O escoamento em torno de corpos tem sido objeto de estudo de muitos pesquisadores e é muito explorado experimental e computacionalmente, devido a sua grande aplicabilidade na engenharia. No entanto, simular computacionalmente este tipo de escoamento requer uma atenção especial ao escolher o tipo malha a ser utilizado. Em muitos casos faz-se necessário o uso de uma malha que se adapte ao contorno do obstáculo, o que pode ocasionar um aumento no esforço computacional. Um maneira de contornar este problema é a utilização do Método das Fronteiras Imersas, que possibilita o uso de malha cartesiana na simulação computacional do escoamento em torno de obstáculos. Isso é possível através da adição de um termo forçante nas equações que modelam o escoamento, e assim as forças que agem sobre o contorno do corpo são transferidas diretamente para a malha. O objetivo deste trabalho de mestrado foi implementar o método das Fronteiras Imersas e simular o escoamento em torno de um cilindro circular em repouso, movimentando-se na mesma direção do escoamento, na direção perpendicular ao escoamento, ou rotacionando em torno do próprio eixo. As simulações computacionais possibilitaram a captura do fenômeno de Atrelagem Síncrona, caracterizado pela sincronia entre a frequência de desprendimento natural de vórtices e a frequência de oscilação do mesmo. O Método das Fronteiras Imersas mostrou um ótimo desempenho quando comparado a resultados experimentais e numéricos encontrados na literatura / The flow around bodies have been studied by many researchers. Both experimental and computational approaches have been extensively explored in researches on flow around bodies and have been applied in many engeneering problems. However, to choose an appropriate type of mesh to perform computational simulations of this type of problem requires special attention. In many cases, it is necessary to use a mesh that is able to conform to the boundary if a given obstacle. The need to perform this adaptation may increase the computational effort. The Immersed Boundary Method enables the use of cartesian meshes to perform computational simulations of flows around obstacles. The idea of this method is to add a forcing term in the equations that model the flow. Thus, the forces applied on the body boundaries are directly transfered to the mesh. The aim of this work was to perform a computational implementation of the Immersed Boundary Method to simulate the flow over a oscilating circular cylinder. This oscilation may be inline with the flow, cross-flow, or rotating. The computational simulations enabled the capture of the lock-in phenomena, which consists of the syncronization between the vortex shedding frequency and the cylinder oscilation frequency. The results obtained from the computational simulations using the Immersed Boundary Method were in good agreement with the numerical and experimental results found in the literature

Neste trabalho, desenvolve-se um método de fronteira imersa para o estudo de escoamento compressível modelado pelas equações de Euler bidimensionais. O método de discretização de diferenças finitas é empregado, usando o método de Steger-Warming de ordem dois para discretizar as variáveis espaciais e o esquema de Runge-Kutta de ordem quatro para discretizar as variáveis temporais. O método da fronteira imersa foi empregado para o estudo de aeroelasticidade computacional em uma seção típica de aerofólio bidimensional com dois movimentos prescritos: torsional e vertical, com o objetivo de se verifcar a eficiência do método e sua aplicabilidade para problemas em aeroelasticidade computacional. Neste estudo desenvolveu-se também um programa de computador para simular escoamentos compressíveis de fluido invíscido utilizando a metodologia proposta. A verificação do código gerado foi feita utilizando o método das soluções manufaturadas e o problema de reflexão de choque oblíquo. A validação foi realizada comparando-se os resultados obtidos para o escoamento ao redor de uma seção circular e de uma seção de aerofólio NACA 0012 com os resultados experimentais, para cada caso. / In this work, an immersed boundary method is developed to study compressible flow modeled by the two-dimensional Euler equations. The finite difference method is employed, using the second order Steger-Warming method to discretizate the space variables and the fourth order Runge-Kutta method to discretizate the time variables. The immersed boundary method was employed to study computational aeroelasticity on a typical two-dimensional airfoil section with two prescribed motion: pitching and plunging, in order to verify the efficiency of the numerical method and its applicability in computational aeroelasticity problems. In this work, a computer program was developed to simulate compressible flows for inviscid fluids using the methodology proposed. The verification of the computational code was performed using the method of manufactured solutions and the oblique shock wave reflection problem. The validation was performed comparing the obtained results for flows around a circular section and a NACA 0012 airfoil section with the experimental results, for each case.

