2014
DOI: 10.1016/j.matdes.2013.08.074
|View full text |Cite
|
Sign up to set email alerts
|

Influence of fabric structure and thickness on the ballistic impact behavior of Ultrahigh molecular weight polyethylene composite laminate

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

7
56
0
1

Year Published

2014
2014
2024
2024

Publication Types

Select...
8
1

Relationship

0
9

Authors

Journals

citations
Cited by 159 publications
(64 citation statements)
references
References 23 publications
7
56
0
1
Order By: Relevance
“…On the other hand, for samples after the fire test, CF+AA has 75.0% and 36.6% greater impact strength than CAFRALL and CARALL, respectively. The result for CARALL shows that alternating layers of the composites causes delamination between the inner layers, as reflected by less travelling distance of the projectile in the sample that indicates less surface energy dissipation [37,38]. Similar result has also been observed in Ref.…”
Section: Resultssupporting
confidence: 85%
“…On the other hand, for samples after the fire test, CF+AA has 75.0% and 36.6% greater impact strength than CAFRALL and CARALL, respectively. The result for CARALL shows that alternating layers of the composites causes delamination between the inner layers, as reflected by less travelling distance of the projectile in the sample that indicates less surface energy dissipation [37,38]. Similar result has also been observed in Ref.…”
Section: Resultssupporting
confidence: 85%
“…9 shows photographs of the cross section of laminates having different thicknesses subjected to an impact velocity of 700 ± 15 m s −1 . The failure modes like shear cutting, matrix cracking, tensile failure and delamination can be seen here as reported in earlier studies [19]. Arrow mark on the figure shows the impact direction.…”
Section: Failure Behavior Of Laminatesmentioning
confidence: 60%
“…8 [19]. The damage in thin laminates is in the form of cone and opening towards the target's exit side.…”
Section: Failure Behavior Of Laminatesmentioning
confidence: 99%
“…The low values of ballistic limit in H3A hybrid composites compared to the H3 hybrid, which consisted of the same number of kenaf layers, denoted the negative effect of the alternative arrangement. This result can be explained by the fact that an alternating arrangement led to delamination between the inner surfaces, presenting less traveling distance for the projectile within the target (Zhang et al 2014). As a result of less travel distance, there was less surface for energy dissipation (Sabet et al 2009).…”
Section: Resultsmentioning
confidence: 99%