“…The laminate used for the experimental study was a carbon fibre reinforced plastic (CFRP) [−30/60] laminate consisting of two plies, each of 0.25 mm thickness. A square laminate of size 150 mm was manufactured using the standard lay‐up procedure using an intermediate carbon fibre‐thermoset prepreg sheet from Hexcel (T800/M21) [10]. The material properties are longitudinal elastic modulus, E 11 = 175 GPa, transverse elastic modulus, E 22 = 8.9 GPa, shear modulus, G = 4.5 GPa, Poisson’s ratio, ν 12 = 0.35, thermal expansion coefficients, α 1 = −0.09 × 10 −6 per °C and α 2 = 30 × 10 −6 per °C.…”