Atherosclerotic plaques with high probability of rupture show the presence of a hot spot due to the accumulation of inflammatory cells. This study utilizes two and three dimensional (2-D and 3-D) arterial geometries containing an atherosclerotic plaque experiencing different levels of inflammation and uses models of heat transfer analysis to determine the temperature distribution in the plaque region. The 2-D studies consider three different vessel geometries: a stenotic straight artery, a bending artery and an arterial bifurcation which model a human aorta, a coronary artery and a carotid bifurcation, respectively. The 3-D model considers a stenotic straight artery using realistic and simplified geometries. Three different blood flow cases are considered: steady-state, transient state and blood flow reduction. In the 3-D model, thermal stress produced by local inflammation is estimated to determine the effect of inflammation over plaque stability. For fluid flow and heat transfer analysis, Navier-Stokes equations and energy equation are solved; for structural analysis, the governing equations are expressed in terms of equilibrium equation, constitutive equation, and compatibility condition, which are are solved using the multi-physics software COMSOL 3.3 (COMSOL, Inc.). Our results indicate that the best location to measure plaque temperature in the presence of blood flow is recommended between the middle and the far edge of the plaque. The blood flow reduction leads to a non-uniform temperature increase ranged from 0.1 to 0.25 oC in the plaque/lumen interface. In 3-D realistic model, the multiple measuring points must be considered to decrease the potential error in temperature measurement even within 1 or 2 mm at centerline region of plaque. The most highly thermal stressed regions with the value of 1.45 Pa are observed at the corners of lipid core and the plaque/lumen interface. The mathematical model developed provides a tool to analyze the factors affecting heat transfer at the plaque surface. The results may contribute to the understanding of the relationship between plaque temperature and the likelihood of rupture, and also provide a tool to better understand arterial wall temperature measurements obtained with novel catheters.

This research study considered subsonic short air-air ejectors with multi-ring entraining diffusers. Many references can be found for the design of air-air ejectors with solid diffusers. However, a limited amount of work has been published specially addressing the performance of short ejectors with entraining diffusers. This study was an experimental and computational investigation of how ejector performance is affected by ejector geometry (i.e. nozzle, mixing tube and diffuser), flow inlet swirl conditions and flow temperature. Ejector performance was quantified in terms of pumping, pressure recovery, wall temperature and velocity and temperature distribution at the diffuser exit. The experiments were conducted on one cold flow wind tunnel and one hot gas wind tunnel. In total, eight ejector systems were tested for this research. Five different swirl conditions and two primary air flow temperatures were studied. Ejector inlet conditions were measured using four fixed 7-hole pressure probes in the annulus. Ejector exit flow conditions were measured using a traversing 7-hole pressure probe with a thermocouple. A parallel computational study was conducted along with the experimental study. The commercial CFD packages, Gambit 2.3 and Fluent 6.2, were selected for meshing and flow solutions. The objective of the computational study was to determine the utility of RANS based CFD model for predicting device performance as design changes were implemented. The computational study was intended to provide practitioners with guidance as to when CFD will provide practical answers to specific questions relating to the ejector performance including ejector pumping, pressure recovery, wall temperatures and velocity and temperature distribution at the diffuser exit. In total, twenty-six complete cold flow experiments and twenty complete hot flow experiments have been completed. A detailed CFD model study has been performed to select the suitable computational domain, mesh density, boundary conditions, turbulence model and near wall treatment. Twenty-four CFD cases were selected to compare with the corresponding experimental data. The experimental results showed that the inlet swirl conditions and the diffuser bent angle had significant effects on the ejector performance. In general, the maximum ejector performance was achieved with the 20° inlet swirl condition. This level of swirl enhanced pressure recovery in the ejector. As the diffuser bent angle increased, the total pumping decreased due to the flow impingement in the diffuser. The oblong ejector generally had better flow mixing performance than the round ejector. For the CFD simulations, the Realizable k-ε turbulence model was found to give reasonable predictions for most of the bulk flow properties such as the total pumping, velocity profiles, swirl levels and back pressure. These were achieved at a reasonable cost in terms of the human efforts and computational resources. The RSM was able to give slightly improved predictions but at a much higher cost in terms of the efforts and computing resources. All of the turbulence models had difficulty predicting the pressure recovery in the mixing tube and diffuser because of their inability to accurately predict flow separation in the core of the swirling primary flow. As a result of this, the turbulence models considered in this work overpredicted the pumping of the mixing tube and underpredicted the pumping of the entraining diffuser. This unresolved issue with the CFD models is an important consideration when designing such devices. / Thesis (Ph.D, Mechanical and Materials Engineering) -- Queen's University, 2008-01-08 00:26:54.931 / This project has been funded by joint contribution from the National Sciences and Engineering Research Council of Canada (NSERC), the Department of National Defence (DND)and W.R. Davis Engineering Ltd.

