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contributor authorJ. J. McGowan
contributor authorH. W. Liu
date accessioned2017-05-08T23:08:49Z
date available2017-05-08T23:08:49Z
date copyrightOctober, 1980
date issued1980
identifier issn0094-4289
identifier otherJEMTA8-26879#341_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93348
description abstractAn accurate knowledge of the dependence of the fatigue crack growth rate (da/dN) on the stress intensity factor range (ΔK) is necessary to perform a safety analysis of any structure. Fatigue crack growth tests are normally performed on simple, two-dimensional finite thickness specimens to determine this dependence. Certain anomalies in this dependence have been observed when specimen thickness and mean stress have been varied. The thickness effect and the mean stress effect on the fatigue crack growth rate are related to the variation in crack closure and the local stress intensity factor along the crack front. A simple model incorporating both of these two effects is proposed. The model is applied to fatigue crack growth data for a nickel-base super alloy (IN-100) with very good success.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Role of Three-Dimensional Effects in Constant Amplitude Fatigue Crack Growth Testing
typeJournal Paper
journal volume102
journal issue4
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3224821
journal fristpage341
journal lastpage346
identifier eissn1528-8889
keywordsTesting
keywordsFatigue cracks
keywordsStress
keywordsThickness
keywordsFracture (Materials)
keywordsNickel
keywordsAlloys AND Safety
treeJournal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 004
contenttypeFulltext


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