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II.1.11.2 In-plane and out-of-plane components

As was done for the motion equations, a decoupling of in-plane laminate thermal conductivity and out-of-plane conductivity is assumed. Therefore, the thermal flux is separated into an in-plane flux:

{q12} = ( q1 q2 ) ,

and the out-of-plane component q3.

Correspondingly, the tensor of thermal conductivity coefficients is separated into an in-plane conductivity tensor:

[λT ] 12 = ( λ11T λ 12T λ12T λ 22T ) ,

and the out-of-plane conductivity λ33T . The “shear” components λ31T and λ23T are neglected in the homogenization theory. (This means that out-of-plane and in-plane conductivities are decoupled.)