Nowadays, the need for three-dimensional miniaturized components is increasing in many areas, such as electronics, biomedics, aerospace and defence, etc. To support the demands, various micro-scale fabrication techniques have been further introduced and developed over the last decades, including micro-electric-mechanical technologies (MEMS and LIGA), laser ablation, and miniature machine tools (mMTs). Each of these techniques has its own benefits, however miniature machine tools are superior to any others in enabling three-dimensional complex geometry with high relative accuracy, and the capability of dealing with a wide range of mechanical materials. Thus, mMTs are emerging as a promising fabrication process. In this work, various researches have been carried out based on the mMTs. The thesis presents micro-machining, in particular, micro-milling force model and three relevant subsystems for miniature machine tools (mMTs), to enhance machining productivity/efficiency and dimensional accuracy of machined parts. The comprehensive force model that predicts micro-endmilling dynamics has been developed. Unlike conventional macro-machining, the cutting mechanism in micro-machining is complex with high level of non-linearity due to the combined effects of edge radius, size, and minimum chip thickness effect, etc., resulting in no chip formation when the chip thickness is below the minimum chip forming thickness. Instead, part of the work material deforms plastically under the edge of a tool and the rest of the material recovers elastically. The developed force model for micro-endmilling is effective to understand the micro-machining process. As a result, the micro-endmilling force model is helpful to improve the quality of machined parts. In addition, three relevant subsystems which deliver maximum machining productivity and efficiency are also introduced. Firstly, ultrasonic atomization-based cutting fluid application system is introduced. During machining, cutting fluid is required at the cutting zone for cooling and lubricating the cutting tool against the workpiece. Improper cutting fluid application leads to significantly increased tool wear, and which results in overall poor machined parts quality. For the micro-machining, conventional cooling methods using high pressure cutting fluid is not viable due to the potential damage and deflection of weak micro-cutting tools. The new atomization-based cutting fluids application technique has been proven to be quite effective in machinability due to its high level of cooling and lubricating. Secondly, an acoustic emission (AE)-based tool tip positioning method is introduced. Tool tip setting is one of the most important factors to be considered in the CNC machine tool. Since several tools with different geometries are employed during machining, overall dimensional accuracy of the machined parts are determined by accurate coordinates of each tool tip. In particular, tool setting is more important due to micro-scale involved in micro-machining. The newly developed system for tool tip positioning determines the accurate coordinates of the tool tip through simple and easy manipulation. At last, with the advance of the 3D micro-fabrication technologies, the machinable miniaturized components are getting complex in geometry, leading to increased demand on dimensional quality control. However, the system development for micro-scale parts is slow and difficult due to complicated detection devices, algorithm, and fabrication of a micro-probe. Consequently, the entire dimensional probing system tends to become bulky and expensive. A new AE-based probing system with a wire-based probe was developed to address this issue with reduced cost and size, and ease of application. / Graduate

As drop-on-demand (DOD) applications continue to gain ground in desktop inkjet-printing, 3D printing, fluid mixing, and other areas the demand for higher frequency operations are beginning to push against the current physical boundaries in DOD technology. The current research is exploring the possibility of controlling drop volume and velocity at high frequency ranges where meniscus vibrations can occur between drop formations and affect drop formation characteristics. A periodic voltage is applied to a piezoelectric disk in order to generate pressure fluctuations in a single nozzle droplet generator, causing the fluid meniscus at the nozzle to vibrate. A single stronger pulse is then superimposed over the periodic waveform at different phases in order to drive drop ejection. The characteristics of the resulting drop, specifically the volume and velocity, are experimentally measured using a high speed camera with precise timing control. The results of these experiments are then compared to a lumped element model (LEM) developed for the droplet generator geometry used. Within the LEM model framework, special attention was given to the definition of a novel method by which one can measure drop volume within an electroacoustic circuit and also allow meniscus dynamics to affect present and future drop formations. Experimental results indicate a strong dependence of both drop volume and drop velocity on the phase of the vibrating meniscus at the start of drop formation. Positive meniscus displacements and momentums resulted in large drop volumes and velocities while negative displacements could reduce drop volume or altogether eliminate drop formation. Specifically, positive displacements and momentum of a vibrating meniscus could lead to drop volumes approximately 50% larger than the original drop volume without a vibrating meniscus. Meanwhile, negative meniscus displacements and momentums were shown to have the ability to completely prevent drop formation. Additional potential for drop characteristic control with a vibrating meniscus is discussed alongside observations on the stabilizing affect the vibrating meniscus appears to have on drop velocity as a function of time. Also, flow visualization of the drop formation is provided to demonstrate the added affect the meniscus vibrations have on the drop shapes and break-off profiles. The LEM model presented demonstrates qualitative agreement with the experimental model, but fails to quantitatively predict drop volumes. Sources of error for the LEM model and potential improvements are discussed. / Graduation date: 2012

19 Dec 2004. / Published through the Information Bridge: DOE Scientific and Technical Information. "IS-T 1983" Fei Tang. 12/19/2004. Report is also available in paper and microfiche from NTIS.

