2014
DOI: 10.1016/j.matdes.2014.02.021
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The influence of stress-controlled tensile fatigue loading on the stress–strain characteristics of AISI 1045 steel

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Cited by 46 publications
(17 citation statements)
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“…The first is cyclic hardening that results in increase of yield limit and tensile strength. 10,21 This behavior was observed at loading cases F1 and F3. Similar behavior was also found in earlier works for the 2017 aluminum alloy, 14 AISI 1045 steel, 21 and Ti6Al4V titanium alloy.…”
Section: Initial Cyclic Loadingsmentioning
confidence: 56%
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“…The first is cyclic hardening that results in increase of yield limit and tensile strength. 10,21 This behavior was observed at loading cases F1 and F3. Similar behavior was also found in earlier works for the 2017 aluminum alloy, 14 AISI 1045 steel, 21 and Ti6Al4V titanium alloy.…”
Section: Initial Cyclic Loadingsmentioning
confidence: 56%
“…10,21 This behavior was observed at loading cases F1 and F3. Similar behavior was also found in earlier works for the 2017 aluminum alloy, 14 AISI 1045 steel, 21 and Ti6Al4V titanium alloy. 22 The other papers concerning subsequent fatigue/impact loadings do not report on the tensile curves after a very low number of pre-fatigue cycles.…”
Section: Initial Cyclic Loadingsmentioning
confidence: 56%
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“…This effect is apparent for fatigue exposures of 25% and 50% of the total fatigue life, however when increased to 75%, a significant decrease in residual flow stress is observed. In this case, two subsequent phenomena are being observed; cyclic hardening during initial cycles (50% fatigue life) followed by cyclic softening with the development of fatigue damage, when approaching and exceeding 75% of the total fatigue life [ 20 ]. This is an important observation in terms of landing gear components, who's dominating loading condition is fatigue.…”
Section: Resultsmentioning
confidence: 99%