Eigenvalue buckling analysis with ABAQUS using shell elements
Eigenvalue buckling analysis with ABAQUS using shell elements
(OP)
Hello,
I am trying to obtain the buckling stress of a thin plate in ABAQUS modelled using shell elements. I loaded the plate with an edge load (force/length) and I obtain the eigenvalues. Do the resulting eigenvalues represent percentages of the buckling stress OR the buckling shell edge load?
Any insight would be much appreciated.
Thanks
I am trying to obtain the buckling stress of a thin plate in ABAQUS modelled using shell elements. I loaded the plate with an edge load (force/length) and I obtain the eigenvalues. Do the resulting eigenvalues represent percentages of the buckling stress OR the buckling shell edge load?
Any insight would be much appreciated.
Thanks




