AN ASSESSMENT OF FLOW REGIME MAPS AND A NUMERICAL HEAT TRANSFER CORRELATION FOR THE STRATIFIED/ANNULAR REGIME OF SHEAR-DRIVEN INTERNAL CONDENSING FLOWS

Several modern-day cooling applications require the incorporation of mini/micro-channel shear-driven flow condensers. There are several design challenges that need to be overcome in order to meet those requirements. The difficulty in developing effective design tools for shear-driven flow condensers is exacerbated due to the lack of a bridge between the physics-based modelling of condensing flows and the current, popular approach based on semi-empirical heat transfer correlations. One of the primary contributors of this disconnect is a lack of understanding caused by the fact that typical heat transfer correlations eliminate the dependence of the heat transfer coefficient on the method of cooling employed on the condenser surface when it may very well not be the case. This is in direct contrast to direct physics-based modeling approaches where the thermal boundary conditions have a direct and huge impact on the heat transfer coefficient values. Typical heat transfer correlations instead introduce vapor quality as one of the variables on which the value of the heat transfer coefficient depends. This study shows how, under certain conditions, a heat transfer correlation from direct physics-based modeling can be equivalent to typical engineering heat transfer correlations without making the same apriori assumptions. Another huge factor that raises doubts on the validity of the heat-transfer correlations is the opacity associated with the application of flow regime maps for internal condensing flows. It is well known that flow regimes influence heat transfer rates strongly. However, several heat transfer correlations ignore flow regimes entirely and present a single heat transfer correlation for all flow regimes. This is believed to be inaccurate since one would expect significant differences in the heat transfer correlations for different flow regimes. Several other studies present a heat transfer correlation for a particular flow regime - however, they ignore the method by which extents of the flow regime is established. This thesis provides a definitive answer (in the context of stratified/annular flows) to: (i) whether a heat transfer correlation can always be independent of the thermal boundary condition and represented as a function of vapor quality, and (ii) whether a heat transfer correlation can be independently obtained for a flow regime without knowing the flow regime boundary (even if the flow regime boundary is represented through a separate and independent correlation). To obtain the results required to arrive at an answer to these questions, this study uses two numerical simulation tools - the approximate but highly efficient Quasi-1D simulation tool and the exact but more expensive 2D Steady Simulation tool. Using these tools and the approximate values of flow regime transitions, a deeper understanding of the current state of knowledge in flow regime maps and heat transfer correlations in shear-driven internal condensing flows is obtained. The ideas presented here can be extended for other flow regimes of shear-driven flows as well. Analogous correlations can also be obtained for internal condensers in the gravity-driven and mixed-driven configuration.

Development of one-dimensional and two-dimensional computational tools that simulate steady internal condensing flows in terrestrial and zero-gravity environments

This dissertation presents an effective quasi one-dimensional (1-D) computational simulation tool and a full two-dimensional (2-D) computational simulation methodology for steady annular/stratified internal condensing flows of pure vapor. These simulation tools are used to investigate internal condensing flows in both gravity as well as shear driven environments. Through accurate numerical simulations of the full two dimensional governing equations, results for laminar/laminar condensing flows inside mm-scale ducts are presented. The methodology has been developed using MATLAB/COMSOL platform and is currently capable of simulating film-wise condensation for steady (and unsteady flows). Moreover, a novel 1-D solution technique, capable of simulating condensing flows inside rectangular and circular ducts with different thermal boundary conditions is also presented. The results obtained from the 2-D scientific tool and 1-D engineering tool, are validated and synthesized with experimental results for gravity dominated flows inside vertical tube and inclined channel; and, also, for shear/pressure driven flows inside horizontal channels. Furthermore, these simulation tools are employed to demonstrate key differences of physics between gravity dominated and shear/pressure driven flows. A transition map that distinguishes shear driven, gravity driven, and “mixed” driven flow zones within the non-dimensional parameter space that govern these duct flows is presented along with the film thickness and heat transfer correlations that are valid in these zones. It has also been shown that internal condensing flows in a micro-meter scale duct experiences shear driven flow, even in different gravitational environments. The full 2-D steady computational tool has been employed to investigate the length of annularity. The result for a shear driven flow in a horizontal channel shows that in absence of any noise or pressure fluctuation at the inlet, the onset of non-annularity is partly due to insufficient shear at the liquid-vapor interface. This result is being further corroborated/investigated by R. R. Naik with the help of the unsteady simulation tool. The condensing flow results and flow physics understanding developed through these simulation tools will be instrumental in reliable design of modern micro-scale and spacebased thermal systems.

