A motion compensated ADV system was evaluated to determine its ability to make measurements necessary for characterizing the variability of the ambient current in the Gulf Stream. The impact of IMU error relative to predicted turbulence spectra was quantified, as well as and the ability of the motion compensation approach to remove sensor motion from the ADV measurements. The presented data processing techniques are shown to allow the evaluated ADV to be effectively utilized for quantifying ambient current fluctuations from 0.02 to 1 Hz (50 to 1 seconds) for dissipation rates as low as 3x10-7. This measurement range is limited on the low frequency end by IMU error, primarily by the calculated transformation matrix, and on the high end by Doppler noise. Inshore testing has revealed a 0.37 Hz oscillation inherent in the towfish designed and manufactured as part of this project, which can nearly be removed using the IMU. / Includes bibliography. / Thesis (M.S.)--Florida Atlantic University, 2014. / FAU Electronic Theses and Dissertations Collection

The numerical method presented in this study attempts to predict the mean, non-uniform flow field upstream of a propeller partially immersed in a thick turbulent boundary layer with an actuator disk using CFD based on RANS in ANSYS FLUENT. Three different configurations, involving an infinitely thin actuator disk in the freestream (Configuration 1), an actuator disk near a wall with a turbulent boundary layer (Configuration 2), and an actuator disk with a hub near a wall with a turbulent boundary layer (Configuration 3), were analyzed for a variety of advance ratios ranging from J = 0.48 to J =1.44. CFD results are shown to be in agreement with previous works and validated with experimental data of reverse flow occurring within the boundary layer above the flat plate upstream of a rotor in the Virginia Tech’s Stability Wind Tunnel facility. Results from Configuration 3 will be used in future aero-acoustic computations. / Includes bibliography. / Thesis (M.S.)--Florida Atlantic University, 2014. / FAU Electronic Theses and Dissertations Collection

Estudos do escoamento em vertedouros em degraus foram realizados experimentalmente por diversos autores, mas a utilização de ferramentas de computação numérica para a simulação destes casos ainda é muito escassa. Neste trabalho realizou-se um estudo da simulação numérica do escoamento sobre vertedores em degraus, utilizando-se um programa de fluidodinâmica computacional (CFD). As configurações geométricas e hidráulicas de alguns autores da literatura foram reproduzidas através das simulações em CFD. Com as simulações testaram-se as equações propostas experimentalmente ou compararam-se diretamente os resultados experimentais com os numéricos. As características dos escoamentos nos vertedouros em degraus que foram analisadas e comparadas são as seguintes: perda ou dissipação de energia, distribuição da velocidade, distribuição da concentração de ar, perfis de pressão do degrau, um estudo da resistência de atrito e um estudo da cavitação. Foram obtidas boas comparações entre os resultados experimentais e numéricos, desta forma, todas estas análises serviram, tanto para validar a utilização das ferramentas de fluidodinâmica computacional, como para caracterizar os escoamentos para uma possível proposta de melhora no desempenho desta estrutura hidráulica. Conhecendo-se o problema da cavitação, buscou-se uma solução para minimizar a ocorrência deste fenômeno no escoamento em vertedouro em degraus. Assim, foi realizado um estudo do escoamento em um aerador de fundo. Neste estudo do aerador de fundo foram caracterizados numericamente os perfis de concentração de ar, os perfis de pressão sob o salto do aerador, os perfis de velocidade e ainda foi realizado um estudo da vazão de ar que alimenta a aeração sob o jato do aerador. Após este estudo do aerador de fundo, uma nova de configuração geométrica foi proposta para o vertedouro em degrau, com a construção de um aerador de fundo no início do escoamento de forma a minimizar o risco de cavitação ou ainda aumentar as vazões máximas de serviço. / Several experimental studies about stepped spillways flow were carried out by several authors, no ever the use of numeric computation tools is still very scarce. This work study numeric simulation in stepped spillways flow was carried out using a computation fluid dynamic (CFD) software. Several hydraulics conditions from the literature were reproduced through simulations by CFD tools. Those simulation results were compared with experimental results. The characteristics of the flow in stepped spillways were analyzed and compared focusing the following aspects: energy dissipation, velocity distribution, air concentration distribution, pressure profiles in the steps, friction resistance and cavitation. The numerical simulation results had a good approximation to the experimental results. All these analyses could be used to validate the use of the computational fluid dynamic tools, to characterize the flow for a possible improvement proposal of this hydraulic structure. The cavitation problem is the great challenge in thigh velocity flows. One solution to reduce the cavitation in the stepped spillways is the construction of a bottom aerator. A numerical study of a bottom aerator was carried out, focusing out of air concentrations, pressures under jet and velocity profiles. It was studied the discharge of air under the jet. As final result, this work proposes a new geometric configuration for stepped spillways with a bottom aerator. This bottom aerator was suggested to be set in the beginning of the spillway chute in order to reduce cavitation risk or to increase the maximum discharge in spillway.

