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Investigation of fatigue crack growth after a single cycle peak overload in IS 1020 steel

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dc.contributor.author Singh, Shamsher Bahadur
dc.date.accessioned 2021-12-28T14:55:14Z
dc.date.available 2021-12-28T14:55:14Z
dc.date.issued 1992
dc.identifier.uri https://www.sciencedirect.com/science/article/abs/pii/030801619290004Y
dc.identifier.uri http://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/3939
dc.description.abstract Crack 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.iso en en_US
dc.publisher Elsiever en_US
dc.subject Civil Engineering en_US
dc.subject Fatigue crack growth en_US
dc.title Investigation of fatigue crack growth after a single cycle peak overload in IS 1020 steel en_US
dc.type Article en_US


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