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dc.relation.isnodouble29bd3bbc-5b4c-4407-90d1-106224a2f0ca*
dc.contributor.authorPANETTIERI, Enrico
IDREF: 228223156
dc.contributor.authorFANTERIA, Daniele
dc.contributor.authorMONTEMURRO, Marco
IDREF: 171660978
dc.contributor.authorFROUSTEY, Catherine
dc.date.accessioned2021-05-14T09:52:20Z
dc.date.available2021-05-14T09:52:20Z
dc.date.issued2016
dc.identifier.issn1359-8368
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/77440
dc.description.abstractEnLow-velocity impacts (LVI) on composite laminates pose significant safety issues since they are able to generate extended damage within the structure, mostly delaminations and matrix cracking, while being hardly detectable in visual inspections. The role of LVI tests at the coupon level is to evaluate quantities that can be useful both in the design process, such as the delamination threshold load, and in dealing with safety issues, that is correlating the internal damage with the indentation depth. This paper aims at providing a benchmark of LVIs on quasi-isotropic carbon/epoxy laminates; 2 laminates are tested, 16 and 24 plies and a total of 8 impact energies have been selected ranging from very low energy impacts up to around 30 J. Delamination threshold loads, shape and extension of délaminations as well as post-impact 3D measurements of the impacted surface have been carried out in order to characterize the behavior of the considered material system in LVIs.The analysis of test results relevant to the lowest energies pointed out that large contact force fluctuations, typically associated to delamination onset, occurred but ultrasonic scans did not reveal any significant internal damage. Due to these unexpected results, such tests were further investigated through a detailed FE model. The results of this investigation highlights the detrimental effects of the dissipative mechanisms of the impactor. A combined numericale-experimental approach is thus proposed to evaluate the effective impact energies.
dc.language.isoen
dc.publisherElsevier
dc.subject.enPMCs
dc.subject.enImpact
dc.subject.enDelamination
dc.subject.enUltrasonics
dc.subject.enPost-impact indentation depth
dc.title.enLow-velocity impact tests on carbon/epoxy composite laminates: A benchmark study
dc.typeArticle de revue
dc.identifier.doi10.1016/j.compositesb.2016.09.057
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]/Mécanique des matériaux [physics.class-ph]
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]/Mécanique des solides [physics.class-ph]
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]/Mécanique des structures [physics.class-ph]
bordeaux.journalComposites Part B: Engineering
bordeaux.page9-21
bordeaux.volume107
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295*
bordeaux.institutionUniversité de Bordeaux
bordeaux.institutionBordeaux INP
bordeaux.institutionCNRS
bordeaux.institutionINRAE
bordeaux.institutionArts et Métiers
bordeaux.peerReviewedoui
hal.identifierhal-01409242
hal.version1
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-01409242v1
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