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dc.contributor.authorKormaníková, Eva
dc.date.accessioned2017-12-19T07:06:45Z
dc.date.available2017-12-19T07:06:45Z
dc.date.issued2017
dc.identifier.citationSborník vědeckých prací Vysoké školy báňské - Technické univerzity Ostrava. Řada stavební. 2017, roč. 17, č. 1, s. 69-72 : il.cs
dc.identifier.urihttp://hdl.handle.net/10084/122555
dc.description.abstractThe paper presents the mixed-mode delamination response of laminate plate made of two sublaminates. To this purpose a sliding load mode of delamination is proposed as failure model. A quasistatic rate-independent delamination problem of laminate plates with a finite thickness is considered. A rate-independent delamination model for a laminated Kirchhoff-Love plate is obtained. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate along the lamination front.cs
dc.format.extent225915 bytes
dc.format.mimetypeapplication/pdf
dc.languageNeuvedenocs
dc.language.isoencs
dc.publisherVysoká škola báňská - Technická univerzita Ostrava
dc.relation.ispartofseriesSborník vědeckých prací Vysoké školy báňské - Technické univerzity Ostrava. Řada stavební
dc.relation.urihttps://www.degruyter.com/downloadpdf/j/tvsb.2017.17.issue-1/tvsb-2017-0009/tvsb-2017-0009.pdf
dc.rights© Vysoká škola báňská - Technická univerzita Ostrava
dc.rights© 2017 Eva Kormaníková, published by De Gruyter Open. This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License. BY-NC-ND 3.0
dc.subjectdelaminationcs
dc.subjectsliding load modecs
dc.subjectmixed response modecs
dc.subjectlaminatecs
dc.subjectplatecs
dc.titleDelamination of composite laminate plate by sliding load modecs
dc.typearticlecs
dc.identifier.doi10.1515/tvsb-2017-0009
dc.rights.accessopenAccess


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