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

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.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.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.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

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