The diploma thesis is focused on the design and evaluation of the concrete monolithic ceiling slab in the shape of semicircular ring, ribs lining this plate and skylights. The result is static calculation and drawing documentation.

Review of axial hydraulic machines and elementary procedures of design hydraulic machines are listed in the first part of thesis. Second part is dedicated axial pump with annular motor and measurement its characteristic curve. In the third part of thesis, procedure of design axial pump with tube motor is described, also there are listed CFD results and characteristic curve of axial pump with tube motor is predicted.

[ES] El proceso de combustión en llamas de difusión de combustible atomizado es un fenómeno multifásico altamente complejo que a día de hoy no se comprende en su totalidad, ya que involucra varios eventos simultáneos, como atomización, vaporización y cinética química. A lo largo de los años, los investigadores han estudiado a fondo la combustión en llamas de combustibles líquidos, con el fin de comprender los procesos fundamentales como clave para reducir las emisiones contaminantes y mejorar la eficiencia de la propulsión de las aeronaves. En los últimos años, la evolución tanto en la tecnología de inyección como en la de combustión ha permitido mejorar el proceso de mezcla por aspersión y la eficiencia del motor y, por tanto, reducir las emisiones contaminantes. Por lo que, diferentes configuraciones de tipo de inyector y distribución de aire dentro de la cámara de combustión han demostrado ser capaces de reducir el consumo de combustible, así como las emisiones de óxidos de nitrógeno y hollín sin afectar el rendimiento del motor. Esta tesis proporciona una metodología experimental para estudiar los efectos de las condiciones de co-flujo, el caudal másico de combustible, el tipo de combustible y el diámetro de salida del quemador sobre la atomización y la combustión de la llama producida en un quemador anular bajo condiciones de operación pobres. La caracterización del chorro sin combustión se realizó mediante dos técnicas ópticas diferentes. Por un lado, se utilizó velocimetría de imagen de partículas para medir los campos de velocidad del espray. Por otro lado, retroiluminación microscópica difusa (MDBI) para medir el tamaño y la velocidad de las gotas. Los resultados mostraron que ambos están controladas principalmente por el tipo de combustible y el caudal másico del mismo. Sin embargo, la variación de la velocidad de co-flujo no mostró un efecto significativo en las características de las gotas (tamaño y velocidad), lo que probablemente se deba a que el campo de visión de la técnica MBDI estaba muy cerca de la punta del inyector. Adicionalmente, al incrementar la temperatura de co-flujo se observó que el diámetro promedio de gota disminuía, lo cual es causado por la evaporación del combustible. Finalmente, las variaciones en los perfiles de tamaño y velocidad de las gotas al variar el diámetro de salida de aire se relacionaron con la variación de la velocidad del co-flow, lo que afectaba la evaporación y el arrastre de las gotas. Para el estudio de la llama en condiciones reactivas, se probó en condiciones de operación que permitan llama estabilizadas, utilizando tres técnicas ópticas diferentes, las cuales se activaron simultáneamente. La extinción de luz difusa se utilizó para determinar el espesor óptico del hollín. Además, se emplearon las técnicas de quimioluminiscencia OH* y MDBI para medir la altura de despegue de la llama y las características de las gotas, respectivamente. Los resultados mostraron que la velocidad y temperatura del co-flujo, y el tipo de combustible influyen fuertemente en la altura de despegue de la llama. Mientras que en la formación hollín los parámetros más influyentes fueron la velocidad del co-flujo y el tipo de combustible. Con respecto a los resultados de la evaporación de las gotas, se observó que el tamaño inicial y las propiedades del combustible controlan su evaporación. El combustible n-Dodecano es el menos volátil y tiene un tamaño de gota inicial más grande y, por lo tanto, las gotas tardaron más en evaporarse, lo que resultó en una mayor longitud de despegue de la llama y una mayor formación de hollín debido a su mayor tendencia a formar hollín. Por el contrario, las gotas de n-Heptano se evaporaron más rápido, lo que resultó en una altura de despegue de la llama más corta y también en una menor formación de hollín. Finalmente, el combustible n-Decano mostró resultados intermedios para la