The first study researched turbulent forced convective heat (mass) transfer down- stream of blockages with round and elongated holes in a rectangular channel. The blockages and the channel had the same cross section, and a distance equal to twice the channel height separated consecutive blockages. Naphthalene sublimation experiments were conducted with four hole aspect ratios (hole-width-to-height ratios) and two hole-to-blockage area ratios (ratios of total hole cross-sectional area to blockage area). The effects of the hole aspect ratio, for each hole-to-blockage area ratio, on the local heat (mass) transfer distribution on the exposed primary channel wall between consecutive blockages were examined. Results showed that the blockages with holes enhanced the average heat (mass) transfer by up to 8.5 and 7.0 times that for fully developed turbulent flow through a smooth channel at the same mass flow rate, respectively, in the smaller and larger hole-to-blockage area ratio (or smaller and larger hole diameter) cases. The elongated holes caused a higher average heat (mass) transfer and a larger spanwise variation of the local heat (mass) transfer on the channel wall than did the round holes. The second study explored the heat transfer enhancement for pool boiling on nano-structured surfaces. Experiments were conducted with three horizontal silicon surfaces, two of which were coated with vertically aligned multi-walled carbon nanotubes (MWCNT) with heights of 9 and 25 ¹m, respectively, and diameters between 8 and 15 nm. The MWCNT arrays were synthesized on the two silicon wafers using chemical vapor deposition. Experimental results were obtained over the nucleate boiling and film boiling regimes under saturated and sub-cooled (5±C and 10±C) boiling conditions. PF-5060 was the test fluid. Results showed that the MWCNT array with a height of 25 ¹m enhanced the nucleate and film boiling heat fluxes on the silicon surface by up to 380% and 60%, respectively, under saturated boiling conditions, and by up to 300% and 80%, respectively, under 10±C sub-cooled boiling conditions, over corresponding heat fluxes on a smooth silicon surface. The MWCNT array with a height of 9 ¹m enhanced the nucleate boiling heat flux as much as the taller array, but did not significantly enhance the wall heat flux in the film boiling regime.

