2015
DOI: 10.1016/j.corsci.2015.06.009
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A continuum damage mechanics model for pit-to-crack transition in AA2024-T3

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Cited by 48 publications
(24 citation statements)
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“…Previous studies have focused on stress corrosion cracking [6,7], corrosion fatigue [8][9][10] and hydrogen-induced cracking [11][12][13] and erosion-corrosion [14][15][16]. It has been reported that 23-33% of the low-alloy steel weight loss was attributed to the mechano-electrochemical effects, while the number could be 55-62% for austenitic stainless steels [17].…”
Section: Introductionmentioning
confidence: 99%
“…Previous studies have focused on stress corrosion cracking [6,7], corrosion fatigue [8][9][10] and hydrogen-induced cracking [11][12][13] and erosion-corrosion [14][15][16]. It has been reported that 23-33% of the low-alloy steel weight loss was attributed to the mechano-electrochemical effects, while the number could be 55-62% for austenitic stainless steels [17].…”
Section: Introductionmentioning
confidence: 99%
“…A model to compute the fatigue life of material (to crack initiation) under corrosion fatigue should takes many variables into consideration: chemical nature of the environment, stress/strain levels, stress ratio and loading frequency. Most investigators agree that CFCI occurs at the surface around corrosion defects [11][12][13][14]. The effect of corrosion on fatigue life of stainless steels is most closely related to the passive film resistance [11,15].…”
Section: Introductionmentioning
confidence: 99%
“…1. competition between pit growth and short crack propagation [1,2], 2. preferential dissolution of plastically deformed material [3,19,20,8,14], 3. local rupture of the passive film by slip bands [4][5][6][21][22][23][24] and 4. lowering of surface energy due to adsorption of specific species from the environment [7].…”
Section: Introductionmentioning
confidence: 99%
“…The stress distribution at semi elliptical corrosion pits in steel showed that aspect ratio is the main parameter affecting stress concentration factor . A continuum damage mechanics model for corrosion‐fatigue damage was presented to study the pit‐to‐crack initiation life in AA2024‐T3 . The model was based on the single dominant flaw approach, assuming that although several pits may be present, only 1 pit grows to a critical depth and transitions to a fatigue crack.…”
Section: Introductionmentioning
confidence: 99%