evaporación de gotas, la altura de despegue de la llama y la formación de hollín. / [CA] El procés de combustió en flames de difusió de combustible atomitzat és un fenomen multifásico altament complex que a hores d'ara no es comprén en la seua totalitat, ja que involucra diversos esdeveniments simultanis, com a atomització, vaporització i cinètica química. Al llarg dels anys, els investi- gadors han estudiat a fons la combustió en flames de combustibles líquids, a fi de comprendre els processos fonamentals com a clau per a reduir les emissions contaminants i millorar l'eficiència de la propulsió de les aeronaus. En els últims anys, l'evolució tant en la tecnologia d'injecció com en la de combustió ha permés millorar el procés de mescla per aspersió i l'eficiència del motor i, per tant, reduir les emissions contaminants. Pel que, diferents configuracions de tipus d'injector i distribució d'aire dins de la cambra de combustió, han demostrat ser capaços de reduir el consum de combustible, així com les emissions d'òxids de nitrogen i sutja sense afectar el rendiment del motor. Aquesta tesi proporciona una metodologia experimental per a estudiar els efectes de les condicions de co-flux, el cabal màssic de combustible, el tipus de combustible i el diàmetre d'eixida del cremador sobre l'atomització i la combustió de la flama produïda en un cremador anul·lar sota condicions d'operació pobres. La caracterització del doll sense combustió es va realitzar mitjançant dues tècniques òptiques diferents. D'una banda, es va utilitzar velocimetría d'imatge de partícules per a mesurar els camps de velocitat de l'esprai. D'altra banda, retroil·luminació microscòpica difusa (MDBI) per a mesurar la grandària i la velocitat de les gotes. Els resultats van mostrar que tots dos estan controlades principalment per la mena de combustible i el cabal màssic d'aquest. No obstant això, la variació de la velocitat de co-flux no va mostrar un efecte significatiu en les característiques de les gotes (grandària i velocitat), la qual cosa probablement es deu al fet que el camp de visió de la tècnica MBDI estava molt prop de la punta de l'injector. Addicionalment, en incrementar la temperatura de co-flux es va observar que el diàmetre mitjà de gota disminuïa, la qual cosa és causat per l'evaporació del combustible. Finalment, les variacions en els perfils de grandària i velocitat de les gotes en variar el diàmetre d'eixida d'aire es van relacionar amb la variació de la velocitat del co-flux, la qual cosa afectava l'evaporació i l'arrossegament de les gotes. Per a l'estudi de la flama en condicions reactives, es va provar en condicions d'operació que permeten flama estabilitzades, utilitzant tres tècniques òptiques diferents, les quals es van activar simultàniament. L'extinció de llum difusa es va utilitzar per a determinar la grossària òptica del sutge. A més, es van emprar les tècniques de quimioluminescència OH* i MDBI per a mesurar l'altura d'enlairament de la flama i les característiques de les gotes, respectivament. Els resultats van mostrar que la velocitat i temperatura del co-flux, i el tipus de combustible influeixen fortament en l'altura d'enlairament de la flama. Mentre que en la formació sutge els paràmetres més influents van ser la velocitat del co-flux i el tipus de combustible. Respecte als resultats de l'evaporació de les gotes, es va observar que la grandària inicial i les propietats del combustible controlen la seua evaporació. El combustible n-Dodecano és el menys volàtil i té una grandària de gota inicial més gran i, per tant, les gotes van tardar més a evaporar-se, la qual cosa va resultar en una major longitud d'enlairament de la flama i una major formació de sutge degut a la seua major tendència a formar sutge. Al contrari, les gotes de n-Heptano es van evaporar més ràpid, la qual cosa va resultar en una altura d'envol de la flama més curta i també en una menor formació de sutja. Finalment, el combustible n-Decano va mostrar resultats intermedis per a l’evaporació de gotes, l’altura d’envol de la flama i la formació de sutja / [EN] The combustion process in spray flames is a highly complex multi-phase phenomenon that is still not completely understood since it involves several simultaneous events, such as atomization, vaporization, and chemical kinetics. Over the years, researchers have studied the combustion in spray flames thoroughly, in order to understand the fundamental processes as key to re- duce pollutant emissions and improve the efficiency of aircraft propulsion. In recent years, the