How to simulate boundary conditions and apply uniformly distributed load to shell element when I do nonlinear analysis of I-BEAM
Hi, everyone:
I am using ABAQUS to do my final dissertation:nonlinear analysis of steel members.
When I simulated the beam with shell element, first I define reference points at both end of the beam and assign 'RIGID BODY/PIN OR TIE' to nodes at the edge,after that I applied bending moments and boundary conditions to both reference points. But after I finished the buckling analysis, the result is not reasonable,the eigen value is about two times the the value I expected.