2016
DOI: 10.1016/j.tafmec.2015.12.015
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Fractographical analysis of fatigue failed Cu–2.55Ni–0.55Si alloy

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Cited by 16 publications
(17 citation statements)
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“…As shown in Figure 7b, the striation pattern could be used to distinguish between fatigue crack initiation and crack propagation, regarded as one of the main features for crack propagation [31]. The length "d" of the rack initiation zone along the crack propagation path was about 20 μm, which confirmed the fatigue crack initiation at the surface/subsurface [29]. Fatigue striations and the secondary crack were observed at the crack propagation zone in Figure 7d,e.…”
Section: Morphology Of the Specimen's Surfacementioning
confidence: 70%
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“…As shown in Figure 7b, the striation pattern could be used to distinguish between fatigue crack initiation and crack propagation, regarded as one of the main features for crack propagation [31]. The length "d" of the rack initiation zone along the crack propagation path was about 20 μm, which confirmed the fatigue crack initiation at the surface/subsurface [29]. Fatigue striations and the secondary crack were observed at the crack propagation zone in Figure 7d,e.…”
Section: Morphology Of the Specimen's Surfacementioning
confidence: 70%
“…The crack propagation path is shown by the arrows in Figure 7a and it also shows the general view of the fracture surfaces [28,29] indicating the areas for (i) crack initiation (CI); (ii) fatigue crack growth, and propagation (CGP), and final fracture (FF). At the end of fatigue crack growth and propagation, the surface of the fracture was rough in Figure 7a.…”
Section: Morphology Of the Specimen's Surfacementioning
confidence: 99%
“…10, the fracture surface had a mixed fracture of dimple and transgranular ruptures in its final fracture region. This study is an extension of our previous report [10] focusing on the fatigue response of a Zr and Cr modified Cu-Ni-Si alloy tested at different stress levels. In the present study, the alloy was subjected to a conventional heat treatment and exhibited higher mechanical properties compared to its cast and forged condition.…”
Section: Resultsmentioning
confidence: 87%
“…The hardness, yield strength and tensile strength values were measured as 215 HV, 520 MPa and 745 MPa, respectively. As similar to our previous investigation on fatigue behaviour of cast and forged alloy (153 HV) having the same composition [10], the aged one was also tested according to ISO 1099 standard. Prior to loading, the specimens were polished to mirror like finish in order to avoid any surface effect on the fatigue behavior of the material under investigation.…”
Section: Experimental Studymentioning
confidence: 95%
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