Treffer: Stiffness and fracture analysis of laminated composites with off-axis ply matrix cracking

Title:
Stiffness and fracture analysis of laminated composites with off-axis ply matrix cracking
Source:
Selected papers from the Joint 8th International Conference on Deformation and Fracture of Composites (DFC-8) and Experimental Techniques and Design in Composite Materials (ETDCM-7), Sheffield, 3-6 April 2005Composites. Part A, Applied science and manufacturing. 38(4):1262-1269
Publisher Information:
Oxford: Elsevier, 2007.
Publication Year:
2007
Physical Description:
print, 25 ref
Original Material:
INIST-CNRS
Subject Terms:
Chemical industry parachemical industry, Industrie chimique et parachimique, Mechanics acoustics, Mécanique et acoustique, Metallurgy, welding, Métallurgie, soudage, Polymers, paint and wood industries, Polymères, industries des peintures et bois, Sciences exactes et technologie, Exact sciences and technology, Physique, Physics, Domaines classiques de la physique (y compris les applications), Fundamental areas of phenomenology (including applications), Mécanique des solides, Solid mechanics, Mécanique des structures et des milieux continus, Structural and continuum mechanics, Elasticité statique (thermoélasticité...), Static elasticity (thermoelasticity...), Mécanique de la rupture (fissure, fatigue, endommagement...), Fracture mechanics (crack, fatigue, damage...), Sciences appliquees, Applied sciences, Industrie des polymeres, peintures, bois, Polymer industry, paints, wood, Technologie des polymères, Technology of polymers, Formes d'application et semiproduits, Forms of application and semi-finished materials, Stratifiés, Laminates, Délaminage, Delamination, Delaminación, Epoxyde résine, Epoxy resin, Epóxido resina, Etude théorique, Theoretical study, Estudio teórico, Fibre carbone, Carbon fiber, Fibra carbón, Fibre minérale, Mineral fiber, Fibra inorgánica, Fibre verre, Glass fiber, Fibra vidrio, Matériau composite, Composite material, Material compuesto, Matériau renforcé fibre, Fiber reinforced material, Material reforzado fibra, Mode empilement, Stacking sequence, Modo apilamiento, Mode rupture, Fracture mode, Modo ruptura, Modélisation, Modeling, Modelización, Mécanique rupture, Fracture mechanics, Mecánica ruptura, Propriété mécanique, Mechanical properties, Propiedad mecánica, Propriété traction, Tensile property, Propiedad tracción, Rupture matrice, Matrix fracture, Ruptura matriz, Résistance fatigue, Fatigue strength, Resistencia fatiga, Stratifié, Laminate, Estratificado, A. Laminates, B. Fracture, B. Mechanical properties, C. Analytical modelling
Document Type:
Konferenz Conference Paper
File Description:
text
Language:
English
Author Affiliations:
Centre for Micro-and Nanomechanics, School of Engineering and Physical Sciences, University of Aberdeen, Eraser Noble Building, Aberdeen AB24 3UE, United Kingdom
Aerospace Engineering, The University of Sheffield, Faculty of Engineering, Sir Frederick Mappin Building, Mappin Street, Sheffield S1 3JD, United Kingdom
ISSN:
1359-835X
Rights:
Copyright 2008 INIST-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Notes:
Physics: solid mechanics

Polymer industry, paints, wood
Accession Number:
edscal.18643060
Database:
PASCAL Archive

Weitere Informationen

Matrix cracks parallel to the fibres in the off-axis plies is the first intralaminar damage mode observed in laminated composites subjected to static or fatigue in-plane tensile loading. They reduce laminate stiffness and strength and trigger development of other damage modes, such as delaminations. This paper is concerned with theoretical modelling of unbalanced symmetric laminates with off-axis ply cracks. Closed-form analytical expressions are derived for Mode I, Mode II and the total strain energy release rates associated with off-axis ply cracking in [0/θ]s laminates. Stiffness reduction due to matrix cracking is also predicted analytically using the Equivalent Constraint Model (ECM) of the damaged laminate. Dependence of the degraded stiffness properties and strain energy release rates on the crack density and ply orientation angle is examined for glass/epoxy and carbon/epoxy laminates. Suitability of a mixed mode fracture criterion to predict the cracking onset strain is also discussed.