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dc.contributor.authorLiu, J.
dc.contributor.authorChen, Wensu
dc.contributor.authorHao, Hong
dc.contributor.authorWang, Z.
dc.date.accessioned2023-04-21T14:25:08Z
dc.date.available2023-04-21T14:25:08Z
dc.date.issued2019
dc.identifier.citationLiu, J. and Chen, W. and Hao, H. and Wang, Z. 2019. Numerical study of low-speed impact response of sandwich panel with tube filled honeycomb core. Composite Structures. 220: pp. 736-748.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/91682
dc.identifier.doi10.1016/j.compstruct.2019.04.023
dc.description.abstract

© 2019 Elsevier Ltd Sandwich panel with Honeycomb Filled with Circular Tubes (HFCT) as core is numerically investigated by using ABAQUS/Explicit in this study. To calibrate the numerical model, the panels equipped with conventional hexagon honeycomb cores are modeled. Good agreement between numerical and experimental results is achieved. The sandwich panels with HFCT are compared with the sandwich panels with Honeycomb and Multi-tube cores of identical mass subjected to vertical and oblique impacts. The maximum displacement of face-sheets, plastic energy absorption, boundary reaction forces and impact load time history are calculated to assess the impact resistant capacity. The panel with HFCT core has smaller rear face-sheet displacement and higher energy absorption capacity as compared to the panels with the Multi-tube and Honeycomb core. Under oblique impact, both HFCT and Multi-tube panels have superior impact resistant capacity than the Honeycomb panel. In addition, the impact resistances of four types of multi-arc tube filled Honeycomb (HFMT) are also analysed. Their performances under vertical and oblique impacts are compared with those of HFCT.

dc.languageEnglish
dc.publisherELSEVIER SCI LTD
dc.relation.sponsoredbyhttp://purl.org/au-research/grants/arc/DE160101116
dc.subjectScience & Technology
dc.subjectTechnology
dc.subjectMechanics
dc.subjectMaterials Science, Composites
dc.subjectMaterials Science
dc.subjectSandwich panel
dc.subjectFilled honeycomb
dc.subjectInteraction
dc.subjectOblique impact
dc.subjectFinite element analysis
dc.subjectSTRUCTURAL INSULATED PANEL
dc.subjectMECHANICAL PERFORMANCE
dc.subjectBENDING BEHAVIOR
dc.subjectBLAST-RESISTANCE
dc.subjectALUMINUM TUBES
dc.subjectPART 2
dc.subjectSIMULATION
dc.subjectCOMPRESSION
dc.subjectLIGHTWEIGHT
dc.subjectSTRENGTH
dc.titleNumerical study of low-speed impact response of sandwich panel with tube filled honeycomb core
dc.typeJournal Article
dcterms.source.volume220
dcterms.source.startPage736
dcterms.source.endPage748
dcterms.source.issn0263-8223
dcterms.source.titleComposite Structures
dc.date.updated2023-04-21T14:25:05Z
curtin.departmentSchool of Civil and Mechanical Engineering
curtin.accessStatusFulltext not available
curtin.facultyFaculty of Science and Engineering
curtin.contributor.orcidHao, Hong [0000-0001-7509-8653]
curtin.contributor.orcidChen, Wensu [0000-0001-9933-8156]
curtin.contributor.researcheridHao, Hong [D-6540-2013]
dcterms.source.eissn1879-1085
curtin.contributor.scopusauthoridHao, Hong [7101908489]
curtin.contributor.scopusauthoridChen, Wensu [54880322000]
curtin.repositoryagreementV3


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