Um dos grandes desafios enfrentados pelos fabricantes de turbinas hidráulicas é prevenir o aparecimento de vibrações induzidas pelo escoamento nas travessas do pré-distribuidor e pás do rotor. Considerando apenas as travessas, e atribuídos a tais vibrações, foram relatados 28 casos de trincas ou ruídos anormais nas últimas décadas, que acarretaram enormes prejuízos associados a reparos, atrasos e perda de geração. O estado da arte na prevenção destes problemas baseia-se na utilização de sofisticados, e caros, programas comerciais de dinâmica dos fluidos computacional para o cálculo transiente do fenômeno. Este trabalho faz uma ampla revisão bibliográfica e levantamento de eventos de trincas ou ruídos ocorridos em travessas nos últimos 50 anos. Propõe, então, um enfoque alternativo, baseado exclusivamente em ferramentas de código aberto. A partir de hipóteses simplificadoras devidamente justificadas, o problema é formulado matematicamente de forma bidimensional, no plano da seção transversal da travessa, levando em conta a interação fluido-estrutura. Nesta estratégia, as equações de Navier-Stokes são resolvidas pelo método dos elementos finitos por meio da biblioteca gratuita oomph-lib. Um código especial em C++ é desenvolvido para o problema de interação fluido-estrutura, no qual o fenômeno de turbulência é levado em consideração por meio de um algoritmo baseado no modelo de Baldwin-Lomax. O método proposto é validado por meio da comparação dos resultados obtidos com referências e medições disponíveis na literatura, que tratam de problemas de barras retangulares suportadas elasticamente. O trabalho finaliza com a aplicação do método a um estudo de caso envolvendo uma travessa particular. / One of the biggest challenges for hydraulic turbine manufacturers is to prevent vortex-induced vibration on the stay vanes and runner blades. Only regarding stay vanes, 28 cases of cracks or unusual noises attributed to such vibrations were reported in the past decades leading to huge costs due to repair, delays and lack of generation. The state of the art today is to use powerful and expensive commercial computational fluid dynamics software to address the required transient phenomena. The present work carries out a comprehensive survey on occurred events in stay vanes during the last 50 years. Then, an alternative approach, based only on free open-source tools, is proposed. From due justified simplifying assumptions, the problem is formulated two-dimensionally, in the stay vane cross section plane, taking the fluid-structure interaction into account. In such a strategy, the Navier-Stokes equations are solved using oomph-lib, an object-oriented, finite-element library. A special C++ computational code is developed to deal with the fluid-structure interaction problem, in which turbulence is considered through a special algorithm, based on the Baldwin-Lomax model. The proposed method is validated through comparisons with an aerodynamics benchmark and an experimental measurement of oscillating rectangular bars both available in the literature. The method is finally applied to a case study of a particular stay vane. Keywords: Hydraulic turbine. Fluid-structure interaction. Vortex-induced vibration.

