2015
DOI: 10.1016/j.ijfatigue.2015.01.014
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Effects of mean stress and fibre volume content on the fatigue-induced damage mechanisms in CFRP

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Cited by 58 publications
(40 citation statements)
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“…The fatigue performance of composites is influenced by the composite system itself. Particularly influential parameters include; fibre and matrix properties, lay-up sequence [18,19], residual stresses due to the manufacturing process or due to discontinuities [20,21] and the maximum to minimum ratio of stress endured by the material [22,23,24,4], ply orientation [4], the fibre/matrix fractions [25], and environmental conditions affecting the composite components [26,27,28]. Exemplary works on the fatigue of composites covered from both experimental [29,22] and theoretical [4,30,31,32] perspectives may assist in the development of improved methods by which means composite failure can be predicted.…”
Section: Mechanics Of Cyclically Loaded Compositesmentioning
confidence: 99%
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“…The fatigue performance of composites is influenced by the composite system itself. Particularly influential parameters include; fibre and matrix properties, lay-up sequence [18,19], residual stresses due to the manufacturing process or due to discontinuities [20,21] and the maximum to minimum ratio of stress endured by the material [22,23,24,4], ply orientation [4], the fibre/matrix fractions [25], and environmental conditions affecting the composite components [26,27,28]. Exemplary works on the fatigue of composites covered from both experimental [29,22] and theoretical [4,30,31,32] perspectives may assist in the development of improved methods by which means composite failure can be predicted.…”
Section: Mechanics Of Cyclically Loaded Compositesmentioning
confidence: 99%
“…They concluded that damage accumulation within the matrix of a composite, decreases as the fibre volume fraction increases. Brunbauer and Pinter [41] conducted an extensive experimental study to discern the effect of mean stress and FVF (30% and 55%) on damage mechanisms in epoxy matrix UD-CFRP. The materials were tested under both static and cyclic conditions in both T-T and T-C modes and oriented 6 at 0 • , 45 • and 90 • .…”
Section: Thermoset and Thermoplastic Matrix Cfrpmentioning
confidence: 99%
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“… Mechanical behavior and damage mechanism in carbon/epoxy laminate with different fiber direction, fiber volume fraction, test angle, applied load type, and fatigue mean stress . [Color figure can be viewed at http://wileyonlinelibrary.com]…”
Section: Fiber Volume Fractionmentioning
confidence: 99%
“…6. Comparison of fatigue life laminates with two different fiber volume fraction, that is, 30 and 55% [17]. strength of the specimen, respectively.…”
Section: Mean Stress and Stress Ratiomentioning
confidence: 99%