[pt] Vibrações induzidas por escoamento tem apresentado cada vez mais importância na indústria do petróleo. A vibração de colunas produção, somada aos ciclos normais de oscilação de temperatura e pressão dos poços, pode causar o desgaste dos diversos micro-componentes presentes no sistema. Uma potencial fonte de perturbação, em poços injetores, é a turbulência do escoamento formado por um jato que sai em alta velocidade da coluna de injeção e atinge a parede do revestimento. No presente estudo, investiga-se o efeito causado por jatos confinados no espaço anular formado por dois tubos concêntricos. A geometria assemelha-se àquela de um poço injetor, entretanto os números de Reynolds analisados são inferiores ao caso real. O objetivo do presente trabalho foi analisar o comportamento desse tipo de escoamento sob diferentes condições, no que diz respeito a número de Reynolds, distância em relação a superfície e número de jatos presentes no espaço anular. O escoamento no interior do espaço anular foi caracterizado com a técnica de velocimetria por imagem de partículas com alta resolução temporal (time resolved PIV). O comportamento dinâmico das perturbações foi analisado e as estruturas espaciais mais relevantes foram estimadas utilizando a decomposição por modos próprios ortogonais. Os resultados mostram que na presença de dois jatos o escoamento o escoamento apresenta flutuações periódicas mais intensas, com frequências bem definidas, sugerindo um acoplamento dos jatos. Foram realizados experimentos para estimar os coeficientes de transferência de calor associados com esse escoamento. Para isso, foram realizados experimentos com aquecimento da superfície do tubo externo. Nos casos com jatos próximos a superfície, os resultados sugerem que ocorre uma redução da transferência de calor na região de estagnação do jato. / [en] Flow induced vibration has shown an increasingly higher relevance in oil and gas industry. The vibration of completion strings, plus normal cycles of wells, can cause premature failure of micro-components present in the system. Flow turbulence is a potential source of vibration for the system. In injection wells, the fluid flows from the inner pipe (completion string) towards the surface of the external pipes (casings). This flow frequently has a turbulent behaviour, due to the high flow rates employed. In the present study, flow resulting from jets in a confined annular space is investigated, for different parameters, including Reynolds number, pipe diameters and number of jets. The geometry resembles that of an injection well, however the Reynolds numbers analyzed are lower than the actual case. The flow field inside the annular space is characterized using time resolved PIV (Particle Image Velocimetry) techniques. The dynamic behavior of the perturbations was analyzed and the most relevant spatial structures were estimated using Proper Orthogonal Decomposition (POD). Results show that, in presence of two jets, flow exhibits intense periodic fluctuations, with well-defined frequencies This suggests the presence of a coupling between jets. Experiments are carried out to estimate the heat transfer coefficients associated with this flow. In the cases with jets close to the surface, results suggest that a reduction of heat transfer occurs in the region of jet stagnation.

