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contributor authorH. S. Goel
contributor authorSatish Chand
date accessioned2017-05-08T23:44:26Z
date available2017-05-08T23:44:26Z
date copyrightApril, 1994
date issued1994
identifier issn0094-4289
identifier otherJEMTA8-26963#168_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113702
description abstractCrack growth rate experiments are conducted by applying an intermediate single overload cycle in constant amplitude load (CAL) tests. For a particular overload ratio, three to four tests are conducted by applying the overload cycle at different crack lengths. The loads are selected in such a way that for a given overload ratio, the size of the overload and CAL monotonic plastic zones are the same at each crack length. A functional form for the crack growth during the retardation was developed that accurately describes all the tests. For comparison, the corresponding CA-load tests are also conducted separately. Finally, a crack growth rate model is developed.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Fatigue Crack Growth Model for Single Overload Tests
typeJournal Paper
journal volume116
journal issue2
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2904268
journal fristpage168
journal lastpage172
identifier eissn1528-8889
keywordsStress
keywordsFracture (Materials)
keywordsCycles AND Fatigue cracks
treeJournal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 002
contenttypeFulltext


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