BUCKLING OF SHEAR DEFORMABLE LAMINATED COMPOSITE PLATES

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	KAM, TY	en_US
dc.contributor.author	CHANG, RR	en_US
dc.date.accessioned	2014-12-08T15:05:02Z	-
dc.date.available	2014-12-08T15:05:02Z	-
dc.date.issued	1992	en_US
dc.identifier.issn	0263-8223	en_US
dc.identifier.uri	http://hdl.handle.net/11536/3572	-
dc.description.abstract	A shear deformable finite element is developed for the buckling analysis of laminated composite plates. The finite element formulation is based on Mindlin's theory in which shear correction factors are derived from the exact expressions for orthotropic materials. A variety of problems on uniaxial and shear bucklings of laminated composite plates are solved. The effects of material properties, plate aspect ratio, length-to-thickness ratio, number of layers and lamination angle on the buckling loads of symmetrically and anti-symmetrically laminated composite plates are investigated. Optimal lamination arrangements of layers for maximizing the buckling loads of the plates are determined.	en_US
dc.language.iso	en_US	en_US
dc.title	BUCKLING OF SHEAR DEFORMABLE LAMINATED COMPOSITE PLATES	en_US
dc.type	Article	en_US
dc.identifier.journal	COMPOSITE STRUCTURES	en_US
dc.citation.volume	22	en_US
dc.citation.issue	4	en_US
dc.citation.spage	223	en_US
dc.citation.epage	234	en_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.department	National Chiao Tung University	en_US
dc.contributor.department	Department of Mechanical Engineering	en_US
dc.identifier.wosnumber	WOS:A1992JW77800006	-
dc.citation.woscount	22	-
顯示於類別：	期刊論文