As Vibrações Induzidas por Escoamentos (VIEs) são dos problemas dinâmicos mais importantes no projeto de trocadores de calor de tipo carcaça e tubos. Esta interação fluido - estrutura pode gerar vibrações de grande amplitude dos tubos ou partes internas do equipamento, o que pode provocar o impacto entre componentes e até falha por fadiga. Várias bancadas experimentais têm sido construídas para o estudo desta interação fluido - estrutura, no entanto, alguns mecanismos de vibração, principalmente aqueles relacionados com escoamentos bifásicos, não são completamente compreendidos. Portanto, neste trabalho, o projeto de uma estrutura dinâmica para o estudo das vibrações induzidas por escoamento bifásico é apresentado. Esta estrutura é composta por um sistema de fios de aço tensionados que permitem que a primeira frequência de ressonância do tubo seja sintonizada. O tubo instrumentado foi instalado numa seção de testes de tubos rígidos em configuração triangular normal com uma razão de passo transversal e diâmetro de 1,26. Os resultados experimentais foram contrastados com uma modelagem teórica desenvolvida para esta estrutura dinâmica. Pôde-se verificar que a primeira frequência de ressonância e seu fator de amortecimento coincidem com os valores estimados pelo modelo, enquanto que a segunda frequência de ressonância apresenta valor teórico 6,6% maior do que o experimental. A seguir, um estudo experimental no ar foi desenvolvido para o reconhecimento dos modos de vibração e as frequências de ressonância da estrutura dinâmica. O fator de amortecimento no ar também foi estimado, o método de Kennedy - Pancu combinado com o algoritmo ERA foi usado para este fim. Assim que a primeira frequência de ressonância foi reconhecida e sintonizada, testes em escoamentos de água foram realizados. A influência da velocidade do escoamento monofásico de água na amplitude de vibração e nas características da Densidade Espectral (PSD) de aceleração foi analisada. Finalmente, testes em escoamento bifásico foram feitos, a sensibilidade do tubo ao escoamento bifásico fica evidente quando analisadas as amplitudes nas PSDs. Além disso, a influência da fração de vazio na amplitude de vibração e no fator de amortecimento foi revisada, no entanto, resultados de estudos anteriores não foram conferidos pelo alto amortecimento concentrado introduzido por alguns elementos construtivos utilizados. / Flow - Induced Vibration (FIV) is the most critical dynamic issue in the design of heat exchangers. This fluid - structure phenomenon may generate high amplitude vibration of tubes or structural parts, which may lead to impacts between internal components or even failure due to fatigue. Many test benches have been constructed to study this fluid - structure interactions, however, some vibration mechanisms, mostly those related to multiphase flow, are not yet fully understood. Therefore, in this work, the design of a dynamic structure for the study of multiphase flow induced vibration is presented. This structure is composed by a system of tensioned piano wires that allow the first natural frequency of the instrumented tube to be calibrated. The tube was installed in a rigid bundle configured in a normal triangular pattern with pitch-todiameter ratio of 1.26. Then, an experimental study in air environment was performed aiming at addressing the mode shapes and resonance frequencies of the dynamic structure. The damping ratio in air environment was also estimated, the Kennedy - Pancu method in combination with the Eigensystem Realization Algorithm have been used to that purpose. Experimental results in air were compared with a theoretical model. The first resonance frequency and its damping factor presented a good agreement with the model, while the second resonance frequency deviated some 6,6% from the predicted value. Tests in water and multiphase flow were also performed. The influence of water flow velocity on vibration amplitudes and on the Power Spectrum Densities (PSDs) has been analyzed. Finally, tests for two - phase water/air flow were carried out; the tube sensitivity to multiphase flow is evident when the vibration level in acceleration PSDs is by analyzed. Also, the influence of void fraction on vibration amplitude and damping ratio have been addressed, however, previous studies could not be validated due to the high damping introduced by some constructive elements of the structure.

The purpose of this study is to investigate the flue gas fan in Mälarenergi’s Unit 6 and try to find what is causing the vibrations increase. The Fast Fourier transform (FFT) method was used for this degree project. A comparison was made with previous studies using FFT in order to pinpoint the source of the problem with vibrations. After a possible source had been identified, a computational fluid dynamics (CFD) simulation was performed using ANSYS to visualize the problem. Two cases were simulated using two different turbulence models: the K-epsilon model and the Large-eddy simulation (LES) model. The result from the CFD simulations was compared with previous studies that used similar turbulence models. The flue gas fan’s high vibrations are most likely flow-induced. The simulation result indicates that LES model performed better than the Kepsilon model. The lack of validation in this degree work means that it is hard to know the accuracy of the model. Based on the simulation results the most promising solution seems to be inlet straighteners. / Syftet med studien är att undersöka rökgasfläkten i Mälarenergis Unit 6 och att försöka hitta vad som orsakar vibrationsökningarna. Fast Fourier transform metoden har används i detta examensarbete. En jämförelse har gjorts med tidigare studier som använt FFT metoden för att kunna urskilja källan till vibrationsproblemet. Efter en rimlig källa hittades så utfördes en CFD-simulering i ANSYS för att visualisera problemet. Två fall simulerades med två olika turbulensmodeller: K-epsilon modellen och Largeeddy simulation modellen. Resultatet från CFD-simuleringarna jämfördes med tidigare studier som använt liknande metoder.  Rökgasfläktens höga vibrationer är med störst sannolikhet flödesinducerad. Simuleringsresultatet indikerar att LES modellen utfördes bättre än Kepsilon modellen. Då det saknas en validering i form av flödesmätningar så är det svårt att säga hur lik modellen är med verkligheten. Baserat på resultatet från simuleringarna så verkar inloppsgaller vara den mest lovande lösningen.

