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Please use this identifier to cite or link to this item: http://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/3939
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dc.contributor.authorSingh, Shamsher Bahadur-
dc.date.accessioned2021-12-28T14:55:14Z-
dc.date.available2021-12-28T14:55:14Z-
dc.date.issued1992-
dc.identifier.urihttps://www.sciencedirect.com/science/article/abs/pii/030801619290004Y-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/3939-
dc.description.abstractCrack propagation experiments were conducted on IS 1020 steel for various overload ratios (1·2, 1·3 and 1·4). On the basis of these experiments one power law is developed to predict the crack propagation delay period. The delay period after application of a single overload was found to increase as the magnitude of the overload increased. Crack growth also decreased after the application of an overload cycle but after a certain number of cycles it tended to return to the crack propagation rate for constant amplitude loading (CAL).en_US
dc.language.isoenen_US
dc.publisherElsieveren_US
dc.subjectCivil Engineeringen_US
dc.subjectFatigue crack growthen_US
dc.titleInvestigation of fatigue crack growth after a single cycle peak overload in IS 1020 steelen_US
dc.typeArticleen_US
Appears in Collections:Department of Civil Engineering

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