“…So, many studies to grasp and describe the fracture behavior of piezoelectric materials under electro-mechanical loading have been done. In most studies, the research orientation carried in general is on the mode of cracking; mode I as in [19,21,38], mode II as in [12] (for a composite laminates material), mode III as in [3][4][5]17,30,36], mixed mode as in [29], or on the model; Griffith model as in [14,21,42], Dugdale-Barenblatt model as in [8,15], or in the position of the crack in the structure; infinite plane as in [19,25], semi-infinite plane as in [8] (for a non-piezoelectric material) or still on the composition of the structure; only one material as in [25], bi-material as in [22,39].…”