As Vibrações Induzidas por Escoamentos (VIEs) são dos problemas dinâmicos mais importantes no projeto de trocadores de calor de tipo carcaça e tubos. Esta interação fluido - estrutura pode gerar vibrações de grande amplitude dos tubos ou partes internas do equipamento, o que pode provocar o impacto entre componentes e até falha por fadiga. Várias bancadas experimentais têm sido construídas para o estudo desta interação fluido - estrutura, no entanto, alguns mecanismos de vibração, principalmente aqueles relacionados com escoamentos bifásicos, não são completamente compreendidos. Portanto, neste trabalho, o projeto de uma estrutura dinâmica para o estudo das vibrações induzidas por escoamento bifásico é apresentado. Esta estrutura é composta por um sistema de fios de aço tensionados que permitem que a primeira frequência de ressonância do tubo seja sintonizada. O tubo instrumentado foi instalado numa seção de testes de tubos rígidos em configuração triangular normal com uma razão de passo transversal e diâmetro de 1,26. Os resultados experimentais foram contrastados com uma modelagem teórica desenvolvida para esta estrutura dinâmica. Pôde-se verificar que a primeira frequência de ressonância e seu fator de amortecimento coincidem com os valores estimados pelo modelo, enquanto que a segunda frequência de ressonância apresenta valor teórico 6,6% maior do que o experimental. A seguir, um estudo experimental no ar foi desenvolvido para o reconhecimento dos modos de vibração e as frequências de ressonância da estrutura dinâmica. O fator de amortecimento no ar também foi estimado, o método de Kennedy - Pancu combinado com o algoritmo ERA foi usado para este fim. Assim que a primeira frequência de ressonância foi reconhecida e sintonizada, testes em escoamentos de água foram realizados. A influência da velocidade do escoamento monofásico de água na amplitude de vibração e nas características da Densidade Espectral (PSD) de aceleração foi analisada. Finalmente, testes em escoamento bifásico foram feitos, a sensibilidade do tubo ao escoamento bifásico fica evidente quando analisadas as amplitudes nas PSDs. Além disso, a influência da fração de vazio na amplitude de vibração e no fator de amortecimento foi revisada, no entanto, resultados de estudos anteriores não foram conferidos pelo alto amortecimento concentrado introduzido por alguns elementos construtivos utilizados. / Flow - Induced Vibration (FIV) is the most critical dynamic issue in the design of heat exchangers. This fluid - structure phenomenon may generate high amplitude vibration of tubes or structural parts, which may lead to impacts between internal components or even failure due to fatigue. Many test benches have been constructed to study this fluid - structure interactions, however, some vibration mechanisms, mostly those related to multiphase flow, are not yet fully understood. Therefore, in this work, the design of a dynamic structure for the study of multiphase flow induced vibration is presented. This structure is composed by a system of tensioned piano wires that allow the first natural frequency of the instrumented tube to be calibrated. The tube was installed in a rigid bundle configured in a normal triangular pattern with pitch-todiameter ratio of 1.26. Then, an experimental study in air environment was performed aiming at addressing the mode shapes and resonance frequencies of the dynamic structure. The damping ratio in air environment was also estimated, the Kennedy - Pancu method in combination with the Eigensystem Realization Algorithm have been used to that purpose. Experimental results in air were compared with a theoretical model. The first resonance frequency and its damping factor presented a good agreement with the model, while the second resonance frequency deviated some 6,6% from the predicted value. Tests in water and multiphase flow were also performed. The influence of water flow velocity on vibration amplitudes and on the Power Spectrum Densities (PSDs) has been analyzed. Finally, tests for two - phase water/air flow were carried out; the tube sensitivity to multiphase flow is evident when the vibration level in acceleration PSDs is by analyzed. Also, the influence of void fraction on vibration amplitude and damping ratio have been addressed, however, previous studies could not be validated due to the high damping introduced by some constructive elements of the structure.