evolution in both injection and combustion technology has allowed to improve the spray mixing process and engine efficiency and hence, reducing pollutant emissions. Therefore, different configurations of injector type and air distribution inside the combustion chamber have proved capable of reducing fuel consumption, as well as emissions of nitrogen oxides and soot without affecting the engine performance. This thesis provides an experimental methodology to study the effects of co-flow conditions, fuel mass flow rate, fuel type and air outlet diameter at the burner exit on the atomization and combustion behavior of the spray flame produced on an annular spray burner under lean conditions. The characterization of the liquid spray without combustion was carried out using two different optical techniques. On the one hand, particle image velocimetry was used to characterize the global velocity fields of the spray. On the other hand, Microscopic diffused back-illumination (MDBI) to measure the size and droplet velocity at a field of view close to the injector tip. The results exhibited that both droplet size and droplet velocity are mainly controlled by the fuel type and fuel mass flow rate. Nevertheless, the variation of the co-flow velocity did not show a significant effect on droplet characteristics (size and velocity), which is likely due to the fact that the field of view of the MDBI technique was located very close to the injector tip. Additionally, by increasing the co-flow temperature, it was observed that the mean droplet size decreased, which is caused by the fuel evaporation process. Finally, the variations in the droplet size and velocity profiles when varying the air outlet diameter were related to the velocity variation when modifying the cross-sectional area at the burner outlet, which affects the evaporation and drag of the drops. On the spray development in reactive conditions, it was investigated in the operating conditions that promote stabilized flames, using three different optical techniques, all of which were triggered simultaneously. The light extinction was used to determine the optical thickness through the soot cloud. In addition, OH* chemiluminescence and the MDBI techniques were employed to measure the flame lift-off height and droplet characteristics, respectively. The results exhibited that the co-flow velocity, co-flow temperature and fuel type strongly influence the flame lift-off height. While in the soot formation the most influential parameters were the co-flow velocity and the type of fuel. Regarding the results of the droplet evaporation, it was observed that the initial droplet sizes and the fuel properties control the droplet evaporation process. n-Dodecane fuel is the least volatile and also exhibited a larger initial droplet size and thus, the droplets took more time to evaporate than the other two fuels, resulting in a longer flame lift-off height and likewise higher soot formation by its greater tendency to form soot. Contrary, n-Heptane droplets evaporated faster, resulting in a shorter flame lift-off height and also less soot formation. Finally, n-Decane showed intermediate results for droplet evaporation, flame lift-off height, and soot formation. / Cardona Vargas, S. (2021). Development of a test rig for the study of the atomization and combustion of a spray flame in an atmospheric annular spray burner at lean conditions [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/179994 / TESIS

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Les tendances climatiques récentes montrent un réchauffement et un adoucissement des couches de surface dans la région du courant circumpolaire antarctique (ACC).Sur la même période, les vents d'ouest pilotant la circulation de l'océan Austral ont significativement augmentés. Cette augmentation est en partie liée à l'intensification du mode annulaire austral (SAM), principal mode de variabilité atmosphérique au sud de 20°S. Dans cette thèse, on s'intéresse à comprendre les effets de la tendance positive du SAM sur les propriétés des masses d'eau formées dans la région de l'ACC.A cette fin, on met en place une stratégie de simulations régionales couplées océan-glace de mer et forcées par une série de scénarios atmosphériques perturbés. Les scénarios atmosphériques sont construits à partir de réanalyses atmosphériques afin de décrire les différentes composantes (dynamiques et thermodynamiques) des changements liés au SAM.En réponse à l'intensification du SAM, les simulations montrent une forte salinisation