Please use this identifier to cite or link to this item: http://earsiv.odu.edu.tr:8080/xmlui/handle/11489/5311
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dc.contributor.authorOzdemir, M.-
dc.contributor.authorSadamoto, S.-
dc.contributor.authorTanaka, S.-
dc.contributor.authorOkazawa, S.-
dc.contributor.authorYu, T. T.-
dc.contributor.authorBui, T. Q.-
dc.date.accessioned2024-03-26T07:25:34Z-
dc.date.available2024-03-26T07:25:34Z-
dc.date.issued2018-
dc.identifier.citationOzdemir, M., Sadamoto, S., Tanaka, S., Okazawa, S., Yu, TT., Bui, TQ. (2018). Application of 6-DOFs meshfree modeling to linear buckling analysis of stiffened plates with curvilinear surfaces. Acta Mech., 229(12), 4995-5012. https://doi.org/10.1007/s00707-018-2275-3en_US
dc.identifier.issn0001-5970-
dc.identifier.issn1619-6937-
dc.identifier.urihttp://dx.doi.org/10.1007/s00707-018-2275-3-
dc.identifier.urihttps://www.webofscience.com/wos/woscc/full-record/WOS:000450983800017-
dc.identifier.urihttp://earsiv.odu.edu.tr:8080/xmlui/handle/11489/5311-
dc.descriptionWoS Categories: Mechanicsen_US
dc.descriptionWeb of Science Index: Science Citation Index Expanded (SCI-EXPANDED)en_US
dc.descriptionResearch Areas: Mechanicsen_US
dc.description.abstractA buckling analysis of stiffened plates including curvilinear surfaces is carried out by an effective meshfree model. The buckling loads and modes computed by the present method are analyzed. Six degrees of freedom (6-DOFs) curved shell meshfree formulation in a convected coordinate system including a drilling rotation component is employed, which enables the assembly of curved shells for the modeling of more complex structures. By this formulation, the assembly of any arbitrary shape of geometry can be modeled in convected coordinates, while the 5-DOFs shell formulation suffers from the modeling of shell assemblies. Particularly, curved shells with straight stiffeners and plates with curvilinear stiffeners are considered. Furthermore, a twisted T-shaped structure where both web and flange have curvilinear geometry is analyzed. A meshfree discretization is employed, with which the reproducing kernel particle method is used as the meshfree interpolant. A boundary singular kernel method is adopted to precisely impose an essential boundary condition and to model folded shell geometries. The accuracy and effectiveness of the proposed method are demonstrated by several shell buckling problems for stiffened plate structures with curvilinear surfaces. The obtained meshfree results are compared with the linear and quadratic shell element results of finite element method ANSYS and discussed.en_US
dc.language.isoengen_US
dc.publisherSPRINGER WIEN-WIENen_US
dc.relation.isversionof10.1007/s00707-018-2275-3en_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectSHEAR-DEFORMABLE PLATES, COMBINED BIAXIAL COMPRESSION/TENSION, CONFORMING NODAL INTEGRATION, LARGE DEFLECTION ANALYSIS, FINITE-ELEMENT, ULTIMATE STRENGTH, LATERAL PRESSURE, FREE-VIBRATION, SHELL, PANELSen_US
dc.titleApplication of 6-DOFs meshfree modeling to linear buckling analysis of stiffened plates with curvilinear surfacesen_US
dc.typearticleen_US
dc.relation.journalACTA MECHANICAen_US
dc.contributor.departmentOrdu Üniversitesien_US
dc.contributor.authorID0000-0002-6426-6639en_US
dc.contributor.authorID0000-0002-6426-6639en_US
dc.identifier.volume229en_US
dc.identifier.issue12en_US
dc.identifier.startpage4995en_US
dc.identifier.endpage5012en_US
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