Vis enkel innførsel

dc.contributor.authorPerillo, Giovanni
dc.contributor.authorGrytten, Frode
dc.contributor.authorSørbø, Steinar
dc.contributor.authorDelhaye, Virgile Roger
dc.date.accessioned2020-12-16T13:30:38Z
dc.date.available2020-12-16T13:30:38Z
dc.date.created2014-11-10T13:23:12Z
dc.date.issued2015
dc.identifier.citationComposites Part B: Engineering. 2015, 69 406-417.en_US
dc.identifier.issn1359-8368
dc.identifier.urihttps://hdl.handle.net/11250/2719860
dc.description.abstractImpacts on pressure vessels, produced by winding glass fibre with vinyl ester resin over a polyethylene liner, were numerically and experimentally investigated in the current work. Pressure vessels were experimentally tested under low velocity impact loads. Different locations and incident energies were tested in order to evaluate the induced damage and the capability of the developed numerical model. An advanced 3-D FE model was used for simulating the impact events. It is based on the combined use of interlaminar and intralaminar damage models. Puck and Hashin failure theories were used to evaluate the intralaminar damages (matrix cracking and fibre failure). Cohesive zone theory, by mean of cohesive elements, was used for modelling delamination onset and propagation. The experimental impact curves were accurately predicted by the numerical model for the different impact locations and energies. The overall damages, both intralaminar and interlaminar, were instead slightly over predicted for all the configurations. The model capabilities to simulate the low velocity impact events on the full scale composite structures were proved.en_US
dc.language.isoengen_US
dc.publisherElsevieren_US
dc.relation.urihttp://ac.els-cdn.com/S1359836814004867/1-s2.0-S1359836814004867-main.pdf?_tid=4ffa038a-68d4-11e4-9cde-00000aacb35f&acdnat=1415622361_a29faefe2caa0a7178cd06beaf13ba7f
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internasjonal*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/deed.no*
dc.subjectFilament windingen_US
dc.subjectMechanical testingen_US
dc.subjectFinite element analysis (FEA)en_US
dc.subjectImpact behaviouren_US
dc.titleNumerical/experimental impact events on filament wound composite pressure vesselen_US
dc.typePeer revieweden_US
dc.typeJournal articleen_US
dc.description.versionacceptedVersionen_US
dc.rights.holderThis is the accepted manuscript of the article.Published version is available at https://doi.org/10.1016/j.compositesb.2014.10.030en_US
dc.source.pagenumber406-417en_US
dc.source.volume69en_US
dc.source.journalComposites Part B: Engineeringen_US
dc.identifier.doi10.1016/j.compositesb.2014.10.030
dc.identifier.cristin1171565
dc.relation.projectNorges forskningsråd: 193238/I40en_US
cristin.unitcode7401,80,6,6
cristin.unitcode7401,80,6,4
cristin.unitnameMaterial- og konstruksjonsmekanikk
cristin.unitnamePolymerer og komposittmaterialer
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode2


Tilhørende fil(er)

Thumbnail

Denne innførselen finnes i følgende samling(er)

Vis enkel innførsel

Attribution-NonCommercial-NoDerivatives 4.0 Internasjonal
Med mindre annet er angitt, så er denne innførselen lisensiert som Attribution-NonCommercial-NoDerivatives 4.0 Internasjonal