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dc.contributor.authorVerma, B B-
dc.contributor.authorKumar, A-
dc.contributor.authorRay, P K-
dc.identifier.citationTransaction of the Indian Institute of Metals, Vol 53, No 6, P 291-295en
dc.descriptionCopyright for this article belongs to Indian Institute of Metalsen
dc.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
dc.format.extent2715778 bytes-
dc.publisherIndian Institute of Metalsen
dc.subjectaluminium alloysen
dc.subjectcopper alloysen
dc.subjectcrack-edge stress field analysisen
dc.subjectfatigue cracksen
dc.subjectmagnesium alloysen
dc.titleFatigue crack growth delay following overloaden
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