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contributor authorK. M. Nikbin
contributor authorD. J. Smith
contributor authorG. A. Webster
date accessioned2017-05-08T23:22:39Z
date available2017-05-08T23:22:39Z
date copyrightApril, 1986
date issued1986
identifier issn0094-4289
identifier otherJEMTA8-26909#186_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101250
description abstractThis paper is concerned with assessing the integrity of cracked engineering components which operate at elevated temperatures. Fracture mechanics parameters are discussed for describing creep crack growth. A model is presented for expressing growth rate in terms of creep damage accumulation in a process zone ahead of the crack tip. Correlations are made with a broad range of materials exhibiting a wide spread of creep ductilities. It is found that individual propagation rates can be predicted with reasonable accuracy from a knowledge only of the material uni-axial creep ductility. An engineering creep crack growth assessment diagram is proposed which is independent of material properties but which is sensitive to the state of stress at the crack tip. Approximate bounds are presented for plane stress and plane strain situations and it is shown that crack growth rates about fifty times faster are expected under plane strain conditions than when plane stress prevails.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Engineering Approach to the Prediction of Creep Crack Growth
typeJournal Paper
journal volume108
journal issue2
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3225859
journal fristpage186
journal lastpage191
identifier eissn1528-8889
keywordsCreep
keywordsFracture (Materials)
keywordsStress
keywordsPlane strain
keywordsMaterials properties
keywordsDuctility
keywordsFracture mechanics AND Temperature
treeJournal of Engineering Materials and Technology:;1986:;volume( 108 ):;issue: 002
contenttypeFulltext


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