| DOI | Resolve DOI: https://doi.org/10.1016/j.proeng.2011.04.013 |
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| Author | Search for: Ellyin, F.; Search for: Zhang, Y.1; Search for: Xia, Z. |
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| Affiliation | - National Research Council of Canada. Aerospace
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| Format | Text, Article |
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| Conference | 11th International Conference on the Mechanical Behavior of Materials, ICM11, 5 June 2011 through 9 June 2011, Como |
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| Subject | 3D models; Angle ply laminate; Damage; Damage initiation; Finite Element; Mesomechanics; Mesoscale; Nonlinear visco-elastic; Periodic boundary conditions; Repeated unit cells; Smeared crack; Stress-strain response; Boundary conditions; Composite materials; Constitutive models; Mechanical engineering; Paper laminates; Three dimensional; Viscoelasticity; Finite element method |
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| Abstract | In this paper, a meso-scale repeated unit cell model for a general [±θ]n angle-ply laminate is developed and the implementation of periodic boundary conditions in a finite element analysis for this 3-D model is presented. A nonlinear viscoelastic constitutive model and a post-damage constitutive model based on the concept of a smeared crack are also incorporated in the finite element analysis. The stress-strain response and the damage initiation and propagation for different values of θ are predicted. © 2011 Published by Elsevier Ltd. |
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| Publication date | 2011 |
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| In | |
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| Language | English |
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| Peer reviewed | Yes |
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| NPARC number | 21271153 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 47031d57-69ee-4754-9334-1b9cc29e4292 |
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| Record created | 2014-03-24 |
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| Record modified | 2020-04-21 |
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