de la couche de mélange océanique ainsi que des eaux modales (SAMW) et intermédiaires (AAIW).L'essentiel de ces changements peut être attribué aux composantes dynamiques du SAM. Dans les régions saisonnières englacées, les composantes thermodynamiques du SAM peuvent jouer un rôle important (en particulier en mer d'Amundsen et en mer de Weddell). Les simulations montrent également le rôle clef joué par la glacede mer dans la médiation des changements atmosphériques vers l'océan intérieur. Ces résultats de simulations suggèrent que le SAM ne serait pas le seul pilote des tendances climatiques récentes dans l'océan Austral. / Recent climate trends show a warming and freshening of the surface layers in the region of the Antarctic Circumpolar Current (ACC). Over the same period, the westerlies driving the circulation of the Southern Ocean have significantly increased. This increase is partly due to the intensification of the Southern Annular Mode (SAM), the main mode of atmospheric variability south of 20°S. In this thesis, we are interested in understanding the effects of the positive trend of the SAM onto the properties of water masses formed in the region of the ACC. To do so, we implement a strategy of regional coupled ocean-sea ice simulations forced by a series of atmospheric disturbance scenarios.These scenarios are constructed from atmospheric reanalyses in order to describe the various components (dynamic and thermodynamic) of the changes related to the SAM. In response to the increase of the SAM, the simulations show a significant salinification of the ocean mixed layer and of the mode water (SAMW) and intermediate water (AAIW).Most of these changes can be attributed to the dynamic components of the SAM. In Seasonal Ice Zone, the thermodynamic components of the SAM can play an important part (especially in Amundsen Sea and Weddell Sea). The simulations also show the key role played by sea ice in mediating atmospheric changes toward the interior ocean.These simulation results suggest that SAM is not the only driver of recent climate trends in the Southern Ocean.

Submitted by Sandro Camargo (sandro.camargo@unipampa.edu.br) on 2015-05-09T22:22:57Z No. of bitstreams: 1 126110018.pdf: 3775876 bytes, checksum: 4a58f20709bf7c39682924a84079246d (MD5) / Made available in DSpace on 2015-05-09T22:22:58Z (GMT). No. of bitstreams: 1 126110018.pdf: 3775876 bytes, checksum: 4a58f20709bf7c39682924a84079246d (MD5) Previous issue date: 2014-09-08 / Neste trabalho, são apresentadas diferentes técnicas que possibilitam a obtenção de característica dupla-faixa para antenas de microfita especificamente voltadas para aplicações em estações rádio-base de telefonia móvel celular no Brasil. As faixas de frequência de interesse encontram-se no intervalo de 0,824 GHz a 0,960 GHz para a banda inferior e 1,710 GHz a 2,165 GHz para a banda superior. Além de atender as especificações técnicas de faixa de passagem, devem ser atendidos os requisitos de coeficiente de reflexão, polarização, ganho, largura de feixe de irradiação e impedância de entrada na faixa de interesse. Primeiramente, para obtenção de antenas de microfita com característica multibanda, descreve-se a técnica em que são dispostas fendas nos elementos irradiadores, onde são estudadas três topologias de antenas, explicando-se os princípios de funcionamento e destacando-se as particularidades de cada geometria. As três antenas são analisadas e projetadas com o auxílio do software comercial de simulação eletromagnética Ansoft Designer ® , visando levantar os parâmetros elétricos através de diversos estudos paramétricos em função da variação das dimensões das antenas para compreender melhor o comportamento de cada estrutura simulada. A antena com elemento irradiador em forma de H foi a única que cumpriu os requisitos em termos de faixa de passagem e diagramas de irradiação para operação em sistemas de telefonia móvel celular. No entanto, esta geometria resultou em dimensões físicas consideráveis, pois necessita da utilização de múltiplas camadas dielétricas, acarretando em um protótipo de volume considerável e de elevado custo de produção. Outra técnica estudada foi a sobreposição de elementos irradiadores, porém a mesma não é investigada detalhadamente em função de o custo de produção da antena ser mais elevado em comparação a topologias coplanares. Em seguida, uma técnica com irradiadores em fenda anelar e dupla alimentação é proposta. A antena é projetada considerando-se duas portas independentes, uma para cada banda de operação, formando