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dc.contributor.authorXu, Y.G.
dc.contributor.authorWang, L.
dc.contributor.authorChen, Yong
dc.contributor.authorTiu, W.
dc.date.accessioned2013-01-29T16:58:28Z
dc.date.available2013-01-29T16:58:28Z
dc.date.issued2012
dc.identifier.citationXu , Y G , Wang , L , Chen , Y & Tiu , W 2012 , ' Load sequence effect on fatigue damage ' , Key Engineering Materials , vol. 488-489 , pp. 545-548 . https://doi.org/10.4028/www.scientific.net/KEM.488-489.545
dc.identifier.issn1013-9826
dc.identifier.otherPURE: 463189
dc.identifier.otherPURE UUID: 8b290966-ecd8-424f-b10f-3b7a0957823c
dc.identifier.otherScopus: 80053978539
dc.identifier.urihttp://hdl.handle.net/2299/9799
dc.descriptionOriginal paper can be found at: http://www.scientific.net/ Copyright Trans Tech Publications
dc.description.abstractReliable damage tolerant design of airframe structures relies on the accurate life prediction of fatigue cracks propagating from a detectable size to the critical size, which is challenging due to the complex load sequence effect under spectrum loading. This paper aims at gaining a further understanding of the complex influence of the loading history on fatigue damage through a detailed numerical simulation of the near-tip crack behaviour using the crack closure concept. The spectrum loading is broken down into a number of simple yet representative loading scenarios with overload/underload superimposed onto the baseline constant amplitude fatigue loading. Detailed finite element (FE) simulation of the plasticity-induced crack closure (PICC) has been carried out to catch the transient behaviour of PICC and link it to the fatigue damage. The load interaction effect has been analysed with the aim to identify the possible dominant loading cycle which could simplify the fatigue life prediction process in the industry. It is concluded that more reliable damage tolerant design can be achieved if the load sequence effect on fatigue damage can be taken into account more accurately for a structure under spectrum loadings.en
dc.format.extent4
dc.language.isoeng
dc.relation.ispartofKey Engineering Materials
dc.subjectcrack closure
dc.subjectfatigue damage
dc.subjectload sequence effect
dc.subjectspectrum loading
dc.titleLoad sequence effect on fatigue damageen
dc.contributor.institutionSchool of Engineering and Technology
dc.contributor.institutionScience & Technology Research Institute
dc.contributor.institutionCentre for Engineering Research
dc.contributor.institutionMaterials and Structures
dc.contributor.institutionSustainable Energy Technologies
dc.contributor.institutionAerospace
dc.description.statusPeer reviewed
dc.identifier.urlhttp://www.scopus.com/inward/record.url?scp=80053978539&partnerID=8YFLogxK
dc.relation.schoolSchool of Engineering and Technology
dcterms.dateAccepted2012
rioxxterms.versionVoR
rioxxterms.versionofrecordhttps://doi.org/10.4028/www.scientific.net/KEM.488-489.545
rioxxterms.typeJournal Article/Review
herts.preservation.rarelyaccessedtrue


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