This dissertation presents a detailed account of the study undertaken on the subject of fouling of Exhaust Gas Recirculator (EGR) coolers. The fouling process in EGR coolers is identified to be due to two primary reasons — deposition of fine soot particles and condensation of hydrocarbons known as dry soot and wet soot fouling, respectively. Several numerical simulations are performed to study the fouling process. Preliminary analysis of the particle forces for representative conditions reveal that drag, thermophoresis and Brownian forces are the significant transport mechanisms and among them, the deposition process is dominated by thermophoresis. Soot deposition in a representative turbulent plain channel shows a direct relationship of the amount of deposition with the near-wall temperature gradient. Subsequently, periodic and developing flow simulations are performed on a wavy channel geometry, a common EGR design for various Reynolds numbers and thermal boundary conditions. Constant heat flux boundary condition is used in the periodic fully-developed calculations, which assist in establishing various deposition trends. The wavy nature of the walls is noted to affect the fouling process, resulting in specific deposition patterns. For the lower Reynolds number flows, significantly higher deposition is observed due to the higher particle residence times. On the other hand, the developing flow calculations facilitate the use of wall temperature distributions that typically exist in EGR coolers. The linear dependence of the amount of deposition on the near-wall temperature gradient or in other words, the heat flux, is ascertained. It is also observed in all the calculations, that for the sub-micron soot particles considered, the deposition process is almost independent of the particle size. In addition, the nature of the flow and heat transfer characteristics and the transition to turbulence in a developing wavy channel are studied in considerable detail. Finally, a study on the condensation of heavy hydrocarbons is undertaken as a post-processing step, which facilitates the prediction of the spatial distribution and time-growth of the combined fouling layer. From the calculations, the maximum thickness of the dry soot layer is observed to be near the entrance, whereas for the wet soot layer, the peak is found to be towards the exit of the EGR cooler. Further, parametric studies are carried out to investigate the effect of various physical properties and inlet conditions on the process of fouling. / Master of Science

Combustion instabilities, induced by the resonant coupling of acoustics and combustion occur in many practical systems such as domestic boilers, gas turbine and rocket engines. They produce pressure and heat release fluctuations that in some extreme cases can provoke mechanical failure or catastrophic damage. These phenomena have been extensively studied in the past, and the basic driving and coupling mechanisms have already been identified. However, it is well known that most systems behave differently at cold start and in the permanent regime and the coupling between the temperature of the solid material and combustion instabilities still remains unclear. The aim of this thesis is to study this mechanism. This work presents an experimental investigation of combustion instabilities for a laminar premixed flame stabilized on a slot burner with controlled wall temperature. For certain operating conditions, the system exhibits a combustion instability locked on the Helmholtz mode of the burner. It is shown that this instability can be controlled and even suppressed by changing solely the temperature of the burner rim. A linear stability analysis is used to identify the parameters playing a role in the resonant coupling and retrieves the features observed experimentally. Detailed experimental studies of the different elementary processes involved in the thermo-acoustic coupling are used to evaluate the sensitivity of these parameters to the wall temperature. Finally a theoretical model of unsteady heat transfer from the flame root to the burner-rim and detailed experimental measurements permit to establish the physical mechanism for the temperature dependance on the flame response.

To meet the constantly restricting emission regulations and develop better strategiesfor engine control systems, thorough knowledge of engine behavior is crucial.One of the characteristics to evaluate engine performance and its capabilityfor power generation is in-cylinder pressure. Indeed, most of the diagnosis andcontrol signals can be obtained by recording the cylinder pressure trace and predictingthe thermodynamic variables [3].This study investigates the correlation between the in-cylinder pressure andtotal trapped gas mass [10] with the main focus on estimating the in-cylinder gasmass as a part of a lab measuring procedure using the in-cylinder pressure sensors,or as a real-time method for implementation in an engine control unit thatare not equipped with the cylinder pressure sensors. The motivation is that precisedetermination of air mass is essential for the fuel control system to convey themost-efficient combustion with lower emissions delivered to the after-treatmentsystem [10].For this purpose, a six-cylinder Diesel engine is used for recording the enginespeed, engine torque, measuring the cylinder pressure profile resolved bythe crank angle, intake and exhaust valve phasing as well as intake and exhaustmanifold pressures and temperatures. Next, the most common ways of estimatingthe in-cylinder trapped gas mass are studied and the most reliable ones areinvestigated in-depth and a model with the acceptable accuracy in different operatingconditions is proposed, explained and implemented. The model in has athermodynamics basis and the relative errors is lower than 3% in all the investigatedtests. Afterwards, the most important findings are highlighted, the sourcesof errors are addressed and a sensitivity analysis is performed to evaluate themodel robustness. Subsequently, method adjustment for other operating conditionsis briefly explained, the potential future work is pointed and a complete setof results is presented in Appendix B.