L’atomisation d’un jet ou d’une nappe liquide assistée par un courant gazeux rapide est couramment utilisée dans l’industrie ainsi qu’en propulsion aéronautique (turboréacteur) et spatiale (moteur-fusée cryotechnique). Plusieurs processus permettent la fragmentation de la structure cohérente liquide en gouttes. L’épluchage, qui intervient à courte distance en aval de l’injection, a été assez largement étudié (Marmottant et Villermaux 2004, Hong et al 2004) et les mécanismes sont assez bien décrits. En revanche, l’origine des instabilités large échelle – ou « flapping » - intervenant plus loin en aval, instabilités qui sont à l’origine de la production de large gouttes, reste mal comprise. Ceci est particulièrement vrai pour des jets cylindriques qui, contrairement au cas de nappes, ont fait l’objet de très peu d’études. Nous nous sommes donc attachés à comprendre l’origine du « flapping », à analyser ses liens avec les instabilités interfaciales de cisaillement, et à quantifier son impact sur la structure du jet ainsi que sur les gouttes produites. Pour cela, des expériences ont été menées en eau/air sur de larges plages de paramètres, aussi bien en termes de vitesses phasiques que des dimensions des veines gaz et liquide. Un soin particulier a été apporté au contrôle des écoulements internes.Pour l’ensemble des géométries, nous avons montré que la longueur du dard liquide est pilotée par le battement large échelle et non par le processus d’épluchage. Par ailleurs, la longueur de brisure présente une décroissance marquée avec la vitesse gaz, puis reste constante au delà d’une vitesse gaz critique. Un modèle a été proposé pour ce comportement asymptotique dans lequel la longueur de brisure est pilotée par le rapport de la vitesse liquide d’injection à une vitesse capillaire construite sur le diamètre liquide.La technique de mesure de la fréquence du battement large échelle mise en œuvre à partir d’images acquises par ombroscopie s’est avérée opérationnelle sur toute la plage de vitesses gaz considérées. Cette fréquence, qui ne varie pas spatialement, présente deux comportements : un premier où elle augmente avec la vitesse gaz, et un second où elle reste indépendante de la vitesse gaz. Ce second régime n’est pas mentionné dans la littérature. Pour le premier régime, le lien entre flapping et instabilité de cisaillement a été démontré en s’appuyant notamment sur des analyses de stabilité. Le nombre de Strouhal associé est piloté par le cisaillement côté gaz. La dépendance de la fréquence de battement à l’épaisseur de vorticité côté gaz est ainsi établie lorsque l’instabilité de cisaillement est pilotée par un mécanisme inviscide. Pour le second régime, le caractère opportuniste du flapping a été démontré l’aide d’une expérience de forçage : le flapping amplifie des structures liquides de longueur d’onde plus grande que celle associée à l’instabilité de cisaillement. Un nombre de Strouhal construit sur le diamètre liquide du jet et la vitesse du jet liquide à la distance de brisure a été proposé. Enfin, le rapport du diamètre du jet liquide à la longueur d’onde de l’instabilité de cisaillement semble pertinent pour définir la frontière entre ces deux régimes.Les tailles des gouttes produites sur l’axe de symétrie ont été mesurées à l’aide d’une sonde optique. Il apparaît que la distribution granulométrique évolue fortement avec la vitesse gaz, et qu’elle est multi-modale, ce qui traduit la présence de plusieurs mécanismes de brisure. La taille moyenne des gouttes décroit globalement comme UG-2, dans la limite de forts nombres de Weber aérodynamique. Cette taille moyenne s’avère aussi très sensible à la géométrie : elle diminue lorsque l’épaisseur gaz augmente jusqu’à atteindre une valeur plancher, et elle croît