flutter of the wing. An attempt to understand the impact the aerofoil shape has on the wing flutter is made by selecting different aerofoil sections that has a varying camber location from the leading edge.