Neste trabalho, o escoamento incompressível ao redor de um cilindro fixo é estudado numericamente através do método de elementos finitos. Foram realizadas simulações bidimensionais no domínio do tempo, com números de Reynolds variando entre 100 e 600, utilizando-se, para tanto, malhas não-estruturadas com elementos triangulares. Pretende-se aqui analisar a eficácia da solução das equações de Navier-Stokes utilizando o método das penalidades, meio pelo qual o acoplamento pressão-velocidade foi tratado. Avalia-se a convergência da solução para diferentes valores do fator de penalidade e sugere-se um método para estimá-lo. Analisa-se, ainda, a sensibilidade da resposta à utilização da matriz de inércia nos formatos consistente e concentrada. Por fim, é realizada a comparação dos coeficientes de arrasto médio, flutuação do coeficiente de sustentação e número de Strouhal obtidos neste trabalho com resultados de outras publicações. / In this work, the incompressible flow around a stationary cylinder is investigated by using the Finite Element Method. Two-dimensional simulations in time domain have been carried out, with Reynolds number varying from 100 to 600, using non-structured meshes with triangular elements. The aim of this work is to analyze the efficiency of Penalty Methods, which is the way that the velocity-pressure coupling problem is treated here, in Navier-Stokes equations solution. The solution convergence from different values of penalty parameter is evaluated and it is suggested a method to estimate it. In addition, it is studied the sensibilty of response when using the mass matrix in consistent or lumped format. At last, a comparison between average drag coefficient, fluctuating lift and Strouhal number obtained here and those found in other publications is shown.

Vortex shedding is an important mechanism, by which the flow around bluff bodies create forces that excite vibratory motion. Vortex-induced vibration (VIV) is studied for a single circular cylinder by means of Computational Fluid Dynamics (CFD) simulations. An arbitrary Lagrangian Eulerian (ALE) formulation is used to achieve the grid deformation needed for VIV. In this thesis, a multifaceted approach is undertaken by which response dynamics and wake interaction are addressed. Four major aspects are considered in the study: the Reynolds number (Re); the mass and damping; the degree-of-freedom for VIV; and the mutual effect between VIV and heat transfer.As attention is paid towards high pre-critical Re flow, the turbulent flow around the cylinder is treated by two turbulence modelling approaches: unsteady Reynolds Averaged Navier Stokes (uRANS), and Large Eddy Simulation (LES). The wake-VIV interaction is analyzed by looking at mean velocities and Reynolds stresses, where decomposition of flow scales is undertaken to explore the evolution of coherent eddy structures, downstream of the cylinder. Conversely, the VIV response is analyzed by considering oscillation amplitude and frequency, in addition to the excitation and inertial dynamics.High turbulence in the separated shear layers disorders the cylinder's VIV response and induces higher amplitudes. The sensitivity for Re is found more pronounced in cylinders with low mass and damping. Meanwhile, VIV is found to enhance wake mixing, and to significantly change the near wake Reynolds stresses. It is suggested that the increase in Re brings a change to the wake patterns, which are known in VIV at lower Re. The kinetic energy production, of near wake eddy structures, is qualitatively altered with the presence of VIV. Furthermore, the surface heat flux is found to cause a noticeable increase in VIV amplitude, as long as it does not disorder the wake correlation. The cylinder's oscillation increases the average value of the Nusselt number (Nu), while the local variance of Nu rises markedly post-separation.

