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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/251

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contributor.authorRay, B C-
contributor.authorBiswas, A-
contributor.authorSinha, P K-
date.accessioned2006-03-02T11:10:40Z-
date.available2006-03-02T11:10:40Z-
date.issued1989-
identifier.citationProceedings of Seminar on Science and Technology of Composites, Adhesives and Sealants, 1989, 28-30 September, Bangalore, P 321-325en
identifier.urihttp://hdl.handle.net/2080/251-
descriptionCopyright belongs to ISAMPE, HAL, The Institution of Engineers, Indiaen
description.abstractFiber-reinforced Composite laminates find wide application as aerospace structural elements. OPne of the important failure modes in the laminated composites is the interlaminar shea. The Characterisation of interlaminar shear properties of glass-epoxy specimens observations depicted by SEM fractographs are also discusseden
format.extent1486186 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherISAMPE, Indiaen
titleOn the Evaluation of Interlaminalr Shear - A Critical Design Parameteren
typeArticleen
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