Au cours de cette thèse, nous nous sommes intéressés à la modélisation des interactions fluide-structure entre un fluide visqueux, incompressible et une structure pouvant être déformable. Après avoir présenté les différentes approches possibles de modélisation, nous introduisons une nouvelle méthode de type frontière immergée : la méthode IPC ("Image Point Correction"). Combinant approches Ghost-Cell et Pénalisation, cette méthode mixte du second degré globalement et localement en vitesse, est validée sur différents cas tests (comparaisons des coefficients aérodynamiques pour des cylindres fixes ou mobiles, sédimentation 2D d'un cylindre). Nous avons ensuite appliqué la méthode IPC à la simulation de la nage. Dans un premier temps, le solveur 2D a été couplé avec un algorithme d'optimisation mathématique afin de déterminer la loi de nage optimale pour une géométrie de poisson donnée. Puis, dans un second temps, nous avons simulé la nage 3D après reconstruction approchée de la géométrie, basée sur des images du nageur. Enfin, grâce à l'outil du squelette, une reconstruction réaliste du poisson est proposée. / The aim of this thesis is to investigate the modeling of fluid-structure interactions. The fluid is viscous and incompressible, and the structure is subject to an imposed deformation. After a survey of the different existing approachs to model fluid-structure interactions, we introduce a new immersed boundary method: the IPC method (”Image Point Correction”). This ap-proach merges Ghost-Cell and Penalty concepts. It is globally and locally second order in velocity, and it is validated through several canonical simulations. Then, we apply the IPC method to fish-like swimming. First, the 2D solver is paired up with a mathematical optimization algorithm to determine the optimal swimming law for a given fish geometry. Secondly, we simulate a 3D swimmer after performing an approximated reconstruction of the geometry based on actual fish pictures. Finally, thanks to the skeleton approach, a realistic reconstruction of the fish is exposed.

On s’intéresse à la simulation d’écoulements compressibles multi-matériaux et, notamment, aux interactions fluide/structure dans les régimes transitoires et en dynamique rapide. Le but est de pouvoir décrire l’évolution de matériaux de lois de comportement très différentes à l’aide d’un modèle unique. Les milieux sont seulement différenciés par leurs équations d’état et sont séparés par une interface dite sharp. Les matériaux peuvent être des fluides ou des solides élastiques et sont soumis à de grandes déformations. Le modèle est écrit dans le formalisme eulérien. Le schéma numérique est résolu sur des grilles cartésiennes pour des simulations en trois dimensions.Une extension du modèle permet de décrire les déformations plastiques des solides. / We are interested in the simulation of compressible multimaterial flows and especially influid/structure interactions in transient states and fast dynamics. We aim to describe the evolution of materials of very different constitutive laws with an unified model. The materials are only differentiated by their own constitutive laws and are separated by a sharp interface. They can be as well fluids or elastic solids and under go large de formations. The model is written in the Eulerian framework. The numerical scheme is solved on Cartesian grids for simulations in three dimensions. An extension of the elastic model is added to describe the plastic deformations of solids.

