2020
DOI: 10.1177/0021998320972471
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Comparison of progressive damage between thermoset and thermoplastic CFRP composites under in-situ tensile loading

Abstract: The in-situ damage progression in three carbon fibre reinforced cross-ply composite systems under tensile loading is examined, namely, carbon IM7/epoxy, carbon IM7/PEEK and carbon AS4/polyamide. Epoxy is a thermoset polymer while polyether ether ketone (PEEK) and polyamide are thermoplastic. The thermoset composite is manufactured in an autoclave using matrix pre-impregnated with unidirectional carbon fibres, while the thermoplastic composites are manufactured using laser-assisted automated tape placement (LAT… Show more

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Cited by 7 publications
(5 citation statements)
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References 13 publications
(18 reference statements)
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“…Fracture is a process of microcrack generation and propagation; the first microcrack is always generated at the debonding point. Similar opinions have been introduced in other reinforced composites [17,18,20]. In CFRP composites, the first debonding point typically depends on the lower value of the interfacial adhesion between fiber and resin, as well as the lowest bearing point of resin matrix [16,21].…”
Section: Fracture Mechanism Of Different Configurationsmentioning
confidence: 71%
“…Fracture is a process of microcrack generation and propagation; the first microcrack is always generated at the debonding point. Similar opinions have been introduced in other reinforced composites [17,18,20]. In CFRP composites, the first debonding point typically depends on the lower value of the interfacial adhesion between fiber and resin, as well as the lowest bearing point of resin matrix [16,21].…”
Section: Fracture Mechanism Of Different Configurationsmentioning
confidence: 71%
“…In an earlier study, Rao et al [ 37 ] studied the mechanical properties and damage mechanisms of the five conditions that were adopted in the current study through in-situ tensile loading. For the AS4/PA12 without autoclave treatment, the failure load and stress were 0.98 kN and 288 MPa, respectively.…”
Section: Materials Manufacturing and Measurementsmentioning
confidence: 99%
“…Whereas composite itself has several advantage and disadvantages and a number of studies has been reported in this area. Some studies investigated the significance of composite materials by considering the different shapes which has been applied the varies loading conditions [ 23 , 24 ]. Also, numerically investigated the energy effect on the impact resistance of an aircraft polymer composite [ 25 ].…”
Section: Introductionmentioning
confidence: 99%