avec le diamètre liquide. / Jet or sheet atomized by a fast coaxial gas jet is currently used in industry, like aeronautical propulsion (turbofan) or spatial propulsion (cryotechnic rocket engine). Many physical processes allows liquid coherent structure fragmentation into drops. Stripping, which appears downstream near injector, has been largely studied (Marmottant et Villermaux 2004, Hong & al 2004), mecanisms has been correctly described.However, the origin of large scale - or 'flapping' instabilities - intervening further downstream, instabilities that are causing the production of large drops, remains poorly understood. This is particularly true for cylindrical jets which, unlike the case of sheets, have been the subject of very few studies. We are therefore committed to understand the origin of the "flapping", to analyze its relationship with interfacial shear instabilities, and to quantify its impact on the structure of the jet as well as on the drops produced. For this, experiments were carried out in water/air on wide set of parameters, both in terms of phasic speed than the dimensions of the gas gap and liquid diameter. Special care were made to the internal flow control.For all the geometries, we showed that the length of the liquid cone is driven by the large scale displacements and not by the stripping process. Furthermore, the length of brokenness jet presents a decline marked with the gas speed, then remains constant beyond a critical gas speed. A model was proposed for this asymptotic behavior in which the break-up length is driven by the report of the liquid injection speed to a capillary speed built on the liquid diameter.Measurement of the frequency of large scale displacement technology has been implemented from images acquired by shadowgraphy proved operational over the gas velocity range considered. This frequency, which varies not spatially, present two behaviors: a first where it increases with the speed of the gas, and a second where it remains independent of the gas speed. This second scheme is not mentioned in the literature. For the original plan, the link between flapping and shear instability has been demonstrated based on analyses of stability. The associated Strouhal number is controlled by the shear gas side. The dependence of the frequency of heartbeat to the thickness of vorticity gas side is thus established when shear instability is driven by an inviscide mechanism. For the second scheme, the opportunistic nature of the flapping has been demonstrated using forcing experience: the flapping amplifies liquid structures of wavelength greater than those associated with shear instability. A Strouhal number built on liquid jet diameter and the speed of the liquid jet at break distance has been proposed. Finally, the ratio of the diameter of the liquid jet at the wavelength of the shear instability seems relevant to define the border between these two regimes.Sizes drops produced on the symmetry axis were measured using an optical probe. It appears that granulometric distribution is evolving strongly with speed gas, and it is multi-modal, reflecting the presence of several mechanisms of brokenness. The average size of the drops decreases overall as UG - 2, in the limit of strong numbers of aerodynamic Weber. This medium size is also very sensitive to geometry: it decreases when the thickness of the gas increases until it reaches a floor value, and it grows with the liquid diameter. Finally, by forcing large amplitude lateral displacement, the average radial distribution of sizes of drops has been made much more homogeneous, and the average size of the drops on the axis has been reduced by a factor of 2. These results therefore open opportunities in terms of control of atomization.

