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contributor authorJulian K. Benz
contributor authorJi Hyun Kim
contributor authorRonald G. Ballinger
date accessioned2017-05-09T00:37:29Z
date available2017-05-09T00:37:29Z
date copyrightOctober, 2010
date issued2010
identifier issn1528-8919
identifier otherJETPEZ-27138#102901_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143069
description abstractThe effect of oxygen partial pressure on crack growth rates in Alloy 617 has been studied using both static and fatigue loadings at 650°C over the oxygen partial pressure range 10−19−10−3 atm. Tests were conducted at either the constant stress intensity factor K for static conditions or the constant ΔK in fatigue. Oxygen concentration was measured on both the inlet and outlet of the test retort as well as in situ with a probe located directly at the specimen surface. For fatigue loading the crack path was observed to be transgranular but crystallographic with a decreasing growth rate as the oxygen concentration decreased. However, for static loading the crack path shifted to intergranular at the same Kmax (fatigue) and exhibited what appears to be an increasing crack growth rate with decreasing oxygen concentration.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Oxygen Potential on Crack Growth in Alloys for Advanced Energy Systems
typeJournal Paper
journal volume132
journal issue10
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3155793
journal fristpage102901
identifier eissn0742-4795
keywordsStress
keywordsFracture (Materials)
keywordsOxygen
keywordsIndium alloys
keywordsFatigue
keywordsFatigue cracks AND Alloys
treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 010
contenttypeFulltext


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