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Title: A peridynamic failure analysis of fiber-reinforced composite laminates using finite element discontinuous Galerkin approximations

Abstract

Here, this paper presents a discontinuous Galerkin weak form for bond-based peridynamic models to predict the damage of fiber-reinforced composite laminates. To represent the anisotropy of a laminate in a peridynamic model, a lamina is simplified as a transversely isotropic medium under a plane stress condition. The laminated structure is modeled by stacking the surface mesh layers along the thickness direction according to the laminate sequence. To avoid a mesh dependence on either the fiber orientation or the discretization, the spherical harmonic expansion theory is employed to construct a function for the micro-elastic modulus in terms of the bond-fiber angle. The laminate material is decomposed into an isotropic matrix material part and a transversely isotropic material part. The bond stiffness can be evaluated using the engineering material constants, based on the equivalence between the elastic energy density in the peridynamic theory and the elastic energy density in the classic continuum mechanics theory. Benchmark tests are conducted to verify the proposed model. Numerical results illustrate that the convergence of simulations with different horizon sizes and meshes can be achieved. In terms of damage analysis, the proposed model can capture the dynamic process of the complex coupling of the inner-layer and delaminationmore » damage modes.« less

Authors:
 [1];  [1]; ORCiD logo [2];  [3];  [4]
  1. Livermore Software Technology Corporation, Livermore, CA (United States)
  2. Oak Ridge National Lab. (ORNL), Oak Ridge, TN (United States). Computer Science and Mathematics Division
  3. Ford Motor Company, Ford Research and Innovation Center, Dearborn, MI (United States)
  4. Univ. of California, Berkeley, CA (United States). Department of Civil and Environmental Engineering
Publication Date:
Research Org.:
Oak Ridge National Laboratory (ORNL), Oak Ridge, TN (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1479710
Grant/Contract Number:  
AC05-00OR22725
Resource Type:
Accepted Manuscript
Journal Name:
International Journal of Fracture
Additional Journal Information:
Journal Volume: 214; Journal Issue: 1; Journal ID: ISSN 0376-9429
Publisher:
Springer
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING; Peridynamic theory; Finite element method; Failure analysis; Discontinuous Galerkin method; Fiber-reinforced composites

Citation Formats

Ren, Bo, Wu, C. T., Seleson, Pablo D., Zeng, Danielle, and Lyu, Dandan. A peridynamic failure analysis of fiber-reinforced composite laminates using finite element discontinuous Galerkin approximations. United States: N. p., 2018. Web. doi:10.1007/s10704-018-0317-4.
Ren, Bo, Wu, C. T., Seleson, Pablo D., Zeng, Danielle, & Lyu, Dandan. A peridynamic failure analysis of fiber-reinforced composite laminates using finite element discontinuous Galerkin approximations. United States. https://doi.org/10.1007/s10704-018-0317-4
Ren, Bo, Wu, C. T., Seleson, Pablo D., Zeng, Danielle, and Lyu, Dandan. Thu . "A peridynamic failure analysis of fiber-reinforced composite laminates using finite element discontinuous Galerkin approximations". United States. https://doi.org/10.1007/s10704-018-0317-4. https://www.osti.gov/servlets/purl/1479710.
@article{osti_1479710,
title = {A peridynamic failure analysis of fiber-reinforced composite laminates using finite element discontinuous Galerkin approximations},
author = {Ren, Bo and Wu, C. T. and Seleson, Pablo D. and Zeng, Danielle and Lyu, Dandan},
abstractNote = {Here, this paper presents a discontinuous Galerkin weak form for bond-based peridynamic models to predict the damage of fiber-reinforced composite laminates. To represent the anisotropy of a laminate in a peridynamic model, a lamina is simplified as a transversely isotropic medium under a plane stress condition. The laminated structure is modeled by stacking the surface mesh layers along the thickness direction according to the laminate sequence. To avoid a mesh dependence on either the fiber orientation or the discretization, the spherical harmonic expansion theory is employed to construct a function for the micro-elastic modulus in terms of the bond-fiber angle. The laminate material is decomposed into an isotropic matrix material part and a transversely isotropic material part. The bond stiffness can be evaluated using the engineering material constants, based on the equivalence between the elastic energy density in the peridynamic theory and the elastic energy density in the classic continuum mechanics theory. Benchmark tests are conducted to verify the proposed model. Numerical results illustrate that the convergence of simulations with different horizon sizes and meshes can be achieved. In terms of damage analysis, the proposed model can capture the dynamic process of the complex coupling of the inner-layer and delamination damage modes.},
doi = {10.1007/s10704-018-0317-4},
journal = {International Journal of Fracture},
number = 1,
volume = 214,
place = {United States},
year = {Thu Oct 04 00:00:00 EDT 2018},
month = {Thu Oct 04 00:00:00 EDT 2018}
}

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Cited by: 14 works
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Figures / Tables:

Fig. 1 Fig. 1: The fiber orientation in a lamina.

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