1976
DOI: 10.1016/0022-3115(76)90015-5
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Time-dependent strain-controlled fatigue behavior of annealed 2 Cr-1 Mo steel for use in nuclear steam generator design

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Cited by 52 publications
(9 citation statements)
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“…[13] ) Observations of surfaces and cross sections for the tension hold tests in oxidizing environments are consistent with previous observations. [1,2,3] The reasonably straight oxide-metal interface observed for tension hold tests is expected in light of the continual spalling of the oxide scale. With each compressive strain reversal, oxide flakes off, exposing large patches of the underlying metal surface which then reoxidize.…”
Section: Discussionmentioning
confidence: 90%
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“…[13] ) Observations of surfaces and cross sections for the tension hold tests in oxidizing environments are consistent with previous observations. [1,2,3] The reasonably straight oxide-metal interface observed for tension hold tests is expected in light of the continual spalling of the oxide scale. With each compressive strain reversal, oxide flakes off, exposing large patches of the underlying metal surface which then reoxidize.…”
Section: Discussionmentioning
confidence: 90%
“…For the air tests, the difference between compression hold test and tension hold test fatigue lifetimes increases as the total strain range is decreased. [2] The relatively high total strain range of 1.0 pct was chosen for this study because there is still a difference between compression hold and tension hold lifetimes, but the test time is not prohibitively long. Under the stress conditions used here, the mean stress that developed during a test was very small (typically between 0 and 15 MPa, as compared to a stress range of approximately 700 MPa) and did not appear to be a factor in favoring one type of hold time over the other.…”
Section: Resultsmentioning
confidence: 99%
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“…This has been verified in 3 Cr-Mo-V steel at 550°C where the exponent of a in vacuum was 2.3 compared with unity in air [S]. Figure 4 is a logarithmic plot of plastic strain range against total strain range for several alloys [3,22,[27][28][29][30] and shows that in the region cp < 0405, a value of y = 0.45 (see equation (2) and Fig. 2) may be used.…”
Section: Application To High Strain Fatiguementioning
confidence: 99%
“…2) may be used. Table 1 presents values of p, the cyclic strain hardening exponent, equation ( l ) , and endurance parameters M and k which have previously been reported [3,22,26,28,301. Initiation data are very rarely quoted but we may use the fact that N i tends to Nf at low strain ranges [13,22].…”
Section: Application To High Strain Fatiguementioning
confidence: 99%