Show simple item record

contributor authorK. M. Lal
contributor authorS. B. L. Garg
contributor authorI. Le May
date accessioned2017-05-08T23:08:57Z
date available2017-05-08T23:08:57Z
date copyrightJanuary, 1980
date issued1980
identifier issn0094-4289
identifier otherJEMTA8-26874#147_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93411
description abstractA detailed analysis of crack closure during fatigue crack propagation has been made using a simplified model. In addition, experimental work has been conducted using eddy current methods to determine crack closure. It was found that the effective stress range factor, U, depends on the applied stress range, stress ratio, yield strength and strain hardening exponent of the material, and that its value stabilizes in about 10 stress cycles for constant stress amplitude loading. Experimental and predicted results were seen to be in good agreement.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn Effective Stress Range Factor in Fatigue
typeJournal Paper
journal volume102
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3224772
journal fristpage147
journal lastpage152
identifier eissn1528-8889
keywordsStress
keywordsFatigue
keywordsFracture (Materials)
keywordsCycles
keywordsFatigue cracks
keywordsWork hardening
keywordsYield strength AND Eddy currents (Electricity)
treeJournal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record