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contributor authorJ. M. Barsom
date accessioned2017-05-09T01:03:38Z
date available2017-05-09T01:03:38Z
date copyrightNovember, 1971
date issued1971
identifier issn1087-1357
identifier otherJMSEFK-27566#1190_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153455
description abstractThe 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleFatigue-Crack Propagation in Steels of Various Yield Strengths
typeJournal Paper
journal volume93
journal issue4
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3428061
journal fristpage1190
journal lastpage1196
identifier eissn1528-8935
keywordsSteel
keywordsFatigue cracks
keywordsFracture (Materials)
keywordsFatigue
keywordsFerrites (Magnetic materials)
keywordsMartensitic steel
keywordsCycles
keywordsStress
keywordsStructural steel
keywordsService life (Equipment)
keywordsTemperature
keywordsInspection
keywordsDisplacement
keywordsEquations
keywordsCrack propagation
keywordsWedges AND Yield strength
treeJournal of Manufacturing Science and Engineering:;1971:;volume( 093 ):;issue: 004
contenttypeFulltext


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