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The effect of stacking sequence on fatigue behaviour of hybrid pineapple leaf fibre/carbon-fibre-reinforced epoxy composites

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cris.virtual.department Universiti Malaysia Perlis
cris.virtual.department Universiti Malaysia Perlis
cris.virtual.department Universiti Malaysia Perlis
cris.virtual.department Universiti Malaysia Perlis
cris.virtualsource.department 56d651a5-ea11-4fee-bcad-d8b23a63b4ad
cris.virtualsource.department ccf016e1-634e-4f03-a0ac-3992409d0f61
cris.virtualsource.department ac65008b-77e0-4bc6-9669-d7e7a6a47ff9
cris.virtualsource.department eb65b572-b01f-4fc6-bed4-f58282658190
dc.contributor.author Mohd Khairul Rabani Hashim
dc.contributor.author Mohd Shukry Abdul Majid
dc.contributor.author Mohd Ridzuan Mohd Jamir
dc.contributor.author Farizul Hafiz Kasim
dc.contributor.author Mohamed Thariq Hameed Sultan
dc.contributor.author Ain Umaira Md Shah
dc.contributor.author Kamarul Arifin Ahmad
dc.contributor.author Adi Azriff Basri
dc.date.accessioned 2024-05-07T03:57:28Z
dc.date.available 2024-05-07T03:57:28Z
dc.date.issued 2021
dc.description.abstract This study examined the fatigue behaviour of pineapple leaf fibre/carbon hybrid laminate composites under various stacking sequences. The vacuum infusion technique was used to fabricate the symmetric quasi-isotropic oriented laminates, in which the stacking was varied. The laminate was tested under static and fatigue tensile load according to ASTM D3039-76 and ASTM D3479-96, respectively. Maximum tensile strength and modulus of 119.34 MPa and 6.86 GPa, respectively, were recorded for the laminate with external PALF ply and internal carbon ply oriented at [± 45°2, 0°/90°2]s (PCCP_45090). The fatigue tests showed that PCCP_45090 and CPPC_09045 (with internal PALF ply and external carbon ply oriented at [0°/90°2, ± 45°2]s) exhibited a higher useful life, especially at the high-stress level of the ultimate tensile strength. The normalised stress against the number of cycles showed that the stacking sequences of different ply orientations affected the fatigue behaviour more than the stacking sequences of the material. The laminate stacking sequence significantly affected the hysteresis energy and stiffness evolution. The scanning electron microscopy images showed that the fatigue failure modes included fibre pull-out, fibre breakage, matrix cracking, debonding, and delamination. The study concluded that PCCP_45090 exhibited an outstanding fatigue performance.
dc.identifier.doi 10.3390/polym13223936
dc.identifier.uri https://www.mdpi.com/2073-4360/13/22/3936/pdf
dc.identifier.uri https://www.mdpi.com/2073-4360/13/22/3936/xml
dc.identifier.uri https://hdl.handle.net/20.500.14170/2405
dc.language.iso en
dc.relation.ispartof Polymers
dc.relation.issn 2073-4360
dc.subject PALF
dc.subject Carbon fibre
dc.subject Hybrid composite
dc.subject Tensile properties
dc.subject Fatigue behaviour
dc.title The effect of stacking sequence on fatigue behaviour of hybrid pineapple leaf fibre/carbon-fibre-reinforced epoxy composites
dc.type journal-article
dspace.entity.type Publication
oaire.citation.endPage 16
oaire.citation.issue 22
oaire.citation.startPage 1
oaire.citation.volume 13
oairecerif.author.affiliation Universiti Malaysia Perlis
oairecerif.author.affiliation Universiti Malaysia Perlis
oairecerif.author.affiliation Universiti Malaysia Perlis
oairecerif.author.affiliation Universiti Malaysia Perlis
oairecerif.author.affiliation Universiti Putra Malaysia
oairecerif.author.affiliation Universiti Putra Malaysia
oairecerif.author.affiliation Universiti Putra Malaysia
oairecerif.author.affiliation Universiti Putra Malaysia
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