The use of computational fluid dynamics to investigate surface ship dynamics and characteristics has been growing during recent years. With technological advancements continuing in leaps and bounds more and more complex simulations are possible. The interests of this paper concern the numerical simulations of a surface effect ship which is a specific type of air cushion vehicle. The simulation work presented here attempts to replicate the model tests involving a generic surface effect ship and demonstrate the value of numerical simulations in understanding air cushion vehicles. The model tests consist of a surface effect ship running through a range of Froude numbers in calm seas and a variety of wave cases. The numerical simulations were developed using CD-adapcos's STAR-CCM+ to model the surface effect ship characteristics and dynamics. The pressurized air cushion and flexible, dynamic seals are of the greatest importance when modeling a surface effect ship; however, some idealizations had to be made. The air cushion fans are represented as constant momentum sources while the seals are represented as shortened and rigid. Throughout the simulations drag, pitch, and heave were constantly monitored for comparison purposes with the model tests. It was found that the rigid skirt approximation accounts for a large portion of error when comparisons were made between the numerical and analytical data. Furthermore, it would be impossible to accurately represent the surface effect ship dynamics in waves with this approximation. An alternative method to modeling the skirts was investigated which would include the use of a porosity function. It was found that the porosity skirt model would allow for cushion pressure to be maintained while limiting the interaction of the rigid skirt and the free surface. The full implementation of porous skirts on the surface effect ship is a difficult challenge as numerical instabilities arise. However, implementing the porous skirt would lead to more accurate calm water simulations and the ability to model the surface effect ship in wave cases. / Master of Science

A system of ordinary differential equations (ODE) is constructed for an air cushion vehicle (ACV). The system is simplified to an equation for the balance of the vertical forces and the equation for the adiabatic compression of the air in the cushion. Air pressure is constantly supplied into the system, but can leak out from underneath the edges of the cushion. A series of regular waves encounters the air cushion, causing a change in volume. Additionally, a computational analysis of the seakeeping of a Surface Effect Ship (SES) is performed using the commercial software WAMIT, which uses low-order, linear potential panel method. The model of the T-Craft consists of catamaran hulls, rigid end skirts, and the interface between the air cushion and the water surface. Beyond the six rigid body degrees of freedom of the T-Craft, additional modes are added for the motion of the interface panels. To verify the method used, the model is benchmarked using computational data for a small-scale barge model and experimental data for a T-Craft model. A comparison is performed for the T-Craft with and without its cushion. The solution for the nonlinear time-domain system is found numerically, and the stability of the system is studied by observing bifurcations with the incoming wave amplitude as the bifurcation parameter. The system experiences a period-doubling bifurcation, from a periodic orbit, to a subharmonic orbit, to a solution with multiple periods. Further increasing the wave amplitude increases the period doubling, eventually leading to chaotic behavior. As a result of the linear-potential simulations, significant differences are found in the seakeeping of the T-Craft when on and off the cushion. These differences are caused by the direct and indirect effects of the cushion (added aerodynamics and a decreased draft). The RAO's of the craft experience changes in amplitude and phase, which will affect the multi-body relative motions. The time-domain model shows very chaotic behaviour that is presented visually in a bifurcation diagram. These linear potential and time-domain methods illustrate the complexity and importance of modelling air-cushion effects.

This thesis presents the results from the computational fluid dynamics simulations of surface effect ship model tests. The model tests being simulated are of a generic T-Craft model running in calm seas through a range of Froude numbers and in two head seas cases with regular waves. Simulations were created using CD-adapco's STAR-CCM+ and feature incompressible water, compressible air, pitch and heave degrees of freedom, and the volume of fluid interface-capturing scheme. The seals are represented with rigid approximations and the air cushion fans are modeled using constant momentum sources. Drag data, cushion pressure data, and free surface elevation contours are presented for the calm seas cases while drag, pressure, heave, and roll data are presented for the head seas cases. The calm seas cases are modeled both with no viscosity and with viscosity and turbulence. All simulations returned rather accurate estimations of the free surface response, ship motions, and body forces. The largest source of error is believed to be due to the rigid seal approximations. While the wake's amplitude is smaller when viscosity is neglected, both viscous and inviscid simulations' estimations of the free surface qualitatively match video footage from the model tests. It was found that shear drag accounts for about a quarter of the total drag in the model test simulations with viscosity, which is a large source of error in inviscid simulations. Adding the shear drag calculated using the ITTC-1957 friction coefficient line to the total drag from the inviscid simulation gives the total drag from the viscous simulations within a 6% difference. / Master of Science

