O fenômeno de vibração induzida por vórtices em travessas de pré-distribuidores de turbinas hidráulicas tem sido estudado nos últimos anos e várias soluções têm sido adotadas para minimizar interferências na estrutura que podem causar fratura por fadiga. O princípio básico das modificações é alterar o perfil da travessa de modo que as frequências de emissão de vórtices não coincidam com as frequências naturais da estrutura. Este trabalho tem como objetivo avaliar através de uma série de simulações computacionais um perfil mais adequado para um pré-distribuidor de turbina Francis. Essas simulações envolvem o cálculo do escoamento ao redor da travessa e da vibração induzida por vórtices nele presentes, bem como uma técnica que combina as análises dinâmicas com uma otimização paramétrica. Para isso, foi utilizado um código comercial de CFD, ANSYS Fluent e o cálculo da resposta estrutural e seu acoplamento com as equações do escoamento foi feito através de uma UDF (User Defined Function). Para validar a metodologia, a resposta estrutural de um corpo prismático sobre base elástica foi calculada e comparada a dados previamente publicados na literatura. Por fim, um código desenvolvido controla a análise fluido-estrutural e passa as variáveis para o otimizador Mode Frontier, que trabalha para encontrar a estrutura mais eficiente variando-se os parâmetros pré-determinados da geometria da peça. A metodologia desenvolvida tem a vantagem de ajudar no projeto de tais componentes sem depender excessivamente de métodos experimentais ou regras empíricas. Dessa forma, torna possível modificar perfis existentes ou desenvolver perfis novos baseado nos melhores critérios de manufatura. / Vortex induced vibration phenomena in hydraulic turbines stay vanes have been studied in the last years and several solutions have been adopted in order to minimize interferences that can cause fatigue in the structure. The basic principle of all modifications is to change the stay vane profile so the natural vortex shedding frequency is different from the natural frequencies of the structure. This work presents a detailed computational simulation of a Francis turbine stay vane whose main objective is to find out a more suitable profile these components should assume. These simulations involve the calculation of the flow around the vanes and the associated vortex induced vibration in the structure in addition to a technique that combines the dynamic analysis with a parametric optimization In order to do that, a commercial CFD code, ANSYS Fluent, was adopted and the calculation of the structural response and its coupling with the flow equations was done with User Defined Functions. Validation of the methodology was made by comparing the structural response of an elastically-mounted prismatic body immersed in uniform flow with previously published data. Finally, a developed code controls the FSI analysis and provides information about the vibrations to the Mode Frontier optimizer, responsible to address the problem and determine the set of parameters that lead to the most efficient structure. The methodology developed has the advantage of helping the design of such components without depending excessively on experimental methods or empirical rules. Also, it allows either modifying existing profiles or choosing the best shape for new ones based on the best manufacturing criteria.

Submitted by Renata Lopes (renatasil82@gmail.com) on 2017-02-24T14:44:47Z No. of bitstreams: 1 marceloribeiro.pdf: 3015247 bytes, checksum: 325fa8dffab659edce18dc9c5f1f485c (MD5) / Approved for entry into archive by Adriana Oliveira (adriana.oliveira@ufjf.edu.br) on 2017-02-24T15:39:52Z (GMT) No. of bitstreams: 1 marceloribeiro.pdf: 3015247 bytes, checksum: 325fa8dffab659edce18dc9c5f1f485c (MD5) / Made available in DSpace on 2017-02-24T15:39:52Z (GMT). No. of bitstreams: 1 marceloribeiro.pdf: 3015247 bytes, checksum: 325fa8dffab659edce18dc9c5f1f485c (MD5) Previous issue date: 2013-04-01 / CAPES - Coordenação de Aperfeiçoamento de Pessoal de Nível Superior / A construção de edifícios, especialmente os mais esbeltos, requer uma análise apurada do comportamento dinâmico da estrutura. Tais estruturas são sujeitas a movimentos induzidos pelo vento, entre outras forças, o que pode causar efeitos indesejáveis tais como desconforto para os usuários ou até mesmo causar o colapso estrutural. Neste cenário, os sistemas de controle são utilizados a fim de atenuar a vibração excessiva. Dentre estes sistemas, aqueles que utilizam respostas dinâmicas das estruturas para a determinação das forças de controle, de um modo geral, quando adequadamente construídos, têm um desempenho satisfatório. Pode-se destacar o sistema de controle com retroalimentação. No entanto, o uso desses controladores em edifícios requer uma certa quantidade de testes e simulações, uma vez que os problemas em qualquer fase do processo de controle pode transformar um controlador ativo em um excitador, o que obviamente não é desejável. Neste trabalho foi realizada uma análise numérica de um modelo de sistema estrutural sujeito a forças dinâmicas de vento, onde as vibrações foram controladas por meio de um sistema de controle ativo. As forças de excitação foram obtidas por análise da fluidodinâmica computacional e as forças de controle foram obtidas aplicando a técnica de controle ótimo. Esta etapa constitui uma das primeiras fases do projeto de um controle. / The construction of buildings, especially the most slender, requires a detailed analysis of the structural dynamic behavior. Such structures are subject to movements induced by the wind and other forces, which can cause undesirable effects such as discomfort for the user or even cause the structural collapse. In this scenario, control systems are used to mitigate excessive vibration. Among these systems, those using dynamic responses of the structures to determine control forces, in general, when properly constructed, have satisfactory performance as control systems with feedback. However, the use of these controllers in buildings requires a certain amount of tests and simulations, since problems at any stage of the control process, may transform an active controller into an excitator, which is obviously undesirable. In this work a numerical analysis of a structural model subject to dynamic wind forces was performed. The excitation forces were obtained by computational uid dynamics analysis and control forces were obtained by applying the technique of optimal control. The present analysis is one of the first phases of a control design.

