In Ansys APDL, We are trying to validate our shell model for nonlinear buckling analysis considering the initial imperfection (as given by Ahmed et. al.) We have attached our results as attached. Though we have got similar results, but not exactly the same as works of literature. In the first model, we have considered the stress-strain graph as provided by Ahmed et al. In the second model we have considered true stress - true strain. In both cases, we have restrained (translation and rotation) our models at both ends. Only at one end, we kept UZ free as we have provided 5 mm (-ve Z direction) deflection at that end.

Kindly suggest an improvement for this model. We have taken the Shell181 element.

How to plot load shortening graph?

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