Numerical simulations of fluid-structure interaction (FSI) problems were performed in an effort to verify and validate a commercially available FSI tool. This tool uses an iterative partitioned coupling scheme between CD-adapco's STAR-CCM+ finite volume fluid solver and Simulia's Abaqus finite element structural solver to simulate the FSI response of a system. Preliminary verification and validation work (VandV) was carried out to understand the numerical behavior of the codes individually and together as a FSI tool. Verification and Validation work that was completed included code order verification of the respective fluid and structural solvers with Couette-Pouiselle flow and Euler-Bernoulli beam theory. These results confirmed the 2nd order accuracy of the spatial discretizations used. Following that, a mixture of solution verifications and model calibrations was performed with the inclusion of the physics models implemented in the solution of the FSI problems. Solution verifications were completed for fluid and structural stand-alone models as well as for the coupled FSI solutions. These results re-confirmed the spatial order of accuracy but for more complex flows and physics models as well as the order of accuracy of the temporal discretizations. In lieu of a good material definition, model calibration is performed to reproduce the experimental results. This work used model calibration for both instances of hyperelastic materials which were presented in the literature as validation cases because these materials were defined as linear elastic. Calibrated, three dimensional models of the bow seal on the University of Michigan bow seal test platform showed the ability to reproduce the experimental results qualitatively through averaging of the forces and seal displacements. These simulations represent the only current 3D results for this case. One significant result of this study is the ability to visualize the flow around the seal and to directly measure the seal resistances at varying cushion pressures, seal immersions, forward speeds, and different seal materials. SES design analysis could greatly benefit from the inclusion of flexible seals in simulations, and this work is a positive step in that direction. In future work, the inclusion of more complex seal geometries and contact will further enhance the capability of this tool. / Ph. D.

Le dioxyde d'uranium irradié (UO2), combustible nucléaire des réacteurs à eau pressurisée, contient deux populations de cavités saturées par des gaz de fission : i. des cavités intergranulaires plutôt lenticulaires, dont la taille varie de quelques dizaines à plusieurs centaines de nanomètres, ii. des cavités intragranulaires plutôt sphériques, dont la taille est de l'ordre du nanomètre. Des travaux récents ont montré qu'il existe un effet de surface à l'échelle des cavités nanométriques qui modifie le comportement élastique effectif du combustible. Ce travail vise à proposer un modèle micromécanique analytique capable de tenir compte de cette microstructure hétérogène ainsi que de l'effet de surface afin de décrire le comportement élastique macroscopique de l'UO2 irradié. La démarche mise en oeuvre est fondée sur une modélisation multi-échelles et s'appuie sur des techniques d'homogénéisation en mécanique des matériaux. L'UO2 irradié est décrit comme un matériau poreux contenant des nanocavités sphériques (cavités intragranulaires) et sphéroïdales (cavités intergranulaires), sous pression et orientées aléatoirement. L'effet de surface présent à l'échelle nanométrique est pris en compte via un modèle d'interface imparfaite cohérente entre la matrice et les cavités. Un modèle original fondé sur l'approche par motifs morphologiques représentatifs a été développé afin de décrire le comportement élastique effectif de ce milieu hétérogène. Le modèle analytique proposé repose sur des hypothèses simplificatrices dont la pertinence est évaluée à partir de simulations numériques par éléments finis qui s'appuient sur une formulation spécifique afin de tenir compte de la présence d'interfaces imparfaites cohérentes. / The irradiated uranium dioxide (UO2), which is the nuclear fuel of pressurized water reactors, contains two populations of cavities saturated by fission gaz: i. intergranular cavities almost lenticular in shape whose size ranges between few tens to several hundred nanometers, ii. intragranular cavities, almost spherical in shape whose size is of the order of the nanometer. Recent studies have shown the existence of a surface effect at the scale of nanometric cavities, which influences the effective elastic behavior of the nuclear fuel. In this work, an analytical micromechanical model, which is able to take into account this heterogeneous microstructure and the surface effect at the nanometric scale, is proposed to describe the macroscopic behavior of the irradiated UO2. The approach is based on a multiscale modeling and homogenization techniques in mechanics of materials. The irradiated UO2 is described as a porous media, which contains pressurized spherical nanocavities (intragranular cavities) and randomly oriented pressurized spheroidal cavities (intergranular cavities). The surface effect is taken into account with imperfect coherent interfaces between the matrix and the cavities. A novel model based on the morphologically representative pattern approach has been developed to describe the effective elastic behavior of this heterogeneous medium. The proposed model relies on assumptions whose relevance is evaluated with finite element simulations which require a specific formulation to take into account the imperfect coherent interfaces.

Ultrasonic Consolidation (UC) is a solid state additive manufacturing process which fabricates three-dimensional objects by ultrasonically joining metal foils together, layer-bylayer, to form a solid part. A wide range of materials can be used to fabricate parts by UC and products with complex internal geometry can be generated by shaping the crosssection throughout the build using Computer Numerically Controlled (CNC) milling. As a result of its ability to embed various secondary materials and fibres in metal matrices, UC has emerged as a potential method of fabricating multi-functional materials and structures.