Orientador: Renato Pavanello / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecanica / Made available in DSpace on 2018-08-10T06:16:16Z (GMT). No. of bitstreams: 1 RomeroCueto_Liliana_M.pdf: 2272152 bytes, checksum: 792e6fbefc070243b8ea9c5f015ace8a (MD5) Previous issue date: 2007 / Resumo: O comportamento de sistemas acoplados fluido-estrutura pode ser modificado pela presença de defeitos estruturais. O estudo desta modificações, usando metodos numericos de simulação, permite aos engenheiros, estimar o novo estado do sistema a partir a avaliação da variação da resposta dinâmica e vibroacustica. Desta forma, a analise de sensibilidade da resposta do sistema, permite verificar a viabilidade da aplicação das tecnicas apresentadas, em tecnicas de detecção de falhas, controle de ruido e otimização estrutural. Este trabalho apresenta um estudo do comportamento vibroacustico de paineis aeronauticos reforçados e a analise de sensibilidade da resposta, destes sistemas, na presença de falhas estruturais. È elaborado um modelo estrutural baseado na teoria de cascas e vigas que é acoplado a um meio fluido acustico interior bi e tridimensional. O metodo de Elementos Finitos é usado para a solução das equações que governam o comportamento acustico-estrutural do sistema acoplado, adotando a formulação não simetrica, com os deslocamentos e pressões como variaveis incognitas dos dominios estrutural e acustico respectivamente. São apresentadas tecnicas analiticas de analise de sensibilidade da resposta em frequencia, estrutural e acustica, em relação as modificações estruturais. A precisão numerica dos metodos de sensibilidade, propostas para o caso vibroacustico, é avaliada usando-se a tecnica da Diferenças Finitas como referencia. Com a finalidade de validar os modelos implementados, são apresentados alguns testes representativos. Na modelagem de paineis aeronauticos, dois modelos de fuselagem de aeronave são apresentados. São calculadas resposta estrutural e vibroacustica e analise de sensibilidade da resposta para modelos de fuselagem 2D e 3D na presença de modificações estruturais / Abstract: The behavior of coupled fluid-structural systems can be modified due to presence of located structural defects. The study of these modifications, by simulation, using numerical methods, allows engineers to predict the new state of the system from the evaluation of structural and acoustic responses. Sensitivity analysis of acoustic and structural responses, with respect to structural geometry modifications, allow to verify the viability to apply techniques to be presented in this work for damage detection, noise control and structural optimization. In this work a formulation for vibro-acoustic sensitivity analysis of aircraft stiffener panels under structural defects is presented. Shells and beams structural elements for two and three-dimensional models coupled with an interior fluid domain are formulated. The Finite Element Method is used to solve the structural-acoustic coupled governing equations, adopting structural displacements and fluid pressure as variables. Structural and vibro-acoustic sensitivity techniques, with respect to structural modifications are presented. The accuracy of sensitivity methods is estimated using the Finite Difference technique as a reference. Respect to aircraft panels models, two fuselage models are described. Dynamic and Vibro-acoustic response and response sensitivity with respect to structural defects are calculated. / Mestrado / Mecanica dos Sólidos e Projeto Mecanico / Mestre em Engenharia Mecânica

A interação entre as ondas vibratórias geradas pela resposta estrutural de uma placa e os modos acústicos de uma cavidade, que é uma das principais fontes de ruído no interior de cabines de automóveis, é estudada empregando técnicas computacionais e experimentais. Para investigar este fenômeno foi construído um protótipo que consiste de uma cavidade feita de acrílico que simula o interior de um veículo. O teto deste modelo pode ser substituído por uma placa de alumínio flexível, para que se possa gerar efeitos de acoplamento entre o campo acústico e a resposta estrutural. Inicialmente, foi feito um estudo analítico do modelo, empregando-se técnicas de elementos finitos com o objetivo de extrair as freqüências naturais e modos vibroacústicos em uma faixa de freqüência abaixo de 300 Hz, em dois casos diferentes: com e sem a presença de assentos dentro da cavidade. Depois disso, o modelo foi submetido a vários testes experimentais, para se obterem as funções de resposta em freqüência, as freqüências naturais vibroacústicas e os modos acústicos e estruturais, usando excitação acústica e estrutural e empregando métodos padrões de análise modal. Para fins de comparação, as FRF\'s vibroacústicas foram obtidas de duas maneiras diferentes: com excitação estrutural e resposta acústica e com excitação acústica e resposta estrutural. As freqüências naturais e os modos vibroacústicos foram medidos usando excitação acústica e