Search results for " Laminates"

showing 10 items of 65 documents

Effects of Nylon 6,6 Nanofibrous Mats on Thermal Properties and Delamination Behavior of High Performance CFRP Laminates

2014

none 8 no Nylon 6,6 electrospun nanofibrous membranes interleaved in Carbon Fibre Reinforced Plastic (CFRP) laminates have been proposed as a means to provide a higher threshold value to delamination on structural sites where composites are more prone to develop such failure. A model, highly crosslinked thus inherently brittle, epoxy matrix was selected for its high Young’s modulus and glass transition temperature exceeding 250 °C. The influence of the Nylon 6,6 nanofibres on the curing behaviour of the matrix and on the thermal and dynamic mechanical properties of the cured resin was investigated. These properties were related to the features of the epoxy resin and of the resin impregnated…

Materials sciencePOLYMERIC NANOFIBERSPolymers and Plasticselectronspun nanofibrous matModuluschemistry.chemical_compoundSettore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineBrittlenessFracture toughnessPOLYMER–MATRIX COMPOSITES (PMCS)Materials ChemistryPOLYMERIC NANOFIBERS; DELAMINATION; THERMAL PROPERTIES; POLYMER–MATRIX COMPOSITES (PMCS)Composite materialCuring (chemistry)Carbon fiber reinforced polymerthermal propertiedelamination fracture toughnessDELAMINATIONGeneral ChemistryEpoxyComposite laminatesNylon 6chemistryvisual_artCeramics and Compositesvisual_art.visual_art_mediumTHERMAL PROPERTIESSettore CHIM/07 - Fondamenti Chimici Delle TecnologieCFRP laminate
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Pinned hybrid glass-flax composite laminates aged in salt-fog environment: Mechanical durability

2019

The aim of the present paper is to study the mechanical performance evolution of pinned hybrid glass-flax composite laminates under environment aging conditions. Hybrid glass-flax fibers/epoxy pinned laminates were exposed to salt-spray fog environmental conditions up to 60 days. With the purpose of assessing the relationship between mechanical performances and failure mechanisms at increasing aging time, single lap joints at varying joint geometry (i.e., hole diameter D and hole distance E from free edge) were characterized after 0 days (i.e., unaged samples), 30 days, and 60 days of salt-fog exposition. Based on this approach, the property&ndash

Materials sciencePolymers and PlasticsComposite number02 engineering and technologyBearing; Failure modes; Glass-flax hybrid coposites; Pinned joints; Salt fog aging010402 general chemistry01 natural sciencesFailure modesArticlelcsh:QD241-441lcsh:Organic chemistryFlexural strengthGlass-flax hybrid copositesComposite materialJoint (geology)Natural fiberPinned jointsFailure modeGeneral ChemistryEpoxyComposite laminates021001 nanoscience & nanotechnologyDurabilityGlass-flax hybrid compositePinned joint0104 chemical sciencesSettore ING-IND/22 - Scienza E Tecnologia Dei MaterialiLap jointSalt fog agingvisual_artBearingvisual_art.visual_art_medium0210 nano-technology
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Experimental assessment of the improved properties during aging of flax/glass hybrid composite laminates for marine applications

2018

The investigation for natural fibers composites in terms of performance, durability, and environmental impact for structural applications in marine environments is a relevant challenge in scientific and industrial field. On this context, the aim of this work is to assess the durability and mechanical stability in severe environment of epoxy/glass–flax hybrid composites. For the sake of comparison, also full flax and glass epoxy composites were investigated. All samples were exposed to salt–fog environmental conditions up to 60 aging days. Wettability behavior during time was compared with water uptake evolution to assess water sensitivity of hybrid composite configurations. Moreover, quasi-…

