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Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/25467
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dc.contributor.authorGiannaros, E-
dc.contributor.authorKotzakolios, A-
dc.contributor.authorKostopoulos, V-
dc.contributor.authorSotiriadis, G-
dc.contributor.authorVignjevic, R-
dc.contributor.authorDjordjevic, N-
dc.contributor.authorBoccaccio, M-
dc.contributor.authorMeo, M-
dc.date.accessioned2022-11-08T18:52:45Z-
dc.date.available2022-11-08T18:52:45Z-
dc.date.issued2021-10-22-
dc.identifierORCiD IDs: Nenad Djordjevic: https://orcid.org/0000-0002-2729-5721; Rade Vignjevic: https://orcid.org/0000-0002-4677-068X.-
dc.identifier104058-
dc.identifier.citationGiannaros, E. et al. (2022) 'Low- and high-fidelity modeling of sandwich-structured composite response to bird strike, as tools for a digital-twin-assisted damage diagnosis', International Journal of Impact Engineering, 160, 104058, pp. 1 - 19. doi: 10.1016/j.ijimpeng.2021.104058.en_US
dc.identifier.issn0734-743X-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/25467-
dc.description.sponsorshipEU, H2020 Smart, Green and Integrated Transport, Aviation program under the acronym EXTREME (Project reference 636549).en_US
dc.format.extent1 - 19 (19)-
dc.format.mediumPrint-Electronic-
dc.languageEnglish-
dc.language.isoen_USen_US
dc.publisherElsevieren_US
dc.rightsCopyright © 2021 Elsevier Ltd. All rights reserved. This is the accepted manuscript version of an article which has been published in final form at https://doi.org/10.1016/j.ijimpeng.2021.104058, made available on this repository under a Creative Commons CC BY-NC-ND attribution licence (https://creativecommons.org/licenses/by-nc-nd/4.0/).-
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/-
dc.subjectbird strikeen_US
dc.subjectcompositesen_US
dc.subjectsandwich panelen_US
dc.subjectFEM-SPHLS-DYNAen_US
dc.subjectsoft body impacten_US
dc.subjectFBG sensorsen_US
dc.subjectdigital twinen_US
dc.titleLow- and high-fidelity modeling of sandwich-structured composite response to bird strike, as tools for a digital-twin-assisted damage diagnosisen_US
dc.typeArticleen_US
dc.identifier.doihttps://doi.org/10.1016/j.ijimpeng.2021.104058-
dc.relation.isPartOfInternational Journal of Impact Engineering-
pubs.publication-statusPublished-
pubs.volume160-
dc.identifier.eissn1879-3509-
dc.rights.holderElsevier Ltd-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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