2018
DOI: 10.1016/j.jmst.2017.06.015
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Transition and fracture shift behavior in LCF test of dissimilar welded joint at elevated temperature

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Cited by 20 publications
(7 citation statements)
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“…LCF tests of 9Cr-1Mo steel with different strain rates (10 −3 /s and 10 −2 /s) under LCF loading were performed by some researchers [22][23][24] at three temperatures (RT, 300 °C and 600 °C), finding that the fatigue life and the plastic strain amplitude increased at higher strain rates for each temperature, which can be attributed to higher fatigue crack growth rate induced by the dynamic strain aging (DSA). In our previous study [25] on the LCF behavior of martensite-bainite dissimilar welded joint at 500 °C, the fatigue failure shifted from bainite BM to OTZ with the increasing strain amplitude, reflecting the load distribution on each zone varied greatly for the inhomogeneous structure with different strain amplitudes.…”
Section: Introductionmentioning
confidence: 90%
“…LCF tests of 9Cr-1Mo steel with different strain rates (10 −3 /s and 10 −2 /s) under LCF loading were performed by some researchers [22][23][24] at three temperatures (RT, 300 °C and 600 °C), finding that the fatigue life and the plastic strain amplitude increased at higher strain rates for each temperature, which can be attributed to higher fatigue crack growth rate induced by the dynamic strain aging (DSA). In our previous study [25] on the LCF behavior of martensite-bainite dissimilar welded joint at 500 °C, the fatigue failure shifted from bainite BM to OTZ with the increasing strain amplitude, reflecting the load distribution on each zone varied greatly for the inhomogeneous structure with different strain amplitudes.…”
Section: Introductionmentioning
confidence: 90%
“…To simulate the stress and strain field in the WM specimen at the half-life cycle, the BM and WM was treated as the elastic-plastic materials and described with the cyclic stress-strain relations. The constitutive model employed for the BM and WM is the Ramberg-Osgood model [13], which can be expressed as: is the stress amplitude and plastic strain amplitude at the half life cycle, respectively, K is the cyclic strength coefficient and n is the cyclic hardening exponent, the value of which will be exhibit in Section 3.2.3. Meanwhile, the HAZ was considered as elastic material due to the extremely higher hardness and yield stress observed in the nanoindentation and micro-tensile tests, which will be shown in Section 3.1.…”
Section: Numerical Proceduresmentioning
confidence: 99%
“…The strain-controlled low cycle fatigue (LCF) and the stress-controlled ratcheting are the major cyclic deformation phenomena under cyclic loadings [5]. In the last several decades, extensively research works on the strain-controlled LCF behavior of welded joints have been published [6][7][8][9][10][11][12][13][14][15][16][17][18][19][20]. Taking the joints as bulk material, the cyclic hardening/softening features and the fatigue strength of several homogenous welded joints (with base metal of Ti6Al4V [6], 9-12% Cr steel [7][8], 7075Al alloy [9], Ni based alloy 617 [4], etc.)…”
Section: Introductionmentioning
confidence: 99%
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