“…In glass-aramid composites, e II is between 40% and 50% of the peak strain for G-M and G-P series and about 90% for G-ML and G-L, indicating the predominance of the crack development stage. Conversely, e II is 29% of the peak strain for S4-C, 2% and 5% for S4-ML and S12-C and, finally, not even detectable for S12-ML, in which the contribution of the reinforcement fabric is largely prevalent with respect to that of the matrix, as already found in [30] for TRC.…”