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contributor authorA. G. Pickett
date accessioned2017-05-09T00:09:35Z
date available2017-05-09T00:09:35Z
date copyrightNovember, 1968
date issued1968
identifier issn1087-1357
identifier otherJMSEFK-27529#620_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128033
description abstractA modification of the notch stress procedure for fatigue-life analysis is presented. The importance of considering the mechanics of the specimen and the effects of the notch on specimen mechanics is illustrated by example. The procedure is applied to correlate the results of small specimen tests with large weld defect specimen tests. The significance of crack-initiation life and crack-propagation life and the dependence of these portions of total fatigue life on specimen geometry and loading is developed.
publisherThe American Society of Mechanical Engineers (ASME)
titlePrediction of Low-Cycle Fatigue Life of Specimens With Fabrication Flaws
typeJournal Paper
journal volume90
journal issue4
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3604698
journal fristpage620
journal lastpage626
identifier eissn1528-8935
keywordsManufacturing
keywordsStress
keywordsFracture (Materials)
keywordsCrack propagation
keywordsFatigue life
keywordsGeometry AND Low cycle fatigue
treeJournal of Manufacturing Science and Engineering:;1968:;volume( 090 ):;issue: 004
contenttypeFulltext


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