“…Based on the individual behaviour of each single layer, the non-linear response of such multi-layered composite is simulated through a homogenisation scheme. Although the non-linear extension of the classical laminate theory is commonly used for this purpose (Berthelot, 1999;Perreux and Lazuardi, 2001), it is convenient to consider instead a scheme based on periodic homogenization (Chatzigeorgiou et al, 2015) It is proposed to identify, at first, the parameters related to the microcracks density evolution (21) and the anelasticity (26) in the transverse tension, namely, R 22 , S, β, γ ∞ c and a 22 . These parameters can be assessed through an incremental load/unload tensile test performed on a [90 o ] 16 laminated specimen (Figure 8a).…”