Dear.
I have an issue with my simulation on ABAQUS. I simulate a crack in a composite laminate [0/45/0] using cohesive surfaces. The crack is therefore explicitely modeled using a traction-separation law and a Benzeggagh-Kenane progressif damage criterion.
My issue appears when ABAQUS calculates the quadratic stress criterion. Indeed, when I calculate manually the criterion using CPRESS and CSHEAR or S12 and S22, I find the right value. However at the nodes before last in the thickness (cf figure), the criterion is over-evaluated by 7%. It leads to the beginning of damage at these nodes instead of the center of the ply.
My questions are :
Why the value is not right only at theses nodes ?
How the quadratic criterion is calculated (which variables are considered) ?
How to fix this problem ?
Thanks.
PS : The figure shows only the 45° ply and the fracture surface as soon as quad criterion meets 1.
PS2 : Periodic conditions are applied around the cell, Surface-to-surface discretization, thinner meshes show the same issue at the before last nodes.