2008
DOI: 10.1016/j.wear.2007.06.016
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Fretting fatigue of rough surfaces

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Cited by 28 publications
(7 citation statements)
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References 14 publications
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“…115 Leonard et al 116 modelled a fretting in a line contact and calculate the severity of wear as a function of the number of cycles using Coulomb law (equation ( 14)) to represent the friction, a FE to represent the stresses and Archard's law to take into account the cumulative damage. Kasarekar et al 117 evaluated the fretting fatigue life depending on the roughness of the surfaces in contact estimating the crack initiation using the Smith Watson Topper fatigue theory and Archard's law to model the wear. Quraishi et al 118 also calculated the fretting fatigue life as a function of friction and loading using the Ramberg-Osgood equation and validated it with experimental results, while Walvekar et al 115 also validated a fretting model that consists of a FEA model that computes the stresses and strains during each cycle and uses an exponential law to model the cumulative fatigue damage.…”
Section: Wearmentioning
confidence: 99%
“…115 Leonard et al 116 modelled a fretting in a line contact and calculate the severity of wear as a function of the number of cycles using Coulomb law (equation ( 14)) to represent the friction, a FE to represent the stresses and Archard's law to take into account the cumulative damage. Kasarekar et al 117 evaluated the fretting fatigue life depending on the roughness of the surfaces in contact estimating the crack initiation using the Smith Watson Topper fatigue theory and Archard's law to model the wear. Quraishi et al 118 also calculated the fretting fatigue life as a function of friction and loading using the Ramberg-Osgood equation and validated it with experimental results, while Walvekar et al 115 also validated a fretting model that consists of a FEA model that computes the stresses and strains during each cycle and uses an exponential law to model the cumulative fatigue damage.…”
Section: Wearmentioning
confidence: 99%
“…7,10,15,18,19,[21][22][23][24][25][26][27] Some authors point out that these criteria may fail if applied to the stress-strain response history calculated on a smooth, unworn model geometry, and provide simulation procedures based on an FE solution for dealing with this issue. 7,10,15,18,19,[21][22][23][24][25][26][27] Some authors point out that these criteria may fail if applied to the stress-strain response history calculated on a smooth, unworn model geometry, and provide simulation procedures based on an FE solution for dealing with this issue.…”
Section: Application Of Plain Fatigue Criteria In Predicting Frettingmentioning
confidence: 99%
“…The application of plain fatigue multi-axial criteria, and modifications of these criteria, to fretting has been published extensively in the literature. 7,10,15,18,19,[21][22][23][24][25][26][27] Some authors point out that these criteria may fail if applied to the stress-strain response history calculated on a smooth, unworn model geometry, and provide simulation procedures based on an FE solution for dealing with this issue. 10,[26][27][28][29][30][31][32] However, the published procedures are very computationally intensive and require special techniques to be implemented in the FE solver subroutines.…”
Section: Application Of Plain Fatigue Criteria In Predicting Frettingmentioning
confidence: 99%
“…Wear process, abrasion in contact and creation of third body will influence dynamic evolution of interface roughness. For very severe contact conditions (Kasarekar et al ., ) often encountered in fretting, initial surface will be totally removed and newly created surface will usually be very complex due to physical and chemical processes taking place at interface. Therefore, multiscale analysis approach should be used to evaluate interface morphology.…”
Section: Introductionmentioning
confidence: 99%