Ce travail porte sur la modélisation d'écoulements turbulents anisothermes dans des milieux macroporeux. Ce problème intéresse de nombreux domaines : échangeurs de chaleur, réacteurs nucléaires, canopées... Notre objectif est de modéliser des écoulements traversant une structure solide selon un approche multi-échelle. L'utilisation d'un opérateur de moyenne spatiale permet ainsi d'obtenir une description homogénéisée des écoulements, tandis que l'aspect turbulent est traité grâce à un opérateur de moyenne statistique. Au cours du processus de moyenne, une partie des informations sur l'état microscopique est perdue. Cela se traduit, à l'échelle macroscopique, par l'apparition de termes inconnus liés à la turbulence (contraintes de Reynolds) et à la présence de la matrice solide (dispersion). C'est sur ces termes de dispersion présents dans les équations macroscopiques de quantité de mouvement et de la température que porte notre travail. Nous proposons un modèle de dispersion thermique qui permet de prédire de façon satisfaisante l'évolution de la température moyenne du fluide pour des écoulements à l'équilibre hydraulique présentant de forts gradients de température ou de flux thermique à la paroi. De plus, un modèle macroscopique de température de paroi basé sur le modèle de température moyenne est dérivé. Il permet de prédire avec précision l'évolution de la température de paroi pour des écoulements hors équilibre thermique. Afin de pouvoir traiter aussi des cas hors équilibre hydraulique, un modèle macroscopique de turbulence est proposé. Une analyse physique détaillée des transferts énergétiques a montré que c'est l'énergie dispersive qui permet de caractériser le déséquilibre hydraulique. Un modèle de turbulence prenant en compte les déséquilibres d'énergie dispersive a donc été dérivé. Il permet de prédire de façon satisfaisante la dynamique d'établissement d'écoulements entrant dans des canaux et de fournir des conditions aux limites précises à la sortie des canaux. Enfin, nous proposons un modèle dynamique pour le tenseur de dispersion basé sur l'énergie dispersive et la dissipation associée. / This works deals with the modelling if anisothermal turbulent flows in macroporous media. This topic concerns many practical applications such as heat exchangers, nuclear reactors, canopies... Our aim is to model flows through porous matrices by means of a multi-scale approach. A macroscopic description of the flows is obtained thanks to a spatial average operator, while a statistical average operator is used to handle turbulence. The successive application of both filters leads to a loss of information. Therefore, at macroscopic scale, unknown contributions linked to turbulence (Reynolds stresses) and the presence of the solid matrix (dispersion) appear. We focus on dispersion terms. We propose a thermal dispersion model for hydrodynamically established flows. Mean temperature predictions obtained with this model are very accurate for channel flows with strong temperature and wall heat flux gradients. We also derive a wall temperature model based the mean temperature model. It gives good macroscopic results for thermally developping flows. In order to be able to simulate hydrodynamically developping flows, a turbulence model is needed. A two-scale analysis of energy transfers within the flow shows that the dynamic behaviour of unbalanced flows can be described using the dispersive kinetic energy. A turbulence model that accounts for dispersive energy is derived. It predicts very well the dynamics of a flows near a channel inlet and provides accurate boundary conditions for exit flows. Finally, a dynamic model based on the dispersive energy and its dissipation rate is proposed for the dispersion tensor.

