Mohammed Amine Bellali
- XFEM and CZM modeling to predict the repair damage by composite patch of aircraft structures: Debonding parameters. In: Composite Structures, v. 266 (Juni 2021). (2021):
- Using CZM and XFEM to predict the damage to aluminum notched plates reinforced with a composite patch. In: Journal of Mechanics of Materials and Structures, v. 15, n. 2 (April 2020). (2020):