2017
DOI: 10.1016/j.ijfatigue.2017.05.028
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Effects of macro-scale corrosion damage feature on fatigue crack initiation and fatigue behavior

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Cited by 60 publications
(36 citation statements)
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“…It was also observed that localized corrosion promoted initiation of multiple cracks, and the presence of the pits causing stress concentration greatly accelerated crack initiation and promoted crack growth. These experimental results are in agreement with the finding reported previously on the fatigue failure of pre‐corroded aluminum alloys 2024 and 7050 . Although the fact that prior localized corrosion causes the degradation of mechanical properties of aluminum alloy and promotes crack initiation although stress concentration is well known, there is still a lack of quantitative analysis of when and where these cracks initiate, and how they evolve and interact leading to final failure, especially for different levels of prior corrosion.…”
Section: Resultssupporting
confidence: 91%
See 1 more Smart Citation
“…It was also observed that localized corrosion promoted initiation of multiple cracks, and the presence of the pits causing stress concentration greatly accelerated crack initiation and promoted crack growth. These experimental results are in agreement with the finding reported previously on the fatigue failure of pre‐corroded aluminum alloys 2024 and 7050 . Although the fact that prior localized corrosion causes the degradation of mechanical properties of aluminum alloy and promotes crack initiation although stress concentration is well known, there is still a lack of quantitative analysis of when and where these cracks initiate, and how they evolve and interact leading to final failure, especially for different levels of prior corrosion.…”
Section: Resultssupporting
confidence: 91%
“…Optical microscopy monitoring of pre‐corroded 7075‐T6 aluminum alloy specimen surfaces, to investigate short crack growth, revealed that short crack growth life under salt water conditions was approximately 5 to 8 times lower than in ambient air . A crack surface marker‐band method was used to determine the short crack growth rate of AA7050‐T7451 samples with macro scale corrosion damage; crack growth rates were shown to converge to comparable values for varied corrosion morphologies …”
Section: Introductionmentioning
confidence: 99%
“…However, it is useful to comment on the fatigue life results presented in Figure 4; there are 4 critical observations. 15,29,75,76 Third, in general, specimens tested in 0.6 M NaCl resulted in shorter fatigue lives than those tested in lab air. However, no clear trend was observed suggesting that this is the expected scatter in fatigue life, consistent with prior observations for fatigue behaviour in various stainless steels.…”
Section: Fatigue Testsmentioning
confidence: 95%
“…47,75,[78][79][80] The local stress/strain fields specific to the corrosion geometry and local microstructure can be used to calculate fatigue indicator parameters, which are micro-mechanical models that aim to capture the local grain-scale driving force for crack formation and small crack propagation. For example, in some instances, a relatively small pit (<90th percentile, with over 100 larger pits existing on the specimen) initiates the cracking.…”
Section: Interpretation and Identification Of The Macro-scale Corromentioning
confidence: 99%
“…47 Image refinement and pit volume calculation was performed using MountainsMaps imaging topography software. [48][49][50] Calculations were made by multiplying the average pit volume by the total number of pits and normalizing for area. The results presented here indicate that the level of resistance (low frequency impedance (Z 0.01 )) afforded by the coating system (where, in this study, any deviation is wholly dependent on the pretreatment as the only variable between the uncoated systems) directly effects the global galvanic protection potential.…”
mentioning
confidence: 99%