2017
DOI: 10.1016/j.ijfatigue.2017.01.039
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A one-parameter nonlinear fatigue damage accumulation model

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Cited by 95 publications
(65 citation statements)
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“…That is, Equation can be given by areaFGA,niareaFGA,Ni=niNif();σp. Furthermore, from the viewpoint of the stress‐dependent theory, the interior damage process can be described by a power function relation, ie, the function f ( σ ; p )is indicated by a fitting parameter q whose magnitude is related to applied stress level. The value of q i at σ i is expressed as qi=2σiσnormalb0.75 where 2/ σ b is the coefficient and the value of σ b represents the value of tensile strength at one cycle. Moreover, in the VHCF regime with lower stress, the net nominal stress in the crack plane should be less than 80% of the yield strength σ s , so Equation can be rewritten as qi=2σi0.8σs0.75. Therefore, the interior damage process at σ i can be expressed as areaFGA,niareaFGA,Ni=niNi()2σi0.8σnormals0.75. Based on the concept of equivalent damage, for a multilevel loading, if the damage curves and final fatigue lives at all applied σ levels, as well as the applied cycles at previous σ levels, are known, so the residual life at the last σ level can be obtained.…”
Section: Resultsmentioning
confidence: 99%
“…That is, Equation can be given by areaFGA,niareaFGA,Ni=niNif();σp. Furthermore, from the viewpoint of the stress‐dependent theory, the interior damage process can be described by a power function relation, ie, the function f ( σ ; p )is indicated by a fitting parameter q whose magnitude is related to applied stress level. The value of q i at σ i is expressed as qi=2σiσnormalb0.75 where 2/ σ b is the coefficient and the value of σ b represents the value of tensile strength at one cycle. Moreover, in the VHCF regime with lower stress, the net nominal stress in the crack plane should be less than 80% of the yield strength σ s , so Equation can be rewritten as qi=2σi0.8σs0.75. Therefore, the interior damage process at σ i can be expressed as areaFGA,niareaFGA,Ni=niNi()2σi0.8σnormals0.75. Based on the concept of equivalent damage, for a multilevel loading, if the damage curves and final fatigue lives at all applied σ levels, as well as the applied cycles at previous σ levels, are known, so the residual life at the last σ level can be obtained.…”
Section: Resultsmentioning
confidence: 99%
“…However, the linear damage accumulation rule would result in an overestimated fatigue life in the case of HL block loading and a shorter predicted fatigue life in the LH loading path . To overcome this shortcoming, numerous nonlinear cumulative fatigue damage models had been proposed considering the influence of loading history . Fatemi et al and Schijve comprehensively reviewed the accumulative fatigue damage models with detailed discussion on the influencing factors.…”
Section: Introductionmentioning
confidence: 99%
“…[10][11][12] To overcome this shortcoming, numerous nonlinear cumulative fatigue damage models had been proposed considering the influence of loading history. [13][14][15][16][17][18][19] Fatemi et al 10 and Schijve 20 comprehensively reviewed the accumulative fatigue damage models with detailed discussion on the influencing factors. Nonlinear damage accumulation theories are generally categorized as S-N diagram related, 21 crack growth related, 22 continuum damage mechanics related, 23 and strain energy related.…”
Section: Introductionmentioning
confidence: 99%
“…More specifically, a proposal on generalization of the Kohout‐Věchet model is elaborated for several fatigue damage parameters. Rege et al presented a nonlinear fatigue damage cumulative model with only one parameter included for residual life estimation. Using an S‐N curve under constant amplitude loading, Theil developed a simple fatigue life prediction method by considering the effect of overloading blocks, which provides more accurate estimations than the Miner's rule.…”
Section: Introductionmentioning
confidence: 99%