A ventilação natural é uma das estratégias mais eficientes para o condicionamento térmico passivo de edificações, ocorrendo por ação dos ventos, por efeito chaminé ou pela combinação de ambos. Em áreas densamente ocupadas, a velocidade do vento é reduzida pelos diversos obstáculos locais, tornando o efeito chaminé e a captação pela cobertura as alternativas mais viáveis para indução da ventilação natural em edificações. Dentre as estratégias de ventilação, destacam-se os sheds, aberturas no telhado, que funcionam como captadores ou extratores de ar, dependendo de sua localização em relação aos ventos dominantes. Apesar de terem um grande potencial, são pouco utilizados devido à falta de dados técnicos acessíveis ao projetista. Além disso, muitas vezes são utilizados para captação ou para extração do ar de forma aleatória, sem uma análise da influência dos parâmetros projetuais na ventilação natural. Essa pesquisa parte da hipótese que existe diferença nesses parâmetros para um shed extrator e para um shed captador de ar e que é possível otimizar a ventilação natural através desses dispositivos. O objetivo geral foi avaliar o impacto de diferentes parâmetros projetuais e climáticos no desempenho de sheds captadores e extratores de ar e propor diretrizes para o projeto desses dispositivos. A metodologia foi composta de estudos paramétricos, a fim de investigar a interdependência de diferentes parâmetros projetuais na ventilação natural por sheds e realizar análises comparativas. O processo baseou-se em análises numéricas através de simulações CFD e a verificação desses resultados por meio de ensaios experimentais em túnel de vento. As análises mostraram uma boa compatibilidade entre os resultados numéricos e experimentais, obtendo uma diferença de no máximo 10% entre as duas ferramentas para a maioria dos pontos monitorados. Com relação às simulações computacionais, constatou-se que o desempenho de sheds é fortemente influenciado pela velocidade e pelos ângulos de incidência dos ventos externos. Além disso, notou-se que existem diferenças nos parâmetros projetuais para um shed extrator e para um captador, sendo que alguns casos apresentaram bons desempenhos em ambas as situações. Por fim, conclui-se que é possível otimizar o uso da ventilação natural através desses dispositivos, sendo que esses resultados auxiliam a prática do projeto arquitetônico na determinação de configurações adequadas. / Natural ventilation is one of the most important strategies for passive cooling of indoor environments. It can occur by wind forces, stack effect or a combination of both strategies. In urban areas the wind speed is reduced due to several obstacles. Stack effect and air intake by the roof can be viable alternatives to induce natural ventilation in buildings. Among the ventilation strategies, sheds can be highlighted. These structures consist of roof openings that work as collectors or extractors of air, depending on their location in relation to the prevailing wind directions. Although they have great potential, they are seldom used by Brazilian architecture, due to lack of technical data available to the designer. Besides, sometimes the sheds are used for air intake or exhaustion without any detailed analysis on the influence of different building design parameters on natural ventilation. The starting hypothesis of this research is that there is a difference in construction parameters for an exhaustion and intake sheds and it is possible to optimize the use of natural ventilation through these devices. The research aims to investigate the potential of air extracting and capturing sheds to promote indoor natural ventilation and proposes guidelines for the design of these devices. The applied methodology consists on parametric studies to investigate the interdependence of different design parameters for natural ventilation in sheds and perform comparative analyzes. The procedure was based on CFD simulations and the verification of such results through experimental tests using wind tunnel. The analyses showed a good compatibility between the numerical and experimental results, obtaining a maximum difference of 10% between the two tools for most of the monitored points. The computer simulations showed that sheds performance is strongly influenced by the external wind speed and its incidence angles. In addition, it was noted that there are differences in design parameters for air extracting and capturing sheds and some cases showed a good performance in both situations. Finally, it was concluded that it is possible to optimize the use of natural ventilation through these devices, and these results support the practice of architectural design in determining appropriate settings.