Depuis le début du millénaire, la simulation numérique directe est apparue comme un outil précieux capable d'étudier l’atomisation d’une goutte isolée par un écoulement à grande vitesse. L’atomisation peut être divisée en deux phases distinctes : l'éclatement se produit d'abord sous la forme d'aplatissement de la goutte, formant également des filaments, puis il se poursuit via l'obtention d'une multitude de gouttes de tailles réduites ce qui complète le processus d’atomisation. Les principaux objectifs pour le présent travail étaient donc d’établir un modèle et une méthode numérique capables d’étudier au mieux ces phénomènes. L'atomisation d’une goutte isolée est présentée et est accompagnée d’une comparaison avec l’expérience qui confirme les capacités du modèle et de la méthode à simuler numériquement les différents processus physiques mis en jeu. Des informations essentielles quant aux mécanismes d’atomisation, non exploitables avec l’expérience, sont décrites et l’objectif d’obtenir des gouttes de tailles réduites est atteint. / Only at the beginning of the millennium, direct numerical simulation has emerged as a valuable tool capable of studying the atomization of an isolated droplet by a high-speed flow. The atomization can be divided into two distinct phases: the aerobreakup occurs first in the form of flattening of the droplet, also forming filaments, and then it continues via the obtaining of a multitude of reduced sizes droplets what completes the process of atomization. The main objectives of this work were therefore to establish a model and a numerical method able to study these phenomena as well as possible. The atomization of an isolated droplet is presented and is accompanied by a comparison with the experiment which confirms the capacities of the model and the method to numerically simulate the different physical processes involved. Essential information on atomization mechanisms, which cannot be exploited with experiments, is described and the objective of obtaining droplets of reduced sizes is achieved.

La réduction des émissions polluantes et l'amélioration des performances des turboréacteurs nécessitent une connaissance détaillée des phénomènes physiques mis en jeu dans une chambre de combustion. L'atomisation du carburant résulte du cisaillement engendré par un fort écoulement d'air généré dans l'injecteur. La simulation numérique directe d'écoulements avec interface permet de simuler l'ensemble du processus d'atomisation. L'utilisation de maillages Cartésiens permet la réalisation de calculs HPC efficaces et précis. Mais, une des complexités de l'atomisation vient d'une interaction forte entre le comportement de la nappe liquide et l'écoulement gazeux dans les conduites de l'injecteur, rendant impératif la simulation de l'injecteur complet. Ceci étant impossible avec des maillages Cartésiens structurés, l'objectif de cette thèse est de développer une méthode d'interface immergée permettant l'inclusion d'objets solides dans un domaine de calcul, indépendamment du maillage, afin de réaliser des DNS du système d'injection complet. Les équations de Navier-Stokes incompressibles diphasiques sont résolues à l'aide d'un algorithme de projection, l'interface liquide-gaz étant transportée avec une méthode CLSVOF conservative en masse et quantité de mouvement. La présence du solide est prise en compte grâce à la méthode d'interface immergée. Cette méthode a été appliquée à la simulation numérique de nappes liquides cisaillées pour une configuration d'injecteur utilisée en essais à l'ONERA et a permis une meilleure prédiction de la fréquence de battement de la nappe. / The reduction of polluting emissions and improvement of aeronautical engines efficiency depends on the detailed knowledge of the physical phenomena encountered in a combustion chamber. Fuel atomization results from the shearing effect induced by the high velocity airflow generated inside the injector. The Direct Numerical Simulation of interfacial flows allows the simulation of the whole atomization process, while Cartesian structured meshes allows efficient and accurate HPC computations. However, the complexity of atomization comes from a strong interaction between the jet behavior and the injector internal flow, which makes essential to simulate the whole injector system. As that is impossible on Cartesian structured grids, the main objective of this thesis is to develop an Immersed Interface Method (IIM) allowing the inclusion of solid objects in the computational domain, independently of the mesh. The incompressible two-phases Navier-Stokes equations are solved using a projection algorithm with the CLSVOF method, conservative in mass and momentum. The solid presence is taken into account using the IIM. The proposed IIM has been applied to the numerical simulation of sheared liquid sheets corresponding to an ONERA experimental configuration and allows a better prediction of the flapping frequencies of the liquid sheet.

