0000000000065151

AUTHOR

Vincenzo Oliveri

showing 10 related works from this author

A Rayleigh-Ritz approach for postbuckling analysis of variable angle tow composite stiffened panels

2018

Abstract A Rayleigh-Ritz solution approach for generally restrained multilayered variable angle tow stiffened plates in postbuckling regime is presented. The plate model is based on the first order shear deformation theory and accounts for geometrical nonlinearity through the von Karman’s assumptions. Stiffened plates are modelled as assembly of plate-like elements and penalty techniques are used to join the elements in the assembled structure and to apply the kinematical boundary conditions. General symmetric and unsymmetric stacking sequences are considered and Legendre orthogonal polynomials are employed to build the trial functions. A computer code was developed to implement the propose…

Rayleigh–Ritz methodEngineeringSource codemedia_common.quotation_subjectComposite numberStructure (category theory)02 engineering and technologyPhysics::Fluid Dynamics0203 mechanical engineeringGeneral Materials ScienceBoundary value problemSettore ING-IND/04 - Costruzioni E Strutture AerospazialiVariable angle tow composites Composite stiffened plates Postbuckling analysis Rayleigh-Ritz method First Order Shear DeformationLegendre polynomialsCivil and Structural Engineeringmedia_commonbusiness.industryMechanical EngineeringStructural engineering021001 nanoscience & nanotechnologyFinite element methodComputer Science Applications020303 mechanical engineering & transportsModeling and SimulationOrthogonal polynomials0210 nano-technologybusinessComputers & Structures
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Post-buckling analysis of cracked multilayered composite plates by pb-2 Rayleigh–Ritz method

2015

Abstract A pb-2 Rayleigh–Ritz variational approach for the analysis of post-buckling behavior of cracked composite plates is presented. The plate is modeled by the first order shear deformation theory taking geometric nonlinearities into account through the von Karman’s theory. General stacking sequences are considered. Cracks are modeled by using subdomain decomposition of the plate coupled with penalty techniques, used to augment the variational statement with the needed continuity conditions along the connected subdomains edges. Numerical procedures have been developed and used to validate the present solution by comparison with available literature results. Original results are then pre…

Rayleigh–Ritz methodEngineeringbusiness.industryShear deformation theoryComposite numberStackingStructural engineeringComposite plateFirst order shear deformation theory (FSDT)First orderCracked platePb2 Ritz methodPhysics::Fluid DynamicsPost-buckling analysiBucklingCeramics and CompositesSettore ING-IND/04 - Costruzioni E Strutture AerospazialibusinessCivil and Structural EngineeringComposite Structures
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Thermo-mechanical post-buckling analysis of variable angle tow composite plate assemblies

2017

peer-reviewed The increasing use of composite materials for lightweight structural applications and the extended tailoring capabilities offered by variable stiffness laminates requires rapid and robust analysis tools that adequately describe the mechanical behaviour of such structures. In this work, a Rayleigh–Ritz solution for generally restrained multilayered stiffened variable angle tow plates in the post-buckling regime is presented. The plate model is based on first-order shear deformation theory and accounts for geometrical nonlinearity through von Kármán’s assumptions. General symmetric and unsymmetric stacking sequences are considered and Legendre orthogonal polynomials are employed…

EngineeringRayleigh-Ritz solutionbusiness.industrycomposite materialsComposite numberCeramics and Composite02 engineering and technologyStructural engineering021001 nanoscience & nanotechnologyFinite element methodPhysics::Fluid Dynamics020303 mechanical engineering & transports0203 mechanical engineeringBucklingComposite plateOrthogonal polynomialsDisplacement fieldCeramics and CompositesBoundary value problemSettore ING-IND/04 - Costruzioni E Strutture Aerospaziali0210 nano-technologybusinessLegendre polynomialsCivil and Structural EngineeringComposite Structures
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Post-Buckling Analysis of Damaged Multilayered Composite Stiffened Plates by Rayleigh-Ritz Method

2016

A Rayleigh-Ritz approach for the analysis of buckling and post-buckling behavior of cracked composite stiffened plates is presented. The structure is modeled as the assembly of plate elements modeled by the first order shear deformation theory and taking geometric nonlinearities into account through the von Karman’s theory assumptions. Continuity along the plate elements connected edges and the enforcement of rigid and elastic restraints of the plate boundaries are obtained by using penalty techniques, which also allow to straightforwardly implement efficient crack modeling strategies. General symmetric and unsymmetric stacking sequences are considered and numerical procedures have been dev…

Rayleigh–Ritz methodcomposite plates cracked plates post-buckling analysis Ritz method first order shear deformation theory (FSDT)Materials sciencebusiness.industryShear deformation theoryComposite numberStacking02 engineering and technologyGeneral MedicineStructural engineeringFirst order01 natural sciencesFinite element methodRitz methodPhysics::Fluid Dynamics010101 applied mathematics020303 mechanical engineering & transports0203 mechanical engineeringBuckling0101 mathematicsbusinessSettore ING-IND/04 - Costruzioni E Strutture Aerospaziali
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Buckling and post-buckling analysis of cracked stiffened panels via an X-Ritz method

2019

Abstract A multi-domain eXtended Ritz formulation, called X-Ritz, for the analysis of buckling and post-buckling of stiffened panels with cracks is presented. The theoretical framework is based on the First-order Shear Deformation Theory and accounts for von Karman's geometric nonlinearities. The structure is modeled as assembly of plate elements. Penalty techniques are used to fulfill the continuity condition along the edges of contiguous elements and to satisfy essential boundary conditions requirements. The use of an extended set of approximating functions allows to model through-the-thickness cracks and to capture the crack opening and tip singular fields as well as the structural behav…