Un nouveau logiciel CFD, LaBS, basé sur la méthode de lattice Boltzmann sur Réseau a été développé dans le cadre d'un projet entre universités et industries. LaBS est utilisé pour la simulation numérique des écoulements thermiques avec un nouveau modèle de frontière immergée pour les conditions limites thermiques. Ce modèle est basé sur la méthode de reconstruction de la fonction de distribution et est évalué pour des conditions limites coincidentes et non-coincidentes avec le maillage, sur le phénomène de diffusion thermique et de convection naturelle.Renault s'intéresse aux situations d'arrêt péage ou de contact coupé, pour lesquelles sont considérés un véhicule roulant à une vitesse soutenue, sur une autoroute par exemple, et qui subit un arrêt ou un ralentissement brutal (avec ou sans contact coupé).Dans ce genre de situation le refroidissement du compartiment moteur qui était assuré par le phénomène de convection forcé durant le roulage laisse place au phénomène de convection naturelle durant les phases de base vitesse ou de vitesse nulle.Le phénomène de convection naturelle est un phénomène lent, qui peut prendre plusieurs minutes à évacuer la chaleur accumulée dans le compartiment moteur. La présence de température élevée pendant une durée trop importante dans le compartiment moteur peut endommager certains composants qui possèdent des seuils de température critique.Pour anticiper ce problème de surchauffe du compartiment moteur, dans lequel un grand nombre de pièces à géométries complexes sont présentes, le phénomène de convection naturelle est étudié avec le nouveau modèle de frontière immergée thermique.%Ce modèle est d'abord testé sur des cas test académique pour validation et est ensuite appliqué au cas d'une voiture réelle.La modélisation des écoulements thermiques avec la méthodes de lattice Boltzmann sur Réseau (LBM) peut-être classée en trois catégories: l'approche multi-vitesse, l'approche hybride et l'approche à deux fonctions de distribution (DDF: Double-Distribution-Function).L'approche multi-vitesse, utilise une équation pour résoudre le champ de vitesse, de densité et de température qui sont résolus avec la LBM. Tandis que l'approche hybride et l'approche DDF utilise un jeux de deux équations, un pour résoudre le champ de vitesse et de densité et l'autre pour résoudre le champ de température.L'approche hybride résout le champ de vitesse et de densité avec la LBM et utilise une méthode de différence finie ou de volume fini pour résoudre le champ de température. L'approche DDF résout quand à elle les deux équations avec la LBM.Le modèle thermique utilisé dans LaBS est basé sur l'approche DDF où les deux équations sont couplées par l'hypothèse de Boussinesq. Le champ de vitesse et de densité est résolu avec un réseau de dix-neuf vitesses discrètes (D3Q19) et champs de température est résolut soit par un réseau à dix-neuf vitesses discrètes (D3Q19) soit par un réseau à sept vitesses discrètes (D3Q7).Le nouveau modèle de frontière immergée décompose la fonction de distribution aux noeuds frontière en sa partie à l'équilibre et hors équilibre. La partie hors équilibre est calculée à partir d'une formulation théorique issus du développement de Chapman-Enskog.La validation du modèle DDF implémenté dans LaBS est faite sur un ensemble de cas test de complexité croissante. Les résultats obtenus avec LaBS sont comparés aux solutions analytiques ou encore à des articles de référence et sont en accord avec les résultats attendus. Ils montrent que qualitativement les résultats sont aussi bons pour le modèle D3Q19/D3Q19 que pour le modèle D3Q19/D3Q7 mais que quantitativement le modèle D3Q19/D3Q19 reste meilleur. / A new three-dimensional CFD solver, LaBS, based on the lattice Boltzmann alogorithms has been developed in a framework of university and industry consortium. In this thesis, this solver is used to simulate thermal flows, with a new thermal boundary condition for immersed solid boundary. The new proposed thermal boundary condition is based on the reconstruction method of the distribution function and is evaluated for immersed solid with coincident and non-coincident wall on the case of diffusion and natural convection phenomena.Renault case study, deals with a vehicle moving at constant speed (highway) that suddently slows down and stops (with or without a cut off contact). In such situation the cooling of the engine compartment first driven by forced convection during taxiing stage, abruptly switches to natural convection in low velocity stages. As natural convection is a slow process, it can take several minutes to remove the accumulated heat in the engine compartment. Such duration could be damaging for some components of the engine compartement which do not tolerate high temperature.In order to anticipate overheating of the engine compartment, where a lot of automotive parts with complex geometry are present and to avoid the above mentioned damages, the phenomenon of natural convection is here studied with the new thermal boundary condition.%The new proposed thermal boundary condition is first tested on academic case studies for validation, and then applied to the case of a real car.The modelling of thermal flows with the lattice Boltzmann method (LBM) can be classified into three categories: the multispeed approach, the hybrid approach and the double-distribution-function (DDF) approach. The multispeed approach, uses only one equation to resolve velocity, density and temperature field, which is solved by the LBM. Whereas the hybrid approach and the DDF approach utilize two sets of equations, one to resolve velocity field and density field and another to resolve temperature field. The hybrid approach solves velocity field and density field by the LBM method and the temperature field by finite-different or finite-volume methods. On the other hand the DDF approach solves the two equations with LBM.The thermal model used in the solver LaBS is based on the coupled DDF approach. In this model, the flow field is solved by a D3Q19 velocity model while the temperature field is solved by a D3Q19 or a D3Q7 velocity model. The coupling between the momentum and the energy transport is made by the boussinesq approximation. The new proposed thermal boundary condition decomposes the distribution function at the boundary node into its equilibrium and non-equilibrium part. The non-equilibrium part is calculated from the theoretical solution based on Chapman-Enskog developement.LaBS thermal model based on the coupled DDF approach is evaluated on a set of cases with increasing complexity. The results obtained with LaBS are compared with analytical solutions or with reference articles and are in a good agreement with the results expected. Results show that the model D3Q19/D3Q7 is qualitatively as good as the model D3Q19/D3Q19 but quantitatively the model D3Q19/D3Q19 remains the best.

