X-Ray Diffraction Study of Low Cycle Fatigue Damage in Plain Carbon SteelSource: Journal of Engineering Materials and Technology:;1977:;volume( 099 ):;issue: 002::page 110DOI: 10.1115/1.3443418Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An X-Ray diffraction analysis of low cycle bending fatigue was conducted on plain carbon steel (SAE 1008) in three conditions, as received (annealed) 20 percent prestrained, and strain aged. The decrease of the surface stresses at maximum and minimum strains, a reduction of the residual surface stress after unloading from the tension cycle, and a decrease of the half-value breadth during the first 20–30 cycles indicate rapid cyclic softening during the initial stages of strain cycling. After this initial period the microstructure of all specimens was found to be independent of the initial material condition. Similarly, the fatigue life as a function of strain range was also independent of the initial condition. X-Ray diffraction line analysis shows no changes for the major portion of the specimen life, from 0.1 Nf to 0.75 Nf . However, a linear relationship between half-value breadth and strain range is noted. It is suggested that this relationship can be utilized for monitoring and diagnostic purposes, particularly to determine the strain range to which a critical part has been subjected.
keyword(s): X-ray diffraction , Carbon steel , Low cycle fatigue , Cycles , Stress , Fatigue life , Tension AND Fatigue ,
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| contributor author | Masato Nagao | |
| contributor author | Volker Weiss | |
| date accessioned | 2017-05-08T23:02:55Z | |
| date available | 2017-05-08T23:02:55Z | |
| date copyright | April, 1977 | |
| date issued | 1977 | |
| identifier issn | 0094-4289 | |
| identifier other | JEMTA8-26852#110_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/89909 | |
| description abstract | An X-Ray diffraction analysis of low cycle bending fatigue was conducted on plain carbon steel (SAE 1008) in three conditions, as received (annealed) 20 percent prestrained, and strain aged. The decrease of the surface stresses at maximum and minimum strains, a reduction of the residual surface stress after unloading from the tension cycle, and a decrease of the half-value breadth during the first 20–30 cycles indicate rapid cyclic softening during the initial stages of strain cycling. After this initial period the microstructure of all specimens was found to be independent of the initial material condition. Similarly, the fatigue life as a function of strain range was also independent of the initial condition. X-Ray diffraction line analysis shows no changes for the major portion of the specimen life, from 0.1 Nf to 0.75 Nf . However, a linear relationship between half-value breadth and strain range is noted. It is suggested that this relationship can be utilized for monitoring and diagnostic purposes, particularly to determine the strain range to which a critical part has been subjected. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | X-Ray Diffraction Study of Low Cycle Fatigue Damage in Plain Carbon Steel | |
| type | Journal Paper | |
| journal volume | 99 | |
| journal issue | 2 | |
| journal title | Journal of Engineering Materials and Technology | |
| identifier doi | 10.1115/1.3443418 | |
| journal fristpage | 110 | |
| journal lastpage | 113 | |
| identifier eissn | 1528-8889 | |
| keywords | X-ray diffraction | |
| keywords | Carbon steel | |
| keywords | Low cycle fatigue | |
| keywords | Cycles | |
| keywords | Stress | |
| keywords | Fatigue life | |
| keywords | Tension AND Fatigue | |
| tree | Journal of Engineering Materials and Technology:;1977:;volume( 099 ):;issue: 002 | |
| contenttype | Fulltext |