Oh, I forgot, 1D Elements can handle this problem as well ( https://www.structuralfea.com/1D_Elements/1D_Elements.html ). It uses MYSTRAN and I attached an example.
Brian
www.espcomposites.com
You can try out eDistribution as well (https://www.espcomposites.com/software/download.html). There is an input for a manual fastener flexibility.
Brian
www.espcomposites.com
Does anyone of know shell element formulations (tri and quad) that have an associated differential stiffness matrix (geometric stiffness matrix)? The MITC elements are quite popular, but we can not find the associated differential stiffness matrix. The objective is to incorporate these...
I am not sure that is a good analogy. A bearing-bypass curve is an interaction curve, but it takes multiple test data points to fit it. Also, the curve itself it a function of various factors (so it takes quite a bit of empirical data to generate a set of curves that could be used for practical...
Some potential users:
- Students who don't want to use limited codes
- Small companies (general)
- Small/large companies that want unlimited number of licenses for large runs
- (Similar to above) Small/large companies that want to use FEM in combination with in-house tools (hybrid solutions)...
You might want to have a look at www.mystran.com. MYSTRAN is similar to NASTRAN (the decks are almost equivalent), but has a modern code base (the NASTRAN source is very old and quite difficult to work with). We are doing to some great things with it. It will be incorporated into FreeCAD at some...
Are you familiar with a beam-column analysis? If not, look it up. In essence, the the magnitude of the moment in the beam-column is analogous to an increasing imperfection.
Brian
www.espcomposites.com
Linear buckling represents the theoretical maximum capability (representative of the slightest imperfection). Any imperfection that is greater than "the slightest" (i.e. a typical nonlinear analysis) will result in a lower buckling load (at least for the initial bifurcation - which is not always...
On the structural analysis side, we would consider global buckling of a column to be the "overall buckling" of the cross section. The entire column curves in this scenario (but the deformed cross section has the same shape throughout the column - at least at the macroscopic level). If we...
Have all 3 solutions converged though? There will be discrepancies when the model is not converged, but I would expect those them to decrease once the model has reached convergence.
Brian
www.espcomposites.com
You can have a look here under the INDIVIDUAL DOCUMENTS section. For the Basic Manual, Page 7 discusses the boundary conditions and some specifics about it. The Validation Cases PDF shows that this approach is accurate for in-plane loading (Nxy loading)...
Items to consider for nonlinear geometry
1. For a linear analysis, the assumption is sin(theta)=theta (small deformation assumption). However, as this assumption changes, so can the result. This will also depend if the force is a "follower force" or not (meaning the angle of the force changes...
Megastructrues,
No, that is not what I am saying. I think I confused you, so I will try to keep it simple. Simply input the load-deflection of the connection to the FEA (whether it is linear or nonlinear, depending on your goals)...that is all. The load-deflection curve may look something like...
Here is a basic overview. There are some details I left out, but this is the basic concept.
1. Start with testing a single joint connection (a single fastener and its plate members). It could be singe shear, double shear, etc. Apply a load to the plate and recover the total deflection. Next, we...
