0000000000117936

AUTHOR

Shaoxiong Liang

showing 5 related works from this author

Quasi-static behaviour and damage assessment of flax/epoxy composites

2015

Experimental investigations were conducted on flax and E-glass fibres reinforced epoxy matrix composites subjected to quasi-static loadings. Flax/epoxy samples having [0]12, [90]12, [0/90]3S and [±45]3S stacking sequences, with a fibre volume fraction of 43% have been tested under tension, compression and in-plane shear loadings. Overall, the compression strength of glass/epoxy was 76% greater than for the flax/epoxy composite. The damage evolution of flax/epoxy of [0/90]3S and [±45]3S samples has been evaluated in terms of transverse crack densities with respect to the load increment. The crack density exhibited a classical “S” shaped pattern for [0/90]3S and linearly for [±45]3S specimens…

010302 applied physicsMatériaux [Sciences de l'ingénieur]Materials sciencePolymer-matrix compositesComposite numberMechanical properties02 engineering and technologyEpoxy matrixEpoxy021001 nanoscience & nanotechnologyE-glass fibres01 natural sciences[SPI]Engineering Sciences [physics]Compressive strengthDamage mechanicsDamage mechanicsvisual_art0103 physical sciencesVolume fractionvisual_art.visual_art_mediumFlax fibresMécanique: Mécanique des matériaux [Sciences de l'ingénieur]Composite material0210 nano-technologyQuasistatic process
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Properties evolution of flax/epoxy composites under fatigue loading

2014

International audience; The tension-tension fatigue behaviour of flax fibre reinforced epoxy matrix composites have been investigated for specimens having [0]12, [90]12, [0/90]3S and [±45]3S lay-ups. The Probabilized Stress-Number of cycles (P-S-N) curves have been determined for each laminate type. The measured stress and strain data allowed to quantify the evolution of the mechanical properties, i.e. stiffness, damping and permanent strain as a function of imposed cycles. Especially, the stiffening phenomenon of flax reinforcements oriented parallel to the loading direction has been confirmed. However, due to the competition between damage development and the fibre stiffening, the increas…

Polymer-matrix composites (PMCs)Matériaux [Sciences de l'ingénieur]Materials scienceFlax fibresPolymer–matrix composites (PMCs)FatigueDamage mechanics[ SPI.MAT ] Engineering Sciences [physics]/MaterialsModulusIndustrial and Manufacturing Engineering[SPI.MAT]Engineering Sciences [physics]/Materials[PHYS.MECA.MEMA]Physics [physics]/Mechanics [physics]/Mechanics of materials [physics.class-ph][SPI]Engineering Sciences [physics]Damage mechanicsDamage mechanics[SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]medicineGeneral Materials ScienceMécanique: Mécanique des matériaux [Sciences de l'ingénieur]Composite materialFatigueMechanical EngineeringStress–strain curveStiffnessEpoxy matrixEpoxyStiffeningMechanics of MaterialsModeling and Simulationvisual_art[ SPI.MECA.MEMA ] Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph][ PHYS.MECA.MEMA ] Physics [physics]/Mechanics [physics]/Mechanics of materials [physics.class-ph]Fatigue loadingvisual_art.visual_art_mediumFlax fibresmedicine.symptomPolymer–matrix composites (PMCs)
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Impact behaviour of flax/epoxy composite plates

2015

This paper presents an experimental investigation of the impact behaviour of flax/epoxy composite plates submitted to low-velocity transverse impact. Low energy drop-weight impact tests have been performed on two types of quasi-isotropic flax/epoxy composites, rectangularly shaped with edges lengths of 142 mm × 94 mm and 2.85 mm thick. Residual properties have been assessed by compression after impact tests. A detailed description of damage development, especially the increase of the rear face crack with respect to the impact energy is given by the microscopic observation. The influence of impact damage on the residual strength is described. A loss of 15%–30% in compression resistance was n…

Materials scienceComposite numberDamage toleranceAerospace EngineeringOcean EngineeringBendingDamage mechanicsDamage mechanicsStructural compositesMécanique: Mécanique des matériaux [Sciences de l'ingénieur]Composite materialSafety Risk Reliability and QualityImpact behaviourCivil and Structural EngineeringMécanique [Sciences de l'ingénieur]Mechanical EngineeringEpoxyCompression (physics)Flax fibreResidual strengthTransverse planeMechanics of Materialsvisual_artAutomotive Engineeringvisual_art.visual_art_mediumDamage toleranceInternational Journal of Impact Engineering
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Study of fatigue behavior of plant fiber reinforced composites : taking into account the variability of properties

2012

The present study focuses on the characterization and comparison of the quasi-static and fatigue properties of flax and glass fibre reinforced composites with an epoxy matrix. An extensive experimental campaign of fatigue tests have been performed using the measured quasi-static tension and in plane-shear properties. It appears that the static and fatigue characteristics of the glass/epoxy composites are higher than that of flax/epoxy ones with similar fibre volume fraction and lay-ups. However, due to the low density of flax reinforcements, the differences between the specific properties of the two materials are low. The measurement of the evolution of the fatigue properties has highlighte…

[SPI.OTHER]Engineering Sciences [physics]/Other[ SPI.OTHER ] Engineering Sciences [physics]/Other[SPI.OTHER] Engineering Sciences [physics]/OtherCrack densityÉléments finisFinis elementsStatiqueLinS-NDensité de fissuresDamageFlaxEndommagementStaticNatural fibresFibres naturellesFatigueMonté-CarloBio-composite
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A comparative study of fatigue behaviour of flax/epoxy and glass/epoxy composites

2012

Experimental investigations on flax and glass fabrics reinforced epoxy specimens, i.e. FFRE and GFRE, submitted to fatigue tests are presented in this paper. Samples having [0/90]3S and [±45]3S stacking sequences, with similar fibre volume fractions have been tested under tension–tension fatigue loading. The specific stress-number of cycles to failure (S–N) curves, show that for the [0/90]3S specimens, FFRE have lower fatigue endurance than GFRE, but the [±45]3S FFRE specimens offer better specific fatigue endurance than similar GFRE, in the studied life range (<2 × 10^6). Overall, the three-stage stiffness degradation is observed in all cases except for [0/90]3S FFRE specimens, which prese…

Materials scienceMatériaux [Sciences de l'ingénieur]A. Polymer–matrix composites (PMCs)[ SPI.MAT ] Engineering Sciences [physics]/MaterialsGlass epoxy[ SPI.MECA.STRU ] Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of the structures [physics.class-ph]02 engineering and technology[SPI.MAT]Engineering Sciences [physics]/Materials0203 mechanical engineeringFLAX FIBERS[SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]B. FatigueComposite materialMécanique: Mécanique des matériaux [Sciences de l'ingénieur]Mécanique: Mécanique des structures [Sciences de l'ingénieur]B. Mechanical propertiesGeneral EngineeringA. Glass fibresEpoxy021001 nanoscience & nanotechnologyStiffening020303 mechanical engineering & transportsStiffness degradationCreep[SPI.MECA.STRU]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Structural mechanics [physics.class-ph]visual_art[ CHIM.MATE ] Chemical Sciences/Material chemistry[ SPI.MECA.MEMA ] Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]Fatigue loadingCeramics and Compositesvisual_art.visual_art_mediumFlax fibres0210 nano-technologyCREEP
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