Please use this identifier to cite or link to this item: https://idr.l2.nitk.ac.in/jspui/handle/123456789/8242
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dc.contributor.authorSangamesh
dc.contributor.authorRavishankar, K.S.
dc.contributor.authorKulkarni, S.M.
dc.date.accessioned2020-03-30T10:18:16Z-
dc.date.available2020-03-30T10:18:16Z-
dc.date.issued2018
dc.identifier.citationAIP Conference Proceedings, 2018, Vol.1953, , pp.-en_US
dc.identifier.urihttp://idr.nitk.ac.in/jspui/handle/123456789/8242-
dc.description.abstractImpact analysis of the composite structure is essential for many fields like automotive, aerospace and naval structure which practically difficult to characterize. In the present study impact analysis of carbon-epoxy (CE) and jute-epoxy (JE) laminates were studied for three different thicknesses. The 3D finite element model was adopted to study the impact forces experienced, energy absorption and fracture behavior of the laminated composites. These laminated composites modeled as a 3D deformable solid element and an impactor at a constant velocity were modeled as a discrete rigid element. The energy absorption and fracture behaviors for various material combinations and thickness were studied. The fracture behavior of these composite showed progressive damage with matrix failure at the initial stage followed by complete fiber breakage. � 2018 Author(s).en_US
dc.titleImpact analysis of natural fiber and synthetic fiber reinforced polymer compositeen_US
dc.typeBook chapteren_US
Appears in Collections:2. Conference Papers

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