2016
DOI: 10.1016/j.proeng.2016.11.674
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Correlations between Damage Accumulation and Strength Degradation of Fiber Reinforced Composites Subjected to Cyclic Loading

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Cited by 9 publications
(7 citation statements)
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“…They disclose greater degradation of material properties under fatigue load than the residual strength model and the change of elastic properties can be easily measured using non-destructive techniques [55,56]. The fatigue residual strength/stiffness models recently proposed in the literature [12,18,36,37,44,46,47,54,57,58,59,60,61,62] take into account different loading parameters. Some of the fatigue models are proposed for constant amplitude loadings or include only selected loading parameters.…”
Section: Fatigue Life Modelmentioning
confidence: 99%
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“…They disclose greater degradation of material properties under fatigue load than the residual strength model and the change of elastic properties can be easily measured using non-destructive techniques [55,56]. The fatigue residual strength/stiffness models recently proposed in the literature [12,18,36,37,44,46,47,54,57,58,59,60,61,62] take into account different loading parameters. Some of the fatigue models are proposed for constant amplitude loadings or include only selected loading parameters.…”
Section: Fatigue Life Modelmentioning
confidence: 99%
“…The expected fatigue lives for performed step-wise fatigue tests using the proposed technique are given in Table 2. It should be noted that fatigue of composites is a stochastic phenomenon and depends on the sequence of different damage accumulation mechanisms occurring at different length scales and the statistical distribution of defects [62]. The fatigue life of composite structures can vary even some two orders of magnitude [73].…”
Section: Fatigue Model Calibrationmentioning
confidence: 99%
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“…Up to date, for the generality and complexity of the fatigue-damage models for the unidirectional FRP materials subjected to multiaxial loading [19][20][21][22], most current studies on the optimization of the anchoring system were conducted based on stress analysis and cannot assess or predict the degree of damage to CFRP rods in the anchoring section under specific fatigue loading. Consequently, experimental studies remain an indispensable means to evaluate the performance of the anchoring system.…”
Section: Introductionmentioning
confidence: 99%
“…The three stages of damage accumulation can be distinguished for a wide variety of composite materials. However, while the extent of the individual stages causing substantial properties' degradation can strongly depend on the layup and fiber's geometry (including short and random continuous fibers), it is observed that the CDS develops in the first cycles decades of fatigue life, namely from 1 to 10 3 cycles, whatever the category of composite in play [8][9][10][11][12][13][14]. The above observations draw to the conclusion that the overall fatigue behavior depends on the behavior of the matrix in situ resulting from the constraint exerted by the reinforcement, which results in complex stress fields under load.…”
Section: Introductionmentioning
confidence: 99%