The aim of this thesis is to realize analysis of problematics of aerodynamic calculations of steam boilers on the part of combustion air. On the basis of project documentation realize evaluations of sectional dissipation factors of each component of inlet tract. Realize calculation of summary pressure (draft) loss. Specify components with highest loss and propose options of their optimization.

MEMS (Micro Electro Mechanical Systems) have received a great deal of attention in both the research and industrial sectors in recent decades. The broad MEMS category, microfluidics, the study of fluid flow through channels measured on the micrometer scale, plays an important role in devices such as compact heat exchangers, chemical and biological sensors, and lab-on-a-chip devices. Most of the research has been focused on how entire systems operate, both experimentally and through simulation. This paper strives, systematically, to map them through experimentation of the previous to untested realm of pressure loss through laminar square-profile sweeping-bend microchannels. Channels were fabricated in silicone and designed so a transducer could detect static pressure across a very specific length of channel with a desired bend. A wide variety of Reynolds numbers, bend radii, and bend angles were repeatedly tested over long periods in order to acquire a complete picture of pressure loss with in the domain of experimentation. Nearly all situations tested were adequately captured with the exception of some very low loss points that were too small to detect accurately. The bends were found to match laminar straight-duct theory at Reynolds numbers below 30. As Reynolds numbers increased, however, minor losses began to build and the total pressure loss across the bend rose above straight-duct predictions. A new loss coefficient equation was produced that properly predicted pressure losses for sweeping-bends at higher Reynolds numbers; while lower flow ranges are left to laminar flow loss for prediction.

<p> An experimental study of turbulent flow of air around a 90º bend is reported in this thesis. Four 90º bends of aspect ratio 1, 3, 5 & 10 and radius ratio 1.0 have been tested in the Reynolds number range of 1 × 10⁵ to 5 × 10⁵. The loss in total pressure across the bend (or elbow) is reported for two discharge conditions (1) and the elbow discharging to a plenum chamber through a constant area duct of a length equal to 4 hydraulic diameters; (2) the elbow discharging to the plenum chamber directly. A comparison of the experimental results is made with the curves given in NACA report L4F26 which have been reproduced in the recently published SAE Aero-Space Manual. </p> <p> Various other flow parameters, such as velocity profiles, turbulence levels and pressure distributions are also given in this thesis. </p> / Thesis / Master of Engineering (ME)

In a gas turbine, a small portion of air is bled from the compressor to provide cooling to keep the turbine at a safe operating temperature. The air flows through several passages in between where the components of the turbine are assembled. In this study, the heat transfer and pressure loss characteristics of two of these passages are investigated experimentally. The first of the two passages investigated is the passage in between the turbine blade root and disc. This passage has a unique geometry resembling an S-shape. The heat transfer and pressure loss characteristic of this passages in not well documented. For this study, a model of the realistic S-shaped passage has been made. In addition, a simplified rectangular duct with hydraulic diameter similar to that of the realistic S-shaped passage was constructed along with three other rectangular passages at aspect ratios, 17.33, 8.81, 3.93, and 2.02. This study aims to determine if rectangular duct correlations are valid for the realistic S-shaped model. Specifically, flow in low Reynolds number ranges of less than 3000 are of interest. With the effect or rotation and aspect ratio being of primary concern in the study, an experimental rig was constructed to measure the heat transfer and pressure loss in these models. The experiments were conducted with both clockwise and counterclockwise rotation to account for the passage on the pressure side and suction side of the passage. The centerline Nusselt number distribution measured to check if the flow was fully developed. The effect of rotation caused swirling, increasing the entrance length in the duct and also enhanced heat transfer. The rotation also enhanced the heat transfer in the fully developed region. The fully developed experimental data for the simplified rectangular ducts showed good correlation with that of literature. However, the realistic S-shaped duct showed lower heat transfer values than the simplified rectangular ducts. Still, the effect of rotation is seen enhancing the rotation inf the realistic S-shaped duct. Additionally, the friction factor which was measured using the cross-sectional average static pressure showed similar results for the realistic S-shaped duct and the simplified rectangular duct. The passage between turbine disc bore and shaft is modeled as an annular duct with inner surface rotation. Flow in the turbulent region is studied and the test sections are made to have short length to hydraulic dimeter ratios. Along the centerline, the onset of Taylor vortices can be seen enhancing the Nusselt number in regions where the flow should be fully developed. This effect can also be seen enhancing the heat transfer in the fully developed region. The presence of Taylor vortices also adds resistance increasing the pressure loss across the duct. / Master of Science / Industrial gas turbines are designed to have an optimum overall pressure ratio for target temperatures rise. The demand for higher efficiency and power continues to push the operating pressure and temperature. Air systems is the flow network to provide necessary cooling to keep the machinery at a safe operating temperature. In this study, two passages of the air system in the turbine are of interest. The passage between turbine blade root and disc, and the passage between the turbine disc and shaft. The effect of rotation on the flow through the two passages are of primary interest with focus on heat transfer and pressure loss characteristics. This experimental study presents unique results as a realistic model of the passage which resembles an S-shape was constructed and tested. The passage in between the turbine disc and shaft forms a rotating annular passage. There is limited data available representing the realistic geometrical shape of the annular passage under rotation. Therefore, the present study aims to present data for more realistic geometry and operating conditions. In addition, simplified rectangular ducts and annular ducts are also tested for comparison purpose. The results of the study showed that the rotation does provide a significant increase in heat transfer and pressure loss in experiment modeling the passage between the turbine blade root and disc. Comparing the realistic S-shape passage and the rectangular passage with similar aspect ratio, the realistic S-shape passage showed less heat transfer and less sensitivity to the effect of rotation. The pressure loss characteristics on the other hand proved to be very similar. For the experiments modeling the passage between turbine disc and shaft, the effect of rotation once again showed to increase the heat transfer and pressure loss. The effect is more prominent when there is less axial flow.

