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dc.contributor.authorSeneviratne, Waruna P.
dc.contributor.authorSaseendran, Vishnu
dc.contributor.authorPerera, Shenal
dc.contributor.authorSaathoff, Brandon L.
dc.contributor.authorRubesinghe, Dhanachandra L.
dc.contributor.authorTomblin, John S.
dc.date.accessioned2020-02-20T20:43:57Z
dc.date.available2020-02-20T20:43:57Z
dc.date.issued2019-09
dc.identifier.citationSeneviratne, Waruna P.; Saseendran, Vishnu; Perera, Shenal; Saathoff, Brandon L.; Rubesinghe, Dhanachandra L.; Tomblin, John S. 2019. Numerical studies on buckling and post-buckling behavior of stiffened curved composite panel with repairs. 34th Technical Conference of the American Society for Composites, ASC 2019en_US
dc.identifier.isbn978-160595602-2
dc.identifier.urihttps://doi.org/10.12783/asc34/31330
dc.identifier.urihttp://hdl.handle.net/10057/17076
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractComposite stiffened panels are widely employed in the aircraft industry. In particular, curved panels stiffened with hat-stringers are utilized in fuselages. The panels comprise of very thin skin to which stringers are attached (co-cured/co-bonded or secondary bonded). The panels are prone to buckling phenomenon when subjected to compression, and other complex loading scenarios. The stiffened panels may be subjected damages induced by low velocity impacts, such as tool-drop. Such a scenario may yield to local reduction in the stiffness, and especially affect post-buckling response of the structure. The primary goal of this research is to develop numerical tools to study buckling and post-buckling response of stiffened composites panels containing repair. Two types of repair are considered: secondary bonded and co-bonded. It is shown that, both repair types are able to restore the panel strength, and influence the post-buckling behavior. The presented finite-element based numerical models of the repair panels are able to capture pre- and post-buckling response. The presented tool is encapsulated as a Abaqus plug-in. The presented methodology paves way.en_US
dc.description.sponsorshipKansas Aviation Research & Technology Growth Initiative program (KART) under the grant no. R51499.en_US
dc.language.isoen_USen_US
dc.publisherDEStech Publicationsen_US
dc.relation.ispartofseries34th Technical Conference of the American Society for Composites, ASC;2019
dc.subjectBucklingen_US
dc.subjectCo-bondeden_US
dc.subjectComposite repairen_US
dc.subjectCurved panelen_US
dc.subjectOmega stringeren_US
dc.subjectPost-bucklingen_US
dc.subjectSecondary-bondeden_US
dc.titleNumerical studies on buckling and post-buckling behavior of stiffened curved composite panel with repairsen_US
dc.typeConference paperen_US
dc.rights.holder© 2019 by DEStech Publications, Inc. and American Society for Composites. All rights reserveden_US


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