Cutout shape and size effects on response of quasi-isotropic composite laminate under uni-axial compression

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DC Field	Value	Language
dc.contributor.author	Singh, Shamsher Bahadur	-
dc.date.accessioned	2021-12-07T05:14:25Z	-
dc.date.available	2021-12-07T05:14:25Z	-
dc.date.issued	2010-06	-
dc.identifier.uri	http://www.techno-press.org/content/?page=article&journal=sem&volume=35&num=3&ordernum=5	-
dc.identifier.uri	http://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/3865	-
dc.description.abstract	Cutouts are often provided in structural and aircraft components for ventilation, for access, inspection, electric lines and fuel lines or sometimes to lighten the structure. This paper addresses the effects of cutout shape (i.e., circular, square, diamond, elliptical-vertical and elliptical-horizontal) and size on buckling and postbuckling response of quasi-isotropic (i.e., (+45/−45/0/90)2s) composite laminate under uni-axial compression. The finite element method is used to carry out the investigation. The formulation is based on first order shear deformation theory and von Karman	en_US
dc.language.iso	en	en_US
dc.publisher	Techno Press	en_US
dc.subject	Civil Engineering	en_US
dc.subject	Buckling	en_US
dc.subject	Composite laminates	en_US
dc.subject	Postbuckling	en_US
dc.title	Cutout shape and size effects on response of quasi-isotropic composite laminate under uni-axial compression	en_US
dc.type	Article	en_US
Appears in Collections:	Department of Civil Engineering

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