STRESS SINGULARITIES IN CRACKED COMPOSITE PLATES.

Theocaris, PS; Demakos, CB

dc.contributor.author	Theocaris, PS	en
dc.contributor.author	Demakos, CB	en
dc.date.accessioned	2014-03-01T01:06:29Z
dc.date.available	2014-03-01T01:06:29Z
dc.date.issued	1985	en
dc.identifier.issn	0376-7426	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/9414
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0021898164&partnerID=40&md5=88dba3e57077b8cebb2c426d88a0adee	en
dc.subject.classification	Mechanics	en
dc.subject.other	FRACTURE MECHANICS	en
dc.subject.other	PLATES - Crack Propagation	en
dc.subject.other	STRUCTURAL ANALYSIS	en
dc.subject.other	CRACKED COMPOSITE PLATES	en
dc.subject.other	STRESS SINGULARITIES	en
dc.subject.other	COMPOSITE STRUCTURES	en
dc.title	STRESS SINGULARITIES IN CRACKED COMPOSITE PLATES.	en
heal.type	journalArticle	en
heal.language	English	en
heal.publicationDate	1985	en
heal.abstract	The order of stress singularity in cracked biwedges met in practical problems was determined in this paper. The composite whole-plane was assumed as consisting of two dissimilar isotropic, homogeneous, and elastic wedges, perfectly bonded along their common interfaces. One of the two wedges was further assumed as containing a semi-infinite crack, which terminated at the vertex of the biwedge. The stress field at the crack tip was produced by the prescribed surface tractions at the outside boundaries of the plate. The dependence of the stress singularity on the geometry of the biwedge and the mechanical properties of the constituent phases was investigated and interesting results were derived concerning the form and the order of the stress singularity at the apex of the biwedge, where the crack also terminates.	en
heal.publisher	OXFORD UNIV PRESS	en
heal.journalName	SM archives	en
dc.identifier.isi	ISI:A1985AUA3600001	en
dc.identifier.volume	10	en
dc.identifier.issue	4	en
dc.identifier.spage	289	en
dc.identifier.epage	312	en