“…10,12,[24][25][26][27][28][29][30][31][32][33] In-plane damage mechanisms can also be captured with micromechanics models including repeating unit cell (RUC) and representative volume element (RVE) techniques, as well as other methods. 5,[34][35][36][37][38][39] Moreover, micromechanics models can be tied to the continuum scale using multiscale methods in which the RUC is homogenized to give the effective response of the continuum. [40][41][42][43][44][45] Commonly used techniques for introducing interlamina damage into a composite simulation include the virtual crack closure technique (VCCT), cohesive zone model (CZM) 10,[46][47][48] and discrete cohesive zone model (DCZM).…”