Investigation of Penetration Behavior of Combined Geometry Shells at Quasi-Static and Intermediate Strain Rates: an Experimental and Numerical Study

dc.contributor.author Turan, Ali Kıvanç
dc.contributor.author Taşdemirci, Alper
dc.contributor.author Kara, Ali
dc.contributor.author Şahin, Selim
dc.contributor.author Güden, Mustafa
dc.date.accessioned 2022-11-17T06:52:02Z
dc.date.available 2022-11-17T06:52:02Z
dc.date.issued 2023
dc.description.abstract In this study, the penetration/perforation behavior of a core material with previously determined static and dynamic crushing characteristics was investigated both experimentally and numerically. Penetration/perforation problems occur due to shrapnel effect when sandwich structures containing energy-absorbing core materials by crushing are exposed to blast loads. The penetration behavior of combined geometry shells consisting of a hemispherical cap and a cylindrical segment was investigated experimentally using blunt, conical and hemispherical penetrator tips. The quasi-static penetration tests were performed in a universal test machine, and the intermediate strain rate penetration tests were performed in a drop weight test device. The numerical models of penetration tests were implemented in LS-DYNA at the test strain rates as well as at the higher strain rates. Results showed that different penetrator geometries induced damage forms of symmetrical tearing, petaling, plugging and inversely formed hemispherical domed cone. The increase in the thickness of core geometry resulted in a decent increase in force–displacement curves, as average of force levels increased around 140%, 200% and 220% for blunt, conical and hemispherical tip penetrators, respectively. Numerical results indicated very good correlation with experimental work and enabled to investigate effect of strain rate and micro-inertia over numerical models at elevated penetrator velocities. Penetration behavior was found to be affected from micro-inertia effects up to a threshold displacement of 4 mm for thicker and 5 mm for thinner core units and strain rate effects were found to be dominant beyond that point. en_US
dc.identifier.doi 10.1016/j.tws.2022.110261
dc.identifier.issn 0263-8231
dc.identifier.issn 0263-8231 en_US
dc.identifier.scopus 2-s2.0-85140804922
dc.identifier.uri https://doi.org/10.1016/j.tws.2022.110261
dc.identifier.uri https://hdl.handle.net/11147/12597
dc.language.iso en en_US
dc.publisher Elsevier en_US
dc.relation Patlamaya Dayanıklı Yarı Küresel Tekrarlı Çekirdek Malzemesi Ihtiva Eden Sandviç Yapıların Geliştirilmesi Ve Optimizasyonu en_US
dc.relation.ispartof Thin-Walled Structures en_US
dc.rights info:eu-repo/semantics/embargoedAccess en_US
dc.subject LSDYNA en_US
dc.subject Micro-inertia en_US
dc.subject Penetration behavior en_US
dc.subject Strain rate sensitivity en_US
dc.title Investigation of Penetration Behavior of Combined Geometry Shells at Quasi-Static and Intermediate Strain Rates: an Experimental and Numerical Study en_US
dc.type Article en_US
dspace.entity.type Publication
gdc.author.id 0000-0002-0081-9476
gdc.author.id 0000-0002-2926-0661
gdc.author.id 0000-0001-6397-8418
gdc.author.id 0000-0002-0081-9476 en_US
gdc.author.id 0000-0002-2926-0661 en_US
gdc.author.id 0000-0001-6397-8418 en_US
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gdc.coar.access embargoed access
gdc.coar.type text::journal::journal article
gdc.collaboration.industrial false
gdc.description.department İzmir Institute of Technology. Mechanical Engineering en_US
gdc.description.publicationcategory Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı en_US
gdc.description.scopusquality Q1
gdc.description.volume 182 en_US
gdc.description.wosquality Q1
gdc.identifier.openalex W4308151097
gdc.identifier.wos WOS:000880807000006
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gdc.oaire.sciencefields 0203 mechanical engineering
gdc.oaire.sciencefields 02 engineering and technology
gdc.oaire.sciencefields 0210 nano-technology
gdc.openalex.collaboration National
gdc.openalex.fwci 0.12300155
gdc.openalex.normalizedpercentile 0.31
gdc.opencitations.count 1
gdc.plumx.crossrefcites 1
gdc.plumx.mendeley 7
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