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Introduction To Continuum Damage Mechanics
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Citations
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Journal ArticleDOI
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates
TL;DR: In this paper, a high-fidelity three-dimensional composite damage model was developed and implemented as a user material subroutine in the commercial finite element package, ABAQUS/Explicit, to predict both low-velocity impact damage and CAI strength of composite laminates.
Journal ArticleDOI
Predicting the Compression-After-Impact (CAI) strength of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates
Haibao Liu,Brian Falzon,Wei Tan +2 more
TL;DR: In this article, the authors presented a model for the numerical simulation of Compression-After-Impact (CAI) of hybrid unidirectional (UD)/woven carbon-fibre reinforced composite laminates.
Journal ArticleDOI
A consistent anisotropic damage model for laminated fiber-reinforced composites using the 3D-version of the Puck failure criterion
José Reinoso,Giuseppe Catalanotti,Antonio Blázquez,Pedro M. A. Areias,Pedro P. Camanho,Federico París +5 more
TL;DR: In this paper, a consistent anisotropic damage model for laminated fiber-reinforced composites relying on the 3D-version of the Puck failure criterion is presented, which is implemented into the implicit FE commercial package ABAQUS using the user-defined capability UMAT.
Journal ArticleDOI
Mechanothermodynamic Entropy and Analysis of Damage State of Complex Systems
TL;DR: An attempt to propose a generalized theory of evolution which is based on the concept of tribo-fatigue entropy, which is determined by the processes of damageability conditioned by thermodynamic and mechanical effects causing to the change of states of any systems.
Journal ArticleDOI
Predicting the crushing behaviour of composite material using high-fidelity finite element modelling
Wei Tan,Brian Falzon,Mark Price +2 more
TL;DR: In this paper, a three-dimensional damage model is presented, which accurately represents the behaviour of composite laminates under crush loading, and both intralaminar and interlaminar failure mechanisms are taken into account.
References
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Journal ArticleDOI
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates
TL;DR: In this paper, a high-fidelity three-dimensional composite damage model was developed and implemented as a user material subroutine in the commercial finite element package, ABAQUS/Explicit, to predict both low-velocity impact damage and CAI strength of composite laminates.
Journal ArticleDOI
Predicting the Compression-After-Impact (CAI) strength of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates
Haibao Liu,Brian Falzon,Wei Tan +2 more
TL;DR: In this article, the authors presented a model for the numerical simulation of Compression-After-Impact (CAI) of hybrid unidirectional (UD)/woven carbon-fibre reinforced composite laminates.
Journal ArticleDOI
A consistent anisotropic damage model for laminated fiber-reinforced composites using the 3D-version of the Puck failure criterion
José Reinoso,Giuseppe Catalanotti,Antonio Blázquez,Pedro M. A. Areias,Pedro P. Camanho,Federico París +5 more
TL;DR: In this paper, a consistent anisotropic damage model for laminated fiber-reinforced composites relying on the 3D-version of the Puck failure criterion is presented, which is implemented into the implicit FE commercial package ABAQUS using the user-defined capability UMAT.
Journal ArticleDOI
Mechanothermodynamic Entropy and Analysis of Damage State of Complex Systems
TL;DR: An attempt to propose a generalized theory of evolution which is based on the concept of tribo-fatigue entropy, which is determined by the processes of damageability conditioned by thermodynamic and mechanical effects causing to the change of states of any systems.
Journal ArticleDOI
Predicting the crushing behaviour of composite material using high-fidelity finite element modelling
Wei Tan,Brian Falzon,Mark Price +2 more
TL;DR: In this paper, a three-dimensional damage model is presented, which accurately represents the behaviour of composite laminates under crush loading, and both intralaminar and interlaminar failure mechanisms are taken into account.