Dynamic response of polypropylene honeycomb/polystyrene foam core sandwich composite panels: Experimental and numerical analysis

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dc.authoridCaliskan, Umut/0000-0002-8043-2799
dc.authoridERDOGAN, OMER/0000-0001-7000-4283
dc.authoriddemirbas, munise didem/0000-0001-8043-6813
dc.contributor.authorCaliskan, Umut
dc.contributor.authorDemirbas, Munise Didem
dc.contributor.authorErdogan, Omer
dc.date.accessioned2024-10-04T18:49:33Z
dc.date.available2024-10-04T18:49:33Z
dc.date.issued2023
dc.departmentBayburt Üniversitesien_US
dc.description.abstractIn this study, dynamically loaded sandwich panels with two different core materials and face sheets made of aluminum alloys (6061-T6) were investigated experimentally and numerically under low-velocity impact. Polypropylene, PP (C3H6)(n) honeycomb and extruded polystyrene foam, XPS (C8H8)(n) were preferred as core material. By using the contact force and kinetic energy changes, which were the impact test results of the sandwich panels, the contact and impact resistance was examined. As a result of the tests, damaged regions and permanent central displacement were determined and energy absorption capabilities were demonstrated for two different structures. The results obtained were compared with the results obtained by the open finite element method. In this study, it was shown that the face-sheet thickness of sandwich panels was an important parameter affecting the impact behavior. The behavior of the core material when the face-sheet loses its rigidity was investigated and it was found that polystyrene foam was more effective in preventing impact damage. However, it was found that using the PP honeycomb or XPS was affected the impact behavior in different points.en_US
dc.identifier.doi10.1080/15376494.2022.2053912
dc.identifier.endpage2397en_US
dc.identifier.issn1537-6494
dc.identifier.issn1537-6532
dc.identifier.issue12en_US
dc.identifier.scopus2-s2.0-85127138389en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage2385en_US
dc.identifier.urihttps://doi.org/10.1080/15376494.2022.2053912
dc.identifier.urihttp://hdl.handle.net/20.500.12403/3206
dc.identifier.volume30en_US
dc.identifier.wosWOS:000772769100001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherTaylor & Francis Incen_US
dc.relation.ispartofMechanics of Advanced Materials and Structuresen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectPolypropylene honeycomb coreen_US
dc.subjectextruded polystyrene foam coreen_US
dc.subjectsandwich panelen_US
dc.subjectimpact behavioren_US
dc.subjectsplit Hopkinson Pressure Testen_US
dc.subjectfinite element modelen_US
dc.titleDynamic response of polypropylene honeycomb/polystyrene foam core sandwich composite panels: Experimental and numerical analysisen_US
dc.typeArticleen_US

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