Abstract
A new three-dimensional (3D) micromechanical model is proposed to simulate the arbitrary multidirectional carbon fiber reinforced polymer (CFRP) composite laminates. Carbon fiber is assumed as transversely isotropic and linear elastic, matrix is assumed as isotropic and elastic–plastic. Maximum strain criterion is used to describe the failure of fiber and matrix. The stresses, strains and damage are described in the fiber and matrix levels, but the debonding between the fiber and matrix and the delamination between two plies are not modeled in the present analysis. Numerical analyses of nonlinear mechanical behavior of angle-ply [±θ]2s under tension are conducted to verify the validity of the present micromechanical model. Numerical results of nonlinear mechanical behavior, negative Poisson's ratio through the thickness direction, and stress distribution on the free edge show good agreement with previous experimental and analytical results.
| Original language | English |
|---|---|
| Pages (from-to) | 507-516 |
| Number of pages | 10 |
| Journal | Composite Structures |
| Volume | 208 |
| DOIs | |
| Publication status | Published - Jan 15 2019 |
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All Science Journal Classification (ASJC) codes
- Ceramics and Composites
- Civil and Structural Engineering
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A micromechanical model for the analysis of multidirectional fiber reinforced polymer laminates. / Deng, Xi; Hu, Junfeng; Wang, Wen Xue; Matsubara, Terutake.
In: Composite Structures, Vol. 208, 15.01.2019, p. 507-516.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - A micromechanical model for the analysis of multidirectional fiber reinforced polymer laminates
AU - Deng, Xi
AU - Hu, Junfeng
AU - Wang, Wen Xue
AU - Matsubara, Terutake
PY - 2019/1/15
Y1 - 2019/1/15
N2 - A new three-dimensional (3D) micromechanical model is proposed to simulate the arbitrary multidirectional carbon fiber reinforced polymer (CFRP) composite laminates. Carbon fiber is assumed as transversely isotropic and linear elastic, matrix is assumed as isotropic and elastic–plastic. Maximum strain criterion is used to describe the failure of fiber and matrix. The stresses, strains and damage are described in the fiber and matrix levels, but the debonding between the fiber and matrix and the delamination between two plies are not modeled in the present analysis. Numerical analyses of nonlinear mechanical behavior of angle-ply [±θ]2s under tension are conducted to verify the validity of the present micromechanical model. Numerical results of nonlinear mechanical behavior, negative Poisson's ratio through the thickness direction, and stress distribution on the free edge show good agreement with previous experimental and analytical results.
AB - A new three-dimensional (3D) micromechanical model is proposed to simulate the arbitrary multidirectional carbon fiber reinforced polymer (CFRP) composite laminates. Carbon fiber is assumed as transversely isotropic and linear elastic, matrix is assumed as isotropic and elastic–plastic. Maximum strain criterion is used to describe the failure of fiber and matrix. The stresses, strains and damage are described in the fiber and matrix levels, but the debonding between the fiber and matrix and the delamination between two plies are not modeled in the present analysis. Numerical analyses of nonlinear mechanical behavior of angle-ply [±θ]2s under tension are conducted to verify the validity of the present micromechanical model. Numerical results of nonlinear mechanical behavior, negative Poisson's ratio through the thickness direction, and stress distribution on the free edge show good agreement with previous experimental and analytical results.
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UR - http://www.scopus.com/inward/citedby.url?scp=85055178853&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2018.10.019
DO - 10.1016/j.compstruct.2018.10.019
M3 - Article
AN - SCOPUS:85055178853
VL - 208
SP - 507
EP - 516
JO - Composite Structures
JF - Composite Structures
SN - 0263-8223
ER -