“…Bacciocchi 233 analysed buckling loads in a 3-phase composite of CNT, polymer, and fibre addressing the influence of non-uniform distribution of fibres along the thickness on the critical buckling load. Power law function was used to define the nonuniform features, which were shown to have a significant D-0.8-15nm,L-10nm-30 µm FEM 0.9-250GPa 49,56,76,161,165,173,176,180,188,190,194,200,204,205,211,215,218,219,222,223,255,258,259,262 D-0.9-30nm,L-12.19nm-30µm, RVE scale-5-110 µm Multiscale 1-225GPa 120,161,165,188,190,200,205,207,212,215,218,219,222,223,257 impact on the buckling response of laminated flat panels. Tsai et al 234 analysed the effect of CNT buckling on CNT reinforced copper matrix composite by characterizing the composite using high-resolution transmission electron microscopy and further analysis based on MD simulations.…”