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NASA NTRS · 20090005991

A Novel Multiscale Physics Based Progressive Failure Methodology for Laminated Composite Structures

Abstract

A variable fidelity, multiscale, physics based finite element procedure for predicting progressive damage and failure of laminated continuous fiber reinforced composites is introduced. At every integration point in a finite element model, progressive damage is accounted for at the lamina-level using thermodynamically based Schapery Theory. Separate failure criteria are applied at either the global-scale or the microscale in two different FEM models. A micromechanics model, the Generalized Method of Cells, is used to evaluate failure criteria at the micro-level. The stress-strain behavior and observed failure mechanisms are compared with experimental results for both models.

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BibTeXRIS

Pineda, Evan J., Waas, Anthony M., Bednarcyk, Brett A., Collier, Craig S., Yarrington, Phillip W.. 2008-12-01. A Novel Multiscale Physics Based Progressive Failure Methodology for Laminated Composite Structures. https://ntrs.nasa.gov/citations/20090005991

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