estrutural. Neste caso, é mostrada a importância do controle da força excitadora. Alguns parâmetros experimentais foram variados, tais como posicionamento das excitações acústica e estrutural e o tipo de suspensão. Finalmente, é apresentada uma compilação das diferentes técnicas para a extração dos parâmetros modais vibroacústicos, propondo novas metodologias para a medição dos modos acústicos e estruturais em freqüências abaixo de 70 Hz, controlando a força excitadora e utilizando métodos de ajuste de curvas. É mostrado que o uso de excitação acústica e estrutural merece alguns cuidados, visto que a aplicação dos métodos traz restrições de acordo com a faixa de freqüência e a escolha da melhor forma de extração dos modos vibroacústicos depende da freqüência estudada. / The interaction between the vibration waves generated by the structural response of a plate and the acoustic modes of a cavity, which is one of the main noise sources in automobile passenger cabin, is addressed employing both computational and experimental techniques. In order to investigate this phenomenon a prototype which consists of a cavity made of acrylic that resembles a vehicle interior was built. The roof of this model can be replaced by a flexible aluminum plate in order to generate coupling effects between the acoustic field and the structural response. Initially an analytical study was performed on the model employing finite element techniques with the aim of extracting the vibroacoustic natural frequencies and mode shapes in a frequency range below 300 Hz in two different cases: with and without the presence of seats inside the cavity. After that, the model was submitted to several experimental tests in order to obtain the frequency response functions, vibroacoustic natural frequencies and mode shapes, using acoustic and structural excitation and employing standard modal testing methods. For comparison purposes, the vibroacoustic FRF\'s were obtained in two different manners: with the structural excitation and acoustic response and with acoustic excitation and structural response. The vibroacoustic natural frequencies and mode shapes were measured employing both acoustic and structural excitation. In this case, it is shown the importance of the control of the exciting force. Some experimental parameters were varied, such as positioning of the acoustic and structural sources and the suspension type. Finally, a compilation of different techniques for the vibroacoustic modal parameters extraction is presented, proposing new methodologies for the acoustic and structural modes measurements in frequencies below 70 Hz, using force control and curve fitting methods. It is shown that both acoustic and structural excitations have restrictions concerning the frequency range and the choice of the better method for the extraction of the vibroacoustic mode shapes and natural frequencies depends on it.

Les écoulements autour de structures en mouvement font l'objet de plusieurs travaux numériques et expérimentaux. L'objectif de ce travail de thèse consiste à montrer la pertinence de la combinaison de la pénalisation volumique avec la méthode de lattice Boltzmann (LBM), dans l'étude du mouvement d'obstacles mobiles dans un écoulement, et de leur interaction avec celui-ci. La LBM,qui est simple et précise à mettre en œuvre, a prouvé ces dernières années son efficacité dans le domaine de la mécanique des fluides. Par ailleurs, la méthode de pénalisation volumique consiste à introduire un terme de pénalisation dans l'équation que l'on souhaite résoudre, afin de prendre en compte l'influence de l'obstacle sur le domaine fluide. Comme cette équation est résolue sur l'ensemble du domaine composé du fluide et du solide, les conditions aux limites à l'interface fluide-solide sont appliquées de façon naturelle. Il semble donc aisé de combiner cette technique avec la méthode de lattice Boltzmann. Nous avons dans un premier temps rappelé les notions de base et les principales caractéristiques de la méthode de lattice Boltzmann. On a présenté quelques exemples d'applications sur des cas tests, que nous avons programmés. Ensuite, une étude bibliographique faisant état des différentes approches qui utilisent la LBM dans l'étude des problèmes d'interaction fluide structure (IFS) a été réalisée. Puis, la combinaison de la pénalisation volumique avec la LBM a été testée avec succès sur l'équation de Burgers monodimensionnelle. La validation s'est portée en premier lieu, sur un écoulement autour d'un solide fixe, puis sur un écoulement autour d'une structure dont le mouvement est imposé, et finalement sur un problème d'IFS de type masse-ressort. La méthode développée a été ensuite testée sur les équations de Navier-Stokes, en considérant un fluide incompressible et une structure rigide. La validation s'est portée tout d'abord sur un écoulement autour d'obstacles immobiles (carré et cylindre), puis autour d'un cylindre mobile en oscillations forcées et libres. Enfin, une dernière application