Please use this identifier to cite or link to this item: https://doi.org/10.1023/A:1011270004881
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dc.titleTensile behaviour of multilayer knitted fabric composites with different stacking configuration
dc.contributor.authorZhang, Y.
dc.contributor.authorHuang, Z.-M.
dc.contributor.authorRamakrishna, S.
dc.date.accessioned2014-10-07T09:11:35Z
dc.date.available2014-10-07T09:11:35Z
dc.date.issued2001
dc.identifier.citationZhang, Y., Huang, Z.-M., Ramakrishna, S. (2001). Tensile behaviour of multilayer knitted fabric composites with different stacking configuration. Applied Composite Materials 8 (4) : 279-295. ScholarBank@NUS Repository. https://doi.org/10.1023/A:1011270004881
dc.identifier.issn0929189X
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/85740
dc.description.abstractIn this paper, multilayer plain weft knitted glass fabric reinforced epoxy composite laminates with different stacking configurations, i.e., [0°]4, [0°/±45°/0°], [0°/90°/90°/0°] and [90°]4, were investigated experimentally. The laminates were uniaxially tensile loaded until final fractures occurred. The experimental results show that with the change in layer stacking structure, a corresponding variation in composite strength and stiffness was achieved. The tensile strength and modulus rank as follows: [0°]4 > [0°/± 45°/0°] > [0°/90°/90°/0°] > [90°]4, which implicates a potential desiguability of Knitted Fabric Composites (KFC) for engineering applications. Failure behaviours of the fractured laminate specimens were examined using a 'matrix digestion and layer peeling' method, based on which the behaviour of each lamina in the laminate can be clearly shown. It was found that an angle-plied lamina in the laminate when subjected to a uniaxial tensile load has a different fracture mode from that of a single ply composite under an off-axial tensile load. This means that the lamina in the laminate is subjected to a more complicated load combination. By comparing the fractured mode of the latter lamina with that of the single ply composite, the load direction sustained by the lamina in the laminate can be identified, which provides a qualitative benchmark for verifying a theoretical simulation.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.1023/A:1011270004881
dc.sourceScopus
dc.subjectExperimentation
dc.subjectFracture mode
dc.subjectInternal load direction
dc.subjectKnitted fabric composites
dc.subjectMechanical properties
dc.subjectMultilayer laminate
dc.subjectStacking configuration
dc.typeArticle
dc.contributor.departmentMECHANICAL ENGINEERING
dc.description.doi10.1023/A:1011270004881
dc.description.sourcetitleApplied Composite Materials
dc.description.volume8
dc.description.issue4
dc.description.page279-295
dc.description.codenAPCME
dc.identifier.isiut000169736300005
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