Dans cette thèse, une nouvelle méthode de frontières immergées a été développée pour la simulation d'interaction fluide-structure, appelée la méthode de frontières immergées mobiles (en langage anglo-saxon: MIBM). L'objectif principal de cette nouvelle méthode est de déplacer arbitrairement les solides à géométrie complexe dans un fluide visqueux incompressible, sans remailler le domaine fluide. Cette nouvelle méthode a l'avantage d'imposer la condition de non-glissement à l'interface d'une manière exacte via une force sans introduire des constantes artificielles modélisant la structure rigide. Cet avantage conduit également à la satisfaction de la condition CFL avec un pas de temps plus grand. Pour un calcul précis de la force induite par les frontières mobiles, un système linéaire a été introduit et résolu par la méthode de gradient conjugué. La méthode proposée peut être intégrée facilement dans des solveurs résolvant les équations de Navier-Stokes. Dans ce travail la MIBM a été mise en œuvre en couplage avec un solveur fluide utilisant une méthode de projection adaptée pour obtenir des solutions d'ordre deux en temps et en espace. Le champ de pression a été obtenu par l'équation de Poisson qui a été résolue à l'aide de la méthode du gradient conjugué préconditionné par la méthode multi-grille. La combinaison de ces deux méthodes a permis un gain de temps considérable par rapport aux méthodes classiques de la résolution des systèmes linéaires. De plus le code de calcul développé a été parallélisé sur l'unité graphique GPU équipée de la bibliothèque CUDA pour aboutir à des hautes performances de calcul. Enfin, comme application de nos travaux sur la MIBM, nous avons étudié le couplage "fort" d'interaction fluide-structure (IFS). Pour ce type de couplage, un schéma implicite partitionné a été adopté dans lequel les conditions à l'interface sont satisfaites via un schéma de type "point fixe". Pour réduire le temps de calcul inhérent à cette application, un nouveau schéma de couplage a été proposé pour éviter la résolution de l'équation de Poisson durant les itérations du "point fixe". Cette nouvelle façon de résoudre les problèmes IFS a montré des performances prometteuses pour des systèmes en IFS complexe. / In this thesis a novel non-body conforming mesh formulation is developed, called the moving immersed boundary method (MIBM), for the numerical simulation of fluid-structure interaction (FSI). The primary goal is to enable solids of complex shape to move arbitrarily in an incompressible viscous fluid, without fitting the solid boundary motion with dynamic meshes. This novel method enforces the no-slip boundary condition exactly at the fluid-solid interface with a boundary force, without introducing any artificial constants to the rigid body formulation. As a result, large time step can be used in current method. To determine the boundary force more efficiently in case of moving boundaries, an additional moving force equation is derived and the resulting system is solved by the conjugate gradient method. The proposed method is highly portable and can be integrated into any fluid solver as a plug-in. In the present thesis, the MIBM is implemented in the fluid solver based on the projection method. In order to obtain results of high accuracy, the rotational incremental pressure correction projection method is adopted, which is free of numerical boundary layer and is second order accurate. To accelerate the calculation of the pressure Poisson equation, the multi-grid method is employed as a preconditioner together with the conjugate gradient method as a solver. The code is further parallelized on the graphics processing unit (GPU) with the CUDA library to enjoy high performance computing. At last, the proposed MIBM is applied to the study of two-way FSI problem. For stability and modularity reasons, a partitioned implicit scheme is selected for this strongly coupled problem. The interface matching of fluid and solid variables is realized through a fixed point iteration. To reduce the computational cost, a novel efficient coupling scheme is proposed by removing the time-consuming pressure Poisson equation from this fixed point interaction. The proposed method has shown a promising performance in modeling complex FSI system.

