Please use this identifier to cite or link to this item: http://10.1.7.192:80/jspui/handle/123456789/7356
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dc.contributor.authorChauhan, Mihir-
dc.contributor.authorSharma, Dharmendra-
dc.contributor.authorDave, Jatin-
dc.date.accessioned2017-01-27T07:37:29Z-
dc.date.available2017-01-27T07:37:29Z-
dc.date.issued2012-12-10-
dc.identifier.citationInternational Congress on Computational Mechanics and Simulation (ICCMS), IIT Hyderabad, December 9 - 12, 2012, Page No. 1 - 9en_US
dc.identifier.urihttp://hdl.handle.net/123456789/7356-
dc.description.abstractIn this paper, the failure strength of an orthotropic lamina with different shaped cutouts is presented for inplane loading. The failure strength of laminate is determined on first ply failure basis by various failure criteria like Hashin – von-Mises, Tsai – Hill, Hashin – Rotem, Tsai – Wu etc. Effect of various parameters like cutout shape, material properties, fiber angle, angle of loading etc. on the failure strength is studied and presented.en_US
dc.relation.ispartofseriesITFME025-5;-
dc.subjectMechanical Faculty Paperen_US
dc.subjectFaculty Paperen_US
dc.subjectITFME025en_US
dc.subjectITFME023en_US
dc.titleFailure Strength of Orthotropic Lamina with Various Shaped Cutoutsen_US
dc.typeFaculty Papersen_US
Appears in Collections:Faculty Paper, ME

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