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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/754

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contributor.authorMohanty, J R-
contributor.authorVerma, B B-
contributor.authorRay, P K-
date.accessioned2008-12-02T07:32:20Z-
date.available2008-12-02T07:32:20Z-
date.issued2009-
identifier.citationInternational Journal of Fatigue, Vol 31, Iss 3, P 418-424en
identifier.urihttp://dx.doi.org/10.1016/j.ijfatigue.2008.07.015-
identifier.urihttp://hdl.handle.net/2080/754-
descriptionCopyright for the paper belongs to Elsevieren
description.abstractIn the present investigation an attempt has been made to introduce a life prediction methodology by adopting an ‘Exponential Model’ that can be used without integration of fatigue crack growth rate curve. The predicted results are compared with experimental crack growth data obtained for 7020-T7 and 2024-T3 aluminum alloy specimens under constant amplitude loading. It is observed that the results obtained from this model are in good agreement with experimental data and cover both stage-II and stage-III of fatigue crack growth curve.en
format.extent279741 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherElsevieren
subjectCrack driving forcesen
subjectConstant amplitude loadingen
subjectExponential modelen
subjectFatigue crack growth rateen
titlePrediction of fatigue crack growth and residual life using an exponential model: Part I (constant amplitude loading)en
typeArticleen
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