Computational study of internal and external condensing flows and experimental synthesis to investigate their attainability and stability in ground-based and space-based environments

This doctoral thesis presents the computational work and synthesis with experiments for internal (tube and channel geometries) as well as external (flow of a pure vapor over a horizontal plate) condensing flows. The computational work obtains accurate numerical simulations of the full two dimensional governing equations for steady and unsteady condensing flows in gravity/0g environments. This doctoral work investigates flow features, flow regimes, attainability issues, stability issues, and responses to boundary fluctuations for condensing flows in different flow situations. This research finds new features of unsteady solutions of condensing flows; reveals interesting differences in gravity and shear driven situations; and discovers novel boundary condition sensitivities of shear driven internal condensing flows. Synthesis of computational and experimental results presented here for gravity driven in-tube flows lays framework for the future two-phase component analysis in any thermal system. It is shown for both gravity and shear driven internal condensing flows that steady governing equations have unique solutions for given inlet pressure, given inlet vapor mass flow rate, and fixed cooling method for condensing surface. But unsteady equations of shear driven internal condensing flows can yield different “quasi-steady” solutions based on different specifications of exit pressure (equivalently exit mass flow rate) concurrent to the inlet pressure specification. This thesis presents a novel categorization of internal condensing flows based on their sensitivity to concurrently applied boundary (inlet and exit) conditions. The computational investigations of an external shear driven flow of vapor condensing over a horizontal plate show limits of applicability of the analytical solution. Simulations for this external condensing flow discuss its stability issues and throw light on flow regime transitions because of ever-present bottom wall vibrations. It is identified that laminar to turbulent transition for these flows can get affected by ever present bottom wall vibrations. Detailed investigations of dynamic stability analysis of this shear driven external condensing flow result in the introduction of a new variable, which characterizes the ratio of strength of the underlying stabilizing attractor to that of destabilizing vibrations. Besides development of CFD tools and computational algorithms, direct application of research done for this thesis is in effective prediction and design of two-phase components in thermal systems used in different applications. Some of the important internal condensing flow results about sensitivities to boundary fluctuations are also expected to be applicable to flow boiling phenomenon. Novel flow sensitivities discovered through this research, if employed effectively after system level analysis, will result in the development of better control strategies in ground and space based two-phase thermal systems.

EXPERIMENTAL INVESTIGATION OF CERTAIN INTERNAL CONDENSING AND BOILING FLOWS: THEIR SENSITIVITY TO PRESSURE FLUCTUATIONS AND HEAT TRANSFER ENHANCEMENTS