Securing water in the right quantities at the right quality for the right price is a major issue around the world. Membranes are making an increasingly important contribution to meeting this need; however their performance is limited by fouling. This thesis reports on an investigation into the fouling of systems related to water treatment using the Direct Observation Through the Membrane (DOTM). The investigation focused on the measurement of critical flux and observation of particle behaviour under a variety of conditions and for a number of different particles. The range of meanings attributed to critical flux in the literature was analysed and several proposals made for the improved use of the concept. In particular, critical flux determination techniques were classified by whether they measure resistance changes or particle deposition; leading to the definition of Critical Resistance and Critical Deposition Fluxes. In this thesis the deposition definition is used exclusively. The effect of Reynolds number and spacer orientation on critical flux was correlated for spacer-filled channels. The heterogeneous deposition patterns observed with regions of heavy deposition next to areas of little or no deposition. This pattern was related to the local hydrodynamics of spacer cells (a few mm2 in size). The correlations developed for critical flux in spacer-filled channels were adjusted for submicron particle size and incorporated into a SpiralWound Module (SWM) leaf model and then used to simulate the fouling of SWM leaves under a range of operating conditions and operating policies. The Mass Balance technique of critical flux determination was also briefly assessed. The applicability of critical flux criteria to SWM arrays was discussed. Fouling, particle behaviour and critical flux were also investigated in air-sparged systems. The post-cleaning water flux was found to be enhanced when the membrane is fouled in the presence of bubbles. The rate of flux decline was reduced by bubbles. Critical flux increased with air flowrate, and decreased with increased liquid flowrate and concentration. Bubbles caused particles to periodically deposit on the membrane. Particles were observed to stream past the membrane under the influence of back-diffusive forces. Video clips of particulate fouling are provided.

This document addresses problems encountered when establishing the very low air-flow speeds required for experimental investigations of the mechanisms of low-Reynolds-number boundary-layer turbulence. Small-scale motions in the near-wall region are important features of turbulent boundary-layer dynamics, and, if these features are to be resolved by measurements in air with conventionally-sized hot-wire probes, a well-behaved canonical turbulent boundary layer must be developed at free stream flow speeds no higher than 4 m/s. However, at such low speeds, the turbulent boundary layers developed on the walls of a wind tunnel are very susceptible to perturbation by non-turbulent time-dependent flow structures which originate upstream from the test section in the laminar flow at the inlet and in the contraction. Four different non-turbulent flow structures have been identified. The first is a result of quasi-two-dimensional separation of the laminar boundary-layer from the surfaces of the wind-tunnel contraction. Potential flow simulations show that susceptibility to this form of separation is reduced by increasing the degree of axisymmetry in the cross-section geometry and by decreasing the streamwise curvature of the concave surfaces. The second source of time-dependence in the laminar boundary-layer flow is an array of weak streamwise vortices produced by Goertler instability. The Goertler vortices can be removed by boundary-layer suction at the contraction exit. The third form of flow perturbation, revealed by visualisation experiments with streamers, is a weak large-scale forced-vortex swirl produced by random spatial fluctuations of temperature at the wind-tunnel inlet. This can be prevented by thorough mixing of the inlet flow; for example, a centrifugal blower installed at the inlet reduces the amplitude of temperature nonuniformity by a factor of about forty and so prevents buoyancy-driven swirl. When subjected to weak pressure gradients near the start of a wind-tunnel contraction, Goertler vortices in laminar wall layers can develop into three-dimensional separations with strong counter-rotating trailing vortices. These trailing vortices are the fourth source of unsteady flow in the test-section. They can be suppressed by a series of appropriately located screens which remove the low-speed-streak precursors of the three-dimensional separations. Elimination of the above four contaminating secondary flows permits the development of a steady uniform downstream flow and well-behaved turbulent wall layers. Measurements of velocity in the turbulent boundary layer of