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dc.contributor.authorJones, Ivor Arthur
dc.contributor.authorXu, Fei
dc.contributor.otherLi, Shuguang
dc.coverage.spatialn/aen_UK
dc.coverage.temporaln/aen_UK
dc.date.accessioned2018-08-14T16:03:09Z
dc.date.available2018-08-14T16:03:09Z
dc.date.issued2018-08-14
dc.identifier.urihttps://rdmc.nottingham.ac.uk/handle/internal/372
dc.identifier.urihttp://dx.doi.org/10.17639/nott.368
dc.descriptionRelates to a paper being submitted. The DOI will be entered when the paper has been published and a DOI assigned.en_UK
dc.description.abstractThis deposit is in two parts and contains the raw data and results for research described in the manuscript A Continuum Damage Model for Transverse Cracking in UD Composites of Linear Viscoelastic Behaviour by Fei Xu, I. Arthur Jones and Shuguang Li, submitted to Composite Structures in August 2018en_UK
dc.language.isoenen_UK
dc.publisherThe University of Nottinghamen_UK
dc.sourcen/aen_UK
dc.subject.lcshComposite materialsen_UK
dc.subject.lcshViscoelasticityen_UK
dc.subject.lcshContinuum mechanicsen_UK
dc.subject.lcshStress relaxation (Physics)en_UK
dc.subject.lcshContinuum damage mechanicsen_UK
dc.titleA continuum damage model for transverse cracking in UD composites of linear viscoelastic behaviour by Fei Xu, I. Arthur Jones and Shuguang Lien_UK
dc.subject.freeComposite materials, linear viscoelasticity, stress relaxation, ASTM D3039/D3039M – 14en_UK
dc.subject.jacsEngineering::Mechanical engineeringen_UK
dc.subject.jacsEngineering::Aerospace engineering::Aerospace engineering not elsewhere classifieden_UK
dc.subject.lcT Technology::TL Motor vehicles. Aeronautics. Astronauticsen_UK
dc.contributor.corporateASRI (Aircraft Strength Research Institute)en_UK
dc.date.collectionApril and May 2017en_UK
dc.coverage.coordinatesn/aen_UK
uon.divisionUniversity of Nottingham, UK Campus::Faculty of Engineeringen_UK
uon.funder.controlledOtheren_UK
uon.datatypeMaterials testing data and processed resultsen_UK
uon.funder.freeAVIC (Aviation Industry Corporation of China)en_UK
uon.collectionmethodStress relaxation tests according to ASTM D3039/D3039M – 14en_UK
uon.rightscontactUniversity of Nottinghamen_UK
uon.institutes-centresUniversity of Nottingham, UK Campus::Aerospace Technology, Institute foren_UK
uon.preservation.rarelyaccessedtrue


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