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dc.contributor.authorBradshaw, Joel Clintonen_US
dc.date.accessioned2010-06-02en_US
dc.date.accessioned2014-03-14T21:36:45Z
dc.date.available2010-06-02en_US
dc.date.available2014-03-14T21:36:45Z
dc.date.issued1975-05-05en_US
dc.date.submitted2010-06-02en_US
dc.identifier.otheretd-06022010-020124en_US
dc.identifier.urihttp://hdl.handle.net/10919/42833
dc.description.abstractThe results obtained from the nonlinearly elastic, geometrically linear beam-column are almost identical to the results obtained by the method of Gurfinkel and Robinson [6] within the linear range of the stress-strain curve. When the displacements become large, the Gurfinkel and Robinson routine tends to give higher estimates of the strain state of the section being analysed as compared to the results via the finite element model. Changing the number of integration points seems to have a stronger effect on the results than refining the mesh.en_US
dc.format.mediumBTDen_US
dc.publisherVirginia Techen_US
dc.relation.haspartLD5655.V855_1975.B73.pdfen_US
dc.subjectload bearing modelsen_US
dc.subject.lccLD5655.V855 1975.B73en_US
dc.titleNonlinear analysis of plane frames.en_US
dc.typethesisen_US
dc.contributor.departmentCivil Engineeringen_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen_US
dc.contributor.committeechairHolzer, Siegfried M.en_US
dc.contributor.committeememberWalker, Richard D.en_US
dc.contributor.committeememberSomers, Arnold E. Jr.en_US
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-06022010-020124/en_US


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