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dc.contributor.authorLee, CRen_US
dc.contributor.authorKam, TYen_US
dc.date.accessioned2014-12-08T15:24:43Z-
dc.date.available2014-12-08T15:24:43Z-
dc.date.issued2006en_US
dc.identifier.isbn0-7354-0312-0en_US
dc.identifier.issn0094-243Xen_US
dc.identifier.urihttp://hdl.handle.net/11536/17164-
dc.description.abstractThis paper presents a method for nondestructively evaluating the system parameters of elastically restrained shear deformable laminated composite plates using measured natural frequencies. The proposed method is established on the basis of a multi-start global minimization method in which an objective function measuring the differences between the predicted and measured natural frequencies is constructed and a design variables normalization technique for expediting the convergence of the search of the solution is adopted. Vibration testing of several laminated composite plates with different boundary conditions was performed. Seven natural frequencies extracted from the vibration data of each of the plates were used in the proposed method to identify the system parameters of the plate. Excellent results have been obtained for the plates.en_US
dc.language.isoen_USen_US
dc.subjectidentificationen_US
dc.subjectcompositesen_US
dc.subjectvibrationen_US
dc.titleMaterial characterization of flexibly supported shear deformable laminated composite platesen_US
dc.typeProceedings Paperen_US
dc.identifier.journalReview of Progress in Quantitative Nondestructive Evaluation, Vols 25A and 25Ben_US
dc.citation.volume820en_US
dc.citation.spage1027en_US
dc.citation.epage1034en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000236275600132-
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