2018
DOI: 10.1088/2053-1591/aadfbb
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2D RVE based micro-mechanical modeling with real microstructures of heat-treated 20MnMoNi55 steel

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Cited by 6 publications
(7 citation statements)
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“…M represents the Taylor factor as mentioned earlier. It was shown in the previous literature 1,2 that as-received 20MnMoNi55 steel shows a yield point elongation phenomenon, whereas the heat-treated 20MnMoNi55 steels (DP steels) exhibit continuous yielding behaviour during the uniaxial monotonic deformation. The yield point elongation behaviour is an aftermath of the Cottrell atmosphere, where the interstitial carbon atoms hindrances in dislocation mobility so the critical stress required to overcome the dislocation barrier is much higher than the stress required to maintain its mobility during deformation.…”
Section: Micromechanical Fe Modellingmentioning
confidence: 95%
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“…M represents the Taylor factor as mentioned earlier. It was shown in the previous literature 1,2 that as-received 20MnMoNi55 steel shows a yield point elongation phenomenon, whereas the heat-treated 20MnMoNi55 steels (DP steels) exhibit continuous yielding behaviour during the uniaxial monotonic deformation. The yield point elongation behaviour is an aftermath of the Cottrell atmosphere, where the interstitial carbon atoms hindrances in dislocation mobility so the critical stress required to overcome the dislocation barrier is much higher than the stress required to maintain its mobility during deformation.…”
Section: Micromechanical Fe Modellingmentioning
confidence: 95%
“…Hence to transform it into ferrite and martensite with a range of fractional variation, a proper design of heat treatment schedules was established based on critical temperatures obtained from the dilatometric test as discussed in a previous article. 2 A 4 mm diameter and 10 mm long cylindrical specimen was used for dilatometric testing where it was heated up to 1100 °C with a heating rate of 1 °C/s. Thus, the obtained temperature versus dilation curve from the experimental result shows the A c1 and A c3 temperatures of about 758 °C and 825 °C, respectively.…”
Section: Experimental Procedures and Determination Of Materials Parametersmentioning
confidence: 99%
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