Space-based (satellite, scientific probe, space station, etc.) and millimeter – to – microscale (such as are used in high power electronics cooling, weapons cooling in aircraft, etc.) condensers and boilers are shear/pressure driven. They are of increasing interest to system engineers for thermal management because flow boilers and flow condensers offer both high fluid flow-rate-specific heat transfer capacity and very low thermal resistance between the fluid and the heat exchange surface, so large amounts of heat may be removed using reasonably-sized devices without the need for excessive temperature differences. However, flow stability issues and degradation of performance of shear/pressure driven condensers and boilers due to non-desirable flow morphology over large portions of their lengths have mostly prevented their use in these applications. This research is part of an ongoing investigation seeking to close the gap between science and engineering by analyzing two key innovations which could help address these problems. First, it is recommended that the condenser and boiler be operated in an innovative flow configuration which provides a non-participating core vapor stream to stabilize the annular flow regime throughout the device length, accomplished in an energy-efficient manner by means of ducted vapor re-circulation. This is demonstrated experimentally. Second, suitable pulsations applied to the vapor entering the condenser or boiler (from the re-circulating vapor stream) greatly reduce the thermal resistance of the already effective annular flow regime. For experiments reported here, application of pulsations increased time-averaged heat-flux up to 900 % at a location within the flow condenser and up to 200 % at a location within the flow boiler, measured at the heat-exchange surface. Traditional fully condensing flows, reported here for comparison purposes, show similar heat-flux enhancements due to imposed pulsations over a range of frequencies. Shear/pressure driven condensing and boiling flow experiments are carried out in horizontal mm-scale channels with heat exchange through the bottom surface. The sides and top of the flow channel are insulated. The fluid is FC-72 from 3M Corporation.

Analysis of air flow past and through the 2415-3S airfoil for an unmanned aerial vehicle with internal propulsion system

This paper deals with the prediction of velocity fields on the 2415-3S airfoil which will be used for an unmanned aerial vehicle with internal propulsion system and in this way analyze the air flow through an internal duct of the airfoil using computational fluid dynamics. The main objective is to evaluate the effect of the internal air flow past the airfoil and how this affects the aerodynamic performance by means of lift and drag forces. For this purpose, three different designs of the internal duct were studied; starting from the base 2415-3S airfoil developed in previous investigation, basing on the hypothesis of decreasing the flow separation produced when the propulsive airflow merges the external flow, and in this way obtaining the best configuration. For that purpose, an exhaustive study of the mesh sensitivity was performed. It was used a non-structured mesh since the computational domain is three-dimensional and complex. The selected mesh contains approximately 12.5 million elements. Both the computational domain and the numerical solution were made with commercial CAD and CFD software, respectively. Air, incompressible and steady was analyzed. The boundary conditions are in concordance with experimental setup in the AF 6109 wind tunnel. The k-e model is utilized to describe the turbulent flow process as followed in references. Results allowed obtaining velocity contours as well as lift and drag coefficients and also the location of separation and reattachment regions in some cases for zero degrees of angle of attack on the internal and external surfaces of the airfoil. Finally, the selection of the configuration with the best aerodynamic performance was made, selecting the option without curved baffles.

Numerical analysis of air flow past the 2415-3S airfoil for an unmanned aerial vehicle with internal propulsion system

This paper deals with the prediction of pressure and velocity fields on the 2415-3S airfoil which will be used for and unmanned aerial vehicle with internal propulsion system and in this way analyze the air flow through an internal duct of the airfoil using computational fluid dynamics. The main objective is to evaluate the effect of the internal air flow past the airfoil and how this affects the aerodynamic performance by means of lift and drag forces. For this purpose, three different designs of the internal duct were studied; starting from the base 2415-3S airfoil developed in previous investigation, basing on the hypothesis of decreasing the flow separation produced when the propulsive airflow merges the external flow, and in this way obtaining the best configuration. For that purpose, an exhaustive study of the mesh sensitivity was performed. It was used a non-structured mesh since the computational domain is tridimensional and complex. The selected mesh contains approximately 12.5 million elements. Both the computational domain and the numerical solution were made with commercial CAD and CFD software respectively. Air, incompressible and steady was analyzed. The boundary conditions are in concordance with experimental setup in the AF 6109 wind tunnel. The k-ε model is utilized to describe the turbulent flow process as followed in references. Results allowed obtaining pressure and velocity contours as well as lift and drag coefficients and also the location of separation and reattachment regions in some cases for zero degrees of angle of attack on the internal and external surfaces of the airfoil. Finally, the selection of the configuration with the best aerodynamic performance was made, selecting the option without curved baffles.