a été portée sur un écoulement entre deux plaques mobiles dans un canal. Nous avons montré que pour tous les cas étudiés, l'approche développée donne de bons résultats, elle reproduit avec précision les résultats de référence. / Flows around moving bodies are the subject of several numerical and experimental studies. The work presented in this document deals with the implementation of a volume penalization technique in a lattice Boltzmann model (LBM), in order to compute flows around moving obstacles. The LBM, which is accurate and easy to implement, has been successfully applied in fluid mechanics during the last decades. It was thus chosen in the present work, for flow computation. Furthermore, the volume penalization technique consists in introducing a volume penalization term into the equation that needs to be solved, in order to take into account the influence of the obstacle on the fluid domain. Since this equation is solved on both fluid and solid domains, the boundary conditions at the fluid-solid interface are naturally applied. Hence this technique seems easy to implement in a lattice Boltzmann framework. In the first chapter, the foundations and the main features of the lattice Boltzmann method are recalled, and several test cases that we simulated are presented. The second chapter deals with a literature review of the techniques developed for the simulation of fluid structure interaction problems in combination with the LBM. In the third chapter, the volume penalization method combined with the LBM was first applied to the one dimensional Burgers equation, considering motionless and moving obstacles (forced motion, and coupling between the fluid force calculated with the penalized Burgers equation and the motion of the obstacle). The combination of the volume penalization approach and the LBM was then employed to solve the incompressible NavierStokes equations, for cases of flows past motionless obstacles (flows over a square obstacle, and past a circular cylinder), and past an oscillating cylinder (where forced and free oscillations of the cylinder were simulated). Finally, this method was also applied to a symmetric Couette flow. For all these simulated cases, a good agreement with numerical results obtained with other techniques, and with results found in literature, was obtained.

Nous étudions de manière expérimentale un cas d’interaction fluide/structure entre une fibre élastique et un milieu granulaire dense proche du jamming. Dans notre dispositif expérimental horinzontal, un milieu granulaire bidimensionnel, aléatoire et dense est en interaction avec une fibre élastique encastrée. L'extrémité encastrée de cette fibre est en translation par rapport aux grains tandis que son extrémité libre fait initialement face au flux de grains dans une géométrie de pénétration, avant de se défléchir par interaction avec les grains. Les paramètres de contrôle de notre système sont la compacité du milieu granulaire, la longueur et la rigidité de la fibre. Notre dispositif nous permet de mesurer la déformée de la fibre, les efforts que les grains exercent sur la fibre, notamment la force de traînée et de suivre les réorganisation du milieu granulaire. Sous certaines conditions expérimentales, nous avons observé que ce système présente plusieurs régimes d'évolution. A faible et à forte déflexions de la fibre, le système connaît une évolution stochastique, liée à la nature aléatoire du milieu granulaire : respectivement de petites fluctuations de la fibre autour de sa position d'équilibre et des événements brusques de balayage de la fibre en flexion associés à des avalanches granulaires. La transition entre ces deux régimes est associée à une brisure de symétrie qui affecte tant la fibre que le milieu granulaire. Dans une première partie, nous étudions comment la déflexion de la fibre est influencée par les paramètres de contrôle, en particulier par l'écart au jamming. Dans une seconde partie, nous montrons qu'une asymétrie de densité se développe dans le milieu granulaire lorsque la fibre est suffisamment défléchie. Dans une troisième partie, nous tentons de comprendre l'évolution des forces mesurées à l'aide de simulations numériques de l'Elastica sur une poutre sous chargement. Enfin, nous proposons un modèle de compaction des grains par la fibre qui est en bon accord avec l'évolution expérimentale du système. Une application de cette thèse est la compréhension des mécanismes de pénétration d'une racine ou d'une tige dans un sol granulaire. / We study experimentally a fluid/structure interaction between an elastic fiber and a dense granular medium near the jamming transition. In our horizontal setup, a bidimensionnal and dense random packing is interacting with a clamped elastic fiber. The clamped end of the fiber is in translation relative to the the grains while the free end faces initially the grain flux in a penetration geometry before being deflected by grain/fiber interactions. The control parameters of our system are