Fatigue crack growth delay following overload

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

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DC Field	Value	Language
dc.contributor.author	Verma, B B	-
dc.contributor.author	Kumar, A	-
dc.contributor.author	Ray, P K	-
dc.date.accessioned	2006-03-23T05:20:34Z	-
dc.date.available	2006-03-23T05:20:34Z	-
dc.date.issued	2000	-
dc.identifier.citation	Transaction of the Indian Institute of Metals, Vol 53, No 6, P 291-295	en
dc.identifier.uri	http://hdl.handle.net/2080/266	-
dc.description	Copyright for this article belongs to Indian Institute of Metals	en
dc.description.abstract	Fatigue 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 length	en
dc.format.extent	2715778 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	Indian Institute of Metals	en
dc.subject	aluminium alloys	en
dc.subject	copper alloys	en
dc.subject	crack-edge stress field analysis	en
dc.subject	fatigue cracks	en
dc.subject	magnesium alloys	en
dc.title	Fatigue crack growth delay following overload	en
dc.type	Article	en
Appears in Collections:	Journal Articles

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