2003
DOI: 10.1016/s1359-835x(02)00115-x
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The development of a low temperature cure modified epoxy resin system for aerospace composites

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Cited by 33 publications
(20 citation statements)
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“…3. These particular voids are likely the result of toughening mechanisms in the adhesive (such as those reported in [33]) rather than a result of sample preparation.…”
Section: Sem Analysis Of Fracture Surfacesmentioning
confidence: 94%
“…3. These particular voids are likely the result of toughening mechanisms in the adhesive (such as those reported in [33]) rather than a result of sample preparation.…”
Section: Sem Analysis Of Fracture Surfacesmentioning
confidence: 94%
“…New types of binders and modifiers are being designed now along with methods for their incorporation into the matrix that are optimized for a specific manufacturing process of PCM production, including modern out-of-autoclave technologies. For example, the authors of [130] described an epoxy system with a decreased curing temperature in which a modifier based on a polyethersulfone copolymer is used. Modifiers of various kinds may be used simultaneously (e.g., thermoplastic and inorganic nanoparticles [131]), and this combination may yield a synergistic effect.…”
Section: Discussionmentioning
confidence: 99%
“…As composite materials often require curing, a process that can be achieved by pressure and temperature or both of these features. It is vital to understand ways of reducing the chance of curing causing adverse effects on the material during forming operations [16,17].…”
Section: Materials Requirementsmentioning
confidence: 99%