Les instabilités de combustion induites par le couplage combustion-acoustique se produisent dans de nombreux systèmes industriels et domestiques tels que les chaudières, les turbines à gaz et les moteurs de fusée. Ces instabilités se traduisent par des fluctuations de pression et un dégagement de chaleur qui peuvent provoquer une défaillance mécanique ou des dégâts désastreux dans certains cas extrêmes. Ces phénomènes ont été largement étudiés par le passé, et les mécanismes responsables du couplage ont déjà été identifiés. Cependant, il apparaît que la plupart des systèmes se comportent différemment lors du démarrage à froid ou en régime permanent. Le couplage entre la température des parois et les instabilités de combustion reste encore méconnu et n’a pas été étudié en détail jusqu’à présent. Dans le cadre de ces travaux de thèse, on s’intéresse à ce mécanisme. Ces travaux présentent une étude expérimentale des instabilités de combustion pour une flamme laminaire de pré-mélange stabilisée sur un brûleur à fente. Pour certaines conditions de fonctionnement, le système présente un mode instable autour du mode de Helmholtz du brûleur. Il est démontré que l’instabilité peut être contrôlée, et même supprimée, en changeant uniquement la température de la surface du brûleur. Une analyse de stabilité linéaire peut être mise en œuvre afin d’identifier les paramètres jouant un rôle dans les mécanismes d’instabilité, et il est possible de modéliser analytiquement les phénomènes observés expérimentalement. Des études expérimentales détaillées de différents processus élémentaires impliqués dans le couplage thermo-acoustique ont été menées pour évaluer la sensibilité de ces paramètres à la température de la paroi. Enfin un modèle théorique du couplage entre le transfert de chaleur instationnaire à la paroi et la fluctuation du pied de flamme a été proposé. Par ailleurs, d’autres mesures expérimentales ont permis de comprendre les mécanismes physiques responsables de la dépendance de la réponse de la flamme à la température de paroi. / Combustion instabilities, induced by the resonant coupling of acoustics and combustion occur in many practical systems such as domestic boilers, gas turbine and rocket engines. They produce pressure and heat release fluctuations that in some extreme cases can provoke mechanical failure or catastrophic damage. These phenomena have been extensively studied in the past, and the basic driving and coupling mechanisms have already been identified. However, it is well known that most systems behave differently at cold start and in the permanent regime and the coupling between the temperature of the solid material and combustion instabilities still remains unclear. The aim of this thesis is to study this mechanism. This work presents an experimental investigation of combustion instabilities for a laminar premixed flame stabilized on a slot burner with controlled wall temperature. For certain operating conditions, the system exhibits a combustion instability locked on the Helmholtz mode of the burner. It is shown that this instability can be controlled and even suppressed by changing solely the temperature of the burner rim. A linear stability analysis is used to identify the parameters playing a role in the resonant coupling and retrieves the features observed experimentally. Detailed experimental studies of the different elementary processes involved in the thermo-acoustic coupling are used to evaluate the sensitivity of these parameters to the wall temperature. Finally a theoretical model of unsteady heat transfer from the flame root to the burner-rim and detailed experimental measurements permit to establish the physical mechanism for the temperature dependance on the flame response.

The quest for higher performances and durability of modern aero-engines requires the understanding of the complex aero-thermal flow experienced in a multi-row environment. In particular, the high and low pressure turbine components have a great impact into the engine overall performance, and improvements in the turbine efficiencies can only be achieved through detailed research on the three-dimensional unsteady aerodynamics and heat transfer. The present thesis presents an experimental study of the aerothermodynamics in one and a half turbine stage, focusing on: the aero-thermal flow in the overtip region of a transonic highly loaded high pressure (HP) rotor, and the aerodynamics and heat transfer of an innovative low pressure (LP) stator with a multi-profile configuration placed downstream of the high pressure turbine, within an s-shaped duct. Advanced instrumentation and measurement techniques were used and developed to perform the experimental investigation in a short-duration turbine test rig where both high spatial and time accuracy is indispensable. The flow field at the rotor shroud was investigated with simultaneous measurements of heat transfer, static pressure and blade tip clearance by using fast response pressure, wall temperature and capacitance probes. Through repeat experiments at the same turbine operating point, the time-averaged and time-resolved adiabatic wall temperature and convective heat transfer coefficient were evaluated. In the frame of new engine architectures, a novel stator for an LP turbine is proposed with a multi-splitter layout that represents a new design solution towards compact, lighter and performing aero-engine turbomachinery. It contains small aero-vanes and large structural aerodynamic airfoils which are used to support the engine shaft and house service devices. The research focuses on the experimental investigation of the global performance, aerodynamics and thermodynamics of this novel HP-LP vane layout. The turbine was / Lavagnoli, S. (2012). On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/17799