Show simple item record

contributor authorVikas Kumar Saxena
contributor authorV. M. Radhakrishnan
date accessioned2017-05-08T23:59:47Z
date available2017-05-08T23:59:47Z
date copyrightJuly, 1999
date issued1999
identifier issn0094-4289
identifier otherJEMTA8-26999#393_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122236
description abstractEffect of thickness on fatigue crack growth (FCG) behavior has been investigated at varying stress ratio in a quaternary Al-Li alloy. The thickness has been observed to influence FCG behavior in two opposite ways, depending on stress ratio. The crack closure concept has been invoked to rationalize the observed behavior. The roughness-induced crack closure is the main governing mechanism in the alloy under investigation. Factors such as fracture surface asperity size and severity of plane strain condition have been argued to affect the extent of crack closure, and consequently, fatigue crack growth behavior.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Wrought Product Thickness and Stress Ratio on Fatigue Crack Growth Behavior of a Quaternary Aluminium-Lithium Alloy
typeJournal Paper
journal volume121
journal issue3
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2812392
journal fristpage393
journal lastpage398
identifier eissn1528-8889
keywordsAluminum
keywordsAlloys
keywordsStress
keywordsFatigue cracks
keywordsLithium
keywordsThickness
keywordsMechanisms
keywordsPlane strain
keywordsFracture (Process) AND Surface roughness
treeJournal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record