Prediction of fatigue crack growth and residual life using an exponential model: Part I (constant amplitude loading)

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

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DC Field	Value	Language
dc.contributor.author	Mohanty, J R	-
dc.contributor.author	Verma, B B	-
dc.contributor.author	Ray, P K	-
dc.date.accessioned	2008-12-02T07:32:20Z	-
dc.date.available	2008-12-02T07:32:20Z	-
dc.date.issued	2009	-
dc.identifier.citation	International Journal of Fatigue, Vol 31, Iss 3, P 418-424	en
dc.identifier.uri	http://dx.doi.org/10.1016/j.ijfatigue.2008.07.015	-
dc.identifier.uri	http://hdl.handle.net/2080/754	-
dc.description	Copyright for the paper belongs to Elsevier	en
dc.description.abstract	In 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
dc.format.extent	279741 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	Elsevier	en
dc.subject	Crack driving forces	en
dc.subject	Constant amplitude loading	en
dc.subject	Exponential model	en
dc.subject	Fatigue crack growth rate	en
dc.title	Prediction of fatigue crack growth and residual life using an exponential model: Part I (constant amplitude loading)	en
dc.type	Article	en
Appears in Collections:	Journal Articles

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