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dc.contributor.authorGUILLAUD, Nicolas
dc.contributor.authorFROUSTEY, Catherine
dc.contributor.author
 hal.structure.identifier
VIOT, Philippe
164351 Institut de Mécanique et d'Ingénierie de Bordeaux [I2M]
dc.contributor.authorDAU, Frédéric
dc.date.accessioned2015
dc.date.available2015
dc.date.issued2014
dc.date.submitted2015
dc.identifier.issn0263-8223
dc.identifier.urihttp://hdl.handle.net/10985/10158
dc.description.abstractThis work focuses on the impact response of composite plates 5 mm thick subjected to uniaxial tension preload. Laminated carbon/epoxy with quasi-isotropic stacking sequence ([0/45/90/-45]2)S samples were used. Doehlert-type design of experiments was proposed to investigate the influence of both preload and impact energy on impact composite responses. Deformation, varying from 300 to 3000 micro-strain, was imposed thanks to a preload device designed for this purpose. Impacts were generated using a home made drop tower. Imposed impact energy was varying from 30 to 214 J. Post-impact damage was characterized by both non-destructive (ultrasound) and destructive (deply) techniques. Influence of the preloading on delamination areas (total and projected) was quantified and found sensitive to the preloading.
dc.language.isoen
dc.publisherElsevier
dc.rightsPost-print
dc.subjectCarbon fibers
dc.subjectComposites
dc.subjectLow-velocity impact
dc.subjectPreloading
dc.subjectThick plate
dc.titleImpact response of thick composite plates under uniaxial tensile preloading
ensam.embargo.terms3 Months
dc.identifier.doi10.1016/j.compstruct.2014.11.021
dc.typdocArticle dans une revue avec comité de lecture
dc.localisationCentre de Bordeaux-Talence
dc.subject.halSciences de l'ingénieur: Mécanique: Matériaux et structures en mécanique
ensam.audienceInternationale
ensam.page172-181
ensam.journalComposite Structures
ensam.volume121
hal.statusunsent


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