Émissions polluantes, les motoristes souhaitent contrôler au mieux l’atomisation du carburant, injecté généralement sous forme de jets ou de nappes liquides. Les essais étant long et coûteux, leur remplacement par un outil numérique capable de simuler le processus d’atomisation permettrait non seulement une réduction des coûts importante mais faciliterait également la phase de conception. Toutefois, en raison du caractère multi-échelle du phénomène, il est difficile de le décrire dans son ensemble avec les approches habituellement utilisées en mécanique des fluides numérique.L’objectif de cette thèse est de concevoir une nouvelle approche qui permettra à terme de simuler l’atomisation pour une configuration industrielle complète. Celle-ci consiste à coupler deux types de modèles. Le premier, dit modèle bifluide, est un modèle à deux fluides compressibles basé sur les équations de Navier-Stokes diphasiques. Celui-ci permet de décrire les grandes échelles du phénomène d’atomisation correspondant à la formation de ligaments et d’amas liquides dans la zone proche de l’injecteur. Le second, dit modèle de spray, est basé sur une équation cinétique. Dans la zone située en aval de l’injecteur, ce dernier permet de décrire de manière statistique l’évolution du brouillard de gouttelettes issues de la fragmentation primaire du jet de carburant. Le point délicat, à la fois sur le plan de la modélisation et sur celui de l’algorithmique, réside dans le couplage des deux modèles. Celui ci a été réalisé grâce à l’introduction de deux modèles auxiliaires permettant de traiter le transfert de liquide entre le modèle bifluide et le modèle de spray par atomisation ou ré-impact.L’approche proposée a été appliquée à la simulation numérique de nappes liquides cisaillées. Les comparaisons entre les résultats numériques et des résultats expérimentaux montrent que le modèle bifluide permet de prévoir l’influence de la géométrie et des conditions d’injection sur l’atomisation primaire de la nappe liquide. Le modèle d’atomisation permet quant à lui, de reproduire le caractère instationnaire des mécanismes de production de gouttes lors du transfert de la phase liquide depuis le modèle bifluide vers celui de spray. Des cas de ré-impact valident également la robustesse et la généralité de la méthodologie de couplage. / In order to improve efficiency of aircraft combustion chambers and reduce polluting emissions,engine manufacturers try to achieve a better control on fuel atomization, which is usually injectedas a jet or liquid sheet. As experiments are expensive and time consuming, a numerical tool able to simulate atomization would be a powerful asset in engine conception design. However, simulation ofthe whole atomization process with commonly used approach in computational fluid dynamics is still prohibitive due to the multi-scale nature of the phenomenon.The objective of this thesis is to develop a new approach allowing the simulation of the spray formation for a industrial configuration in the near future. This involves coupling of two types of models.The first one, called two-fluid model, is based on the Navier-Stokes equations for two immiscible compressible fluids. This one is used to describe the large scales of the atomization mechanism corresponding to the formation of ligaments and liquids blobs in the near-injector area. The second one,called spray model, is based on a kinetic equation. Further downstream from the injector, this model describes statistically the evolution of the droplet cloud produced by the primary fragmentation of liquid jet. The main difficulty, in terms of both modeling and algorithmic, is the coupling of these twomodels.This has been achieved by introducing an atomization and an impact models which ensure liquid transfer between the two-fluid model and the spray model.This new approach was applied to the numerical simulation of sheared liquid sheets. Comparisons between numerical and experimental results show how the two-fluid model predicts the influence of injector geometry and injection conditions on the primary atomization of the liquid sheet. Concerning droplets production, the atomization model is able to reproduce the unsteady nature of this mechanism when transferring liquid phase from the two-fluid model to the spray model. Test cases for the impact model also validate the robustness and generality of the coupling approach.

