I am doing modelling of Fiber metal laminates by using a solid plate element The model having large cutout is showing more buckling load than smaller?

I have modelled the plate using 11 ply layer in composite layup manager in ABAQUS including the Aluminum and glass fiber layers. Al/0/90/0/90/Al/90/0/90/0/Al is the layup. I am using Aluminum with...

23 July 2020 6,550 2 View