uma antena de dois acessos altamente isolados. Simulações com o software HFSS TM mostraram que é possível satisfazer as especificações para operação em estações rádio-base de telefonia móvel celular. A grande vantagem desta estrutura é a possibilidade de utilização de apenas um laminado de micro-ondas, o que reduz o custo de produção em comparação a outras topologias. Protótipos foram construídos e caracterizados experimentalmente para validar o projeto realizado no simulador eletromagnético. Constatou-se a presença de discrepâncias entre os resultados simulados e medidos. Após simulações paramétricas, verificou-se que o processo de construção alterou a geometria do protótipo em relação ao modelo de simulação. Após a inclusão das imperfeições do processo construtivo no modelo, foi possível estimar as mudanças necessárias no protótipo. Após os devidos ajustes realizados em bancada, os resultados medidos exibiram boa concordância com a previsão teórica. Por fim, realizou-se um estudo de viabilidade da utilização da antena em fenda anelar dupla-faixa para composição de uma rede de antenas para estações rádio-base. A análise teve como principal objetivo verificar a possibilidade de síntese de diagramas de irradiação em forma de cossecante ao quadrado em ambas as bandas de operação. Excelente resultado foi obtido para a banda inferior, enquanto que algumas limitações foram encontradas na banda superior. / In this work we present different techniques for achieving the dual-band feature for microstrip antennas aimed to be used in the mobile communication base stations of Brazil. The focused frequency range for lower and higher bands is in the 0.824-0.960 GHz and 1.710-2.165 GHz intervals, respectively. In addition to comply with the technical specifications, the solution is also supposed to meet the requirements of return loss, polarization, gain, beamwidth radiation and input impedance in the focused frequency range. Initially, in order to obtain microstrip antennas with dual-band characteristic, we describe the technique in which slots are placed in the irradiating elements. Three antenna topologies are analyzed in its operation principles, emphasizing the particularities of each geometry. The antennas are designed with support of Ansoft Designer ® , a commercial software that simulates electromagnetic features, in order to find out the electrical parameters through parametric studies and to better understand the behavior of each simulated structure. These studies considered the variation in the dimensions of antennas. The H-shaped microstrip antenna was the only one able to fulfill the requirements of bandwidth and irradiation diagrams for operation in mobile communication. However, this geometry originated an antenna of considerable physical dimensions, because it requires the use of multiple dielectric layers, resulting in a prototype of considerable volume and high production cost. Another technique studied was the stacking of irradiating elements. However it isn’t investigated in detail because of the production cost of the antenna, which is higher than the ones of coplanar topologies. After all that, we propose a technique based in annular-slot antennas and double feed. The antenna is designed considering two independent ports, one for each band of operation, making an antenna of two highly insulated accesses. Simulations by the HFSS TM software have shown that it’s possible to comply with the specifications for operation in base stations of the mobile communication. The biggest advantage of this structure over other topologies is that it may be made of only one microwave laminate, reducing the production cost. Prototypes were built and measured to validate the design in the electromagnetic simulator. It was noted the discrepancies between the simulated and measured results. After running parametric simulations, we found out that the building process of the prototype changed the geometry of the simulation model. We included these imperfections in the model and it was possible to estimate the necessary changes in the prototype. After inclusion of the adjustments, the measured results behaved just alike the theoretical prediction. Finally, we’ve done a feasibility study on the use of the dual-band annular slot antenna for making an array of antennas for base stations. The study aimed to verify the suitability of synthetizing squared-cosecant shaped pattern in both operation bands. We got excellent results for the lower band, although some limitations were found for the higher band.

