An angle composite laminate $(+45/-45]32$S has the following stiffness matrices and subjected to Nxx $=0\mathrm{.}1$N$/$mm$.$ The ply thickness is $0\mathrm{.}013$ mm$.$ Determine the stresses in each layer of the laminate.

$=-45$ deg: $11=40\mathrm{.}11$ GPa, $22=40\mathrm{.}11$ GPa, $12=33\mathrm{.}61$ GPa, $66=34\mathrm{.}57$ GPa, $16=-31\mathrm{.}3$GPa, $26=-31\mathrm{.}3$ GPa

$=+45$ deg: $11=40\mathrm{.}11$ GPa, $22=40\mathrm{.}11$ GPa, $12=33\mathrm{.}61$ GPa, $66=34\mathrm{.}57$ GPa, $16=31\mathrm{.}3$GPa, $26=31\mathrm{.}3$ GPa

$($Reference "FIBER REINFORCED COMPOSITES: Materials, Manufacturing, and Design $3$rd$"$ edition chapter $3$ example $3\mathrm{.}6$ & problem $3\mathrm{.}48)$