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Thank you very much Simon.
Your answer leads me to another question. I did not know which theory was being used, so I tried to change the G1z and G2z (transverse shear modulus). The results of the analysis when those modulus were very low changed significantly. In the classical theory, isn't that not supposed to happen as the transverse deformations are not taken into account?

Altair Community Member
Updated by Simon Križnik
OptiStruct uses classical lamination theory to calculate effective stiffness and mass density of the composite shell. This is done automatically within the code using the properties of individual plies.
The composite inter-laminar stress is calculated based on the first-order shear deformation laminated plate theory.
Hi,
according to Optistruct help (page 22):
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