CFD Modelling of Direct Contact Condensation in Suppression Pools by Applying Condensation Models of Separated Flow

The condensation rate has to be high in the safety pressure suppression pool systems of Boiling Water Reactors (BWR) in order to fulfill their safety function. The phenomena due to such a high direct contact condensation (DCC) rate turn out to be very challenging to be analysed either with experiments or numerical simulations. In this thesis, the suppression pool experiments carried out in the POOLEX facility of Lappeenranta University of Technology were simulated. Two different condensation modes were modelled by using the 2-phase CFD codes NEPTUNE CFD and TransAT. The DCC models applied were the typical ones to be used for separated flows in channels, and their applicability to the rapidly condensing flow in the condensation pool context had not been tested earlier. A low Reynolds number case was the first to be simulated. The POOLEX experiment STB-31 was operated near the conditions between the ’quasi-steady oscillatory interface condensation’ mode and the ’condensation within the blowdown pipe’ mode. The condensation models of Lakehal et al. and Coste & Lavi´eville predicted the condensation rate quite accurately, while the other tested ones overestimated it. It was possible to get the direct phase change solution to settle near to the measured values, but a very high resolution of calculation grid was needed. Secondly, a high Reynolds number case corresponding to the ’chugging’ mode was simulated. The POOLEX experiment STB-28 was chosen, because various standard and highspeed video samples of bubbles were recorded during it. In order to extract numerical information from the video material, a pattern recognition procedure was programmed. The bubble size distributions and the frequencies of chugging were calculated with this procedure. With the statistical data of the bubble sizes and temporal data of the bubble/jet appearance, it was possible to compare the condensation rates between the experiment and the CFD simulations. In the chugging simulations, a spherically curvilinear calculation grid at the blowdown pipe exit improved the convergence and decreased the required cell count. The compressible flow solver with complete steam-tables was beneficial for the numerical success of the simulations. The Hughes-Duffey model and, to some extent, the Coste & Lavi´eville model produced realistic chugging behavior. The initial level of the steam/water interface was an important factor to determine the initiation of the chugging. If the interface was initialized with a water level high enough inside the blowdown pipe, the vigorous penetration of a water plug into the pool created a turbulent wake which invoked the chugging that was self-sustaining. A 3D simulation with a suitable DCC model produced qualitatively very realistic shapes of the chugging bubbles and jets. The comparative FFT analysis of the bubble size data and the pool bottom pressure data gave useful information to distinguish the eigenmodes of chugging, bubbling, and pool structure oscillations.

Implementação do TFM na Sakthi Portugal com recurso à metodologia Kaizen

No âmbito da unidade curricular Dissertação/Projeto/Estágio do 2ºano do Mestrado em Engenharia mecânica – Ramo Gestão Industrial do Instituto Superior de Engenharia do Porto, o presente trabalho de dissertação foi enquadrado num projeto industrial de melhoria com Instituto Kaizen, empresa de consultoria operacional. O projeto foi desenvolvido numa empresa de produção de componentes em ferro nodular destinados à indústria automóvel do mercado europeu, a Sakthi Portugal,SA. A realização deste projeto teve como objetivo a implementação do sistema de planeamento em Pull (produção puxada) na logística interna da Sakthi Portugal,SA recorrendo à metodologia Kaizen. Esta metodologia consiste na aplicação de ferramentas de TFM - Total Flow Management, integradas no Kaizen Management System. Neste projeto recorreu-se especialmente a um dos pilares que o constituem, o pilar do “Fluxo da Logística Interna”. Neste pilar encontram-se as várias metodologias utilizadas na otimização do fluxo de material e informação na logística interna. Estas metodologias foram aplicadas, com o objetivo do sistema produtivo operar de acordo com a necessidade do cliente, obtendo deste modo a minimização dos custo e o aumento da produtividade e qualidade. Em resultado da aplicação da metodologia seguida, foi possível atingir-se os objetivos definidos inicialmente e em alguns casos foi possível superar esses objetivos. Em função da abordagem integrada que foi seguida, conseguiu-se uma diminuição do “lead time” do processo de fabrico, redução dos produtos em curso de fabrico, libertação de espaço e redução de inventários. Estas melhorias resultaram numa movimentação interna na fábrica mais facilitada e num aumento global da produtividade. Como consequência positiva dos efeitos deste trabalho, pode-se apontar o facto de que a Sakthi Portugal SA aumentou a sua competitividade por tornar-se numa empresa mais dinâmica, mais adaptada ao mercado e com níveis de satisfação do cliente muito superiores.

