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Hello to all,
I m mahendra and i want few suggesions for my final year project Regarding Non-Linear buckling of composite Wind Turbine. I have done Linear Buckling and got a BLF=1.3 which is fine as per GL Guidlines. I m using Ansys12 Edu ver. and Shell 281 Element type with section properties. For load application i m using pilot node at 9 airfoils on the full blade.
Then i have applies Mx and My on that load application points.
In Non-Linear Analysis i m not getting the convergence as i m applying load on one node or at all the 9 points.
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