0209 industrial biotechnologyPost-bucklingShear deformation theoryStructure (category theory)Aerospace Engineering02 engineering and technology01 natural sciences010305 fluids & plasmasRitz methodSet (abstract data type)020901 industrial engineering & automation0103 physical sciencesStiffened panelBoundary value problemSingle domainSettore ING-IND/04 - Costruzioni E Strutture AerospazialiMathematicsCrackbusiness.industryBucklingThin-walled structureX-Ritz methodStructural engineeringFinite element methodBucklingbusiness
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Ritz Solution for Transient Analysis of Variable-Stiffness Shell Structures

2020

The dynamic response of thin-walled structures is driven by mass and stiffness distribution. As such, variable-stiffness (VS) composites offer opportunities to tune structural dynamic responses. To this extent, efficient analysis tools become increasingly important for structural analysis and design purposes. In this work, an efficient and versatile Ritz method for free vibrations and linear transient analysis of VS doubly curved shell structures is presented. VS shell structures are modeled as an assembly of shell-like domains. The shell kinematics is based on the first-order shear deformation theory, and no further assumption is made on the shallowness or on the thinness of the structure.…

musculoskeletal diseasesanimal structuresMaterials scienceDistribution (number theory)Shell (structure)Aerospace Engineeringmacromolecular substances02 engineering and technologyVariable angle tow composites Composite shells Ritz method01 natural sciencesSpherical shellData preparation010305 fluids & plasmasComputer Science::RoboticsPhysics::Fluid Dynamics0203 mechanical engineering0103 physical sciencesmedicineComposite material020301 aerospace & aeronauticsVariable stiffnesstechnology industry and agricultureStiffnessequipment and suppliesTransient analysisFinite element methodmedicine.symptomAIAA Journal
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A non-linear Ritz method for progressive failure analysis of variable angle tow composite laminates

2022

A Ritz formulation for non-linear analysis of damage initiation and evolution in variable angle tow composite plates under progressive loading is presented. The model is built on a few key items. It assumes first order shear deformation theory kinematics and non-liner strains in the von Karman sense. The constitutive relationships are formulated in the framework of continuum damage mechanics at the ply level, so that each laminate layer can experience in-plane damage initiation and evolution, then reflected in material softening and loss of local stiffness. A Ritz polynomial expansion of the primary variables and the minimization of the total potential energy provide the discrete solution e…

Mechanics of MaterialsContinuum damage mechanics failure analysis variable angle tow composites Ritz method non-linear analysisMechanical EngineeringGeneral MathematicsGeneral Materials ScienceSettore ING-IND/04 - Costruzioni E Strutture AerospazialiCivil and Structural Engineering
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Buckling and Postbuckling of Stiffened Composite Panels with Cracks and Delaminations by Ritz Approach

2017

A Ritz approach for the analysis of buckling and post-buckling of stiffened composite panels with through-the-thickness cracks and/or delaminations is presented. The structure is modeled as the assembly of plate elements whose behavior is described by the First-order Shear Deformation Theory and von Karman’s geometric nonlinearities. Penalty techniques ensure continuity along the edges of contiguous plate elements and the enforcement of the restraints on the external boundaries. They are also used to avoid interpenetration problems. General symmetric and unsymmetric stacking sequences are considered. A computer code has been developed and used to validate the proposed method, comparing the …

Engineeringbusiness.industryShear deformation theoryComposite numberAerospace Engineering02 engineering and technologyStructural engineeringStress distribution021001 nanoscience & nanotechnologyFinite element methodData preparation020303 mechanical engineering & transportscracked plates0203 mechanical engineeringBucklingComposite platesSettore ING-IND/04 - Costruzioni E Strutture Aerospaziali0210 nano-technologyMaterial propertiesbusinesspostbucklingAIAA Journal
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Ritz Model for Damage Analysis in Variable Angle Tow Composite Plates

2022

In this work, a Ritz method is developed for progressive damage analysis of multilayered variable angle tow (VAT) composite plates under geometrically non-linear strains. The proposed model adopts a first order shear deformation theory and considers geometric non-linearities through the von Karman assumptions. A meso-modelling approach based on Continuum Damage Mechanics is adopted for analysing the initiation and evolution of damage. The onset of damage is predicted using the Hashin’s criteria. Four damage indices are defined and computed for expressing the degradation of the mechanical properties of the material, both for fibers and matrix under either tension and compression loading. A s…

Composite materialFracture and damage mechanicSettore ING-IND/04 - Costruzioni E Strutture AerospazialiRitz method
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Investigation of buckling characteristics of cracked variable stiffness composite plates by an eXtended Ritz approach

2021

Abstract Variable Angle Tow (VAT) composite plates are characterized by in-plane variable stiffness properties, which opens to new concepts of stiffness tailoring and optimization to achieve higher structural performance for advanced lightweight structures where damage tolerance consideration are often mandatory. In this paper, a single-domain eXtended Ritz formulation is proposed to study the buckling behaviour of variable stiffness laminated cracked plates. The plate behaviour is described by the first order shear deformation theory whose generalized displacements, namely reference plane translations and rotations, are expressed via suitable admissible trial functions. These consist of a …

business.industryMechanical EngineeringBoundary (topology)Stiffness020101 civil engineering02 engineering and technologyBuilding and ConstructionStructural engineering0201 civil engineering020303 mechanical engineering & transports0203 mechanical engineeringBucklingSpecial functionsOrthogonal polynomialsmedicineBoundary value problemmedicine.symptombusinessBuckling Cracked plates Extended Ritz method Variable stiffness X-RitzSettore ING-IND/04 - Costruzioni E Strutture AerospazialiDamage toleranceCivil and Structural EngineeringMathematicsEnergy functional
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