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Numerical Simulation of Glass-Fiber-Reinforced Aluminum Laminates with Diverse Impact Damage
This paper presents a finite element model used to simulate the impact response of a fiber metal laminate. The load-time history, maximum deflection, and damage progression caused by impact loading were examined using an explicit finite element model. Two- and three-dimensional failure criteria in t...
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Published in: | AIAA journal 2010-03, Vol.48 (3), p.676-687 |
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Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | This paper presents a finite element model used to simulate the impact response of a fiber metal laminate. The load-time history, maximum deflection, and damage progression caused by impact loading were examined using an explicit finite element model. Two- and three-dimensional failure criteria in the commercial finite element code ABAQUS are used to model stiffness degradation in the glass-fiber-reinforced composite layers of the laminates. The finite element results showed good agreement with experimental measurements. [PUBLICATION ABSTRACT] |
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ISSN: | 0001-1452 1533-385X |
DOI: | 10.2514/1.45551 |