A study of damage development in a weft knitted fabric reinforced composite. Part 1: Experiments using model sandwich laminates

Coupons consisting of single layers of Milano weft knitted glass fabric reinforced epoxy resin have been tested with the knitted fabric oriented at various angles to the loading direction, alone and sandwiched between outer layers of unidirectional glass/epoxy reinforcement. The sandwich coupons ena...

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Published inComposites. Part A, Applied science and manufacturing Vol. 38; no. 7; pp. 1773 - 1793
Main Authors Rios, C.R., Ogin, S.L., Lekakou, C., Leong, K.H.
Format Journal Article
LanguageEnglish
Published Oxford Elsevier Ltd 01.07.2007
Elsevier
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Abstract Coupons consisting of single layers of Milano weft knitted glass fabric reinforced epoxy resin have been tested with the knitted fabric oriented at various angles to the loading direction, alone and sandwiched between outer layers of unidirectional glass/epoxy reinforcement. The sandwich coupons enable the initiation of damage to be observed directly. Tensile tests have shown that the first damage occurs as microdebonding between the loop cross-over points in the knitted fabric structure. Matrix cracking damage develops from these initiation sites and the pattern of cracking is intimately related to the fabric architecture and the fabric orientation with respect to the loading direction. Cyclic tests of sandwich specimens, and a representation of the results in terms of cumulative strain, indicate that some of the acoustic emission activity during loading and unloading of the specimens is likely to be associated with the debonding and pulling-out of knitted fabric tows across the fracture surfaces of the matrix cracks.
AbstractList Coupons consisting of single layers of Milano weft knitted glass fabric reinforced epoxy resin have been tested with the knitted fabric oriented at various angles to the loading direction, alone and sandwiched between outer layers of unidirectional glass/epoxy reinforcement. The sandwich coupons enable the initiation of damage to be observed directly. Tensile tests have shown that the first damage occurs as microdebonding between the loop cross-over points in the knitted fabric structure. Matrix cracking damage develops from these initiation sites and the pattern of cracking is intimately related to the fabric architecture and the fabric orientation with respect to the loading direction. Cyclic tests of sandwich specimens, and a representation of the results in terms of cumulative strain, indicate that some of the acoustic emission activity during loading and unloading of the specimens is likely to be associated with the debonding and pulling-out of knitted fabric tows across the fracture surfaces of the matrix cracks.
Author Rios, C.R.
Ogin, S.L.
Lekakou, C.
Leong, K.H.
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  organization: Cooperative Research Centre for Advanced Composites Structures Ltd. (CRC-ACS), 506 Lorimer Street, Fishermans Bend, VIC 3207, Australia
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Issue 7
Keywords D. Mechanical testing
D. Acoustic emission
D. Fractography
D. Electron microscopy
Stacking sequence
Laminate
Unidirectional fiber material
Fiber reinforced material
Sandwich structure
Epoxy resin
Mechanical properties
Tensile property
Experimental study
Mineral fiber
Composite material
Glass fiber fabric
Knitted fabrics
Woven material
Damaging
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SubjectTerms Applied sciences
D. Acoustic emission
D. Electron microscopy
D. Fractography
D. Mechanical testing
Exact sciences and technology
Forms of application and semi-finished materials
Laminates
Polymer industry, paints, wood
Technology of polymers
Title A study of damage development in a weft knitted fabric reinforced composite. Part 1: Experiments using model sandwich laminates
URI https://dx.doi.org/10.1016/j.compositesa.2006.02.027
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