The research in this thesis focuses on the investigation of tidal turbines using a small scale horizontal axis tidal turbine and a 2D hydrofoil testing rig, combining experiments with simulations to provide comprehensive results and to better understand some of the variables that affect their performance. The experimental campaigns were carried out at the University of Victoria fluids research lab and the Sustainable Systems Design Lab (SSDL). The experimental testing rigs were re-designed by the author and are now fully automated, including a friendly graphical user interface for easy implementation. Particle image velocimetry (PIV) technique was used as the quantitative flow visualization method to obtain the time-averaged flow fields. This thesis presents three investigations. The first study aims to quantify the impacts of channel blockage, free surface effects and foundations on hydrokinetic turbine performance, using porous discs and an axial flow rotor. The results were used to cross-validate computational fluid dynamics (CFD) simulations. It was found that as wall blockage increases, thrust and power are incremented with and without the inclusion of free surface deformation. Discrepancies between simulations and experimental results on free surface effects compared to a slip wall were obtained and hence further research is recommended and the author gives some advice on how to proceed in this investigation. The second study determines the performance of four hydrofoil candidates over a range of low Reynolds number (Re), delivering useful information that can be applied to low Re energy conversion systems and, specifically in this case, to improve the performance of the small scale tidal turbine at the SSDL lab. The study combines the 2D hydrofoil test rig along with PIV measurements in order to experimentally obtain lift and drag coefficients. The experiments were carried out in the recirculating flume tank over the range of low Re expected for the small scale rotor rig, in order to provide more accurate results to improve rotor blade design. In addition, numerical simulations using XFOIL, a viscid-inviscid coupled method, were introduced to the study. These results were analysed against experiments to find the most suitable parameters for reliable performance prediction. The final results suggested that adding a numerical trip at a certain chordwise distance produced more reliable results. Finally, an experimental study on turbine rotor performance and tip vortex behavior was performed using again the rotor rig and PIV. Blade design and rotor performance were assessed, showing good agreement with Blade Element Momentum (BEM) simulations, particularly at predicting the tip speed ratio corresponding to the maximum power coefficient point. Regarding the wake structure, tip vortex locations (shed from the blade tips) were captured using PIV in the near wake region, showing evidence of wake expansion. The velocity and vorticity fields are also provided to contribute to the development and validation of CFD and potential flow codes. / Graduate / 0548 / 0547 / 0538 / iafranch@uvic.ca

Les travaux réalisées lors de cette thèse s'intéressent aux dynamiques de mouvement, de réaction et de constitution des fonctions imines. Les aldéhydes les plus réactives pour cette réaction de condensation ont été identifiées. Un processus d'échange intramoléculaire aléatoire rapide a été observé entre le salicylaldéhyde et l'éthylènediamine dont la vitesse est contrôlée par les substituants, la longueur de la chaîne amine, le solvant et la température. Cette observation conduità l'élaboration de mouvements de déplacement d'abord non-directionnels puis développés pour devenir directionnels. Une sélectivité dynamique réactionnelle a été introduite sur des mélanges d'aldéhydes et d'amines. Elle a été baptisée simpléxité et est utilisée pour de la protection de fonctions. Enfin, la nature dynamique de l'imine a été étudiée à l'interface solide-liquide parmicroscopie à effet tunnel et montre une accélération et une amplification des produits formées sur la surface. / This thesis reports on the intertwined motional, reactional and constitutional dynamics of imines. It goes from acquiring the basic data about the reaction to applications in various fields of Chemistry. The most reactive aldehydes for the reaction were identified and their reactivities were explained by physical-organic chemistry methods. An intramolecular motion was observed for simple diamines. This observation led to introduction of a non-directional small molecule walking, and eventually to development of a directional walker. A representation of dynamic combinatorial libraries was proposed and then was used for analysis of aldehyde-amine libraries, which exhibit selective amplification of a given species due to the complexity of its composition. This phenomenon was called simplexity. The simplexity example was then used as a concept for dynamic selective protecting groups in acylation of amines. Also, the dynamic imine linkage was also studied on the solid-liquid interface. It was found that the reactions taking place at the graphite surface are largely accelerated and that the formation of the largest molecules is amplified due to the surface.

A Computational Fluid Dynamics (CFD) tool is developed in this thesis to solve complex fluid-structure interaction (FSI) problems. The fluid domain is based on Smoothed Particle Hydro-dynamics (SPH) and the structural domain employs large-deformation Finite Element Method (FEM). Validation tests of SPH and FEM are first performed individually. A loosely-coupled SPH-FEM model is then proposed for solving FSI problems. Validation results of two benchmark FSI problems are illustrated (Antoci et al., 2007; Souto-Iglesias et al., 2008). The first test case is flow in a sloshing tank interacting with an elastic body and the second one is dam-break flow through an elastic gate. The results obtained with the SPH-FEM model show good agreement with published results and suggest that the SPH-FEM model is a viable and effective numerical tool for FSI problems. This research is then applied to simulate a two-dimensional free-stream flow interacting with a deformable, pressurized surface, such as an ACV/SES bow seal. The dynamics of deformable surfaces such as the skirt/seal systems of the ACV/SES utilize the large-deformation FEM model. The fluid part including the air inside the chamber and water are simulated by SPH. A validation case is performed to investigate the application of SPH-FEM model in ACV/SES via comparison with experimental data (Zalek and Doctors, 2010). The thesis provides the theory of the SPH and FEM models incorporated and the derivation of the loosely-coupled SPH-FEM model. The validation results have suggested that this SPH-FEM model can be readily applied to skirt/seal dynamics of ACV/SES interacting with free-surface flow. / Ph. D.