the test-section have been obtained by hot-wire anemometry. When a hot-wire probe is located within the viscous sublayer, heat transfer from the hot-wire filament to the wall produces significant errors in the measurements of both the mean and the fluctuating velocity components. This error is known as wall-proximity effect and two successful methods are developed for removing it from the hot-wire signal. The first method is based on the observation that, if all experimental parameters except flow speed and distance from the wall are fixed, the velocity error may be expressed nondimensionally as a function of only one parameter, in the form DeltaU^+=f(y^+). The second method, which also accommodates the effect of changing the hot-wire overheat ratio, is based on a dimensional analyis of heat transfer to the wall. Velocity measurements in the turbulent boundary layer at the mid-plane of a nearly square test-section duct have established that, when the boundary-layer thickness is less than one quarter of the duct height, mean-velocity characteristics are indistinguishable from those of a two-dimensional flat-plate boundary layer. In thicker mid-plane boundary layers, the mean-velocity characteristics are affected by stress-induced secondary flow and by lateral constriction of the boundary-layer wake region. A significant difference between flat-plate and duct boundary layers is also observed in momentum-balance calculations. The momentum-integral equation for a duct requires definitions of momentumd and displacement thickness which are different from those given for flat-plate boundary layers. Momentum-thickness growth rates predicted by the momentum-integral equation for a duct agree closely with measurements of the newly defined duct momentum thickness. Such agreement cannot be obtained in terms of standard flat-plate momentum thickness. In duct boundary layers with Reynolds numbers Re_theta between 400 and 2600, similarity in the wake-region distributions of streamwise turbulence statistics has been obtained by normalising distance from the wall with the flat-plate momentum thickness, theta_2. This result indicates that, in contrast with the mean velocity characteristics, the structure of mid-plane turbulence does not depend on the proportion of duct cross-section occupied by boundary layers and is essentially the same as in a flat-plate boundary layer. For Reynolds numbers less than 400, both wall-region and wake-region similarity fail because near-wall turbulence events interact strongly with the free stream flow and because large scale turbulence motions are directly influenced by the wall. In these conditions, which exist in both duct and flat-plate turbulent boundary layers, there is no distinct near-wall or wake region, and the behaviour of turbulence throughout the boundary layer depends on both wall variables and on outer region variables simultaneously. / Thesis (Ph.D.)--School of Mechanical Engineering, 1998.

The longitudinal fluctuations at a point in the core of air flowing through a 15 cm. diameter pipe at a mean centerline velocity of 13.4 and 29.5 m/sec. were measured with a hot-wire anemometer. This signal, after analog to digital conversion, was stored in the form of digital samples on an ICT computer drum storage device. This method of data recording includes the effect of all eddy frequencies from DC upwards and the presence of large, slow eddies in the longitudinal direction became apparent in the subsequent autocorrelations. The longitudinal dispersion of a tracer material injected on the axis of the pipe was measured over short distances with pulses of approx. 20 msecs. duration of radioactive Krypton-85, detected at two downstream stations by small surface-barrier radiation detectors. By varying the separation of these two stations, an asymptotic mixing coefficient was established which was very much greater than the corresponding transverse mixing coefficient measured by other workers. The method proposed by Philip (4) for the prediction of the Lagrangian time autocorrelation from the Eulerian velocity measurements was examined with the correlation data of Baldwin and the data obtained in this investigation. The method applied to the unfiltered correlation data in the present measurements in a non-isotropic field to predict a longitudinal turbulent Peclet no. was found to predict a value in the region measured experimentally. When the present velocity data was filtered to remove the low-frequency components and give a turbulence intensity equal to that measured in a radial direction in previous dispersion measurements, the mixing coefficient predicted with Philip's method was found to agree very well with the transverse mixing coefficient reported in these investigations. A value is also suggested for the longitudinal Peclet number in the absence of the low frequency fluctuations. / Thesis (Ph.D.)-University of Natal, Durban, 1970.

