2018
DOI: 10.1016/j.tafmec.2017.12.003
|View full text |Cite
|
Sign up to set email alerts
|

Experimental study of fatigue crack growth in raw and annealed pure copper with considering cyclic plastic effects

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

2
4
0

Year Published

2018
2018
2021
2021

Publication Types

Select...
9

Relationship

1
8

Authors

Journals

citations
Cited by 12 publications
(6 citation statements)
references
References 17 publications
2
4
0
Order By: Relevance
“…The slope of the linear fitting, providing the Paris law exponent m as shown in Eq. 3, was found to be 1.65±0.25, which agrees well with the lower bound of literature value of 2 to 4 for pure copper [31]. This suggests that a large joint defect, which leads to a higher SIF range ΔK, will result in a higher fatigue crack growth rate, hence shorten the fatigue life exponentially.…”
Section: Failure Modesupporting
confidence: 88%
See 1 more Smart Citation
“…The slope of the linear fitting, providing the Paris law exponent m as shown in Eq. 3, was found to be 1.65±0.25, which agrees well with the lower bound of literature value of 2 to 4 for pure copper [31]. This suggests that a large joint defect, which leads to a higher SIF range ΔK, will result in a higher fatigue crack growth rate, hence shorten the fatigue life exponentially.…”
Section: Failure Modesupporting
confidence: 88%
“…where C, C2, m, Δσ and π are all constants, thus the initial fatigue crack growth rate can be simplified as a function of the initial defect area A. According to literature, in the linear elastic fracture mechanics (LEFM) regime, the exponent m is in the range of 3 to 5 for steels [30] and 2 to 4 for pure copper [31]. However, the initial crack size (Fig.…”
Section: Failure Modementioning
confidence: 99%
“…Brünig et al 10 studied the stress–strain effect on the fracture mode of an aluminum alloy, and established an anisotropic fracture model for ductile metals. Seifi and Hosseini 11 studied crack growth in copper under cyclic loading, and the simulated results were consistent with the experimental ones. Bjurenstedt et al 12 conducted a tensile test to evaluate the role of Fe-rich intermetallics on the crack initiation in Al–Si alloys.…”
Section: Instructionsupporting
confidence: 69%
“…For obtaining a preliminary estimate of the CIKH components from the stabilized hysteresis loop (Figure A) in the suggested methodology, the following equations are used: σyIH=σmaxσemin2, α=σmax+σemin2, where σyIH is stabilized yield stress due to IH, α is backstress due to KH, σ max is the peak stress in tension to compression half cycle, σemin is yield stress during load reversal for the half cycle. Similar method to estimate the IH and KH components have been used by earlier investigators too …”
Section: Summary Of the Suggested Methodologymentioning
confidence: 98%