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Differential Equations of Stiffened Panels

dc.contributor.authorRigo, Philippeen_US
dc.date.accessioned2012-06-21T21:26:30Z
dc.date.available2012-06-21T21:26:30Z
dc.date.issued2001-03-01en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/91690
dc.description.abstractThis text presents the theory used to implement in the LBR5 software an analytical solution of the stiffened panels governing equations. For that purpose, Fourier series expansions are used to solve the governing differential equations. &&In the present analysis, cylindrical shells are used as the reference panels. Stiffened plates are considered as a simplified case of the more general cylindrical shell. In the LBR-5 software, plates are analyzed as being cylindrical shells having a very large radius (q=1.0 10lo rn). &&The present method has been developed for fast and accurate linear elastic analysis of stiffened structures, particularly in regard to structural optimization.en_US
dc.publisherUniversity of Michiganen_US
dc.titleDifferential Equations of Stiffened Panelsen_US
dc.typeTechnical Reporten_US
dc.subject.hlbsecondlevelNaval Architecture and Marine Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.contributor.affiliationumDepartment of Naval Architecture and Marine Engineeringen_US
dc.contributor.affiliationotherDept. of Naval Architecture, ANAST, University of Liege, Belgiumen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/91690/1/Publication_No_348.pdf
dc.owningcollnameNaval Architecture & Marine Engineering (NA&ME)


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