This document addresses problems encountered when establishing the very low air-flow speeds required for experimental investigations of the mechanisms of low-Reynolds-number boundary-layer turbulence. Small-scale motions in the near-wall region are important features of turbulent boundary-layer dynamics, and, if these features are to be resolved by measurements in air with conventionally-sized hot-wire probes, a well-behaved canonical turbulent boundary layer must be developed at free stream flow speeds no higher than 4 m/s. However, at such low speeds, the turbulent boundary layers developed on the walls of a wind tunnel are very susceptible to perturbation by non-turbulent time-dependent flow structures which originate upstream from the test section in the laminar flow at the inlet and in the contraction. Four different non-turbulent flow structures have been identified. The first is a result of quasi-two-dimensional separation of the laminar boundary-layer from the surfaces of the wind-tunnel contraction. Potential flow simulations show that susceptibility to this form of separation is reduced by increasing the degree of axisymmetry in the cross-section geometry and by decreasing the streamwise curvature of the concave surfaces. The second source of time-dependence in the laminar boundary-layer flow is an array of weak streamwise vortices produced by Goertler instability. The Goertler vortices can be removed by boundary-layer suction at the contraction exit. The third form of flow perturbation, revealed by visualisation experiments with streamers, is a weak large-scale forced-vortex swirl produced by random spatial fluctuations of temperature at the wind-tunnel inlet. This can be prevented by thorough mixing of the inlet flow; for example, a centrifugal blower installed at the inlet reduces the amplitude of temperature nonuniformity by a factor of about forty and so prevents buoyancy-driven swirl. When subjected to weak pressure gradients near the start of a wind-tunnel contraction, Goertler vortices in laminar wall layers can develop into three-dimensional separations with strong counter-rotating trailing vortices. These trailing vortices are the fourth source of unsteady flow in the test-section. They can be suppressed by a series of appropriately located screens which remove the low-speed-streak precursors of the three-dimensional separations. Elimination of the above four contaminating secondary flows permits the development of a steady uniform downstream flow and well-behaved turbulent wall layers. Measurements of velocity in the turbulent boundary layer of the test-section have been obtained by hot-wire anemometry. When a hot-wire probe is located within the viscous sublayer, heat transfer from the hot-wire filament to the wall produces significant errors in the measurements of both the mean and the fluctuating velocity components. This error is known as wall-proximity effect and two successful methods are developed for removing it from the hot-wire signal. The first method is based on the observation that, if all experimental parameters except flow speed and distance from the wall are fixed, the velocity error may be expressed nondimensionally as a function of only one parameter, in the form DeltaU^+=f(y^+). The second method, which also accommodates the effect of changing the hot-wire overheat ratio, is based on a dimensional analyis of heat transfer to the wall. Velocity measurements in the turbulent boundary layer at the mid-plane of a nearly square test-section duct have established that, when the boundary-layer thickness is less than one quarter of the duct height, mean-velocity characteristics are indistinguishable from those of a two-dimensional flat-plate boundary layer. In thicker mid-plane boundary layers, the mean-velocity characteristics are affected by stress-induced secondary flow and by lateral constriction of the boundary-layer wake region. A significant difference between flat-plate and duct boundary layers is also observed in momentum-balance calculations. The momentum-integral equation for a duct requires definitions of momentumd and displacement thickness which are different from those given for flat-plate boundary layers. Momentum-thickness growth rates predicted by the momentum-integral equation for a duct agree closely with measurements of the newly defined duct momentum thickness. Such agreement cannot be obtained in terms of standard flat-plate momentum thickness. In duct boundary layers with Reynolds numbers Re_theta between 400 and 2600, similarity in the wake-region distributions of streamwise turbulence statistics has been obtained by normalising distance from the wall with the flat-plate momentum thickness, theta_2. This result indicates that, in contrast with the mean velocity characteristics, the structure of mid-plane turbulence does not depend on the proportion of duct cross-section occupied by boundary layers and is essentially the same as in a flat-plate boundary layer. For Reynolds numbers less than 400, both wall-region and wake-region similarity fail because near-wall turbulence events interact strongly with the free stream flow and because large scale turbulence motions are directly influenced by the wall. In these conditions, which exist in both duct and flat-plate turbulent boundary layers, there is no distinct near-wall or wake region, and the behaviour of turbulence throughout the boundary layer depends on both wall variables and on outer region variables simultaneously. / Thesis (Ph.D.)--School of Mechanical Engineering, 1998.