Les capsules, formées d’une goutte protégée par une membrane élastique, sont très présentes naturellement et dans diverses applications industrielles, mais peu d’études ont exploré les phénomènes transitoires de leur relaxation. L’objectif est d’étudier l’influence de l’inertie et du confinement sur la relaxation d’une capsule sphérique (1) pré-déformée en ellipsoïde et relâchée dans un canal carré où le fluide est au repos, (2) sous écoulement dans un canal carré à expansion soudaine (‘marche’). La capsule est modélisée comme un fluide Newtonien dans une membrane hyper-élastique sans épaisseur ni viscosité, et simulée en couplant les méthodes Volumes Finis - Eléments Finis - frontières immergées. Sa relaxation dans un fluide au repos comporte 3 phases : amorçage du mouvement du fluide, phases rapide puis lente de rétraction de la membrane. Trois régimes existent selon le rapport de confinement et le rapport des nombres de Reynolds et capillaire : amortissements pur, critique ou oscillant. Un modèle de Kelvin-Voigt inertiel est proposé pour prédire les temps de réponse et aussi appliqué à une capsule en écoulement dans le canal microfluidique avec marche. La comparaison aux simulations 3D montre sa pertinence aux temps courts de la relaxation. Ces travaux ouvrent la voie à l’étude d’écoulements transitoires de capsules confinées dans des systèmes microfluidiques complexes. / Capsules, made of a drop protected by an elastic membrane, are widly present in nature and in diverse industrial applications, but few studies have explored the transient phenomena governing their relaxation. The objective of the PhD is to study the influence of inertia and confinement on the relaxation of a spherical capsule (1) pre-deformed into an ellipsoid and released in a square channel where the fluid is quiescent, (2) flowing in a square channel with a sudden expansion (‘step’). The capsule is modeled as a Newtonian fluid in a hyperelastic membrane without thickness or viscosity and is simulated coupling the Finite Volume - Finite Element - Immersed Boundary Methods. Its relaxation in a quiescent fluid exhibits three phases: the initiation of the fluid motion, the rapid and then slow retraction phases of the membrane. Three regimes exist depending on the confinement ratio and the Reynolds to capillary number ratio: pure, critical or oscillating damping. A Kelvin-Voigt inertial model is proposed to predict the response time constants and also applied to a capsule flowing in the microfluidic channel with a step. The comparison to 3D simulations shows its relevance at short relaxation times. This work paves the way to the study of transient flows of capsules confined in microfluidic devices.

Les tubes des générateurs de vapeur des centrales nucléaires vibrent sous l'effet d'écoulement eau/vapeur. Pour appréhender ce phénomène et le comprendre, des expériences à échelles réduites sont réalisées. La simulation numérique a montré son habilité à reproduire l'interaction fluide-structure sur ce type de géométrie pour des écoulements monophasiques. L'objectif est désormais de faire de même en écoulement diphasique et de caractériser les propriétés physiques du mélange liquide/gaz influant sur la vibration.Pour se faire, un code CFD avec une approche bi-fluide est utilisé. Une méthode dite de "Discrete forcing" est implémentée pour permettre le mouvement imposé de corps solides au sein d'un écoulement à plusieurs phases. Celle-ci est alros validée sur des cas simples et intégraux avec une comparaison systématique à des résultats expérimentaux ou théoriques.En se basant sur un algorithme implicite existant dans la littérature, un couplage fluide-structure utilisant cette méthode de suivi d'interface est implémenté. Validé sur des cas monophasiques et diphasiques, ce couplage offre désormais la possibilité de déplacer un solide en fonction des forces fluides diphasiques qui lui sont appliquées.Les différentes méthodes numériques présentes dans NEPTUNE_CFD sont ensuite évaluées pour un écoulement fréon/fréon au travers d'un faisceau de tubes inclinés. La nécessité d'utiliser des modèles dit "multi-régime" est mis en avant.Afin de déterminer l'influence sur l'écoulement des différentes propriétés physiques d'un mélange diphasique, plusieurs cas simples sont réalisés.Finalement, l'application industrielle cible, un écoulement eau/fréon dans un faisceau de tubes à pas carré, est simulée et comparée à un écoulement en conditions réelles (eau/vapeur à 70 bar). Les vibrations induites par écoulement monophasique puis diphasique sont correctement reproduites sur des cas dit de "faisabilité". / In nuclear power plants, steam generator tubes vibrate because of