The effect of the orientation of a crack on the critical buckling load in a hybrid composite

dc.contributor.author	Hamani, N
dc.contributor.author	Ouinas, D
dc.date.accessioned	2022-05-30T09:45:56Z
dc.date.available	2022-05-30T09:45:56Z
dc.date.issued	2015-11-26
dc.identifier.uri	http://depot.umc.edu.dz/handle/123456789/12208
dc.description.abstract	In this work an analysis of buckling was carried out on rectangular plates hybrid composites with and without circular notch using the finite element method. The buckling strength of the laminated plate subjected to the uniaxial compression is highlighted according to the orientations of the fibers. The results show that increasing the thickness of the aluminum layer significantly improves the resistance to buckling. Whatever the orientation of the crack the critical buckling load remains stable
dc.language.iso	en
dc.publisher	Université Frères Mentouri - Constantine 1
dc.subject	buckling
dc.subject	hybrid composites
dc.subject	finite element analysis
dc.subject	crack
dc.title	The effect of the orientation of a crack on the critical buckling load in a hybrid composite
dc.type	Article