% Assemble global stiffness matrix K = [D11, D12, D16; D12, D22, D26; D16, D26, D66];
where $M_x$, $M_y$, and $M_{xy}$ are the bending and twisting moments, $q$ is the transverse load, $D_{ij}$ are the flexural stiffnesses, and $\kappa_x$, $\kappa_y$, and $\kappa_{xy}$ are the curvatures.
The following MATLAB code performs a bending analysis of a composite plate using FSDT:
% Assemble global stiffness matrix K = [D11, D12, D16; D12, D22, D26; D16, D26, D66];
where $M_x$, $M_y$, and $M_{xy}$ are the bending and twisting moments, $q$ is the transverse load, $D_{ij}$ are the flexural stiffnesses, and $\kappa_x$, $\kappa_y$, and $\kappa_{xy}$ are the curvatures.
The following MATLAB code performs a bending analysis of a composite plate using FSDT:
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