steam/water cross-flows. In order to understant this phenomenon, reduced-scale experiments are performed. Numerical simulations have shown their ability to accurately reproduce the vibration induced by a single phase flow in a tube bundle. The aim of the present work is to do the same with two-phase flow and to characterize the effect of the mixture physical properties on vibration.To do so, a CFD code based on a two-fluid approach is used. A "discrete forcing" method is implemented in order to allow solid body motion in a two-phase flow. The validation is performed with simple and industrial cases using experimental and theoretical results.Using an existing implicit algorithm, a fluid-structure coupling based on the developed interface tracking method is implemented. Validated for single and two-phase flows, it is now possible to have solid motion induced by fluid forces.The different numerical models dedicated to two-phase flows are then evaluated on a freon/freon flow across an inclined tube bundle. The use of a multi-regime model is required. In order to investigate the role of the different physical properties on the vibration, three simple studies are performed.Finally, the industrial application, a freon/water flow across a square pitch tube bundle, is performed. First, it is compared to a steam/water flow in order to characterize the discrepancies when we are using a modeling mixture. Then, the vibration induced by single- and two-phase flows is reproduced by the developed method on feasibility test cases.

[pt] O escoamento de cápsulas suspensas em uma fase líquida através de canais e capilares micrométricos representa um problema complexo que ocorre em diferentes aplicações, de glóbulos vermelhos em hemodinâmica até escoamento em meios porosos. Em aplicações de meios porosos, a compreensão da dinâmica na microescala é fundamental para avaliar o comportamento macroscópico do escoamento. Canais e capilares com constrição podem ser usados para modelar uma garganta conectando dois poros adjacentes. O escoamento de uma cápsula suspensa através de tais modelos foi analisado para avaliar as características do escoamento considerando os efeitos inerciais (isto é, número de Reynolds finito), incluindo a máxima diferença de pressão necessária para empurrar uma cápsula através da constrição em função do raio da cápsula, a tensão inicial e o material da membrana, geometria do canal e do capilar, assim como as condições de escoamento. De fato, neste estudo, a resposta da pressão é fundamental para avaliar o efeito de bloqueio da cápsula. As fases líquidas internas e externas foram descritas pelas equações de Navier-Stokes, enquanto que a dinâmica da membrana da cápsula foi modelada por uma estrutura flexível 1-D tipo mola. O problema de interação fluido-estrutura foi resolvido usando o método de elementos finitos acoplado ao método de fronteira imersa. Os resultados mostraram a redução da mobilidade da fase contínua devido à presença da cápsula através da constrição. Tais resultados podem ser usados para projetar microcápsulas para bloquear caminhos preferenciais de fluxo da água no processo de deslocamento de óleo em meios porosos. / [en] The flow of capsules suspended in a liquid phase through small channels and capillaries poses a complex problem presented in different applications, from red blood cells on hemodynamics to flow in porous media. In applications of porous media, the understanding of microscale dynamics is fundamental to assess the macroscopic flow behavior. Constricted channels and capillaries can be used to model a pore throat connecting two adjacent pore bodies. The flow of a suspended capsule through such models was analyzed to evaluate the flow characteristics considering inertial effects (i.e. finite Reynolds numbers), including the maximum pressure difference required to push a capsule through the constriction as a function of capsule radius, initial membrane tension, membrane material, channel and capillary geometries, as well as flow conditions. In fact, in this study, the pressure response is fundamental in order to assess the capsule blocking mechanism. Inner and outer liquid phases were described by the Navier-Stokes equations and capsule membrane dynamics was modeled by a 1-D spring-like flexible structure. The fluid-structure interaction problem was solved using the finite element method coupled with the immersed boundary method. Results showed the mobility reduction of the continuous phase due to the presence of a capsule as it flows through the constriction. Such results can be used to design microcapsules to block preferential water flow paths in oil displacement process in porous media.

