Show simple item record

dc.contributor.authorHosseini, Mahdi
dc.contributor.authorGaff, Milan
dc.contributor.authorKonvalinka, Petr
dc.contributor.authorLi, Haitao
dc.contributor.authorMaňák, Hynek
dc.contributor.authorJoshua, Jensin
dc.contributor.authorM. R., Keerthana
dc.contributor.authorHosseini, Ahmad
dc.contributor.authorGhosh, Pritam
dc.contributor.authorHui, David
dc.date.accessioned2025-04-09T00:03:30Z
dc.date.available2025-04-09T00:03:30Z
dc.date.issued2025
dc.identifier.issn1544-0478 Sherpa/RoMEO, JCR
dc.identifier.urihttps://repozitar.mendelu.cz/xmlui/handle/20.500.12698/2054
dc.description.abstractThe study estimates the residual property of [Jute/Kevlar/Jute] and [Kevlar/Jute/Kevlar] hybrid composite laminates with multiple drilled holes. The laminates are prepared using a compression molding technique with Kevlar and Jute as reinforcements in two different stacking sequences. Post-fabrication, holes are drilled with two different center diameters 4 mm and 12 mm and multiple holes are drilled with two different effective lengths from the center hole, i.e. 2 mm and 4 mm. Compression testing is conducted using a Universal Testing Machine (UTM) to assess the compression strength of the specimens without drilled and with drilled specimens. The damage reduction factor, residual strength ratio, residual load carrying capacity and the effective stress post damage are then evaluated for the laminates with drilled holes at different effective lengths. The article is intended to suggest possible reduction in strength on introduction of natural fiber in an existing construction so that based on requirement, existing structures can be optimized. The study aims to measure the reduction in compressive residual strength due to stress concentrations introduced by drilling. Testing showed that the laminate configuration KK05 exhibited the highest residual compressive strength, retaining approximately 85% of its original strength after drilling, making it ideal for applications requiring high durability.en
dc.format2464151
dc.publisherTaylor & Francis Inc.
dc.relation.ispartofJournal of Natural Fibers
dc.relation.urihttps://doi.org/10.1080/15440478.2025.2464151
dc.rightsCC BY 4.0
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subjectKevlaren
dc.subjectJute/Epoxyen
dc.subjectdrillingen
dc.subjectcompression moldingen
dc.subjectuniversal testing machineen
dc.subjectcritical hole toleranceen
dc.subjectresidual compressive strengthen
dc.titleExperimental Study on the Residual Property of Kevlar-Jute/Epoxy Hybrid Composite Laminates with Multiple Drilled Holesen
dc.typeJ_ČLÁNEK
dc.date.updated2025-04-09T00:03:30Z
dc.description.versionOA
local.identifier.doi10.1080/15440478.2025.2464151
local.identifier.scopus2-s2.0-85218343849
local.identifier.wos001422009600001
local.number1
local.volume22
local.identifier.obd43928061
local.identifier.e-issn1544-046X
dc.identifier.orcidGaff, Milan 0000-0003-2380-328X
dc.identifier.orcidMaňák, Hynek 0000-0001-9163-7469
local.contributor.affiliationLDF


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record

CC BY 4.0
Except where otherwise noted, this item's license is described as CC BY 4.0