Submitted by Maria Medeiros (maria.dilva1@ufcg.edu.br) on 2018-07-19T11:09:50Z No. of bitstreams: 1 SÍLVIO ALVES MOREIRA - TESE (PPGEP) 2013.pdf: 2013926 bytes, checksum: 3885f27bb2f69434b23233a4b6146158 (MD5) / Made available in DSpace on 2018-07-19T11:09:51Z (GMT). No. of bitstreams: 1 SÍLVIO ALVES MOREIRA - TESE (PPGEP) 2013.pdf: 2013926 bytes, checksum: 3885f27bb2f69434b23233a4b6146158 (MD5) Previous issue date: 2013-02-02 / Capes / No planeta em que vivemos, hoje com mais de sete bilhões de habitantes, é necessário rever conceitos para melhorar o mecanismo de produção e conservação de alimentos e evitar altos custos com tratamento de efluentes gerados por desperdício de matéria. Um exemplo significativo é o caso dos abatedouros de animais, especialmente bovinos, que lançam o sangue nos corpos de água causando poluição ambiental. Para minimizar estes impactos, foi desenvolvido um sistema automatizado de secagem por atomização para produção de proteína animal com o aproveitamento do sangue bovino. O sistema de secagem automático, construído com materiais de baixo custo e fácil aquisição, em módulos com possibilidade de alterações na configuração, apresenta capacidade de evaporação de 2,6 kg.h-1 de água e facilidade na operação. Os ensaios preliminares forneceram informações para atuação nas principais causas da baixa eficiência no processo de secagem por atomização. Com as ações adotadas foram obtidos resultados satisfatórios para a proposta do projeto. As principais características do sangue em pó obtido foram: boa fluidez; granulometria adequada à reconstituição e condições para armazenamento sem a petrificação do produto com a conservação da coloração. O sangue em pó com umidade em base úmida de 4,7% apresenta uma eficiência de produção de 67% e um rendimento de coleta de pó de 77%. A principal variável controlada foi a temperatura de saída, pela manipulação da vazão da suspensão, que têm influência direta na umidade do pó obtido. / Nowadays, with more than seven billion inhabitants living in the planet it is necessary to revise concepts to improve efficiency in the mechanisms of food production within the food chain and avoid high costs of wastewater treatment and high concentrations of organic matter. A significant example is the case of animals’ slaughterhouses, especially the bovine, that shed the blood into water bodies causing environmental pollution. To minimize these effects, an automated spray drying system was developed for animal protein production making use of the bovine blood. The automatic drying system, built with materials of cost low and acquisition easy in modules with a possibility of changes in layout, points out water evaporation capacity of 2.6 kg.h-1 and operation ease. Preliminary runs provided information to operate the main causes of low efficiency in the process of spray drying process. With the adopted actions satisfactory results were obtained for the project proposes. The main results were a blood powder with a particle size suitable for reconstitution, good fluidity and storage conditions for the product preserving its color without petrifying it. The blood powder with moisture content on a wet basis of 4.7% has a production efficiency of 67% and a powder collection efficiency of 77%. The main controlled variable was the output temperature through the suspension flow rate manipulation, which has a direct influence on the moisture content of the obtained powder.

The first step on the way to understanding the complicated dynamics of spray is to study the behavior of isolated droplets. In many industrial and natural processes such as turbulent combustion, agricultural sprays, spray cooler, falling raindrops and cloud evolution the droplet is subjected to a chaotic unsteady external flow field. The interaction between the liquid and gaseous phases results in very intricate droplet dynamics like capillary instabilities, atomization, droplet collision and coalescence and vaporization, to name a few. In this dissertation, the focus is on shape oscillations, atomization and vaporization dynamics of pendant and sessile droplets. A droplet residing on a substrate which vibrates vertically at ultrasonic frequency will exhibit different modes of shape oscillation. The competition between capillary forces and inertia forces is basically responsible for these oscillations. However, when an acoustic force field is introduced asymmetrically around the droplet, we discover with the help of ultra high-speed imaging, a new droplet spreading phase. This new method of droplet manipulation could nd application in micro fluidics and lab-on-a-chip systems. By lading the droplet with nanoparticles, the spreading rate can be easily controlled. The spreading phase is followed by an atomization phase where surface ligaments grow to disintegrate into daughter droplets; the intensity of atomization is found to decrease with increase in fluid viscosity. The ability to control atomization characteristics of droplets by lading them with nanoparticles is a powerful technique that may be implemented in spray coolers and combustors to control the spray characteristics or combustion efficiency. Both the spreading and ligament dynamics have been theoretically simulated and the physics behind the observed trends is explained. The growth rate of the ligaments is found to be governed by Weber number modified to include the acoustic pressure level of the standing wave. The frequency of ligament breakup is found to decrease with fluid viscosity and this observation is adequately supported by a theory developed