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OPTIMAL PARAMERERS FOR CURING GRAPHITE-EPOXY COMPOSITE LAMINATES

dc.citation.epage363en_US
dc.citation.issue1-4en_US
dc.citation.spage357en_US
dc.citation.volume48en_US
dc.contributor.authorKAM, TYen_US
dc.contributor.authorLAI, FMen_US
dc.contributor.authorSHER, HFen_US
dc.contributor.department交大名義發表zh_TW
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentNational Chiao Tung Universityen_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.date.accessioned2014-12-08T15:03:34Z
dc.date.available2014-12-08T15:03:34Z
dc.date.issued1995-01-15en_US
dc.description.abstractThe optimal curing parameters of a cure cycle for achieving maximum mechanical properties of Gr/ep composite laminates are determined via a multi-level optimization approach. Laminated composite specimens cured under various pressures, temperatures and times are tested with an Instron testing machine. Test results: are then used in the proposed multi-level optimization method to determine the optimal curing parameters. The effects of the curing parameters on the mechanical properties of the laminates are studied and discussed It was found that a cure cycle with two pressure-temperature-time steps can yield composite laminates with comparatively good material properties.en_US
dc.identifier.issn0924-0136en_US
dc.identifier.journalJOURNAL OF MATERIALS PROCESSING TECHNOLOGYen_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/2101
dc.identifier.wosnumberWOS:A1995QJ33500044
dc.language.isoen_USen_US
dc.titleOPTIMAL PARAMERERS FOR CURING GRAPHITE-EPOXY COMPOSITE LAMINATESen_US
dc.typeArticle; Proceedings Paperen_US

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