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2020
DOI: 10.1007/978-3-030-51834-9_98
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Anisotropic Deformation and Fracture Mechanisms of an Additively Manufactured Ni-Based Superalloy

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Cited by 4 publications
(10 citation statements)
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“…7, a large drop in elongation to failure can be seen for the 0°specimens from 600°C to 700°C. Similar behaviour was also observed for a similar SLM alloy [52], where the drop in ductility is caused by grain boundary embrittlement. Since the 0°specimens has more grain boundaries perpendicular to the loading direction, this effect is larger in these specimens compared to 90°specimens.…”
Section: Tensile Testssupporting
confidence: 81%
“…7, a large drop in elongation to failure can be seen for the 0°specimens from 600°C to 700°C. Similar behaviour was also observed for a similar SLM alloy [52], where the drop in ductility is caused by grain boundary embrittlement. Since the 0°specimens has more grain boundaries perpendicular to the loading direction, this effect is larger in these specimens compared to 90°specimens.…”
Section: Tensile Testssupporting
confidence: 81%
“…In the as-LPBFprocessed nickel-based superalloy, the average cellular interspacing is in the narrow range of 400-600 nm, see e.g. LPBF IN718 [162], LPBF IN625 [179], LPBF Hastelloy X [180,181], LPBF IN939 [182], LPBF IN738LC [86], and LPBF CM247LC [183]. Based on these arguments, the .…”
Section: )mentioning
confidence: 98%
“…Deformation twinning is a stress-dependent deformation mechanism that can be dominant at low temperature or at high strain rate [69]. The critical stress for twinning is determined by the crystallographic orientation, where the relation of critical stress, σ <011> < σ <111> < σ <001> can be found [30,70,71]. Yet, the deformation twins are found at the grains with the crystallographic orientation close to <111>//LD instead of <011>//LD in Fig.…”
Section: Deformation Twinningmentioning
confidence: 99%
“…In our previous study on high temperature tensile behaviours of LPBF HX [23,27], we observe that the grain boundaries become weaker at elevated temperature and a significant ductility loss takes place at 700 • C under a strain rate of 10 − 3 /s. In the continuous work, the significant creep damage associated with the applied slow strain rate of 10 − 5 /s and 10 − 6 /s was investigated [28]. For the slow strain rate of 10 − 5 /s and 10 − 6 /s, continuous softening right after yielding caused by creep damage was observed, which is a significant difference to the strain rate of 10 − 3 /s.…”
Section: Introductionmentioning
confidence: 99%
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