Hi everyone,

I am designing a composite material in Abaqus and testing different lay-ups to reduce peel force where possible. I have modelled my parts using solids, so I cannot use laminar layers.

In order to assign the material properties, do any of you have orthotropic or anisotropic values for standard carbon fibre and glass materials? (In the form D1111, D1112 etc.)

Any help would be appreciated!