Thesis (MSc (Mathematical Sciences. Applied Mathematics))--University of Stellenbosch, 2007. / The understanding and quantitative description of fluid flowthrough porousmedia, is a science which has been going on for many years and investigated in a variety of disciplines. Studies in this field have primarily been based on models, which can either be described as empirical or theoretical. Part of the current study is to understand fluid flow in porous media through studying three recent theoretical pore-scale models based on the concept of a Representative Unit Cell (RUC), to represent a porous medium. Amongst other assumptions, these models assumed plane Poiseuille flow throughout each pore section of a rectangular RUC. The main objective of this study is to numerically verify this assumption using Computational Fluid Dynamics (CFD) software, FLUENT version 6.2.16. Attention is also paid to comparison between these models with the experimental data, obtained during the model tests of airflow through a timber stack end, undertaken in a wind tunnel. The laminar and intermediate airflow through a timber stack end is simulated using the commercial software FLUENT, and the results are validated against the theoretical pore-scale models and experimental data. Two turbulence models which are, the Standard k − e and Reynolds-Stress models are used in these computations, the aimbeing to determine howwell they are able to reproduce the experimental data. The numerical results are in good agreement with one of the theoretical models presented and the experimental data.

Elementos de materiais flexíveis são empregados em diversas aplicações na engenharia, como por exemplo, em pás de turbinas eólicas. O comportamento do escoamento é afetado pela alteração na forma da estrutura. Muitas vezes, seu movimento e deformação são induzidos pelas próprias forças fluidodinâmicas. O trabalho apresenta o estudo de escoamentos externos envolvendo a interação fluido-estrutura, com o interesse voltado ao comportamento de pás de turbinas eólicas. Simulações numéricas são realizadas com o intuito de avaliar o efeito que a deformação da estrutura, devido à resposta elástica às forças oriundas do escoamento, tem nas próprias forças fluidodinâmicas. A plataforma ANSYS Workbench é utilizada, combinando o software ANSYS CFX para a análise do fluido e o ANSYS Mechanical para a análise da estrutura. Como validação do método, o escoamento laminar sobre um cilindro apoiado elasticamente é estudado e comparado com dados da literatura. O caso escolhido para o presente trabalho é o de um escoamento turbulento sobre um elemento de pá, fixo em uma das suas extremidades e livre na outra. A geometria da pá é retangular com o perfil NACA 0012 e o modelo de turbulência utilizado é o k-ω SST. Os resultados demonstram a influência significativa que a deformação da estrutura tem nas forças fluidodinâmicas de sustentação e arrasto e concordam com a literatura existente. / Elements of flexible materials are employed in several engineering applications, for instance, in wind turbine blades. The flow behavior is affected by any change in the shape of the structure. Often, its displacement and deformation are induced by the fluid-dynamic forces themselves. This paper presents the study of an external flow using fluid-structure interaction (FSI), focused on the behavior of wind turbine blades. Numerical simulations are performed in order to evaluate the effect that the deformation of the structure, caused by the elastic response to the flow forces, has on the fluid-dynamic forces themselves. The ANSYS Workbench platform is used, combining the software ANSYS CFX for the fluid analysis and ANSYS Mechanical for the structural analysis. As a form of validation of this method, the laminar flow over an elastically mounted cylinder is studied and compared with literature data. The chosen case for this work is a turbulent flow over a 3D blade element, fixed at one end and free at the other. The blade geometry is rectangular with the NACA 0012 profile and the turbulence model used is the k-ω SST. The results demonstrate the significant influence that the deformation of the structure has on the fluid-dynamic lift and drag forces, leading to an agreement with the existing literature.