2015
DOI: 10.1016/j.compositesa.2015.02.023
|View full text |Cite
|
Sign up to set email alerts
|

Rapidly cured out-of-autoclave laminates: Understanding and controlling the effect of voids on laminate fracture toughness

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
16
0

Year Published

2015
2015
2024
2024

Publication Types

Select...
9

Relationship

0
9

Authors

Journals

citations
Cited by 17 publications
(16 citation statements)
references
References 23 publications
0
16
0
Order By: Relevance
“…These voids are mostly observed in the resin-rich regions of the material. The presence of large voids is expected to be detrimental to the mechanical properties due to their deleterious effects on the crack propagation in the resin-rich, inter-tow regions [44,45,46,47]. Voids are also one of the concerns for long-term durability of composites as they accelerate moisture uptake [48].…”
Section: Resultsmentioning
confidence: 99%
“…These voids are mostly observed in the resin-rich regions of the material. The presence of large voids is expected to be detrimental to the mechanical properties due to their deleterious effects on the crack propagation in the resin-rich, inter-tow regions [44,45,46,47]. Voids are also one of the concerns for long-term durability of composites as they accelerate moisture uptake [48].…”
Section: Resultsmentioning
confidence: 99%
“…Voids are formed primarily due to entrapped air within carbon fibre/epoxy prepreg prior to lay-up and aqueous volatiles emitted from the resin during the cure stage. 27,28 According to the TGA-based methodology, the void content can be obtained by equation (2). Figure 4(d) presents the relationship between the different curing processes and void content of composite laminates.…”
Section: Resultsmentioning
confidence: 99%
“…The methodology highlighted in Refs. 23,24 was adopted in order to investigate the effect of random vibration on the development and morphology of voids at four pre-defined points in time within the cure cycle, as shown in Figure 2(b). Laminates were labeled L 1 , L 2 , L 3 , and L 4 , which corresponded to the end of the first ramp, 15 min into the 80°C hold, 30 min into the 80°C hold, and the end of the second ramp, respectively.…”
Section: Methodsmentioning
confidence: 99%