An Engineering Solution for using Coarse Meshes in the Simulation of Delamination with Cohesive Zone Models

Abstract

NASA/TM-2005-213547


This paper presents a methodology to determine the parameters used in the simulation of delamination in composite materials using decohesion finite elements. A closed-form expression is developed to define the stiffness of the cohesive layer. A novel procedure that allows the use of coarser meshes of decohesion elements in large-scale computations is proposed. The procedure ensures that the energy dissipated by the fracture process is correctly computed. It is shown that coarse-meshed models defined using the approach proposed here yield the same results as the models with finer meshes normally used in the simulation of fracture processes

Document Type

Article


Published version

Language

English

Publisher

National Aeronautics and Space Administration

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