Materials sciencePolymers and PlasticsGlass fiber02 engineering and technologyGeneral ChemistryComposite laminates010402 general chemistry021001 nanoscience & nanotechnology01 natural sciencesDurability0104 chemical sciencesSurfaces Coatings and Filmsnatural fibershybrid compositeMaterials Chemistrydurabilitymechanical propertieComposite material0210 nano-technologydurability; glass fibers; hybrid composites; mechanical properties; natural fibers; Chemistry (all); Surfaces Coatings and Films; Polymers and Plastics; Materials Chemistry2506 Metals and Alloysglass fiberJournal of Applied Polymer Science
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Effect of glass fiber hybridization on the durability in salt-fog environment of pinned flax composites

2021

The aim of the present paper is to evaluate the effect of the hybridization with external layers of glass fibers on the durability of flax fiber reinforced composites in severe aging conditions. To this scope, full glass, full flax and hybrid glass–flax pinned laminates were exposed to a salt-fog environment for up to 60 days. Double-lap pinned joint tests were performed to assess the pin-hole joints performances at varying the laminate stacking sequence. In order to better discriminate the relationship between the mechanical behavior and the fracture mechanisms of joints at increasing the aging time, different geometries (i.e., by varying both the hole diameter D and the free edge distance…

Materials sciencePolymers and PlasticsHybrid composite laminatesGlass fiberStackingOrganic chemistrySalt-fog agingFailure modesArticlelaw.inventionFlax fiberBearing; Failure modes; Flax; Hybrid composite laminates; Salt-fog agingbearing; salt-fog aging; flax; failure modes; hybrid composite laminatesQD241-441lawFlaxBearing capacityComposite materialJoint (geology)Bearing (mechanical)General ChemistryDurabilitySettore ING-IND/22 - Scienza E Tecnologia Dei MaterialiBearingFracture (geology)Bearing Failure modes Flax Hybrid composite laminates Salt-fog aging
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AN ACCURATE METHOD TO PREDICT THE STRESS CONCENTRATION IN COMPOSITE LAMINATES WITH A CIRCULAR HOLE UNDER TENSILE LOADING

2007

The paper presents a theoretical-numerical hybrid method for determining the stresses distribution in composite laminates containing a circular hole and subjected to uniaxial tensile loading. The method is based upon an appropriate corrective function allowing a simple and rapid evaluation of stress distributions in a generic plate of finite width with a hole based on the theoretical stresses distribution in an infinite plate with the same hole geometry and material. In order to verify the accuracy of the method proposed, various numerical and experimental tests have been performed by considering different laminate lay-ups; in particular, the experimental results have shown that a combined …

Materials sciencePolymers and Plasticsbusiness.industryGeneral MathematicsStructural engineeringComposite laminatesFibre-reinforced plasticCondensed Matter PhysicsFRACTUREBiomaterialsStress (mechanics)Settore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineDistribution (mathematics)Mechanics of MaterialsPLATESolid mechanicsUltimate tensile strengthCeramics and CompositesFracture (geology)NOTCHED STRENGTHComposite materialbusinessStress concentration
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Salt spray fog ageing of hybrid composite/metal rivet joints for automotive applications

2017

Abstract The present experimental investigation aims to investigate the effect of salt-fog exposition on the mechanical behaviour of composite/metal riveted joints. To this aim, two kinds of joint were exposed to salt-fog environmental conditions according to ASTM B117 standard, for fifteen weeks. In particular, two composite laminates (i.e. glass fibre and carbon fibre/epoxy composites) were used as composite substrate joined with the metal substrate (i.e. aluminium alloy Al 6060). Single-lap shear tests were carried out in order to evaluate the evolution of the mechanical performances and the damage mechanisms of the riveted joints during the ageing exposition. The results evidence that t…

Materials scienceSalt-fogAluminium alloyGlass fiberComposite numberComposite02 engineering and technologyIndustrial and Manufacturing EngineeringCorrosion0203 mechanical engineeringAluminium alloyRivetComposite materialRivetingJoint (geology)Mechanical EngineeringMetallurgyHybrid jointEpoxyComposite laminates021001 nanoscience & nanotechnologyEnvironmental degradationSettore ING-IND/22 - Scienza E Tecnologia Dei Materiali020303 mechanical engineering & transportsMechanics of Materialsvisual_artCeramics and Compositesvisual_art.visual_art_mediumAluminium alloy; Composites; Environmental degradation; Hybrid joints; Riveting; Salt-fog0210 nano-technologyComposites Part B: Engineering
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Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates

