Hi,
I am working on delaminated composite materials. For analysis I was trying to use ansys or lusas but not able to model proerly . I need help to model the following problem.
32 layer laminated plate length 300mm
width 250mm
delaminated between 8th and 9th layer from the top and location is 100mm from left eadge and delaminated width 50mm. Simply supported in all four eadges.
lay ups are symmetric and assume any material property (E11, E12, E22, nu, G12 etc)
Problem : buckling load and mode shape to be determined.
I would like to learn the modelling . Is there any modelling tutorials or examples?
thank you.
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