Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/22322
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dc.contributor.authorGintalas, M-
dc.contributor.authorAinsworth, RA-
dc.date.accessioned2021-02-27T16:34:01Z-
dc.date.available2021-02-27T16:34:01Z-
dc.date.issued2021-02-20-
dc.identifierORCiD: Marius Gintalas https://orcid.org/0000-0003-4596-5730-
dc.identifierORCiD: R.A. Ainsworth https://orcid.org/0000-0001-9635-461X-
dc.identifier107609-
dc.identifier.citationGintalas, M. and Ainsworth, R.A. (2021) 'A constraint correction method based on use of a single test specimen', Engineering Fracture Mechanics, 247, 107609, pp. 1 - 22. doi: 10.1016/j.engfracmech.2021.107609.en_US
dc.identifier.issn0013-7944-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/22322-
dc.description.abstractCommonly, fracture toughness tests on deeply cracked specimens are used to assess defects in large-scale components. The paper presents a method for selection of test specimen type, size and crack length in order to obtain fracture toughness estimates relevant to defects in cracked pipes. The method uses available closed-form -stress, stress intensity factor and limit load solutions to determine the required specimen dimensions. The paper reports elastic–plastic finite element analyses for single edge notched bend (SENB) and single edge notched tension (SENT) specimens and cracked pipes which demonstrate good agreement of the matching approach, although care is needed in selecting the appropriate limit load solution for SENT geometries.-
dc.format.extent1 - 22-
dc.languageEnglish-
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.rightsAttribution 4.0 International-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subjectconstrainten_US
dc.subjectfracture toughnessen_US
dc.subjectcomponent assessmenten_US
dc.titleA constraint correction method based on use of a single test specimenen_US
dc.typeArticleen_US
dc.identifier.doihttps://doi.org/10.1016/j.engfracmech.2021.107609-
dc.relation.isPartOfEngineering Fracture Mechanics-
pubs.publication-statusPublished-
pubs.volume247-
dc.identifier.eissn1873-7315-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dcterms.dateAccepted2021-02-10-
dc.rights.holderThe Authors-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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