2004

An empirical model is proposed for the stress ratio effect on the fatigue delamination growth rate in composite laminates under single-mode loading, intending to provide a simple and accurate description tool in engineering application. The model is based on heuristic considerations of damage accumulation ahead of the crack. Linear cumulative assumption is used for damage estimation. Comparison of the prediction based on the proposed model with the test results for different carbon, glass, and alumina fibre-reinforced composites at several stress ratios shows reasonable agreement.

Materials scienceStress ratioMechanical EngineeringDelaminationComposite laminatesIndustrial and Manufacturing EngineeringdelaminationStress (mechanics)fatigue crack growthMechanics of MaterialsModeling and Simulationpolymer matrix compositesfatigue modellingGeneral Materials ScienceGrowth rateComposite materialINTERNATIONAL JOURNAL OF FATIGUE
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Determination of the residual stresses in composite laminate using the compliance method

2005

Residual stresses play an important role on the mechanical behavior of composite laminate. The development of new methods to determine the residual stresses gradient within the laminates is necessary. This article presents the adaptation of the compliance method in the case of composite laminates carbon/epoxy [02/902]s. The incremental drilling of a constant width groove allows for each increment to measure the strains (using strain gages) and displacements (using an optical device) of particularly points of the structure surface. These experimental data are compared with results given by a finite elements simulation. This comparison allows to raise the residual stresses in the composite la…

Materials science[SPI] Engineering Sciences [physics]Composite number02 engineering and technologyCompliance method[SPI]Engineering Sciences [physics]0203 mechanical engineeringResidual stress[SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]General Materials ScienceComposite materialStrain gaugeGroove (music)ComputingMilieux_MISCELLANEOUSbusiness.industryMechanical EngineeringEpoxyStructural engineeringComposite laminates021001 nanoscience & nanotechnologyCondensed Matter PhysicsFinite element method020303 mechanical engineering & transportsMechanics of Materialsvisual_artvisual_art.visual_art_medium0210 nano-technologybusiness
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Electroelastic Analysis of Piezoelectric Composite Laminates by Boundary Integral Equations

2004

A boundary integral representation for the electroelastic state in piezoelectric composite laminates subjected to axial extension, bending, torsion, shear/bending, and electric loadings is proposed. The governing equations are presented in terms of electromechanical generalized variables by the use of a suitable matrix notation. Thus, the three-dimensional electroelasticity solution for piezoelectric composite laminates is generated from a set of two partially coupled differential equations defined on the cross section of each individual ply within the laminate. These ply equations are linked through the interface conditions, which allow restoration of the model of the laminate as a whole. …

Materials sciencebusiness.industryNumerical analysisPiezoelectricityAerospace EngineeringTorsion (mechanics)Mechanical engineeringStructural engineeringFiber-reinforced compositeComposite laminatesPiezoelectricitylaminates boundary element methodMethod of characteristicsSettore ING-IND/04 - Costruzioni E Strutture AerospazialibusinessActuatorBoundary element methodAIAA Journal
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Interlaminar stresses in laminated composite beam-type structures under shear/bending

2000

A boundary integral model for composite laminates under out-of-plane shear/bending is presented. The formulation proposed allows one to determine the elastic response of generally stacked composite laminates having general shape of the cross section. The integral equations governing the ply behavior within the laminate are deduced starting from the reciprocity theorem for beam-type structures. The ply integral equations are obtained by employing the analytical expression of the fundamental solution of generalized plane strain anisotropic problems. The laminate model is completed by imposing the displacement and stress continuity along the interfaces and the external boundary conditions. The…

Mathematical analysisFundamental solutionAerospace EngineeringGeometryBoundary value problemComposite laminatesAnisotropyBoundary element methodIntegral equationPlane stressMathematicsStress concentrationAIAA Journal
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