2010
DOI: 10.4028/www.scientific.net/amr.160-162.226
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A New Pair of Cumulative Fatigue Damage Models for Composite Materials

Abstract: Fatigue damage growth can be described by the gradual reduction of the stiffness and strength, and damage expressed by the two degradation methods are equivalent. According this assumption, a pair of cumulative fatigue damage models based on residual stiffness and residual strength is proposed, and then the connection between the two damage indices is established. The two damage models follow equation with the same form, but the parameters in them are not equal. Each of the two models contains three unknown pa… Show more

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Cited by 3 publications
(4 citation statements)
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“…) When a laminate is subjected to certain fatigue loading, the material properties degradation may be reflected by the changes of stiffness and strength, and it is assumed that under the same damage state, the damage described by residual stiffness and by residual strength is completely equivalent, accordingly, a pair of cumulative fatigue damage models are developed to simulate damage evolution of overall life range in composites, these equations are presented in previous work [3]:…”
Section: Proposed Fatigue Damage Accumulation Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…) When a laminate is subjected to certain fatigue loading, the material properties degradation may be reflected by the changes of stiffness and strength, and it is assumed that under the same damage state, the damage described by residual stiffness and by residual strength is completely equivalent, accordingly, a pair of cumulative fatigue damage models are developed to simulate damage evolution of overall life range in composites, these equations are presented in previous work [3]:…”
Section: Proposed Fatigue Damage Accumulation Modelmentioning
confidence: 99%
“…If unable to get the parameter m, may refer to the Ref. [3], m varies from 1.2 to 2.6 and an average value m=1.7 is suggested.…”
Section: Proposed Fatigue Damage Accumulation Modelmentioning
confidence: 99%
“…3,4 Generally, it is believed that the fatigue damage mechanisms of wind turbine rotor blade composites are very complicated, various forms of fatigue damage may appear during the fatigue process, such as matrix cracking, fiber/ matrix interface debonding and fiber fracture. 5 To avoid disastrous accidents, it is critical to predict fatigue life of wind turbine rotor blade under the random loads. Zhang et al 6 presented a fatigue life evaluation method for wind turbine rotor blade based on the multistage loading accumulative damage theory.…”
Section: Introductionmentioning
confidence: 99%
“…3,4 Generally, it is believed that the fatigue damage mechanisms of wind turbine rotor blade composites are very complicated, various forms of fatigue damage may appear during the fatigue process, such as matrix cracking, fiber/matrix interface debonding and fiber fracture. 5…”
Section: Introductionmentioning
confidence: 99%