Vibroacoustics of 2D gradient auxetic hexagonal honeycomb sandwich panels

dc.contributor.authorMazloomi, Mohammad Sadegh
dc.contributor.authorRanjbar, Mostafa
dc.contributor.authorBoldrin, Luca
dc.contributor.authorScarpa, Fabrizio
dc.contributor.authorPatsias, Sophoclis
dc.contributor.authorOzada, Neriman
dc.date.accessioned2026-02-06T18:37:32Z
dc.date.issued2018
dc.departmentDoğu Akdeniz Üniversitesi
dc.description.abstractThis paper describes the vibroacoustic behavior of sandwich panels with a novel core topology made from 2-dimensionally gradient auxetic hexagonal honeycombs. The 2D gradient core enables a tailoring of localized mechanical properties of the sandwich structure in different regions of the panel. A homogenized finite element modeling has been used to initially determine the mechanical properties of the structures. The natural frequencies and the radiated sound power level of the sandwich plate with the homogenized properties have been calculated and verified with those obtained from a full-scale detailed model of the sandwich structure. The geometry of the 2-dimensionally gradient auxetic core has been then optimized using two different techniques in order to minimize the radiated sound power level over the frequency range of 0 to 200 Hz. The optimized design of the 2-D gradient core shows a remarkable reduction of the radiated sound power level for the sandwich structure when taking into account the mass of the panels. The results of this study provide new insights about the vibroacoustic behavior of hexagonal auxetic sandwich structures with complex core geometry.
dc.description.sponsorshipRolls-Royce plc through the Composites University Technology Centre (UTC) at the University of Bristol, UK; Rolls-Royce plc and Technology Strategy Board (TSB)
dc.description.sponsorshipThe authors would like to acknowledge Rolls-Royce plc for the support of this work through the Composites University Technology Centre (UTC) at the University of Bristol, UK. Special acknowledgements go also to the Strategic Investment in Low carbon Engine Technology (SILOET) programme supported by Rolls-Royce plc and Technology Strategy Board (TSB).
dc.identifier.doi10.1016/j.compstruct.2017.10.077
dc.identifier.endpage603
dc.identifier.issn0263-8223
dc.identifier.issn1879-1085
dc.identifier.orcid0000-0002-9670-7371
dc.identifier.orcid0000-0002-5470-4834
dc.identifier.scopus2-s2.0-85041382141
dc.identifier.scopusqualityQ1
dc.identifier.startpage593
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2017.10.077
dc.identifier.urihttps://hdl.handle.net/11129/12521
dc.identifier.volume187
dc.identifier.wosWOS:000424749400050
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherElsevier Sci Ltd
dc.relation.ispartofComposite Structures
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WoS_20260204
dc.subjectAuxetic
dc.subjectHexagonal
dc.subject2-D gradient
dc.subjectSandwich panel
dc.subjectVibroacoustic
dc.subjectOptimization
dc.subjectGenetic algorithm
dc.subjectMMA
dc.titleVibroacoustics of 2D gradient auxetic hexagonal honeycomb sandwich panels
dc.typeArticle

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