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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/266

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contributor.authorVerma, B B-
contributor.authorKumar, A-
contributor.authorRay, P K-
date.accessioned2006-03-23T05:20:34Z-
date.available2006-03-23T05:20:34Z-
date.issued2000-
identifier.citationTransaction of the Indian Institute of Metals, Vol 53, No 6, P 291-295en
identifier.urihttp://hdl.handle.net/2080/266-
descriptionCopyright for this article belongs to Indian Institute of Metalsen
description.abstractFatigue crack growth retardation behaviour on application of single overload cycle in 2024-T3 aluminium-alloy sheet has been studied. It is concluded that a critical value of overloading ratio is required to develop substantial crack growth retardation. The overload induced crack tip plastic zone and crack closure level have been found to control the delay behaviour significantly. It is also found that a power relationship exists between delay cycles and retarded crack lengthen
format.extent2715778 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherIndian Institute of Metalsen
subjectaluminium alloysen
subjectcopper alloysen
subjectcrack-edge stress field analysisen
subjectfatigue cracksen
subjectmagnesium alloysen
titleFatigue crack growth delay following overloaden
typeArticleen
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