Topic: Unexpected Stresses in Shell Elements
Hi,
I am modelling a steel plate which is subjected to out of plane loading. Shell elements with 6 layers are used. The strain hardening of the steel material is defined close to zero. Hence, stresses higher than yield stress are not expected.
When comparing with experimental results, the stiffness agrees well; however, for the maximum load capacity of the plate, the FE results are as high as twice of the experimental data.
Also, normal stresses and the max principal stresses are considerably higher than what they can be in accordance to the material definition.
Could you please let me know if you have any suggestions to fix the problem?
Thank you.