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dc.contributor.authorKim, CW-
dc.contributor.authorHwang, W-
dc.contributor.authorPark, HC-
dc.contributor.authorHan, KS-
dc.contributor.author황운봉-
dc.date.accessioned2016-03-31T13:54:25Z-
dc.date.available2016-03-31T13:54:25Z-
dc.date.issued1997-01-
dc.identifier.citationCOMPOSITE STRUCTURES-
dc.identifier.citationv.39-
dc.identifier.citationno.3-4-
dc.identifier.citationpp.283-288-
dc.identifier.issn0263-8223-
dc.identifier.other1998-OAK-0000000178-
dc.identifier.urihttps://oasis.postech.ac.kr/handle/2014.oak/20805-
dc.description.abstractOptimum fiber orientations of laminated composite plates for the maximum strength are found under multiple inplane loading conditions. Tsai-Wu failure criterion is taken as objective function. Based on the state space method, effective optimal design formulation is developed and solution procedure is described with the emphasis on the method of calculations of the design sensitivities. Numerical results are presented for the several test problems. (C) 1998 Published by Elsevier Science Ltd. All rights reserved.-
dc.description.statementofresponsibilityX-
dc.publisherELSEVIER SCI LTD-
dc.subjectOPTIMUM DESIGN-
dc.subjectCOMPOSITE PLATES-
dc.subjectLAYER THICKNESS-
dc.subjectCRITERION-
dc.subjectANGLE-
dc.titleStacking sequence optimization of laminated plates-
dc.typeConference-
dc.contributor.college기계공학과-
dc.author.googleKim, CW-
dc.author.googleHwang, W-
dc.author.googlePark, HC-
dc.author.googleHan, KS-
dc.relation.volume39-
dc.relation.issue3-4-
dc.relation.startpage283-
dc.relation.lastpage288-
dc.contributor.id10053430-
dc.publisher.locationUK-
dc.relation.journalCOMPOSITE STRUCTURES-
dc.relation.indexSCI급, SCOPUS 등재논문-
dc.relation.sciSCIE-
dc.collections.nameConference Papers-
dc.type.docTypeProceedings Paper-

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