There can be also surprisingly large inaccuracy when fully integrated beam elements are used with plasticity and when the mesh of beam elements is not significantly refined:
this what i found in 2016 for preliminary review. i did not refined the model and investigate further, it seems beam element in CalculiX mostly dependent on how user modeling.
please, don’t judge quickly about the reliability and accuracy or even a bugs cause your model may inappropriate to set (i.e mesh, element type & additional restraint) or limitation itself.
i seen many user direct compared to 1D/2D classical element were is not comparable due to expanding element in CalculiX and generates knot or MPC existence. user need different model approach to refined and set up properly.
or an example from FreeCAD forums, it’s clear for me when someone notify about shear-locking and hourglassing.
some notify: beam element in CalculiX is unique, advances and challenging. no matter how it, keep imaging as solid element and MPC existences not as simple as classical element.
To compare with the theoretical result I guess the same strategy. Idealization of a pure pinned support and rotation around the x axis constrained.
I have tested on a 6meters UPN160 with distributed Self weight and agreement with the theory is reached in this case with just 4xB32R. Not bad at all.
PropSection, v1.0.4, is a free software that provides the shear center of any custom section.
I guess we just need to add an extra ofsset to locate properly the custom beam to avoid the twist. I will test later and post the result with and without correction. Let’s see if it works .
It is an excellent option, I’ve been using SectionProperties for at least 2 years and it has grown a lot since then. It offers many possibilities. Recommended.
Too bad it doesn’t have even a simple GUI. Is rotating and merging built-in sections the only way to analyze non-standard shapes ? It would be great if there was any open-source software allowing users to import a drawing of the cross-section from CAD software like FreeCAD.
I used it in the past for the D-box structure of aircraft wings, the skin (leading edge structure) was imported from a *.dat file and merged onto an I-shaped member (stringers+spars). Today probably it is easier than before, but it was a relatively difficult task to do the first time. But the code was automated and parametrized so later changes were easier.
classical beam element ignoring shear center position and twist effect. however CalculiX does it properly, so only center of gravity is required to place the section plane of beam element.
finding center of gravity in sections does not necessary to use any external software, it can be simple steps to be done.
I have positioned two UPN160 one with respect to the center of gravity and the second with respect to the Shear Center.
I have not been able to completely avoid rotation without a minimum constrain (rotational spring).
That’s a good point for this technique as it seems able to model bending/twist. ¿Is that possible Xyont or am i reading incorrecftly the displacements?
i did not see into detail since no loading input available, but it seems the loads come from self weight (gravity) or point load and simple supported.
if that’s true, then second figures as predicted to shown rotated movement due to eccentricity of the support. it will raised to unstable structure for no rotation restraint applied.
shear center and twist only apply with concentrated point loads or line loads along member at some eccentricity in position. so it’s related to loads not the beam element position itself.
it seems eccentricity and twist only considered by beam element in CalculiX when user defined the member distributed load transferred to webs. this assumption given correct assumption since any transversal load must resisted by stiff part.
above true assumption are ignored by many classical beam element. this what i mean before, another condition is required to test and validate.