Constitutive Relationship in a Composite Lamina
The constitutive relationship in a composite lamina is specially orthotropic in
nature and is given by the following equation:
Where,
Q11 = E1 /(1- ? 12 ? 21 ),
Q12 = ? 12 E2 /(1- ? 12 ? 21 ),
Q22 = E2 /(1- ?12 ?21 ),
Q66 = G12
E1 for a composite is obtained by using rule of mix and fibre & matrix volume
fraction as follows:
E1 = E1f Vf + E1m Vm
However in the transverse direction, estimating the modulus of elasticity is
more difficult. A simple model based on springs in series (matrix and
reinforcing elements both modelled as springs connected in series). Thus,
1/E2 = Vf /E2f + Vm /E2m
The same principle is used to estimate the shear modulus of the lamina.
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