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dc.contributor.authorWalker, Mark
dc.contributor.authorHamilton, Ryan Jason
dc.date.accessioned2011-08-01T06:12:48Z
dc.date.available2011-08-01T06:12:48Z
dc.date.issued2005
dc.identifier.urihttp://hdl.handle.net/10321/631
dc.descriptionOriginally published in: Engineering Optimization, Vol. 37, No. 2, 2005.en_US
dc.description.abstractThis article describes a procedure to design symmetrically laminated plates for maximum buckling load with manufacturing uncertainty in the ply angle, which is the design variable. It is assumed that the probability of any tolerance value occurring within the tolerance band, compared with any other, is equal. The methodology is flexible enough to allow any appropriate problem formulation and search algorithm to be substituted. Three different tolerance scenarios are used for the purposes of illustrating the methodology, and plates with varying aspect ratios and loading ratios are optimally designed and compared.en_US
dc.format.extentpp. 135-144 (11 p.)en_US
dc.language.isoenen_US
dc.publisherTaylor & Francisen_US
dc.rightsThe electronic version of the article published in Engineering Optimization 2005, 37(2): 135-144 © 2005 copyright Taylor & Francis. Engineering Optimization available online at: http://www.tandfonline.com/loi/geno20en_US
dc.subjectStructural optimizationen_US
dc.subjectManufacturing uncertaintyen_US
dc.subjectFibre-reinforced laminatesen_US
dc.subjectBucklingen_US
dc.titleA technique for optimally designing fibre-reinforced laminated plates with manufacturing uncertainties for maximum buckling strengthen_US
dc.typeArticleen_US
dc.publisher.urihttp://dx.doi.org/10.1080/03052150412331298371en_US


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