Search results for " Fracture toughness"

showing 10 items of 17 documents

The effect of through-thickness compressive stress on mode II interlaminar fracture toughness

2017

Abstract The effect of through-thickness compressive stress on mode II interlaminar fracture toughness is investigated experimentally and replicated numerically. The modified Transverse Crack Tensile specimen recently proposed by the authors is used, together with an experimental device designed to apply a constant transverse compressive stress on the surface of the specimen. Experiments are conducted using IM7/8552 specimens for different compressive stresses, ranging from 0 to 100 MPa, covering all the practical applications commonly encountered in the aeronautical industry (e.g., tightened filled holes or bolted joints). It is shown that mode II interlaminar fracture toughness increases …

Compressive stressMaterials science/dk/atira/pure/subjectarea/asjc/2200/220502 engineering and technologyStress (mechanics)Settore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineFracture toughness0203 mechanical engineeringUltimate tensile strength/dk/atira/pure/subjectarea/asjc/2500/2503Composite materialSettore ING-IND/04 - Costruzioni E Strutture AerospazialiCivil and Structural Engineeringbusiness.industryMode (statistics)Numerical modelsStructural engineering021001 nanoscience & nanotechnologySettore ING-IND/02 - Costruzioni E Impianti Navali E MariniTransverse planeSettore ING-IND/22 - Scienza E Tecnologia Dei Materiali020303 mechanical engineering & transportsCompressive strengthMode II delaminationBolted jointCeramics and CompositesSettore ICAR/08 - Scienza Delle Costruzioni0210 nano-technologybusinessInterlaminar fracture toughnessComposite Structures
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ELECTROSPUN NANOFIBROUS MATS IN FIBRE REINFORCED EPOXY LAMINATES

ElectrospinningInterlaminar fracture toughneHydrothermal agingNanofiberFiber reinforced epoxy composites; Electrospinning; Nanofiber; Interlaminar fracture toughness; Hydrothermal agingFiber reinforced epoxy composite
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Infrared Thermography assisted evaluation of static and fatigue Mode II fracture toughness in FRP composites

2019

Abstract The work proposes the combined use of a Modified Transverse Crack Tension (MTCT) test coupon and Infrared Thermography, to evaluate the static and fatigue behaviour of Fibre Reinforced Polymer composites under Mode II delamination. Artificial delaminations starters are added to the TCT coupon, whose effects on the Strain Energy Release Rate are discussed. Infrared Thermography and Thermoelastic Stress Analysis are implemented to investigate stresses and delaminations growths on two FRP materials: a pre-preg IM7/8552 carbon fibre-epoxy and a glass-fibre reinforced epoxy laminates. The thermographic, thermoelastic and second harmonic signals have been obtained and used to monitor the…

Materials science/dk/atira/pure/subjectarea/asjc/2200/220502 engineering and technologyPolymer Matrix CompositeStress (mechanics)Settore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineThermoelastic dampingFracture toughness0203 mechanical engineeringThermoelastic Stress Analysis/dk/atira/pure/subjectarea/asjc/2500/2503Composite materialFatigueDelamination Fracture ToughneMode IICivil and Structural EngineeringStrain energy release ratePolymer Matrix CompositesDelamination Fracture ToughnessDelaminationEpoxyFibre-reinforced plastic021001 nanoscience & nanotechnology020303 mechanical engineering & transportsvisual_artThermographyvisual_art.visual_art_mediumCeramics and Composites0210 nano-technology
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Thermoelastic Stress Analysis of modified Transverse Cut Tensile composite specimens under pure Mode II fatigue delamination

2018

The present work investigates the behaviour of a Transvers Crack Tensile (TCT) specimen undergoing fatigue loading, by means of a Thermoelastic Stress Analysis (TSA) experimental setup. The TCT is a tensile composite specimen where a number of internal layers are cut through the beam width. The presence of such transverse notch favours the formation of interlaminar Mode II delaminations, starting from the notch tips and propagating between the cut and continuous plies. In this work, a modification is adopted to the classic TCT specimen, where insert films, mimicking artificial delaminations, are laid across the notch tips. This is done with the purpose to favour a pure Mode II and a symmetr…

Materials science/dk/atira/pure/subjectarea/asjc/2200/2205Composite number02 engineering and technologyEdge (geometry)Stress (mechanics)Settore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineThermoelastic damping0203 mechanical engineeringMaterials Science(all)Ultimate tensile strengthThermoelastic Stress AnalysisComposite materialFatigueEarth-Surface ProcessesDelamination Fracture ToughneMode IICivil and Structural EngineeringDelamination Fracture ToughnessMechanical EngineeringDelaminationFibre-reinforced plastic021001 nanoscience & nanotechnologyFibre Reinforced CompositeTransverse plane020303 mechanical engineering & transports/dk/atira/pure/subjectarea/asjc/2500Mechanics of MaterialsFibre Reinforced Composites/dk/atira/pure/subjectarea/asjc/2200/22100210 nano-technology/dk/atira/pure/subjectarea/asjc/2200/2211
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Effect of hydrothermal ageing on the thermal and delamination fracture behaviour of CFRP composites

