XFEM and CZM modeling to predict the repair damage by composite patch of aircraft structures: Debonding parameters
Mohammed Amine Bellali, B. Sérier, Mohamed Mokhtari, R.D.S.G. Campilho, F. Lebon, Hamida Fekirini
Topics & Concepts
Materials scienceCohesive zone modelAdhesiveComposite materialStructural engineeringComposite numberLap jointDeflection (physics)Shear (geology)Fracture mechanicsLayer (electronics)EngineeringPhysicsOpticsMechanical Behavior of CompositesNumerical methods in engineeringFatigue and fracture mechanics