“…Considering a homogeneous and biaxial residual stress state in the interior of the layers in a laminated composite, the residual stress ( σ res, i ) in i th layer can be analytically calculated as follows, where E i , ν i , and α i are the elastic modulus, Poisson's ratio, and thermal expansion coefficient of the i th layer, respectively. The elastic modulus of Al 2 O 3 and graphite are 375 and 10 GPa, and the Poisson's ratios are 0.26 and 0.17, respectively.…”