based on the evolution crater on the droplet surface. Turning now to the pendant droplets, by decomposing the droplet shape into Legendre modes, the shape oscillations exhibited by a droplet hanging from the junction of cross-wire placed at the center of an air jet is studied. Both high-speed imaging and hot-wire anemometry are employed. The driving force of oscillation of droplets subjected to the air jet is proved to be the inherent pressure fluctuations in the jet. The effect of surface tension, viscosity and Reynolds number on the shape oscillation level has been examined. The first experimental evidence of viscous attenuation of lower frequencies in a particular mode in glycerol/water mixture is reported. A theoretical model was developed to simulate the droplet shape oscillations induced by different ambient flow fields like pulsatile flow, vortical flow and flow with broadband energy spectrum. The time of interaction of the droplet with an eddy in the flow is found to be very crucial in determining the amplitude of oscillation of the droplet. The shorter the interaction time, the higher are the chances of the droplet oscillation being pushed into resonance. Finally, the heat transfer and droplet regression dynamics of pendant droplets in a hot air stream of various chemical compositions (like conventional fuels, alternative fuels and nanosuspensions) have been experimentally analyzed using high speed imaging. The droplet is deployed at the junction of cross-wire at the centre of a vertical air jet. A hybrid timescale has been proposed which incorporates the effects of latent heat of vaporization, saturation vapor pressure and thermal diffusivity. This timescale in essence encapsulates the different parameters that influence the droplet vaporization rate. The analysis further permitted the evaluation of the effect of various parameters such as surrounding temperature, Reynolds number, far-field vapor presence, impurity content and agglomeration dynamics (nanosuspensions) in the droplet.

Disponibilidade dos recursos energéticos junto com o despertar da consciência ambiental criaram um interesse por uma condição climática sensível compatível com os recursos disponíveis. Dentro desse cenário o trabalho se volta à necessidade de se criarem e manterem ambientes industriais termicamente adequados aos processos de produção para minimizar as interferências que as condições ambientais exercem sobre os custos dos processos de produtivos e sobre o consumo energético. Os sistemas de resfriamento evaporativo, por sua vez, têm sido a ferramenta de maior potencial de aplicação na criação de ambientes termicamente adequados aos processos. Este modelo revisto de conforto térmico nos coloca um passo à frente para o aumento eficiência energética na construção de projeto de climatização vinculados a temperaturas interiores que atendam conjuntamente tanto aos ocupantes como às atividades que desenvolvem no interior da área climatizada. Apesar de esse sistema apresentar vantagens operacionais, quando comparado a outros sistemas convencionais, existem certas limitações no seu desempenho. Uma das maiores dificuldades das instalações destes sistemas reside na existência de incertezas em qualquer resultado. Possibilitar um controle dos parâmetros, minimizando os erros de aplicação, evitando criar no ambiente um desconforto de tal grau que inviabilize sua aplicação, é o fundamento deste trabalho. A busca passa a ser pela garantia da aceitabilidade dos resultados do sistema projetado e seus limites de aplicabilidade. O estudo das variáveis que interferem no processo do resfriamento por micro aspersão permitiu desenvolver um processo que alterara esses parâmetros durante o funcionamento do sistema, interferindo, conforme a necessidade no seu desempenho, garantindo a completa evaporação da água micro aspergida. / Energy resources along with an environmental conscience awakening has created an interest in sensitive climate together with a more understanding regarding the use of available resources. Inside this scenario our work focus on the needs of creating and maintaining industrial environments thermally suited to these production processes that seeking to minimize interference that environmental conditions have on the costs of production processes and energy consumption. Evaporative cooling systems, in turn, has been a interesting tool to be used in the creation of thermally suitable environments to these processes. This new revised thermal comfort model puts us a step forward to increase energy efficiency in elaborating air treatment projects linked to indoor temperatures that meet both the occupants and the activities that develop inside the controlled area. Although this system has operational advantages when compared to other conventional systems, there are some limitations in their performance. A major difficulty of the installation envolving these systems is about the existence of uncertainty in any results. To allow the control of these parameters in order to minimize the errors in this kind of application and to avoid creating environmental discomfort to such a degree that prevent the implementation, it is the foundation of this work. The search is to ensure the acceptability of the results of the system designed and their limits of applicability. The study of the variables that affect the cooling process by misting allowed us to develop a process that altered these parameters during operation of the system, interfering, as required in its performance, ensuring complete evaporation of water applied by misting in the area.