the packing fraction of the medium, the length and the rigidity of the fiber. Our setup allows us to measure the deflected shape of the fiber, the forces exerted by the grains on the fiber (including the drag force) and to follow the reorganizations of the granular medium. Under some experimental conditions, we observed that this system exhibits several regimes of evolution. For low and large fiber deflections, the system evolves stochastically as a consequence of the random nature of the granular medium : respectively small fluctuations of the fiber around its equilibrium position and sudden events of unlozding of the fiber in flexion associated to granular avalanches. The transition between those two regimes is associated with a symmetry breaking that affects the granular medium as well as the fiber. In a first part, we study how the fiber deflection is influenced by the control parameters, particularly by the distance to jamming. In a second part, we show that a packing fraction asymmetry appears in the granular medium when the fiber is deflected enough. In a third part, we try to understand the evolution of the measured forces using numerical simulations of the Elastica on a constrained beam. Finally, we propose a model of compaction of the grains by the fiber that is in a good aggreement with the experimental evolution of the system. An application of this thesis is the understanding of the mechanisms involved in the penetration of a root or a beam in a granular soil.

In the presented thesis work, the meshfree method with distance fields was coupled with the lattice Boltzmann method to obtain solutions of fluid-structure interaction problems. The thesis work involved development and implementation of numerical algorithms, data structure, and software. Numerical and computational properties of the coupling algorithm combining the meshfree method with distance fields and the lattice Boltzmann method were investigated. Convergence and accuracy of the methodology was validated by analytical solutions. The research was focused on fluid-structure interaction solutions in complex, mesh-resistant domains as both the lattice Boltzmann method and the meshfree method with distance fields are particularly adept in these situations. Furthermore, the fluid solution provided by the lattice Boltzmann method is massively scalable, allowing extensive use of cutting edge parallel computing resources to accelerate this phase of the solution process. The meshfree method with distance fields allows for exact satisfaction of boundary conditions making it possible to exactly capture the effects of the fluid field on the solid structure.

The heart is a complex organ and much is still unknown about its mechanical function. In order to use simulations to study heart mechanics, fluid and solid components and their interaction should be incorporated into any numerical model. Many previous studies have focused on myocardium motion or blood flow separately, while neglecting their interaction. Previous fluid-structure interaction (FSI) simulations of heart mechanics have made simplifying assumptions about their solid models, which prevented them from accurately predicting the stress-stain behaviour of the myocardium. In this work, a numerical model of the canine left ventricle (LV) is presented, which serves to address the limitations of previous studies. A canine LV myocardium material model was developed for use in conjunction with a commercial finite element code. The material model was modified from its original form to make it suitable for use in simulations. Further, numerical constraints were imposed when calculating the material parameter values, to ensure that the model would be strictly convex. An initial geometry and non-zero stress state are required to start cardiac cycle simulations. These were generated by the static inflation of a passive LV model to an end-diastolic pressure. Comparisons with previous measurements verified that the calculated geometry was representative of end diastole. Stresses calculated at the specified end diastolic pressure showed complex spatial variations, illustrating the superiority of the present approach over a specification of an arbitrary stress distribution to an end-diastolic geometry. In the third part of this study, FSI simulations of the mechanics of the LV were performed over the cardiac cycle. Calculated LV cavity pressures agreed well with previous measurements during most of the cardiac cycle, but deviated from them during rapid filling, which resulted in non-physiological backflow. This study is the first one to present a detailed analysis of the temporal and spatial variations of the properties of both the solid and the fluid components of the canine LV. The observed development of non-uniform pressure distributions in the LV cavity confirms the advantage of performing FSI simulations rather than imposing a uniform fluid pressure on the inner surface of the myocardium during solid-only simulations.

