2017
DOI: 10.1016/j.compositesa.2017.07.007
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Effect of residual stress on the matrix fatigue cracking of rapidly cured epoxy/anhydride composites

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Cited by 29 publications
(12 citation statements)
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“…Joosten et al, who investigated and characterized interlaminar fatigue caused by residual stresses on epoxy composites, utilized the rapid reaction between epoxy and anhydride moieties. 96 They employed a system comprising of a cyclohexylmethyl-3,4-epoxy-cyclohexane carboxylate, bi-functional cycloaliphatic epoxy infusion resin with an anhydride hardener and imidazole catalyst in their laminate manufacture. Initial cure for each composite laminate was carried out using the Resin Transfer Molding (RTM) process.…”
Section: Rapid Cure Resinsmentioning
confidence: 99%
“…Joosten et al, who investigated and characterized interlaminar fatigue caused by residual stresses on epoxy composites, utilized the rapid reaction between epoxy and anhydride moieties. 96 They employed a system comprising of a cyclohexylmethyl-3,4-epoxy-cyclohexane carboxylate, bi-functional cycloaliphatic epoxy infusion resin with an anhydride hardener and imidazole catalyst in their laminate manufacture. Initial cure for each composite laminate was carried out using the Resin Transfer Molding (RTM) process.…”
Section: Rapid Cure Resinsmentioning
confidence: 99%
“…Moreover, the approach is superior to FEM in terms of computational efficiency and accuracy. 5-It has been noted that the Pagano's and McCartney's solutions [28][29][30][31] can also be derived from a fully stressbased variational approach.…”
Section: -mentioning
confidence: 99%
“…In the current paper, a novel variational model is developed to overcome the mentioned drawbacks and to deal with the problem of free-edge interlaminar stress and displacement analysis in laminate strips with general lay-ups (possibly made of many thin plies) under in-plane, bending and uniform thermal loading conditions. The analysis takes into account the effects of thermal residual stresses [29]. The one single fundamental assumption is that the inplane transverse and shear stresses are linear through-thickness of each ply.…”
Section: Introductionmentioning
confidence: 99%
“…Some studies have been done about anticipating residual stresses caused during the curing process, 14 and also, some other about effects of addition of nanoparticles 15 and cure cycle speed. 16 Some other researchers presented some optimization studies for minimizing residual stresses of fiber-reinforced polymer composites based on finding optimum values for the curing cycle parameters. 17,18…”
Section: Introductionmentioning
confidence: 99%