2014
DOI: 10.1016/j.mspro.2014.06.273
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Effect of SiC Particles on Fatigue Crack Growth Behavior of SiC Particulate-reinforced Al-Si Alloy Composites Produced by Spray Forming

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Cited by 21 publications
(13 citation statements)
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“…These modified JC models can well describe the stress-strain characteristics of theirs materials. The expression of the most widely used in these provided modified JC models is shown in equation (13). To determine whether this modified JC model is suitable for spray-deposition SiCp/ 7055Al composites, the equation (13) is verified.…”
Section: Modified Johnson-cook Modelmentioning
confidence: 99%
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“…These modified JC models can well describe the stress-strain characteristics of theirs materials. The expression of the most widely used in these provided modified JC models is shown in equation (13). To determine whether this modified JC model is suitable for spray-deposition SiCp/ 7055Al composites, the equation (13) is verified.…”
Section: Modified Johnson-cook Modelmentioning
confidence: 99%
“…Rearrange equation (13) and take natural logarithm on both sides, could be obtained equation (17) * obtained from the slopes of those graphs. As shown in figure 10, when the strain rates are 0.001 s −1 , 0.01 s −1 , and 0.1 s −1 , the values of  l l e + ln 1 2 * are obtained as −0.0084, −0.0067, −0.0056, respectively.…”
Section: Modified Johnson-cook Modelmentioning
confidence: 99%
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“…The occurrence of particle fracture is usually insignificant at smaller crack sizes but it rises with the rise of maximum stress intensity and becomes constant during fast fracture (Kumai et al, 1990;Shang et al, 1988;Sugimura & Suresh, 1992). Li et al, (Li, Liang, Chen, Zhu, & Chen, 2014) mentioned that smaller SiC particles (4.5 μm) displayed higher resistance to fatigue crack compare to the composite with 20 μm SiC particles and unreinforced alloy. The crack in 4.5 μm reinforced SiC particles induced higher level of fatigue crack closure which reduce crack growth.…”
Section: Introductionmentioning
confidence: 99%
“…It is well known that cracks due to fatigue usually start from free surface (Li et al, 2014) as it undergoes maximum loading and thus the free surfaces generated from diverse machining processes show wide range of fatigue behaviour (Zlatin and Field 1973). Therefore, machining induced residual stresses, surface morphology microstructure (phases, plastic deformation, tears, voids, pits, burrs, cracks etc.…”
Section: Introductionmentioning
confidence: 99%