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1、【设备动力工程师,国电联合动力技术有限公司】前程无忧官方招聘网站Thispaperdetailstheconceptualdesignoptimisationoftheconfigurationandcompositelay-upsusedtoreplacetheconventionalhoneycombstiffenedstructureofaKruegerflap.Themultiplecompositelaminatesselectedforredesigningthelay-upswithinaninitialsymmetricalq
2、uasi-isotropicplyconfigurationof[0/45/?45/90]s,hadtodemonstratefullorthotropiccharacteristics.Inordertoconstructanumericalprocesstooptimisetherequiredmulti-layeredcompositeshells,acommercialfiniteelementcode,Ansys,wasusedtodevelopaparametricanalysisfile.Thisanalysissubrouti
3、newasthenintegratedintoanAnsysParametricDesignLanguagecodeembeddingtheobjectiveoftheoptimisationprocess––massminimisation––aswellasalltheconstraintsandtheallowabledomainsoftheparameters.Thepaper,initsconclusion,presentsacomparisonbetweentheoriginalproductandtheoptimaldesign
4、,andreviewstheadvantagesofthefutureimplementationofthisdesign.175UsingmulticriterionoptimizationforstrengthdesignofcompositelaminatesOriginalResearchArticleCompositeStructures,Volume62,Issues3-4,2003,Pages329-333PetriKere,MikkoLyly,JuhaniKoskiClosepreview
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7、latedreferenceworkarticlesAbstractAbstract
8、Figures/TablesFigures/Tables
9、ReferencesReferencesAbstractUsingmulticriterionoptimizationmethodsforweightminimizationoffailurestrengthcontrolledcompositestructuresisdescribed.Acompositelay-updesignproblemforminimizingthenumberoflaye
10、rsunderstrengthconstraintswithrespecttomultipleloadingconditionsisformulated.Theconstrainedproblemistransferredintoasequenceofunconstrainedproblemsandsolvedwithaninteractivedescentmethod.Atypicaldesigncyclethatcomprisesthefiniteelementmeshgeneratorandsolveraswellasthelamina
11、teanalysisandoptimizationmodulesisillustratedwithanumericalexample.ArticleOutline1.Introduction2.Thestructuraloptimizationproblem3.Structuralanalysiswiththeshellmodel4.Solvingthemulticriterionoptimizationproblem5.Numericalexample6.ConclusionsAcknowledgementsReferencesPurcha
12、se176Asimplifiedapproachtocontinuousdamageofcompositematerialsandmicromechanicalan