Find A$,$ B$,$ and D matrices for the $3-$ply laminate as shown in the figure below. Assume stiffness matrix Q as follows:

For layers $1$ and $3$

$E_f=230$GPa,$E_m=3\mathrm{.}5$GPa,$v_f=0\mathrm{.}2,v_m=0\mathrm{.}3$

For layer $2$

$[Q{]}_0=\left[\begin{array}{ccc}13& 2\mathrm{.}5& 0\\ 2\mathrm{.}5& 1& 0\\ 0& 0& 3\mathrm{.}5\end{array}\right]$