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dc.date.accessioned2013-03-12T08:19:19Z
dc.date.available2013-03-12T08:19:19Z
dc.date.issued2003en_US
dc.date.submitted2011-04-20en_US
dc.identifier.urihttp://hdl.handle.net/10852/10176
dc.description.abstractBuckling of stiffened plates with arbitrarily oriented stiffeners and of shells are considered. The main objective of the work, presented as a thesis for a cand. scient. degree (master equivalent) at the University of Oslo, has been to develop computational models for direct calculation of the structural response using the Rayleigh-Ritz method. The deflections are represented by trigonometric functions. All combinations of biaxial in-plane compression, tension and shear are included in the formulations. Estimation of the ultimate strength is found using the first yield as the collapse criterion. The formulations derived are implemented in a Fortran computer code. Numerical results are obtained for a variety of stiffener orientations and geometries. The results are compared to finite element analysis results and are found, in most cases, to be conservative compared to the finite element calculation results.eng
dc.language.isonoben_US
dc.publisherMatematisk Institutt, Universitetet i Oslo
dc.relation.ispartofPreprint series. Research Report in Mechanics http://urn.nb.no/URN:NBN:no-23419
dc.relation.urihttp://urn.nb.no/URN:NBN:no-23419
dc.rights© The Author(s) (2003). This material is protected by copyright law. Without explicit authorisation, reproduction is only allowed in so far as it is permitted by law or by agreement with a collecting society.
dc.titleKnekning av plater og skall i skipskonstruksjoner / Buckling of plates and shells in ship structuresen_US
dc.typeResearch reporten_US
dc.date.updated2011-04-20en_US
dc.rights.holderCopyright 2003 The Author(s)
dc.creator.authorBrubak, Larsen_US
dc.subject.nsiVDP::410en_US
dc.identifier.urnURN:NBN:no-27669en_US
dc.type.documentForskningsrapporten_US
dc.identifier.duo116680en_US
dc.identifier.fulltextFulltext https://www.duo.uio.no/bitstream/handle/10852/10176/1/mech-03-03.pdf


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