Celui-ci a pour objectif de valider l'ensemble des modèles physiques utilisés dans un code de simulation numérique pour simuler un écoulement de type annulaire dispersé en conduite rencontré lors d'une procédure de lavage à eau utilisé dans les raffineries. Pour ce faire une banque de données expérimentale est mise en place sur des configurations représentatives de celles utilisées en condition industrielle. La géométrie retenue comporte une zone horizontale d'injection rectiligne avec un injecteur central, suivi d'un coude à 90° situé dans un plan vertical. Différentes conditions expérimentales permettent d'étudier l'influence de la vitesse du gaz, de la condition d'injection du brouillard et de la pression sur les différents processus physiques. Ces résultats comprenant des visualisations du brouillard et du film pariétale, des mesures de taille et de distribution de gouttes,des mesures de débit et d'épaisseur de film, sont analysés pour faire ressortir les principaux mécanismes d'interaction entre le gaz et la phase dispersée, le gaz et le film liquide pariétal et la phase dispersée et le film pariétal. En parallèle, des premières simulations, avec une approche RANS, sont réalisées avec le code CEDRE de l'ONERA et les résultats sont confrontés aux mesures. / This work has been realised within a CIFRE contract with TOTAL. Its aim was to validate all the physical models used in a computation, which simulates an annular dispersed flow through a pipe used in a water washing process in refinery plants. That is why, a whole set of data has been gathered using experimental boundary conditions which are representative to those used in industrial configurations. The geometry is made of a horizontal pipe with a centred nozzle followed by a 90º elbow in the vertical plane. Several experimental boundary conditions enable one to study the influence of the gas velocity, the type of the spray injection and the pressure on the different physical phenomena. These results including spray and liquid film visualisations, droplets distribution and size measurements as well as liquid film thickness and mass flow measurements were analysed in order to extract the main interaction mechanism between the gas and the dispersed phase, the gas and the liquid film, and the dispersed phase and the annular liquid film. Meanwhile, simulations using a RANS approach were realized with the ONERA code named CEDRE and its results were compared to the gathered measurements.

<p> Efficiency is an essential metric for assessing turbine performance. Modern turbines rely heavily on numerical computational fluid dynamic (CFD) tools for design improvement. With more compact turbines leading to lower aspect ratio airfoils, the influence of secondary flows is significant on performance. Secondary flows and detached flows, in general, remain a challenge for commercial CFD solvers; hence, there is a need for high fidelity experimental data to tune these solvers used by turbine designers. Efficiency measurements in engine-representative test rigs are challenging for multiple reasons; an inherent problem to any experiment is to remove the effects specific to the turbine rig. This problem is compounded by the narrow uncertainty band required, ideally less than 0.5% uncertainty, to detect the incremental improvements achieved by turbine designers.  