Numerical simulation of the crushing process of a corrugated composite plate

The significant potential of composite materials as highly effective energy absorbers has contributed to their increasing usage in the aerospace, automotive, and railway industries. Traditionally, the development of crashworthiness composites design relies upon laborious and costly experimental test...

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Vydané v:Composites. Part A, Applied science and manufacturing Ročník 42; číslo 9; s. 1119 - 1126
Hlavní autori: Sokolinsky, Vladimir S., Indermuehle, Kyle C., Hurtado, Juan A.
Médium: Journal Article
Jazyk:English
Vydavateľské údaje: Kidlington Elsevier Ltd 01.09.2011
Elsevier
Predmet:
A. Fabrics/textiles
absorption
Aircraft components
Applied sciences
C. Computational modelling
C. Damage mechanics
C. Finite element analysis (FEA)
composite materials
Computer simulation
Corrugated plates
Crushing
Crushing response
delamination
energy
Exact sciences and technology
Fabrics
Finite element method
Forms of application and semi-finished materials
industry
Laminates
Mathematical analysis
Mathematical models
Polymer industry, paints, wood
product development
Technology of polymers
testing
C. Computational modelling
Crushing response
C. Finite element analysis (FEA)
C. Damage mechanics
A. Fabrics/textiles
Fracture mechanics
Laminate
Epoxy resin
Theoretical study
Mechanical properties
Compressive strength
Mineral fiber
Modeling
Composite material
Finite element method
Corrugated plate
Numerical simulation
Woven material
Energy absorption
Delamination
Crush
Fracture mode
Carbon fiber
ISSN:1359-835X, 1878-5840
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Popis
Shrnutí:The significant potential of composite materials as highly effective energy absorbers has contributed to their increasing usage in the aerospace, automotive, and railway industries. Traditionally, the development of crashworthiness composites design relies upon laborious and costly experimental testing. Therefore, the ability to simulate accurately the crushing response of composites and their energy absorption mechanisms can significantly reduce the product development cycle and cost. The present work presents a physics-based finite element model of a corrugated carbon–epoxy fabric composite plate subject to quasi-static crushing. The model accounts for both intralaminar (in-plane) and interlaminar (delamination) failure mechanisms. The in-plane response of the fabric plies is modeled using a proposed constitutive model that has been implemented in the commercial finite element code Abaqus/Explicit; and the delamination response of the composite plate is simulated using the cohesive surface capability in Abaqus. The results of the Abaqus/Explicit simulations show very good quantitative and qualitative agreement with the experimental data, thus demonstrating that the proposed methodology and tools can be used for realistic crush simulations of composite structures.
Bibliografia:http://dx.doi.org/10.1016/j.compositesa.2011.04.017
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ISSN:1359-835X
1878-5840
DOI:10.1016/j.compositesa.2011.04.017