2013
DOI: 10.1080/09243046.2013.777172
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Anisomorphic constant fatigue life diagrams for quasi-isotropic woven fabric carbon/epoxy laminates under different hygro-thermal environments

Abstract: The effect of absorbed moisture on the fatigue strength of a plain-weave roving fabric carbon/epoxy quasi-isotropic laminate under constant amplitude loading at different stress ratios has been examined. First, constant amplitude fatigue tests are performed at room and high temperatures (HT), respectively, on the specimens immersed in hot water until saturation as well as on the specimens kept in a dry place. The results indicate that the fatigue lives of wet specimens are shorter than those of dry specimens, … Show more

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Cited by 44 publications
(19 citation statements)
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“…Finally, Kawai, Yagihashi, Hoshi, and Iwahori (2013) further developed their models discussed previously in Section 13.3.1 to include the combined effect of temperature and moisture. Constant fatigue life diagrams were derived for quasi-isotropic woven carbon/epoxy composites under dry and wet conditions.…”
Section: Effect Of Environmental Conditions and Pre-damagementioning
confidence: 99%
“…Finally, Kawai, Yagihashi, Hoshi, and Iwahori (2013) further developed their models discussed previously in Section 13.3.1 to include the combined effect of temperature and moisture. Constant fatigue life diagrams were derived for quasi-isotropic woven carbon/epoxy composites under dry and wet conditions.…”
Section: Effect Of Environmental Conditions and Pre-damagementioning
confidence: 99%
“…The hygrothermal conditioning of PEEK matrix CFRP is reported to have little influence on its T-T fatigue life compared to dry composites [214]. This is in stark contrast to epoxy matrix CFRP, which shows not only a strong decline in properties compared to dry composites, but are moreover highly sensitive to the loading regimen (R ratio) [215,216,217,218].…”
Section: Effects Of Water On Cfrp and Fatiguementioning
confidence: 98%
“…Many posit that these are bell-shaped curves, regardless of the types of carbon fibres and matrix resins used [239,241,242,247,243]. The CFL diagram for has been used for several different kinds of CFRP laminates [248,249,250,251,252,253,254]. Recently, it was shown by [255] that a unidirectional carbon/epoxy composite, under (T-T) loading (0 < R < 1) and (T-C) (R < 0) loading, has a steeper S-N curve slope than (C-C) loaded (R > 1) composites.…”
Section: Fatigue Damage In Cfrp Compositesmentioning
confidence: 99%
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“…[1,2] Some kinds of heatresistant polymer matrix-based composites (PMCs) (e.g. bismaleimide or polyimide resin systems) are currently being used on structures for both military and commercial aircraft.…”
Section: Introductionmentioning
confidence: 99%