This paper deals with the interply delamination modelisation in lamina
ted composites with ceramic matrix, under impact. This physical phenom
ena is a contact lost between two plies. The developed approach is a s
liding interface method. It consists of the resolution of Riemann's pr
oblem, based on a constitutive damage law of the interface ply and tak
ing into account the coupling between different damage mechanics. The
solver is implanted in the code DYNA3D. Its mean interest is the accur
acy of the normal velocity calculation at the contact interface.