Honeycomb laminate analysis
Hi,
Asking for advice on how to analyse an aluminum honeycomb panel. The layup is 0.5mm aluminium sheet, 20mm aluminium honeycomb structure and a final aluminium sheet. These make up a plate of 400x400mm. How should I set this up for best analysis in Creo Simulate? I'm thinking the Shell feature would be the right way and make a laminate material. Should one then have the honeycomb as a material type, to be defined, or should one define a Laminate Stiffness and use that shell as the middle layer?
Alternatively define the honeycomb material as an Orthotropic material and apply that to a geometric part representing the honeycomb core?
Furthermore, any hints or suggestions to such properties, as I have not yet dealt with honeycomb structural properties?
Thanks