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.

No description available.

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.

No description available.

The aim of this Master’s thesis was to study the dynamic behaviour of a special type ofpedestrian timber bridge with a single diagonal arch - a design proposal made in a previousstudent project. The bridge is intended to be built as a gateway to the Alfred Nobel’s Björkbornin the municipality of Karlskoga. The original plan for this thesis was to build and test adownscaled model in order to verify theoretical investigations. The laboratory testing washowever not possible to be performed, therefore the study was conducted only by means ofanalytical and numerical tools. Both a downscaled model and a full-scale bridge model wereanalysed and compared in order to find proper scale parameters. Different studies wereperformed on the models by means of the finite element method in order to investigate theinfluence of relevant parameters on dynamic behaviour of the bridge. A scale factor wasdetermined which allows for the translation of results from the downscaled model to the fullscale model. Results showed that the dynamic behaviour of this type of bridge is rathercomplicated, and the original design needs to be somewhat modified to meet the comfortcriterion for pedestrians. An increase of the width of the arch, a proper arrangement of thecables, and adoption of longitudinal steel beams under the deck were found to be efficientmethods to improve the dynamic performance of the bridge. Future work should includeexperiments on a downscaled model to validate these theoretical solutions.

<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)

Os resultados de uma simulação numérica são apresentados para amplitudes de vibração induzidas por um escoamento transversal num feixe tubular no regime de instabilidade fluidelástica.O feixe tubular considerado tem geometria e características iguais às de uma instalação equivalente descrita na literatura, para a qual estão disponíveis as medições experimentais das amplitudes de vibração no regime de instabilidade elástica.O arranjo tipo triângulo rodado tem uma relação passo/diâmetro de 1,375 e consiste de um tubo móvel cercado por 134 tubos rígidos.A simulação numérica foi efetuada através de um software comercial de CFD (Computational Fluid dynamics).Para a região em torno de cada tubo foi considerada uma malha com dimensões do elemento crescendo geometricamente na direção normal ao tubo com fator de crescimento 1,13 , sendo a dimensão do elemento adjacente ao tubo igual a 0,1% do diâmetro externo do tubo.Na simulação numérica o escoamento foi considerado incompressível, monofásico, turbulento e bidimensional. Os dados do escoamento foram considerados idênticos aos das experiências da instalação descrita na literatura.Os resultados obtidos para as amplitudes pela simulação numérica são comparados com os resultados obtidos experimentalmente na instalação acima citada.Os desvios da maioria dos valores calculados em relação aos valores experimentais estão numa faixa aceitável. Isto mostra que existe a possibilidade de utilização, num futuro próximo, de CFD para análise deste tipo de problemas. / Results from a numerical simulation are reported for amplitudes of cross-flow induced vibrations at the fluid elastic instability regime in a tube bank. The tube bank has identical geometry and characteristics as for an experimental facility described in the literature, for which there are experimental measurements of the amplitudes of vibrations at the fluid elastic instability regime.The rotated triangular array has a pitch ratio of 1.375 and consists of 1 movable tube surrounded by 134 rigid tubes. The numerical simulations were accomplished with a commercial CFD (Computational Fluid Dynamics) software. For the region around each tube, a mesh with elements dimensions growing geometrically normal to the tube was considered, with growing factor 1.13, and the dimension for the element adjacent to the tube wall was set to 0.1% of the tube external diameter. The flow was considered incompressible, monophasic, turbulent and two-dimensional for the numerical simulation. The flow data considered were the same as for the experiments at the facility. The results presented in this paper for the amplitudes obtained by numerical simulation are compared with the experimental results obtained in the above mentioned experimental facility.The differences between the calculated values and the experimental values are acceptable. This show that in the near future there is the possibility to use CFD for these kind of problems.