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contributor authorG. R. Yoder
contributor authorL. A. Cooley
contributor authorT. W. Crooker
date accessioned2017-05-08T23:06:55Z
date available2017-05-08T23:06:55Z
date copyrightJanuary, 1979
date issued1979
identifier issn0094-4289
identifier otherJEMTA8-26867#86_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92243
description abstractFatigue crack growth rates (da/dN) in ambient laboratory air have been determined for a wide variety of materials from four basic α + β titanium alloy systems. Each material was cyclically loaded with a haversine waveform and a load ratio, R = 0.10. The results indicate that, at a constant value of stress-intensity range (ΔK), the width of the da/dN data band exceeds an order of magnitude. For example, at ΔK = 21 MPa·m1/2 , a 50-fold difference in fatigue crack propagation rates is observed. Analysis of the crack growth rate data at this point indicates a systematic dependence on grain size (l ), viz. that da/dN decreases with increasing l . An interpretation of this effect is offered in terms of reversed (cyclic) plastic zone size considerations.
publisherThe American Society of Mechanical Engineers (ASME)
title50-Fold Difference in Region-II Fatigue Crack Propagation Resistance of Titanium Alloys: A Grain-Size Effect
typeJournal Paper
journal volume101
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3443656
journal fristpage86
journal lastpage90
identifier eissn1528-8889
keywordsElectrical resistance
keywordsTitanium alloys
keywordsFatigue cracks
keywordsGrain size
keywordsStress AND Fracture (Materials)
treeJournal of Engineering Materials and Technology:;1979:;volume( 101 ):;issue: 001
contenttypeFulltext


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