Aplicação da metodologia Kaizen em gestão de armazém de peças

Mestrado em Engenharia Mecânica - Especialização em Gestão Industrial

Melhoria do processo produtivo na Sakthi Portugal aplicação da metodologia Kaizen

No âmbito da unidade curricular Dissertação/Projeto/Estágio do 2ºano do Mestrado em Engenharia mecânica – Ramo Gestão Industrial do Instituto Superior de Engenharia do Porto, o presente trabalho de dissertação foi enquadrado num projeto industrial de melhoria com o Instituto Kaizen. O projeto foi desenvolvido num dos maiores fornecedores europeus de componentes em ferro fundido para a indústria automóvel, a Sakthi Portugal SA. A indústria automóvel é um dos mais importantes e exigentes sectores da organização industrial, e por isso é imprescindível que todos os recursos cingidos sejam capazes de enfrentar os requisitos do meio em questão. Para responder de uma forma mais eficiente, a Sakthi Portugal deu início à implementação de um conjunto de ações de melhoria para rentabilizar os seus recursos, respondendo ao mesmo tempo a problemas recorrentes no seu processo de planeamento produtivo Este trabalho pretende avaliar e analisar as ações e decisões tomadas na organização com o propósito de aumentar a produtividade do processo produtivo, reduzindo ao mesmo tempo custos e problemas que afetam todo o fluxo do processo. Em resultado da aplicação da metodologia Kaizen, foi possível atingir-se os objetivos definidos inicialmente, superando-se algumas barreiras que se pensavam intransponíveis. Estas melhorias resultaram numa movimentação interna na fábrica mais facilitada e num aumento global da produtividade. Como consequência positiva dos efeitos deste trabalho, pode apontar-se o facto de que, a Sakthi Portugal SA, aumentou a sua competitividade ao tornar-se numa empresa mais dinâmica, mais adaptada ao mercado e com níveis de satisfação do cliente muito superiores.

Tehtaan sisäisten materiaalivirtojen kehittäminen layoutsuunnittelun avulla

Työn tavoitteena oli kehittää tehtaan sisäisiä materiaalivirtoja layoutia muuttamalla ja materiaalinkäsittelyä parantamalla. Kehityksen seurauksena tulisi materiaalinkäsittelyn henkilökuntaa pystyä siirtämään tuotannon tehtäviin. Aluksi selvitettiin tehtaan toiminta, tuotteet ja prosessit, jonka jälkeen tehtiin layoutsuunnitteluun liittyvien teorioiden avulla kvantitatiivisia ja kvalitatiivisia arviointeja materiaalivirroista. Arvioinneissa havaittiin layoutsuunnittelun kannalta tärkeät asiat sekä yhteydet osastojen/työpisteiden välillä, mikä oli lähtökohtana uudelle layoutsuunnitelmalle. Työ oli kaksivaiheinen. Ensimmäisessä vaiheessa kehitettiin tehtaan nykyisiä materiaalivirtoja muuttamalla nykyistä layoutia ja parantamalla materiaalinkäsittelyä. Muutos pyrittiin pitämään hyvin kevyenä ja nykyiseen layoutiin tehtiin kaksi perusratkaisua. Kummassakin perusratkaisussa saadaan koneiden siirroilla materiaalivirtojen kannalta tärkeät koneet etusijalle sekä lisää tarvittavaa varastotilaa. Lisätilan saaminen varastoille vähentää myös tarpeetonta materiaalinkäsittelyä. Toisessa vaiheessa suunniteltiin layout laajennettuun tehdastilaan. Ensisijaisena tavoitteena oli logistinen toimivuus. Laajennuksen layoutsuunnitelmassa määritettiin kvantitatiivisten ja kvalitatiivisten arviointien avulla osastojen paikat ja koot sekä mietittiin kunkin osaston yksityiskohtaisessa suunnittelussa huomioon otettavia asioita. Suunnitelma on lähtökohtana yksityiskohtaisille suunnitelmille. Tärkeää layoutin suunnittelussa ja toteuttamisessa on huomioida layoutin käyttäjien eli työntekijöiden mielipiteet.