Efficiency measurements carried out in engine-representative turbine rigs have traditionally relied upon strong assumptions, such as neglecting heat transfer effects. Furthermore, prior to this research there was no framework to compute uncertainty propagation that combines both inputs from experiments and computational tools. </p> <p>This dissertation presents a comprehensive methodology to obtain high-fidelity adiabatic efficiency data in engine-representative turbine facilities. This dissertation presents probabilistic sampling techniques to allow for uncertainty propagation. The effect of rig-specific effects such as heat transfer and gas properties, on efficiency is demonstrated. Sources of uncertainty are identified, and a framework is presented which divides the sources into bias and stochastic. The framework allows the combination of experimental and numerical uncertainty. The accuracy of temperature and aerodynamic pressure probes, used for efficiency determination, is quantified. Corrections for those effects are presented that rely on hybrid numerical and experimental methods. Uncertainty is propagated through these methods using numerical sampling. </p> <p>Finally, two test cases are presented, a stator vane in an annular cascade and a two-stage turbine in a rotating rig. The performance is analyzed using the methods and corrections developed. The uncertainty on the measured efficiency is similar to literature but the uncertainty framework allows an uncertainty estimate on the adiabatic efficiency. </p>

Tato dizertační práce se zabývá dvěma případy interakce tělesa s tekutinou (FSI). První z nich se zabývá analýzou vzájemné interakce mezi rotorem čerpadla a kapalinou uvnitř těsnící spáry. Vliv těsnící spáry na dynamiku celého stoje je popsán pomocí dynamických parametrů, které jsou také označovaný jako přídavné účinky. V současnosti používané modely těsnících spár používají pro stanovení dynamických parametrů řadu zjednodušujících předpokladů. V této práci je prezentováno pět různých analýz dynamických parametrů těsnící spáry čerpadla na okysličovadlo. Každá z těchto pěti analýz používá jinou míru zjednodušení výpočetního modelu. V případě největšího zjednodušení je modelován pouze objem kapaliny uvnitř těsnící spáry. Nejkomplexnější analýza pro stanovení dynamických parametrů těsnící spáry používá pro výpočet model celého čerpadla s excentrickou polohou rotoru. Druhá část této dizertační práce definuje novou metodu pro řešení interakce kapaliny s pružným tělesem. Tato metoda využívá řešení inverzního problému kmitání. Přímý problém kmitání, který je také označován jako problém vlastních hodnot, používá jako vstupy pro řešení matice hmotnosti, tuhosti a tlumení, které jsou dohromady označovány jako koeficientové matice, na základě kterých je v nejobecnějším případě stanovena Jordanovská matice a také modální matice pravostranných a levostranných vlastních vektorů. Při řešení inverzního problému kmitání jsou stanoveny koeficientové matice na základě Jordanovské matice a modálních matic pravostranných a levostranných vlastních vektorů. Existují dva případy inverzního problému kmitání. V případě, že jsou známy všechny vstupní vlastní čísla a vlastní vektory, pak se jedná o tzv. plný problém. Naopak v případě, že alespoň 1 mód kmitání soustavy není znám, tak se jedná o tzv. částečný problém. V této práci je prezentováno 5 algoritmů pro řešení inverzního problému v kmitání. Nicméně pro každý typ inverzního problému kmitání je prezentován jeden univerzální algoritmus. Algoritmus pro řešení plných problémů byl poprvé prezentován v roce 1979 Otakarem Daňkem. Algoritmy pro řešení částečných problémů, které jsou prezentovány v této práci, jsou vůbec prvními algoritmy pro řešení tohoto typu inverzního problému kmitání. Univerzální algoritmus pro řešení částečných problémů je označován jako algoritmus pro řešení částečných problémů s volbou doplňkových vlastních hodnot. Aplikace těchto dvou univerzálních algoritmů pro řešení inverzního problému kmitání pro případ plných i částečných problémů je ukázána na řešení dvou případů interakce pružného tělesa s kapalinou.

