Levy-Type Boundary Fourier Analysis of Thick Cross-Ply Panels with Negative Gaussian Curvature

dc.contributor.authorChaudhuri, Reaz A.
dc.contributor.authorÖktem, Ahmet Sinan
dc.contributor.authorGuedes Soares, C.
dc.date.accessioned2025-10-29T11:09:25Z
dc.date.issued2015
dc.departmentFakülteler, Mühendislik Fakültesi, Makine Mühendisliği Bölümü
dc.description.abstractA boundary-discontinuous generalized double Fourier-series-based solution to the problem of deformation of a finite-dimensional general cross-ply thick, doubly curved panel with negative Gaussian curvature and of rectangular planform, modeled using a higher-order shear deformation theory, is presented. This spectral method is used to solve a system of five highly coupled, linear partial differential equations, generated by the higher-order shear deformation theory-based laminated shell analysis, with the simply supported of type 2 boundary condition prescribed on two opposite edges, whereas the remaining two edges are subjected to the simply supported of type 3 constraint. The hitherto unavailable important numerical results presented include sensitivity of the predicted response quantities of interest to shell geometry (negative or positive Gaussian curvature), lamination and thickness effects, as well as their interactions.
dc.description.sponsorshipCENTEC from the Fundacao para a Ciencia e Tecnologia (FCT)
dc.description.sponsorshipFCT [SFRH/BPD/47687/2008]
dc.description.sponsorshipFundação para a Ciência e a Tecnologia [SFRH/BPD/47687/2008] Funding Source: FCT
dc.description.sponsorshipThis research was performed during the first author's summer research contract at the Centre for Marine Technology and Engineering (CENTEC), Instituto Superior Tecnico, which was financed by CENTEC from the annual funding received from the Fundacao para a Ciencia e Tecnologia (FCT). The second author was also funded by the FCT under contract SFRH/BPD/47687/2008. The authors also gratefully acknowledge the assistance of Ozgur Kalbaran in the computation of the ANSYS results.
dc.identifier.doi10.2514/1.J053440
dc.identifier.endpage2503
dc.identifier.issn0001-1452
dc.identifier.issn1533-385X
dc.identifier.issue9
dc.identifier.orcid0000-0003-0982-1860
dc.identifier.scopus2-s2.0-84940981298
dc.identifier.scopusqualityQ1
dc.identifier.startpage2492
dc.identifier.urihttps://doi.org/10.2514/1.J053440
dc.identifier.urihttps://hdl.handle.net/20.500.14854/5820
dc.identifier.volume53
dc.identifier.wosWOS:000359983400006
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherAmer Inst Aeronautics Astronautics
dc.relation.ispartofAiaa Journal
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20251020
dc.subjectDoubly-Curved Panels
dc.subjectFrequency-Response
dc.subjectCylindrical-Shells
dc.subjectShear Deformation
dc.subjectFree-Vibration
dc.subjectPlates
dc.subjectSensitivity
dc.subjectConstraint
dc.subjectFormulation
dc.subjectLamination
dc.titleLevy-Type Boundary Fourier Analysis of Thick Cross-Ply Panels with Negative Gaussian Curvature
dc.typeArticle

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