Tiedonkulun merkitys erilaisissa tuotannonohjausympäristöissä

Tämä kandidaatintyö käsittelee yrityksen sisäisen tiedonkulun merkitystä erilaisissa tuotannonohjausympäristöissä. Työn tavoitteena on selvittää millaisia tietotarpeita tuotannonohjauksella on, miten tuotannonohjausmuoto vaikuttaa tietotarpeisiin sekä onko puutteellisen tiedonkulun seurauksilla erilainen merkitys asiakastilauksen kytkentäpisteen (CODP) mukaisissa tuotantoympäristöissä. Lisäksi työ antaa teoriakatsauksen tuotannonohjausprosessista sekä yrityksen sisäisestä tiedonkulusta. Tutkielman perusteella voidaan todeta, että tuotannonohjausmuodot vaikuttavat tietotarpeisiin ja että puutteellisen tiedonkulun seurauksilla on erilainen merkitys erilaisissa tuotantoympäristöissä. Yleisesti voidaan todeta, että mitä aikaisemmassa vaiheessa CODP on, sitä merkittävämpiä seuraukset ovat. Koska sisäisen tiedonkulun, tuotannonohjausmuotojen sekä puutteellisen tiedonkulun seurausten välisestä merkityksestä ei ole varsinaisesti julkaistu aiempaa tutkimusta, olisi lisätutkimus myös tarpeellista.

Ionospheric Signatures of Pulsed Magnetopause Reconnection

The concept of zero-flow equilibria of the magnetosphere-ionosphere system leads to a large number of predictions concerning the ionospheric signatures of pulsed magnetopause reconnection. These include: poleward-moving F-region electron temperature enhancements and associated transient 630nm emission; associated poleward plasma flow which, compared to the pulsed variation of the reconnection rate, is highly smoothed by induction effects; oscillatory latitudinal motion of the open/closed field line boundary; phase lag of plasma flow enhancements after equatorward motions of the boundary; azimuthal plasma flow bursts, coincident in time and space with the 630nm-dominant auroral transients, only when the magnitude of the By component of the interplanetary magnetic field (IMF) is large; azimuthal-then-poleward motion of 630nm-dominant transients at a velocity which at all times equals the internal plasma flow velocity; 557.7nm-dominant transients on one edge of the 630nm-dominant transient (initially, and for large |By|, on the poleward or equatorward edge depending on the polarity of IMF By); tailward expansion of the flow response at several km s-1; and discrete steps in the cusp ion dispersion signature between the polewardmoving structures. This paper discusses these predictions and how all have recently been confirmed by combinations of observations by optical instruments on the Svalbard Islands, the EISCAT radars and the DMSP and DE satellites.

Análise de integridade física de barragens de terra a partir da integração do método geofísico da eletrorresistividade com ensaios geotécnicos

Pós-graduação em Geociências e Meio Ambiente - IGCE

Análise de integridade física de barragens de terra a partir da integração do método geofísico da eletrorresistividade com ensaios geotécnicos

Pós-graduação em Geociências e Meio Ambiente - IGCE