2014

Abstract This work investigates the hydrothermal ageing behaviour of a carbon fibre reinforced laminate and its epoxy matrix in bulk conditions. A model DGEBA epoxy is employed, and water uptake and dynamic mechanical thermal (DMTA) analyses have been performed on both the composites and bulk resin. Fracture toughness of the bulk resin has been measured, evidencing a substantially unmodified critical stress intensity factor KIC, although the evidence of plasticisation effects given by DMTA. Interlaminar Mode I fracture toughness of the composite showed a variable trend towards slight decreases or slight increases, according to the prevailing toughening or embrittling mechanisms activated by…

Materials scienceMechanical EngineeringPolymer–matrix composites (PMCs) Fracture toughness Environmental degradation Thermal analysisComposite numberDelaminationEpoxyDynamic mechanical analysisIndustrial and Manufacturing EngineeringHydrothermal circulationSettore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineFracture toughnessMechanics of MaterialsAgeingvisual_artCeramics and Compositesvisual_art.visual_art_mediumFracture (geology)Settore CHIM/07 - Fondamenti Chimici Delle TecnologieComposite material
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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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A methodology for the rapid characterization of Mode II delamination fatigue threshold in FRP composites

2019

Abstract A new methodology to measure the Mode II interlaminar fracture in fatigue for FRP composites is developed. The proposed methodology uses a Modified Transvers Crack Tensile (MTCT) specimen and is able to characterize the near threshold behavior in a robust, easier and significantly faster way than standard procedures. Analytical formulae, able to link the crack growth rate to the load or strain amplitudes, were found and verified, and their importance was explained, in particular, for what concerns the characterisation of the near threshold behavior. Experiments were performed both in load and strain control, while the delamination growth was monitored using different techniques inc…

Materials scienceParis law0211 other engineering and technologies02 engineering and technologySettore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineThermoelastic damping0203 mechanical engineeringMaterials Science(all)Ultimate tensile strengthGeneral Materials ScienceComposite materialMode II fracture toughneFatigue021101 geological & geomatics engineeringMode II fracture toughnessMechanical EngineeringFibre reinforced compositeMode (statistics)Transverse crack tensile specimenFibre-reinforced plasticNear threshold020303 mechanical engineering & transports/dk/atira/pure/subjectarea/asjc/2500Mechanics of MaterialsCompatibility (mechanics)/dk/atira/pure/subjectarea/asjc/2200/2210Fibre reinforced compositesIndustrial material/dk/atira/pure/subjectarea/asjc/2200/2211
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Radiation curing of carbon fibre composites

2014

Epoxy/carbon fibre reinforced composites were produced by means of e-beam irradiation through a pulsed 10 MeV electron beam accelerator. The matrix consisted of a difunctional epoxy monomer (DGEBA) and an initiator of cationic polymerisation, while the reinforcement was a unidirectional high modulus carbon fibre fabric. Dynamic mechanical thermal analysis was carried out in order to determine the cross-linking degree. The analysis pointed out a nonuniformity in the cross-linking degree of the e-beam cured panels, with the formation of clusters at low Tg (glass transition temperature) and clusters at high Tg. An out-of-mould post irradiation thermal treatment on e-beam cured samples provides…

RadiationMaterials scienceModulusThermal treatmentEpoxyFracture toughnessvisual_artvisual_art.visual_art_mediumSettore CHIM/07 - Fondamenti Chimici Delle TecnologieComposite materialGlass transitionThermal analysisBeam (structure)Curing (chemistry)Carbon fibre reinforced epoxy resin Radiation curingDynamic mechanical thermal analysisDelamination fracture toughness
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The durability of carbon fiber/epoxy composites under hydrothermal ageing

2011

Studies on fibre reinforced composites are now receiving greater attention. Industrial applications have been successful in areas like aerospace, automobile, marine, construction and sporting goods. The first generation of epoxy resins for use in carbon fibre composites are able to achieve optimized high stiffness modules and high heat resistance by a high crosslink density, reached through thermal curing. However, these formulations can be very toxic and brittle with low crack resistance, which was a major disadvantage for structural applications. In the last years the use of ionizing radiation as alternative to thermal curing has been proposed as an environmentally friendly process. Furth…

Settore ICAR/11 - Produzione EdiliziaDurability carbon fiber composites hydrothermal ageing fracture toughness
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The effect of the through-the-thickness compressive stress on mode II interlaminar fracture toughness

2017

The effect of through-the-thickness compressive stress on the mode II interlaminar fracture toughness is investigated experimentally and replicated numerically. The modified Transverse Crack Tensile specimen recently proposed by the authors is used, together with an experimental device designed to apply a constant transverse compressive stress on the surface of the specimen. Experiments are conducted using IM7/8552 specimens for different compressive stresses, ranging from 0 to 100 MPa, covering all the practical applications commonly encountered in the aeronautical industry (e.g., tightened filled holes or bolted joints). It is shown that the mode II interlaminar fracture toughness increas…

Settore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineInterlaminar fracture toughness Mode II delamination Compressive stress
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