rh 142,
I think you have very crude understanding of non-linear buckling analysis. But its ok. I will try my best to explain it to you.
One good thing about Ansys is its help documentation, where you can get very good information. I would strong recommend you to read through 'how to perform non-linear buckling analysis'. Dont mix up non-linear static analysis with non-linear buckling analysis. As i've mentioned to you in my earlier reply, non-linear buckling analysis takes into consideration structural imperfection magnitude (upgeom).
Structural imperfection magnitude can be obtained in many reference standards or rules or handbook. and this should correspond to the 'imperfect' shape or the eigenmodes you would obtain from the eigen buckling analysis. And as you can see, you have to perform an eigenbuckling analysis to determine the eigenmodes, else its tricky to determine the structural mode responses.
Simplified, you MUST to do ALL the followings: (a) perform linear static analysis with pstres,on (b) perform eigenbuckling analysis (c) determine which mode shape you wanted to use in the non-linear analysis, typically the 1st mode will be crucial (d) determine the imperfection magnitude from any reference (i always refer to DNV OS C 401, as fabrication tolerance) (e) impose non-linear material model, geometry, apply imperfection on the eigen mode you choose and solve using progressive load increments (f) your ultimate buckling load corresponds to your last converged substep.
Hope this helps!
Yoman228,
The FE solver source codes are more or less the same. So the results will be almost identical. The difference is on the pre-post facilities you have in a FE program.
Explicit codes like ls dyna gives better dynamic result if you are trying to investigate buckling load problem beyond the snap thru point. Good luck to you.
Yugabalan K