Search results for " free vibrations"

showing 4 items of 4 documents

Free vibrations of anisotropic panels

2004

A meshfree approach, called Displacement Boundary Method, for the analysis of in-plane and out-of-plane free vibrations of anisotropic plates is presented. The discretization process is based on the use of a modified variational principle and the static fundamental solutions of the problem operators. The stiffness and mass matrices are frequencyindependent, symmetric and positive definite and their computation requires boundary integrations of regular kernels only. Thus, the final resolving system can be solved with classical approaches by using standard numerical procedures. Numerical results are presented to show the accuracy and effectiveness of the method.

Meshless methods meshfree methods boundary element method free vibrations anisotropic plates.Settore ING-IND/04 - Costruzioni E Strutture Aerospaziali
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A closed-form solution for natural frequencies of thin-walled cylinders with clamped edges

2016

Abstract This paper presents an approximate closed-form solution for the free-vibration problem of thin-walled clamped–clamped cylinders. The used indefinite equations of motion are classic. They derive from Reissner׳s version of Love׳s theory, properly modified with Donnell׳s assumptions, but an innovative approach has been used to find the equations of natural frequencies, based on a solving technique similar to Rayleigh׳s method, on the Hamilton׳s principle and on a proper constructions of the eigenfuctions. Thanks to the used approach, given the geometric and mechanical characteristics of the cylinder, the model provides the natural frequencies via a sequence of explicit algebraic equat…

SequenceMechanical EngineeringEquations of motionNatural frequency02 engineering and technology021001 nanoscience & nanotechnologyCondensed Matter PhysicsSettore ING-IND/13 - Meccanica Applicata Alle MacchineCircular cylindrical shell Natural frequencies Free vibrations Hamilton's principleFinite element methodsymbols.namesakeAlgebraic equation020303 mechanical engineering & transports0203 mechanical engineeringMechanics of MaterialsNormal modeCalculussymbolsApplied mathematicsGeneral Materials ScienceHamilton's principleClosed-form expression0210 nano-technologyCivil and Structural EngineeringMathematicsInternational Journal of Mechanical Sciences
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Nonlinear free vibrations of composite structures via the X-Ritz method

2020

The analysis of large amplitude vibrations of thin-walled cracked structures build as plate assembly is considered in this study. The problem is addressed via a Ritz approach, called X-Ritz, based on the first order shear deformation theory and von K´arm´an’s geometric nonlinearity assumptions. The trial functions are expressed as series of regular orthogonal polynomial products supplemented with special functions able to represent the crack behaviour; boundary functions are used to guarantee the fulfillment of the kinematic boundary conditions. Results are presented, which illustrate the influence of cracks on the stiffening effect due to large amplitude vibrations.

X-Ritz methodSettore ING-IND/04 - Costruzioni E Strutture Aerospazialinonliner free vibrations composite structures
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Nonlinear free vibrations analysis of cracked composite stiffened plates via X-Ritz approach

2019

Thin and moderately thick composite multi-layered plates are widely employed in naval and aerospace structures. They can experience the presence of cracks, generated for example by corrosion, fatigue or accidental external causes, which aect their static and dynamic behaviour. As regard the dynamic characteristics of plates, many studies have focused on the linear vibration analysis of both isotropic and composite thin and thick plates, providing for a comprehensive knowledge of the plate dynamic behaviour. However, for an accurate appraisal of the plate dynamics, in some applications it is needed to investigate the nonlinear free vibration problem; a literature survey evidences that the la…

X-Ritzcracked plates nonlinear free vibrationsSettore ING-IND/04 - Costruzioni E Strutture Aerospaziali
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