In this research, an elastic cylinder that utilized vortex-induced vibration (VIV) was applied to improve convective heat transfer rates by disrupting the thermal boundary layer. Rigid and elastic cylinders were placed across a fluid channel. Vortex shedding around the cylinder led to the periodic vibration of the cylinder. As a result, the flow-structure interaction (FSI) increased the disruption of the thermal boundary layer, and therefore, improved the mixing process at the boundary. This study aims to improve convective heat transfer rate by increasing the perturbation in the fluid flow. A three-dimensional numerical model was constructed to simulate the effects of different flow channel geometries, including a channel with a stationary rigid cylinder, a channel with a elastic cylinder, a channel with two elastic cylinders of the same diameter, and a channel with two elastic cylinders of different diameters. Through the numerical simulations, the channel maximum wall temperature was found to be reduced by approximately 10% with a stationary cylinder and by around 17% when introducing an elastic cylinder in the channel compared with the channel without the cylinder. Channels with two-cylinder conditions were also studied in the current research. The additional cylinder with the same diameter in the fluid channel only reduced the surface wall temperature by 3% compared to the channel without any cylinders because the volume of the second cylinder could occupy some space, and therefore, reduce the effect of the convective heat transfer. By reducing the diameter of the second cylinder by 25% increased the effect of the convection heat transfer and reduced the maximum wall temperature by around 15%. Compared to the channel with no cylinder, the introduction of cylinders into the channel flow was found to increase the average Nusselt number by 55% with the insertion of a stationary rigid cylinder, by 85% with the insertion of an elastic cylinder, by 58% with the insertion of two cylinders of the same diameter, and by approximately 70% with the insertion of two cylinders of different diameters (the second cylinder having the smaller diameter). Furthermore, it was also found that the maximum local Nusselt number could be enhanced by around 200%-400% at the entrance of the fluid channel by using the elastic cylinders compared to the channel without cylinders.

One of the primary objectives of voice research is to better understand the biomechanics of voice production and how changes in properties of the vocal folds (VFs) affect voice ability and quality. Synthetic VF models provide a way to observe how changes in geometry and material property affect voice biomechanics. This thesis seeks to evaluate an approach of using a genetic algorithm to design synthetic VF models in three ways: first, through the development of a computationally cost-effective 3D vocal fold model; second, by creating and optimizing a variation of this model; and third, by validating the approach. To reduce computation times, a user-defined function (UDF) was implemented in low-fidelity 2D and 3D computational VF models. The UDF replaced the conventional meshed fluid domain with the mechanical energy equation. The UDF was implemented in the commercial finite element code ADINA and verified to produce results that were similar to those of 2D and 3D VF models with meshed fluid domains. Computation times were reduced by 86% for 2D VF models and 74% for 3D VF models while core vibratory characteristic changes were less than 5%. The results from using the UDF demonstrate that computation times could be reduced while still producing acceptable results. A genetic algorithm optimizer was developed to study the effects of altering geometry and material elasticity on frequency, closed quotient (CQ), and maximum flow declination rate (MFDR). The objective was to achieve frequency and CQ values within the normal human physiological range while maximizing MFDR. The resulting models enabled an exploration of trends between objective and design variables. Significant trends and aspects of model variability are discussed. The results demonstrate the benefit of using a structured model exploration method to create models with desirable characteristics. Two synthetic VF models were fabricated to validate predictions made by models produced by the genetic algorithm. Fabricated models were subjected to tests where frequency, CQ, and sound pressure level were measured. Trends between computational and synthetic VF model responses are discussed. The results show that predicted frequency trends between computational and synthetic models were similar, trends for closed quotient were inconclusive, and relationships between MFDR and sound pressure level remained consistent. Overall, while discrepancies between computational and synthetic VF model results were observed and areas in need of further study are noted, the study results provide evidence of potential for using the present optimization method to design synthetic VF models.