Este trabalho consiste no desenvolvimento de ferramentas computacionais para análise não linear geométrica de interação fluido-casca utilizando o Método dos Elementos Finitos (MEF). O algoritmo para dinâmica dos fluidos é explícito e a integração temporal é baseada em linhas características. O código computacional é capaz de simular as equações de Navier-Stokes para escoamentos compressíveis tanto na descrição Euleriana como na descrição Lagrangeana-Euleriana arbitrária (ALE), na qual é possível prescrever movimentos para a malha do fluido. A estrutura é modelada em descrição Lagrangeana total através de uma formulação de MEF para análise dinâmica não linear geométrica de cascas baseada no teorema da mínima energia potencial total escrito em função das posições nodais e vetores generalizados e não em deslocamentos e rotações. Essa característica evita o uso de aproximações de grandes rotações. Dois modelos de acoplamentos são desenvolvidos. O primeiro modelo, ideal para problemas onde a escala de deslocamentos não é muito grande comparada com as dimensões do domínio do fluido, é baseado na descrição ALE e o acoplamento entre as duas diferentes malhas é feito através do mapeamento das posições locais dos nós do contorno do fluido sobre os elementos de casca e vice-versa, evitando a necessidade de coincidência entre os nós da casca e do fluido. A malha do fluido é adaptada dinamicamente usando um procedimento simples baseado nas posições e velocidades nodais da casca. O segundo modelo de acoplamento, ideal para problemas com grande escala de deslocamentos tais como estruturas infláveis, considera a casca imersa na malha do fluido e consiste em um procedimento robusto baseado em curvas de nível da função distância assinalada do contorno, o qual integra o algoritmo Lagrangeano de casca com o Fluido em descrição Euleriana, sem necessidade de movimentação da malha do fluido, onde a representação computacional do fluido se resume a uma malha não estruturada maior ou igual ao domínio inicial do fluido e a interface fluido-casca dentro da malha do fluido é identificada por meio de curvas de nível da função distância assinalada do contorno. Ambos os modelos são testados através de exemplos numéricos mostrando robustez e eficiência. Finalmente, como uma sugestão para o futuro desenvolvimento desta pesquisa, iniciaram-se estudos relativos a funções B-splines. O uso desse tipo de funções deverá resolver problemas de estabilidade relativos a oscilações espúrias devidas ao uso de polinômios de Lagrange para a representação de descontinuidades. / This work consists of the development of computational tools for nonlinear geometric fluid-shell interaction analysis using the Finite Element Method (FEM). The fluid solver is explicit and its time integration based on characteristics. The computational code is able to simulate the Navier-Stokes equations for compressible flows written in the Eulerian description as well as in the arbitrary Lagrangian-Eulerian (ALE) description, enabling movements prescription for the fluid mesh. The structure is modeled in a total Lagrangian description, using a FEM formulation to deal with geometrical nonlinear dynamics of shells based on the minimum potential energy theorem written regarding nodal positions and generalized unconstrained vectors, not displacements and rotations, avoiding the use of large rotation approximations. Two partitioned coupling models are developed. The first model, ideal for simulations where the displacements scale is not very large compared to the fluid domain, is based on the ALE description and the coupling between the two different meshes is done by mapping the fluid boundary nodes local positions over the shell elements and vice-versa, avoiding the need for matching fluid and shell nodes. The fluid mesh is adapted using a simple approach based on shell nodal positions and velocities. The second model, ideal for problems with large scales of displacements such as inflatable structures, is based on immersed boundary and consists of a robust level-set based approach that integrates the Lagrangian shell finite and the Eulerian finite element high speed fluid flow solver, with no need for mesh adaptation, where the fluid representation relies on a fixed unstructured mesh larger or equal to the initial fluid domain and the fluid-shell interface inside the fluid mesh is tracked with level sets of a boundary signed distance function. Both models are tested with numerical examples, showing efficiency and robustness. Finally, as a suggestion for future development of this research, we started studies relatives to B-Spline functions. The use of this kind of functions should solve stability problems related to spurious oscillations due to the use of Lagrange polynomials for representing discontinuities.