Droplet growth processes in a cumulus cloud, beginning from its inception at sub-micron scale up to drizzle drop size of few hundred microns, in an average duration of about half hour, has been a topic of intense research. In particular role of turbulence in aiding droplet growth in clouds has been of immense interest. Motivated by this question, we have performed experiments in which turbulent natural convection coupled with phase change is set up inside a tall vertical insulated tube, by heating water located at tube bottom and circulating cold air at tube top. The resulting moist turbulent natural convection flow in the tube is expected to be axially homogeneous. Mixing of air masses of differing temperature and moisture content leads to condensation of water vapor into droplets, on aerosols available inside the tube. We there-fore have droplets in a turbulent flow, in which phase change is coupled to turbulence dynamics, just as in clouds. We obtain a linear mean-temperature pro le in the tube away from its ends. Because there is net flux of water vapor through the tube, there is a weak mean axial flow, but which is small compared to turbulent velocity fluctuations. We have experimented with two setups, the major difference between them being that in one setup, called AC setup, tube is open to atmosphere at its top and hence has higher aerosol concentration inside the tube, while the other setup, called RINAC setup, is closed to atmosphere and due to presence of aerosol filters has lower aerosol concentration inside the tube. Also in the latter setup, cold air temperature at tube top can be reduced to sub-zero levels. In both setups, turbulence attains a stationary state and is characterized by Rayleigh number based on temperature gradient inside the tube away from its ends, which is 107. A significant result from our experiments is that in RINAC setup, we obtain a broadened droplet size distribution at mid-height of tube which includes a few droplets of size 36 m, which in real clouds marks the beginning of rapid growth of droplets due to collisions among them by virtue of their interaction with turbulence. This shows that for broadening of droplet size distribution, high turbulence levels prevalent in clouds is not strictly necessary. Second part of our study comprises two pieces of theoretical work. First, we deal with the problem of a large collector drop settling amidst a population of smaller droplets whose spatial distribution is homogeneous in the direction of fall. This problem is relevant to the last stage of droplet growth in clouds, when the droplets have grown large enough that they interact weakly with turbulence and begin to settle under gravity. We propose a new method to solve this problem in which collision process is treated as a discrete stochastic process, and reproduce Telford's solution in which collision is treated as a homogeneous Poisson process. We then show how our method may be easily generalized to non-Poisson collision process. Second, we propose a new method to detect droplet clusters in images. This method is based on nearest neighbor relationship between droplets and does not employ arbitrary numerical criteria. Also this method has desirable invariance properties, in particular under the operation of uniform scaling of all distances and addition/deletion of empty space in an image, which therefore renders the proposed method robust. This method has advantage in dealing with highly clustered distributions, where cluster properties vary over the image and therefore average of properties computed over the entire image could be misleading.

[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

<p>  </p> <p>Part I studies the lubricant sprays and droplets in a rotary compressor. Air conditioning (AC) systems are now widely used in residential and commercial environments, while the compressor is the most important element in the AC system, and rotary compressors are often used in split AC appliances, whose number is estimated to reach 3.7 billion in 2050. In a rotary compressor, the lubricant oil atomizes into small droplets due to the differential pressure in and out of the cylinder. Part of the lubricant oil droplets carried by the refrigerant vapor will ultimately exhaust from the compressor through the discharge pipe. The ratio of the discharged oil volume to the total oil volume is characterized as the Oil Discharge Ratio (ODR). High ODR will reduce the reliability of the compressor and deteriorate the heat transfer of the condenser and the evaporator, resulting in decreased efficiency. Thus, controlling the ODR is a key issue for the design of the rotary compressor.</p> <p>In Part I, rotary compressors were modified to provide optical access into its internal space, i.e., the lower cavity (refers to the space between the cylinder and the motor), above the rotor/stator, and at the discharge tube level. The modified rotary compressors’ operation was supported by a test rig which provided a wide range of operating conditions, e.g., pressure and frequency. Thus, in-situ optical measurements, e.g., shadowgraph and holograph, can be performed to visualize the lubricant sprays and droplets in the rotary compressor. An image processing routine containing the Canny operator and Convolutional Neural-Network was developed to identify droplets from high-resolution shadowgraph images, while Particle Image Velocimetry (PIV) and Optical Flow Velocimetry (OFV) were applied to calculate the spray and droplet’s velocities with time-resolved shadowgraph images. Parallel Four-Step Phase Shifting Holograph (PFSPSH) located the droplets’ positions in a three-dimensional volume under the specific operating condition.</p> <p>Both primary and secondary atomization were observed in the rotary compressor, while primary atomization is the major source of droplet production. The droplet size distributions versus the frequency, vertical direction, radial direction, and pressure are obtained. It is observed that the droplet characteristic mean diameters increase with the frequency and pressure. They also become larger in the outer region above the rotor/stator and keep constant in the radial direction at the discharge tube level. The penetration velocity of the lubricant spray is calculated in the lower cavity. An outward shift of the jet core combined with an outward velocity component was observed. Additionally, horizontal swirling velocity above the rotor/stator and at the discharge tube level and the vertical recirculation velocity above the rotor/stator are characterized. The volume fraction of droplets was also characterized under the specific operating condition. The results provide detailed experimental data to set up the boundary conditions used in CFD. They also show that the droplets in the upper cavity are mostly from the discharge process of the cylinder in the lower cavity. The results support a droplet pathway model in the rotary compressor, which can guide the optimization of future rotary compressors.</p> <p>Evaporation is commonly seen in hydrology, agriculture, combustion, refrigeration, welding, etc. And it always accompanies heat and mass transfer at the liquid-gas interface and is affected by the substance’s properties, the environment’s pressure, temperature, convection, and so on. PFSPSH in Part I aims to retrieve the phase information for holograph reconstruction. Part II further explores the application of the PFSPSH technology in Part I to observe the evaporation process of acetone, where the phase disturbance caused by the vapor is used to reconstruct the vapor concentration in space. The method is called Parallel Four-Step Phase Shifting Interferometer (PFSPSI). The first case studies the evaporation process of the acetone contained in a liquid pool with uniform air flow in a low-speed wind tunnel. The mole fractions of the acetone vapor near the liquid-air interface with different air speeds are characterized. The second case studies the evaporation process of acetone droplets levitated by an ultrasound levitator. The mole fraction of the acetone vapor near the liquid-air interface is characterized by assuming an axisymmetric field and using the analytical solution of the inverse Abel transform. The asymmetric pattern of the acetone vapor field is observed, which is considered due to the drastic sound pressure change at the stand wave location produced by the ultrasound levitator. The mass transfer of the evaporation process by the vapor’s mole fraction is calculated and compared with the mass transfer calculated by the droplet size change. It is observed that the mass transfer by the vapor’s mole fraction is generally smaller than the mass transfer calculated by the droplet size change, which can be explained by the convection process induced by the acoustic streaming.</p>