<p>This thesis investigates the characteristics of a long aspect ratio synthetic jet actuator and its application for the active control of the vibrations of the downstream cylinder in a tandem cylinder arrangement.</p> <p>A long aspect ratio synthetic jet is produced through an axial slit along part of the length of a cylinder. The jet is excited acoustically by a pair of loudspeakers mounted at the cylinder terminations. The study compares between the performance of two different slits with aspect ratios of 273 and 773. The comparison is based on the spanwise distribution of the mean jet velocity and phase between the jet velocity fluctuations and the excitation signal. Three different frequencies and amplitudes are used to excite the speakers covering the range of frequencies used in the control application.</p> <p>For both cases studied the mean centerline velocity of the jet increases with increasing the amplitude of the exciting signal, but decreases with increasing its frequency. Moreover, velocity deficits of up to 30% are evident as the midspan of the cylinder is approached from either end. Similar trends are also observed for the centerline phase distributions of the velocity fluctuations, with deficits of up to 130°. However, it is observed that for the long slit case the deficits in both the velocity and phase distributions are much larger than those for the short one.</p> <p>The synthetic jet is then mounted in the upstream cylinder of a tandem cylinder arrangement to be used as a control actuator for controlling the vibrations of the downstream cylinder. A simple feedback control mechanism is used at a Reynolds</p> <p>number of about 6.3x104. This Reynolds number corresponds to the case where the iii</p> <p>downstream cylinder’s response is dominated with two frequency components, one at the resonance frequency of the cylinder, which is excited by broadband turbulence in the flow, and the other at the vortex shedding frequency. Both slits studied for the characterization experiments are used to compare their performance as control actuators.</p> <p>Both jets produce comparable reductions in the vibration of the downstream cylinder. A reduction of about 20% in the total RMS amplitude of the vibrations signal is achieved. This amounts to a reduction of about 50% in the resonant peak and an average value of about 40% in the vortex shedding peak. The optimal values of gain and time lag of the controller are then used to investigate the effect of the jet on the flow. It is found that the short slit jet produced an effect that was traced up to 1.875 diameters downstream, while the effect of the long slit jet dropped dramatically very close to the upstream cylinder.</p> / Master of Applied Science (MASc)

This thesis provides a comprehensive investigation of flow-sound-structure coupling in spring-loaded valves subjected to air flow. While they are commonly used in a multitude of applications, these types of valves have been found to experience severe vibrations when interaction is present among the structure, the hydrodynamic field, and the acoustic field for a range of operational valve structural characteristics, flow parameters, and connected piping length. The first part of this investigation was aimed at characterizing experimentally the valve’s dynamic behaviour and the parameters affecting the onset of self-excited instability. The occurrence of instability was mainly driven by the presence of acoustic feedback: the connected length of piping had to be sufficiently long, with a longer pipe correlating to more severe vibrations. In addition, it was found that the valve’s oscillation frequency depends on the modal characteristics of the combined valve piping system, rather than the structural natural frequency alone. Furthermore, an increase in the valve’s spring stiffness caused the vibrations to become more severe. Meanwhile, other parameters such as initial spring preload force and valve plate area only had moderate effects on the stability behaviour of the valve. The second part of the investigation sought to develop a theoretical model that could simulate the valve’s response when subjected to air flow while considering the effects of acoustic feedback and impact on the seat and limiter. Thus, a structural model of the valve was developed based on a single-degree-of-freedom model of the system with impact computed based on a pseudo-force method. The hydrodynamic field relied on a one dimensional unsteady Bernoulli description of the flow. Finally, the acoustic interaction was accounted for using the one-dimensional wave equation resolved using a finite difference scheme. The model has demonstrated remarkable agreement with the experimental results. It has shown an ability to predict the modal characteristics of the system as well as correctly predict the effect of increased stiffness or increased piping length on vibration amplitude. The final part of the investigation consisted in designing countermeasures to mitigate the effects of this self-excited instability mechanism. A concentric Helmholtz-type cavity resonator, an orifice plate, and an anechoic termination are placed at the downstream side of a model valve which were seen to be unstable in the experimental and modelling phases of the investigation. All tested devices were able to eliminate the self excited instability mechanism. The applicability and robustness of each of these methods were discussed. / Thesis / Doctor of Philosophy (PhD)