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Journal ArticleDOI

Prediction of compressive strength of carbon–epoxy laminates containing delamination by using a mixed-mode damage model

TLDR
In this paper, a numerical analysis for predicting the residual compressive strength of delaminated plates is proposed, where the delamination propagation is modelled by using a damage model based on the indirect use of fracture mechanics.
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This article is published in Composite Structures.The article was published on 2000-10-01. It has received 88 citations till now. The article focuses on the topics: Composite laminates & Compressive strength.

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Citations
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Discrete cohesive zone model for mixed-mode fracture using finite element analysis

TL;DR: In this paper, the discrete cohesive zone model (DCZM) is implemented using the finite element (FE) method to simulate fracture initiation and subsequent growth when material non-linear effects are significant.
Journal ArticleDOI

Review of methodologies for composite material modelling incorporating failure

TL;DR: The Cooperative Research Centre for Advanced Composite Structures (CRC-ACS) is leading a currently running collaborative project to develop a methodology for determining mechanical behaviour and failure in composite structures as discussed by the authors.
Journal ArticleDOI

A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens

TL;DR: A concise constitutive law for cohesive interfaces is proposed in this paper, which not only accounts for mixed-mode delamination propagation in composite materials, but also satisfactorily deal with mode ratio change during debonding process.

Mixed-Mode Decohesion Elements for Analyses of Progressive Delamination

TL;DR: In this paper, an 8-node decohesion element with mixed mode capability is proposed and demonstrated at the interface between solid finite elements to model the initiation and propagation of delamination.
References
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Journal ArticleDOI

Progressive Delamination Using Interface Elements

TL;DR: In this paper, a method for modelling progressive mixed-mode delamination in fiber composites is described, which is incorporated within the non-linear finite element method, and is based on the use of interface elements in conjunction with softening relationships between the stresses and the relative displacements.
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Interlaminar interface modelling for the prediction of delamination

TL;DR: In this article, a laminate is modelled as a stacking sequence of homogeneous layers and interlaminar interfaces, where the interface is a threedimensional medium the thickness of which is negligible compared to the in-plane dimensions.
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Delamination analysis by damage mechanics: Some applications

TL;DR: In this paper, the composite laminate is modeled at a meso scale as a stacking of homogeneous layers connected by interfaces, and both onset of delamination and its propagation on a short distance are predicted.
Journal ArticleDOI

Modeling Compression Failure after Low Velocity Impact on Laminated Composites Using Interface Elements

TL;DR: In this article, a numerical model for predicting the compression failure of laminated composites containing delamination caused by low velocity impact was developed, which is compatible with twenty-seven node isoparametric hexahedral elements and enables modeling the behavior of the damaged interface.
Journal ArticleDOI

Analysis of a Laminate with a Postbuckled Embedded Delamination, Including Contact Effects

TL;DR: In this paper, the behavior of a postbuckled embedded delamination was studied using geometrically-nonlinear 3-D finite element analysis, and the analysis showed that the postbuckling deformation can lead to matrix cracking and fiber breakage in addition to delamination growth.
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