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contributor authorM. C. Dubourg
contributor authorB. Villechaise
date accessioned2017-05-08T23:39:40Z
date available2017-05-08T23:39:40Z
date copyrightJuly, 1992
date issued1992
identifier issn0742-4787
identifier otherJOTRE9-28497#455_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110915
description abstractThis paper analyzes the effects of multiple cracks situated in the contact zone vicinity of an elastic isotropic component, modeled as a half-plane. Friction between the crack faces is taken into account using Coulomb’s law. Straight arbitrarily oriented cracks are considered. Any contact condition can be modeled between the crack faces as well as any loading condition over the half-plane surface, including complete loading cycles. The method has been tested for up to 5 cracks and shows no limitation in crack number. Further, the method is general as no prior assumptions concerning the state of the crack, i.e., the slip-stick-open configurations along the crack are required. The stress intensity factors (SIFs) calculated for two crack configuration are compared with those obtained for single cracks.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis of Multiple Fatigue Cracks—Part I: Theory
typeJournal Paper
journal volume114
journal issue3
journal titleJournal of Tribology
identifier doi10.1115/1.2920905
journal fristpage455
journal lastpage461
identifier eissn1528-8897
keywordsFriction
keywordsCoulomb's law
keywordsStress
keywordsFracture (Materials)
keywordsCycles AND Fatigue cracks
treeJournal of Tribology:;1992:;volume( 114 ):;issue: 003
contenttypeFulltext


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