Search results for " Delamination"

showing 10 items of 21 documents

Cohesive Model for the Simulation of Crack Initiation and Propagation in Mixed-Mode I/II in Composite Materials

2019

A cohesive element able to connect and simulate crack growth between independently modeled finite element subdomains with non-matching meshes is proposed and validated. The approach is based on penalty constraints and has several advantages over conventional FE techniques in disconnecting two regions of a model during crack growth. The most important is the ability to release portion of the interface that are smaller than the local finite element length. Thus, the growth of delamination is not limited to advancing by releasing nodes of the FE model, which is a limitation common to the methods found in the literature. Furthermore, it is possible to vary the penalty parameter within the cohes…

0301 basic medicineCommercial softwareCohesive elementMaterials science030102 biochemistry & molecular biologyInterface (computing)Delamination02 engineering and technologyFinite element . Cohesive element . Penalty method . Composite materials . Delamination . Mixed-mode propagation021001 nanoscience & nanotechnologyMixed modeFinite element method03 medical and health sciencesSettore ING-IND/14 - Progettazione Meccanica E Costruzione Di MacchineCeramics and CompositesPenalty methodPolygon meshComposite material0210 nano-technology
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BE contact analysis of delamination cracks actively repaired trhough piezoelectric active patches

2009

Active Repair Piezoelectric Materials Boundary Element Method Delamination Cracks Friction
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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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Delamination study of through-thickness reinforced composite laminates via two-phase interface model

2007

A technique to enhance the strength of the composite laminates in the thickness direction consists in inserting through-thickness reinforcement, by which the potential delamination crack faces are bridged in order to increase the interlaminar fracture strength. In this paper, the composite delamination is analyzed in the context of non-linear fracture mechanics making use of the interface concept. The presence of the reinforcement fibres provides an anisotropic elastic and post-elastic mechanical response, which herein is described by an original two-phase interface model. The two phases, namely the adhesive joint (or matrix of the composite) and the reinforcement, are characterized by thei…

Fiber pull-outMaterials scienceB. Interfacebusiness.industryB. DelaminationDelaminationComposite numberFracture mechanicsContext (language use)Structural engineeringA. FibreComposite laminatesFlexural strengthMechanics of MaterialsE. StitchingCeramics and CompositesComposite materialbusinessJoint (geology)
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The role of friction in the 3ENF and 4ENF delamination tests: an analytical solution

2018

In composite structures, the presence and growth of delamination mechanisms in static or fatigue loading conditions is of paramount interest and the American Society for Testing and Materials (ASTM) has adopted the three-points bend end-notched flexure test (3ENF) as the standard for measurement of mode II toughness. The drawback of the 3ENF test is the unstable crack growth and a modified version of the test, namely the four points bend end-notched flexure test (4ENF), has been proposed. The main advantage of the 4ENF over the 3ENF is that crack growth is stable under displacement control, but it can be strong influenced by the interlaminar frictional effects. The effect of frictional cont…

Friction Delamination ToughnessSettore ICAR/08 - Scienza Delle Costruzioni
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Cohesive-frictional interface model with oligocyclic degradation of surfaces roughness

2008

The present work is devoted to the constitutive modelling, through the classical interface kinematical formulation, of the mechanical behaviour of the internal adhesive layers, connecting different bodies. The proposed interface constitutive model couples a cohesive behaviour with a frictional one and it is able to follow the transition from the sound condition to the fully cracked one by means of a specific interpretation of the damage variable. In the fully cracked condition, the dilatancy exhaustion and the frictional strength degradation are also modelled.

Interface cyclic loading delaminationSettore ICAR/08 - Scienza Delle Costruzioni
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Cohesive delamination and frictional contact on joining surface via XFEM

2018

In the present paper, the complex mechanical behaviour of the surfaces joining two different bodies is analysed by a cohesive-frictional interface constitutive model. The kinematical behaviour is characterized by the presence of discontinuous displacement fields, that take place at the internal connecting surfaces, both in the fully cohesive phase and in the delamination one. Generally, in order to catch discontinuous displacement fields, internal connecting surfaces (adhesive layers) are modelled by means of interface elements, which connect, node by node, the meshes of the joined bodies, requiring the mesh to be conforming to the geometry of the single bodies and to the relevant connectin…

Materials scienceDiscretizationConstitutive equationGeometry02 engineering and technology01 natural sciencesdelaminationDiscontinuity (geotechnical engineering)0203 mechanical engineeringlcsh:TA401-492Polygon mesh0101 mathematicsjoined solidsExtended finite element methodCurvilinear coordinatescohesive-frictionalXFEMjoined solidjoined solids; interface; XFEM; cohesive-frictional; delaminationFinite element method010101 applied mathematics020303 mechanical engineering & transportsinterfacelcsh:Materials of engineering and construction. Mechanics of materialsAdhesiveSettore ICAR/08 - Scienza Delle CostruzioniAIMS Materials Science
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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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Numerical analysis of a piezoelectric structural health monitoring system for composite flange-skin delamination detection

2013

Abstract In this paper, a piezoelectric based Structural Health Monitoring (SHM) system is proposed to detect skin/stiffener debonding and delamination cracks proper of laminated composite structures. The SHM system is analyzed by means of a boundary element code implemented in the framework of piezoelectricity. The multidomain technique, coupled with an interface spring model, is used to model laminated composite structures as well as the bonding between the host delaminated structure and the piezoelectric sensor. Static sensitivity analyses are firstly performed on a drop-ply delaminated structure in order to identify a suitable configuration for the sensor. Then, the dynamic electromecha…

Materials sciencePiezoelectric sensorbusiness.industryDelaminationComposite numberFracture mechanicsStructural engineeringFlangePiezoelectricityCeramics and CompositesStructural health monitoringComposite materialComposite flange-skin Piezoelectric sensor Structural health monitoring DelaminationSettore ING-IND/04 - Costruzioni E Strutture AerospazialibusinessBoundary element methodCivil and Structural EngineeringComposite Structures
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An extrinsic interface developed in an equilibrium based finite element formulation

2019

Abstract The phenomenon of delamination in composite material is studied in the framework of hybrid equilibrium based formulation with extrinsic cohesive zone model. The hybrid equilibrium formulation is a stress based approaches defined in the class of statically admissible solutions. The formulation is based on the nine-node triangular element with quadratic stress field which implicitly satisfy the homogeneous equilibrium equations. The inter-element equilibrium condition and the boundary equilibrium condition are imposed by considering independent side displacement fields as interfacial Lagrangian variable, in a classical hybrid formulation. The hybrid equilibrium element formulation is…

PhysicsCohesive Zone Model Delamination Extrinsic interface Hybrid equilibrium elementBoundary (topology)02 engineering and technologyMechanics021001 nanoscience & nanotechnologyDisplacement (vector)Finite element methodStress (mechanics)Stress fieldCohesive zone model020303 mechanical engineering & transportsQuadratic equation0203 mechanical engineeringDamage mechanicsSettore ICAR/08 - Scienza Delle Costruzioni0210 nano-technologyEarth-Surface ProcessesProcedia Structural Integrity
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