La physique de nage d’une nageoire caudale flexible est étudiée expérimentalement grâce à une plaque flexible immergée dans un écoulement uniforme. Le bord d’attaque est forcé par un mouvement harmonique, tandis que le bord de fuite répond passivement au forçage. Une résonance en amplitude dans la réponse est mise en évidence et révèle une forte interaction entre les fréquences naturelles de la plaque et celles du forçage. Les résultats expérimentaux suggèrent un rôle non trivial de l’amplitude de forçage, qui souligne le rôle des non linéarités dans ce problème. Pour avoir une meilleure compréhension de l'origine de ces non linéarités, un modèle analytique faiblement non linéaire a été développé. Nous supposons une plaque d'épaisseur nulle immergée dans un écoulement potentiel, sujette à une force de traînée résistive. La déflection de la plaque a ensuite été décomposée en un mode rigide, mimant le forçage en pilonnement et en modes propres de flexion d’une poutre dans le vide. Les prédictions de la réponse en amplitude et en fréquence du système forcé sont alors calculées. Les fréquences de résonances, ainsi que l’enveloppe de la déflection, sont en bon accord avec les résultats expérimentaux. Les performances du système, mesurées à travers la poussée générée, est également correctement prédite par la modélisation. L’accord entre les expériences et le modèle est étendu à une étude trouvée dans la littérature. Une optimisation analytique a été conduite et étendue à l’application de la bio-robotique. / The physics of the swimming with a flexible caudal fin is studied experimentally by the means of an elastic plate immersed in a uniform water flow. The leading edge of the plate is forced into a harmonic motion, while its trailing edge responds passively to this actuation. A resonance response in amplitude is demonstrated, revealing a strong interaction between the natural frequencies of the plate and the forcing frequencies. Experimental results suggest a non-trivial role of the forcing amplitude, emphasizing the role of non linearities in this problem. To gain better insight into the origin of these non linearities, a weakly non linear model is developed. We model a quasi two-dimensional plate of zero thickness immersed in a potential flow and subject to a resistive drag-like force. The plate deflection is then decomposed into a forcing heaving mode and natural flexural modes. Predictions of the response in amplitude and frequency to a heave forcing system are then calculated. The frequencies of the resonances, as well as the shapes of the deflection, match the experimental results. The performance of the system measured through the generated thrust, is well predicted by the modelling. The experimental and modelling results presented here show (very) good agreement with the literature. Finally, an analytical optimization is undertaken and potential applications to bio-robotic are suggested.

In this thesis we study efficient parallel iterative solution algorithms for multi-physics problems. In particular, we consider fluid structure interaction (FSI) problems, a type of multi-physics problem in which a fluid and a deformable solid interact. All computations were performed in Oomph-Lib, a finite element library for the simulation of multi-physics problems. In Oomph-Lib, the constituent problems in a multi-physics problem are coupled monolithically, and the resulting system of non-linear equations solved with Newton's method. This requires the solution of sequences of large, sparse linear systems, for which optimal solvers are essential. The linear systems arising from the monolithic discretisation of multi-physics problems are natural candidates for solution with block-preconditioned Krylov subspace methods.We developed a generic framework for the implementation of block preconditioners within Oomph-Lib. Furthermore the framework is parallelised to facilitate the efficient solution of very large problems. This framework enables the reuse of all of Oomph-Lib's existing linear algebra infrastructure and preconditioners (including block preconditioners). We will demonstrate that a wide range of block preconditioners can be seamlessly implemented in this framework, leading to optimal iterative solvers with good parallel scaling.We concentrate on the development of an effective preconditioner for a FSI problem formulated in an arbitrary Lagrangian Eulerian (ALE) framework with pseudo-solid node updates (for the deforming fluid mesh). We begin by considering the pseudo-solid subsidiary problem; the deformation of a solid governed by equations of large displacement elasticity, subject to a prescribed boundary displacement imposed with Lagrange multiplier. We present a robust, optimal, augmented-Lagrangian type preconditioner for the resulting saddle-point linear system and prove analytically tight bounds for the spectrum of the preconditioned operator with respect to the discrete problem size.This pseudo-solid preconditioner is incorporated into a block preconditioner for the full FSI problem. One key feature of the FSI preconditioner is that existing optimal single physics preconditioners (such as the well known Navier-Stokes Least Squares Commutator preconditioner) can be employed to approximately solve the linear systems associated with the constituent sub-problems. We evaluate its performance on selected 2D and 3D problems. The preconditioner is optimal for most problems considered. In cases when sub-optimality is detected, we explain the reasons for such behavior and suggest potential improvements.

