The objective of the present work is to investigate mode I and mode II delamination behaviour of chopped strand mat (CSM) E-glass reinforced vinyl ester (VE) composite. Double cantilever beam and end notched flexure tests were carried out to evaluate the mode I and mode II delamination, respectively. The fracture toughnesses were calculated using the experimental calibration method. Results showed that the average mode I and mode II fracture toughnesses were 185 and 2386 N m−1, respectively. Furthermore, the mode II–mode I ratio for this material was 12.9. This value was the highest when compared with other composite materials from the literature. Finally, through scanning electron micrographs, the dominant failure mechanisms were found to ...
The use of composite materials in primary aerospace structures is continually increasing due to thei...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
An overview is presented of the fracture behaviour and failure mechanisms of composite laminates con...
The objective of the present work is to investigate mode I and mode II delamination behaviour of cho...
An investigation of the influence of pre-crack conditions on the fracture behavior of a unidirection...
Glass-fibre-reinforced composites are increasingly used for structural applications. However, like h...
In recent decades, natural fibres are getting their attention as reinforcement in composite material...
A round-robin test programme has been carried out to characterise the mode I interlaminar fracture b...
Delamination between layers in composite materials is a major structural failure. The delamination r...
The goal of this research is to understand the fracture characteristics of woven EGlass/ Derakane 80...
The present paper is concerned with Mode I and Mode II delamination tests performed on three differe...
International audienceWoven composites are well-known for their good transverse properties and for t...
Various vinyl-ester (VE)/poly(acrylonitrile-butadiene-styrene) (ABS) blends were used for interlayer...
Delamination is a common kind of failure observed in various composites. Delamination due to the ope...
The main aim of this work is to examine fracture toughness improvement mechanisms of a composite mat...
The use of composite materials in primary aerospace structures is continually increasing due to thei...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
An overview is presented of the fracture behaviour and failure mechanisms of composite laminates con...
The objective of the present work is to investigate mode I and mode II delamination behaviour of cho...
An investigation of the influence of pre-crack conditions on the fracture behavior of a unidirection...
Glass-fibre-reinforced composites are increasingly used for structural applications. However, like h...
In recent decades, natural fibres are getting their attention as reinforcement in composite material...
A round-robin test programme has been carried out to characterise the mode I interlaminar fracture b...
Delamination between layers in composite materials is a major structural failure. The delamination r...
The goal of this research is to understand the fracture characteristics of woven EGlass/ Derakane 80...
The present paper is concerned with Mode I and Mode II delamination tests performed on three differe...
International audienceWoven composites are well-known for their good transverse properties and for t...
Various vinyl-ester (VE)/poly(acrylonitrile-butadiene-styrene) (ABS) blends were used for interlayer...
Delamination is a common kind of failure observed in various composites. Delamination due to the ope...
The main aim of this work is to examine fracture toughness improvement mechanisms of a composite mat...
The use of composite materials in primary aerospace structures is continually increasing due to thei...
Vulnerability to delaminations is one of the major weaknesses of advanced laminated composite struct...
An overview is presented of the fracture behaviour and failure mechanisms of composite laminates con...