Fatigue-Crack Propagation in Steels of Various Yield StrengthsSource: Journal of Manufacturing Science and Engineering:;1971:;volume( 093 ):;issue: 004::page 1190Author:J. M. Barsom
DOI: 10.1115/1.3428061Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The useful life of highly constrained welded structures subjected to cyclic loads often depends on the crack-propagation behavior of the material. Thus, to predict the service life of many structures and to establish safe inspection intervals, an understanding of the rate of fatigue-crack propagation in steel is required. Accordingly, an investigation was conducted to determine the fatigue-crack-growth rates in structural steels ranging in yield strength from 36 to 191 ksi; for this study, wedge-opening-loading (WOL) specimens were used. The tests were conducted at room temperature in an air environment, and the results were compared with published fatigue-crack-growth data for steels having similar yield strengths. The results showed that the primary factor affecting fatigue-crack-growth rates in structural steels is the applied stress-intensity-factor range, ΔKI , and that conservative estimates of fatigue-crack growth per cycle of loading, da/dN, for martensitic steels are obtained from the relationship dadN=0.66×10−8(ΔKI)2.25 where a is in inches and ΔKI is in ksi in. Similarly, the data showed that conservative estimates of da/dN for ferrite-pearlite steels are obtained from the relationship dadN=3.6 ×10−10(ΔKI)3 As indicated in these equations, the fatigue-crack-growth rates were higher for martensitic steels than for ferrite-pearlite steels. The data also showed that the fatigue-crack growth per cycle accelerated for all the steels, and that this transition from the above relationships to increased rates occurred when the crack-opening-displacement range, Δδ, which is a measure of the strain range at the crack tip, reaches a critical value. The fatigue-rate transition in martensitic steels occurred when Δδ was about 1.6 × 10−3 in. However, the fatigue-rate transition in ferrite-pearlite steels occurred at a Δδ value slightly higher than 1.6 × 10−3 in. A model based on micro structural considerations is presented, which accounts for these differences in the fatigue-crack-growth behavior between martensitic and ferrite-pearlite steels.
keyword(s): Steel , Fatigue cracks , Fracture (Materials) , Fatigue , Ferrites (Magnetic materials) , Martensitic steel , Cycles , Stress , Structural steel , Service life (Equipment) , Temperature , Inspection , Displacement , Equations , Crack propagation , Wedges AND Yield strength ,
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| contributor author | J. M. Barsom | |
| date accessioned | 2017-05-09T01:03:38Z | |
| date available | 2017-05-09T01:03:38Z | |
| date copyright | November, 1971 | |
| date issued | 1971 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27566#1190_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/153455 | |
| description abstract | The useful life of highly constrained welded structures subjected to cyclic loads often depends on the crack-propagation behavior of the material. Thus, to predict the service life of many structures and to establish safe inspection intervals, an understanding of the rate of fatigue-crack propagation in steel is required. Accordingly, an investigation was conducted to determine the fatigue-crack-growth rates in structural steels ranging in yield strength from 36 to 191 ksi; for this study, wedge-opening-loading (WOL) specimens were used. The tests were conducted at room temperature in an air environment, and the results were compared with published fatigue-crack-growth data for steels having similar yield strengths. The results showed that the primary factor affecting fatigue-crack-growth rates in structural steels is the applied stress-intensity-factor range, ΔKI , and that conservative estimates of fatigue-crack growth per cycle of loading, da/dN, for martensitic steels are obtained from the relationship dadN=0.66×10−8(ΔKI)2.25 where a is in inches and ΔKI is in ksi in. Similarly, the data showed that conservative estimates of da/dN for ferrite-pearlite steels are obtained from the relationship dadN=3.6 ×10−10(ΔKI)3 As indicated in these equations, the fatigue-crack-growth rates were higher for martensitic steels than for ferrite-pearlite steels. The data also showed that the fatigue-crack growth per cycle accelerated for all the steels, and that this transition from the above relationships to increased rates occurred when the crack-opening-displacement range, Δδ, which is a measure of the strain range at the crack tip, reaches a critical value. The fatigue-rate transition in martensitic steels occurred when Δδ was about 1.6 × 10−3 in. However, the fatigue-rate transition in ferrite-pearlite steels occurred at a Δδ value slightly higher than 1.6 × 10−3 in. A model based on micro structural considerations is presented, which accounts for these differences in the fatigue-crack-growth behavior between martensitic and ferrite-pearlite steels. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Fatigue-Crack Propagation in Steels of Various Yield Strengths | |
| type | Journal Paper | |
| journal volume | 93 | |
| journal issue | 4 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3428061 | |
| journal fristpage | 1190 | |
| journal lastpage | 1196 | |
| identifier eissn | 1528-8935 | |
| keywords | Steel | |
| keywords | Fatigue cracks | |
| keywords | Fracture (Materials) | |
| keywords | Fatigue | |
| keywords | Ferrites (Magnetic materials) | |
| keywords | Martensitic steel | |
| keywords | Cycles | |
| keywords | Stress | |
| keywords | Structural steel | |
| keywords | Service life (Equipment) | |
| keywords | Temperature | |
| keywords | Inspection | |
| keywords | Displacement | |
| keywords | Equations | |
| keywords | Crack propagation | |
| keywords | Wedges AND Yield strength | |
| tree | Journal of Manufacturing Science and Engineering:;1971:;volume( 093 ):;issue: 004 | |
| contenttype | Fulltext |