2015
DOI: 10.1007/s12221-015-0640-6
|View full text |Cite
|
Sign up to set email alerts
|

Behavioural observation of laminated polymer composite under uniaxial quasi-static and cyclic loads

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

1
5
0

Year Published

2015
2015
2024
2024

Publication Types

Select...
9

Relationship

2
7

Authors

Journals

citations
Cited by 15 publications
(6 citation statements)
references
References 31 publications
1
5
0
Order By: Relevance
“…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%