2015
DOI: 10.1007/s12221-015-0640-6
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Behavioural observation of laminated polymer composite under uniaxial quasi-static and cyclic loads

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Cited by 14 publications
(6 citation statements)
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“…However, Figure 9 shows that the first stage of failure is characterized by adhesive fracture due to debonding of the interface between the fiber and matrix, specifically in the fibers perpendicularly oriented to the length and located in the middle of the skins. Similar results with these types of failure were obtained in earlier studies [22]. The SC3S reached this stage of failure at around 95% of its total life and the SC5S at around 98%.…”
Section: Failure and Fracture Analysissupporting
confidence: 90%
“…However, Figure 9 shows that the first stage of failure is characterized by adhesive fracture due to debonding of the interface between the fiber and matrix, specifically in the fibers perpendicularly oriented to the length and located in the middle of the skins. Similar results with these types of failure were obtained in earlier studies [22]. The SC3S reached this stage of failure at around 95% of its total life and the SC5S at around 98%.…”
Section: Failure and Fracture Analysissupporting
confidence: 90%
“…In composite material structures, if delamination of plies occurs between each lamination structure, it means a progressive failure mode has occurred. The failure mode, can be divided into three stages: damage initiation, damage propagation and total perforation (fracture) [12,15,16]. The results obtained in this experimental shows in the range of accepted, but need more investigation related on the actual condition of table tennis blade condition.…”
Section: Figure 6 Energy Absorption Of Kenaf Composite Structuresmentioning
confidence: 76%
“…A resin and hardener mixture of 3:1 was used to obtain optimum matrix composition. Material properties, obtained from literature, are shown in Table .…”
Section: Methodsmentioning
confidence: 99%