Thermoelectric generators (TEG) are re-emerging technology that can be used to recover heat waste from commercial and industrial processes to generate electricity, enhancing fuel utilization and lowering greenhouse gas emissions. TEG modules are solid-state heat engines that produce no noise or vibration during operation. Notably, TEG modules are also able to operate at low-temperature differences, which makes them ideal for a wide range of heat waste recovery applications. Annular thermoelectric generator (ATEG) modules are optimal in applications where either the heat source or sink are round in shape. Bi2Te3 solution-based compounds are of significant interest in the application of thermoelectric materials (TE) used in low-temperature cooling and power generation applications. The main objective of the current work is to design a mechanically reliable ring-shaped ATEG module with a predictable performance using spark plasma sintered Bi2Te3 TE material for low temperature waste heat recovery applications. In terms of structure, this work is divided into two parts. The first part investigates how the use of a powder pre-treatment technique affects the mechanical and thermoelectric properties of P- and N-type Bi2Te3. In addition, part one also presents the measurements of these materials’ mechanical and thermoelectric properties, which serve as inputs for the finite element models used to design thermoelectric modules with parallel and perpendicular configurations vis-a-vis the sintering pressing direction. The second part evaluates the thermoelectric performance and thermal stresses of a ring-shaped ATEG couple that has been integrated between hot-side and cold-side heat exchangers. To this end, two configurations are compared with respect to their heat/electrical current flow paths: one that allows for radial flow (radial configuration), and one that allows for axial flow (axial configuration). The P- and N-type Bi2Te3 powder was treated using a mechanically agitated fluidized powder reduction facility that was built in-house. The characteristic uniaxial tensile strength of the P-type Bi0.4Sb1.6Te3 increased from 13.9 MPa to 26.3 MPa parallel to the sintering pressure, and from 16.3 MPa to 30.6 MPa perpendicular to the sintering pressure following oxide reduction using 5% H2 ˗ 95% Ar at 380 ℃ for 24 h. The figure of merit, ZT, increased from 0.35 to 0.80 and from 0.42 to 1.13 at room temperature (25 ℃) in the parallel and the perpendicular directions, respectively, after the surface oxide reduction treatment. On the other hand, the annealing effects of the oxide reduction pr-treatment of the N-type (Bi0.95 Sb0.05)2(Se0.05 Te0.95)3 using 5% H2 ˗ 95% Ar at 380 ℃ for 24 h were found to be responsible for the majority of the mechanical properties and ZT enhancement. Additionally, the characteristic uniaxial tensile strengths for this material increased from 30.4 to 34.1 MPa and from 30.8 to 38 MPa in the parallel and the perpendicular directions, respectively. The ZTmax (150 ℃) increased from 0.54 to 0.63 in both the parallel and perpendicular directions due to oxide reduction, while annealing led to an increase to 0.58 and 0.62 in the parallel and the perpendicular directions, respectively. An analytical model was constructed to compare the thermoelectric performance of the two configurations under three different hot-side thermal resistances, and a 3D coupled finite element ANSYS model was constructed to study and compare the thermal stresses of the two configurations at different dimensions. The two models were then used to create 2D maps in order to investigate the effects of ATEG couple configuration and dimensions, as well as the hot-side thermal resistance, with the goal of identifying the optimum design. The optimization of module geometry requires a trade-off between performance and mechanical reliability. The results of these investigations showed that increases in the temperature difference across the ATEG couple (ΔT) led to increases in both power and thermal stresses in both configurations. When both configurations were generating the same power at ΔT = 105 ℃, the thermal stresses in the radial configuration were as much as 67 MPa higher than those in the axial configuration due to the formation of additional tensile hoop stresses. The lowest thermal stress obtained for the axial couple configuration was 67.8 MPa, which was achieved when the couple had an outer diameter of 16 mm, an axial thickness of 1 mm, a ΔT of 14.8 ℃, and power generation of 10.4 mW per couple. The maximum thermal stress values were located at the corners of the interface between the solder and the TE rings due to the mismatched coefficient of thermal expansion. This thesis makes a novel contribution to the state-of-the-art literature in ring-shaped ATEG modules, as it details a well-characterised spark plasma sintered Bi2Te3 TE material and a methodology for designing a ring-shaped ATEG module with reliable, robust, and predictable thermoelectric and mechanical performance. The details of the contribution made by this work have been disseminated in the form of three journal publications, which have been integrated into this sandwich Ph.D. thesis. / Thesis / Doctor of Science (PhD)