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dc.contributor.authorLAEUFFER, Hortense
dc.contributor.authorGUIOT, Brice
dc.contributor.authorWAHL, Jean-Christophe
dc.contributor.author
 hal.structure.identifier
LAVELLE, Florian
307314 Centre National d'Études Spatiales [Toulouse] [CNES]
dc.contributor.authorBOIS, Christophe
dc.contributor.author
 hal.structure.identifier
PERRY, Nicolas
164351 Institut de Mécanique et d'Ingénierie de Bordeaux [I2M]
dc.date.accessioned2018
dc.date.available2018
dc.date.issued2016
dc.date.submitted2018
dc.identifier.urihttp://hdl.handle.net/10985/12834
dc.description.abstractThe aim of this study is to provide a relevant description of damage growth and the resultant crack network to predict leaks in liner-less composite vessels. Tensile tests were carried out on three different laminates: [02/90n/02], [+45/-45]2s and [0/+67.5/-67.5]s. Number n varies from 1 to 3 in order to study the effect of ply thickness. Transverse crack and delamination at crack tips were identified with an optical microscope during tensile loading. A length of 100 mm was observed for several loading levels to evaluate statistical effects. Results highlight a preliminary step in the damage scenario with small crack densities before a second step where the crack growth speeds up. In bulk, cross-section examinations showed that no delamination occurred at crack tip in the material of the study (M21 T700). Cross-section examinations were also performed on [+45/-45]2s and [0/+67.5/-67.5]s layups in order to bypass the issue of free edge effects. Damage state in those layups was shown to be significantly different in the bulk than at the surface. Observations of the damage state in bulk for those layups demonstrated that there is no transverse crack in [+45/-45]2s specimens subjected to shear strains up to 4%, and that interactions between damage of consecutive plies strongly impact both the damage kinetics and the arrangement of cracks. These elements are fundamental for the assessment of permeability performance, and will be introduced in the predictive model.
dc.description.sponsorshipCo-financement CNES et Région Aquitaine
dc.language.isoen
dc.rightsPost-print
dc.subjectComposite laminate
dc.subjectDamage
dc.subjectMatrix cracking
dc.subjectMicro-delamination
dc.subjectEdge Effects
dc.subjectCrack network
dc.titleRelationship between damage and permeability in liner-less composite tanks : experimental study at the lamina level
dc.typdocCommunication avec acte
dc.localisationCentre de Bordeaux-Talence
dc.subject.halSciences de l'ingénieur: Mécanique
ensam.audienceInternationale
ensam.conference.titleEuropean Conference on Spacecraft Structures, Materials and Environmental Testing
ensam.conference.date2016-09
ensam.countryFrance
ensam.title.proceedingProceedings of the European Conference on Spacecraft Structures, Materials and Environmental Testing
ensam.page1-9
ensam.cityToulouse
ensam.peerReviewingNon
ensam.invitedCommunicationNon
ensam.proceedingOui
hal.identifierhal-01755560
hal.version1
hal.statusaccept


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