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Von Mises stress composite panel

- October 31, 2025 at 12:18 pm
  
  s281303
  Subscriber
  
  I am analysing a composite plate subjected to pressure on the upper face and constrained at the short sides.
  I would like to obtain the von Mises sigma results for the isotropic material at the centre of the layout, but I am unable to do so. I have set the correct number of integration point parameters and I obtain the stress for the other layers, but not for that one.
- November 1, 2025 at 8:01 pm
  s281303
  Subscriber
  PS: in the model i'm using PART_COMPOSITE and two different materials: 001_ELASTIC and 054_ENHANCED_COMPOSITE_DAMAGE.
  Layers have differents thickness, 0.2 mm composite skin and 5 mm the mat_elastic

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