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Optimal design of fibre-reinforced laminated plates accounting for manufacturing uncertainty

dc.contributor.authorWalker, Marken_US
dc.date.accessioned2011-08-01T08:12:04Z
dc.date.available2011-08-01T08:12:04Z
dc.date.issued2005
dc.descriptionOriginally published in: International journal of mechanics and materials in design, Vol. 2, No. 3-4, 2005.en_US
dc.description.abstractA procedure to design symmetrically laminated plates under buckling loads for minimum weight with manufacturing uncertainty (tolerance) in the ply angle and plate thickness, which are the design variables, is described. A minimum buckling load capacity is the design constraint implemented. It is assumed that the probability of any tolerance value occurring within the tolerance band, compared with any other, is equal, and thus the approach is a worst case scenario approach. The effects of bending–twisting coupling are neglected in implementing the procedure, and the Downhill Simplex method is used as the search technique, but the methodology is flexible and allows any appropriate problem formulation and search algorithm to be substituted. Two 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. The results demonstrate the importance of carrying out design optimisation of composite structures with the effects of manufacturing tolerances included.en_US
dc.format.extentpp. 147–155 (9 p.)en_US
dc.identifier.doihttps://doi.org/10.1007/s10999-006-0002-z
dc.identifier.urihttp://hdl.handle.net/10321/651
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.publisher.urihttp://www.springerlink.com/content/g6g74t1u24815808/fulltext.pdfen_US
dc.rightsThe electronic version of the article published in International Journal of Mechanics and Materials in Design 2005, 2(3-4): 1-9 © 2005 copyright Springer. International Journal of Mechanics and Materials in Design available online at: http://www.springerlink.com/content/g6g74t1u24815808/en_US
dc.subjectBuckling loadsen_US
dc.subjectCompositesen_US
dc.subjectMinimum weighten_US
dc.subjectOptimal design techniqueen_US
dc.subjectTolerancesen_US
dc.titleOptimal design of fibre-reinforced laminated plates accounting for manufacturing uncertaintyen_US
dc.typeArticleen_US

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