1997
DOI: 10.1016/s0266-3538(97)00036-5
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Why interface testing by single-fibre methods can be misleading

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Cited by 121 publications
(57 citation statements)
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“…E.g., the coarser the fibre the higher L c . Moreover, it is known that the debonding between a fibre and a matrix under mechanical loading usually starts at the fibre end [36,37]. In composites with the same fibre mass shorter fibres mean a higher number of fibre ends where debonding can start.…”
Section: Fibre Length Distributionmentioning
confidence: 99%
“…E.g., the coarser the fibre the higher L c . Moreover, it is known that the debonding between a fibre and a matrix under mechanical loading usually starts at the fibre end [36,37]. In composites with the same fibre mass shorter fibres mean a higher number of fibre ends where debonding can start.…”
Section: Fibre Length Distributionmentioning
confidence: 99%
“…Highly oriented graphitic planes are formed on the outer surface of carbon fibre by heat treatment during manufacture [53]. This highly aligned outer layer is typically 1.5 lm thick [53] and relatively weak [54,55], and removal of this layer can increase the tensile strength [56] and improve the interface strength in carbon fibre/epoxy systems [57]. It has also been suggested that the removal of the outer layer removes surface flaws, which are known to be a significant factor for tensile strength properties [56].…”
Section: The Effect Of Fibre Degradationmentioning
confidence: 99%
“…The force eventually reaches a plateau value which is proportional to the dynamic friction. Complete load loss at debonding is likely caused by the release of strain in the fibre, coupled with the fibre undergoing Poisson's shrinkage at high fibre strain values [54]. This would result in the fibre contracting whilst the droplet was sliding at low friction, causing the droplet to 'jump' a section of the fibre [15].…”
Section: The Effect Of Coupling Agentmentioning
confidence: 99%
“…Characteristics of bres and matrix itself [1,2,3], bre loading [4,5,6], bre/matrix adhesion [7,8,9], bre orientation [10,11], bre length [1,12,13], compaction (a good compaction means a low volume of voids) [14] and the production process as well as the procedural settings aect the composite properties clearly. It is well known that compression moulded (CM) long glass bre-reinforced composites display higher strength and impact strength values than short glass brereinforced injection moulded (IM) composites [4,5,10].…”
Section: Introductionmentioning
confidence: 99%