Les buts principaux recherchés de la présente thèse visent au développement et à l’expertise d’une méthodologie de simulation numérique des problèmes d’interactions fluides-structures. Afin de cerner progressivement le problème étudié, nous nous sommes intéressés en premier lieu à la simulation numérique des écoulements autour d’obstacles solides, plus particulièrement au phénomène d’éclatements tourbillonnaires dans la zone de sillage d’obstacles de différentes formes. Nous avons utilisé la méthode des éléments finis en adoptant la technique de stabilisation GLS (Galerkin Least-Square). Pour le traitement de la turbulence, nous avons opté pour la méthode LES (Large-Eddy Simulation) en utilisant le filtre de Smagorinsky. En deuxième phase, nous nous sommes intéressés aux écoulements en milieux déformables. Nous avons entrepris la formulation ALE (Arbitrairement Lagrangienne Eulérienne) en considérant un maillage déformable. Pour la mise à jour de la grille du maillage dynamique, nous avons utilisé une approche pseudo-élastique. Afin d’expertiser la méthodologie mise en oeuvre, nous avons choisi d’aborder le problème des ballottements à la surface libre de réservoirs partiellement remplis de liquide. En dernière partie, nous nous sommes intéressés au comportement vibratoire d’un corps solide sous l’effet d’un écoulement de fluide. Par l’utilisation d’un algorithme de couplage totalement implicite basé sur la méthode de Gauss-Seidel par Bloc, nous avons abordé le phénomène des instabilités aéroélastiques des ponts à haubans. Pour la validation du modèle numérique traitant les interactions fluides-structures par les données expérimentales, nous nous sommes intéressés au comportement vibratoire d’une maquette sectionnelle d’un tablier de pont réel sous l’effet d’un vent soufflant uniforme. / The main goals sought by this thesis target the development and expertise of a methodology for numerical simulation of fluid-structure interactions problems. In order to identify the studied problem progressively, we are interested primarily in numerical simulation of flows around bluff bodies, especially the phenomenon of vortex shedding in the wake zone of a bluff body of different shapes. We used the finite element method by adopting the stabilized GLS (Galerkin Least-Square) technique. For the treatment of turbulence, we opted the LES (Large-Eddy Simulation) method using the Smagorinsky filter. In the second phase, we were interested in flows in deformable media. We undertook the ALE (Arbitrary Lagrangian Eulerian) formulation by considering a deformable mesh. To update the grid of the dynamic mesh, we used a pseudo-elastic approach. To appraise the implemented methodology, we decided to approach the problem of sloshing at the free surface of a tank partially filled with liquid. In the final part, we were interested in vibration behavior of a solid body under the effect of fluid flow. By using a fully implicit coupling algorithm based on a relaxed Bloc Gauss-Seidel method, we studied the phenomenon of aeroelastic instability of cable-stayed bridges. To validate the numerical model treating fluid-structure interactions by experimental data, we investigated the vibration behavior of a real deck sectional model under the effect of a uniform wind.