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Shell + Beam Elements Linear Static
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Hello all,
I am doing a linear static analysis on a wing section comprising shells and beams. The shells are PLA 1mm thick and the beams are CFRP 2mm diameter. I've drawn sketches to represent the beams and used 'idealisations' to define cross section.
We've tested this wing in the shed (yes in the shed) and it fails at around 375N force with a max downward deflection of 22.5mm. However the FE model is not tying up with the shed results.
Any help anyone can offer me in this matter will be highly appreciated.
Model zip file attached.
Regards,
Raam