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Applied Composite Materials
Erschienen in: Applied Composite Materials 4/2014

01.08.2014

Identification of Fracture Toughness for Discrete Damage Mechanics Analysis of Glass-Epoxy Laminates

verfasst von: E. J. Barbero, F. A. Cosso, X. Martinez

Erschienen in: Applied Composite Materials | Ausgabe 4/2014

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Abstract

A methodology for determination of the intralaminar fracture toughness is presented, based on fitting discrete damage mechanics (DDM) model predictions to available experimental data. DDM is constitutive model that, when incorporated into commercial finite element software via user material subroutines, is able to predict intralaminar transverse and shear damage initiation and evolution in terms of the fracture toughness of the composite. The applicability of the DDM model is studied by comparison to available experimental data for Glass-Epoxy laminates. Sensitivity of the DDM model to h- and p-refinement is studied. Also, the effect of in-situ correction of strength is highlighted.
Vorheriger Artikel Influential Factors of Z-pin Bridging Force
Nächster Artikel The Friction Force Determination of Large-Sized Composite Rods in Pultrusion

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Fußnoten
1
Abaqus and Simulia are trademarks or registered trademarks of Dassault Systèmes or its subsidiaries in the United States and/or other countries.
 
2
Ansys®; is a registered trademark of ANSYS Inc.
 
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Metadaten
Titel
Identification of Fracture Toughness for Discrete Damage Mechanics Analysis of Glass-Epoxy Laminates
verfasst von
E. J. Barbero
F. A. Cosso
X. Martinez
Publikationsdatum
01.08.2014
Verlag
Springer Netherlands
Erschienen in
Applied Composite Materials / Ausgabe 4/2014
Print ISSN: 0929-189X
Elektronische ISSN: 1573-4897
DOI
https://doi.org/10.1007/s10443-013-9359-y

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