Steam turbines are widely used in various industrial applications, primarily for power extraction. However, deviation for operating design conditions is a frequent occurrence for such machines, and therefore, understanding their performance at off design conditions is critical to ensure that the needs of the power demanding systems are met as well as ensuring safe operation of the steam turbines. In this thesis, the aerodynamic performance of three different turbine airfoil sections ( baseline, mid radius and tip profile) as a function of angle of incidence and exit Mach numbers, is numerically computed at 0.3 axial chords downstream of the trailing edge. It was found that the average loss coefficient was low, owing to the fact that the flow over the airfoils was well behaved. The loss coefficient also showed a slight decrease with exit Mach number for all three profiles. The mid radius and tip profiles showed near identical performance due to similarity in their geometries. It was also found out that the baseline profile showed a trend of substantial increase in losses at positive incidences, due to the development of an adverse pressure zone on the blade suction side surface. The mid radius profile showed high insensitivity to angle of incidence as well as low exit flow angle deviation in comparison to the baseline blade. / Master of Science

Pumping is the most efficient transportation and placing method for concrete. Despite the immense progress in the field of concrete technology in the last years, so far there are still neither official regulations nor verified theoretical foundations to be used for the assessment and accurate prediction pumping behaviour of ordinary and high performance concretes. This thesis aims at purposefully investigating pumping of modern concretes and bridging the existing knowledge gap. The main achievement of the present research is the development and verification of a sitecompliant and scientifically based methodology for characterisation and prediction of fresh concrete pumping behaviour. The research focus is set on the importance of the forming lubricating layer (LL) during pumping. Within an extended experimental program, the properties of the LL are captured and quantified. They determine the reduction of friction at the pipe wallconcrete interface and thereby govern the concrete flow. It is proven that the composition and the rheological properties of the forming LL exert an enormous impact on pumping since most of the induced shear stress by pumping pressure is concentrated in this layer. In a further step, the flow pattern of concrete is analytically and numerically determined. The concrete exhibits various principal flow types which are already defined at low flow rates: plug flow in case of strainhardening cementbased composite (SHCC), partial concrete bulk shear in ordinary concretes and pronounced bulk shear for selfcompacting concrete (SCC). The results from the fullscale pumping campaign are confronted with the existing pressure performance nomogram on the determination of pumping parameters. The nomogram’s prediction capacity is extended and verified for highly flowable concretes by replacing the slump and flow table results with the viscosity parameter of the LL. Furthermore, the challenges during pumping of concrete, inter alia, priming of the pipeline, blockage formation and final cleaning, are exemplified, and recommendations for the practitioners are provided. Finally, the transfer of the developed scientifically based and ready to use methodology on site is strongly advocated as a part of the future in situ rheology monitoring concept towards envisaged full automation of concrete production and casting processes.:ZUSAMMENFASSUNG V ABSTRACT VII VORWORT DES HERAUSGEBERS IX DANKSAGUNG XI SYMBOLS XVII INTRODUCTION 1 1.1 FLASHLIGHTS ON HISTORY 1 1.2 MOTIVATION 1 1.3 RESEARCH FIELD 3 1.4 RESEARCH CONCEPT 6 1.5 ECONOMIC RELEVANCE 8 1.6 STRUCTURE AND BOUNDARIES OF THE THESIS 10 STATE OF THE ART 13 2.1 GENERAL 13 2.2 CONCRETE FLOW IN PIPELINE 13 2.3 INFLUENCE OF CONCRETE RHEOLOGY ON PUMPING BEHAVIOUR 16 2.3.1 CEMENT HYDRATION 16 2.3.2 MIXTURE COMPOSITION 17 2.3.2.1 WATER-TO-BINDER RATIO AND PASTE VOLUME 18 2.3.2.2 AGGREGATES 20 2.3.2.3 ADMIXTURES AS PUMPING AIDS 22 2.3.3 HYDRODYNAMIC INTERACTIONS 25 2.3.4 SHEAR HISTORY 27 2.3.5 TEMPERATURE 28 2.4 FORMATION OF LUBRICATING LAYER 30 2.4.1 FLOW-INDUCED PARTICLE MIGRATION 30 2.4.2 PROPERTIES 31 2.4.3 EXPERIMENTAL CHARACTERISATION 32 2.5 BOUNDARY CONDITIONS 32 2.6 PUMPING EQUIPMENT 34 2.7 PRIMING 35 3 APPLIED METHODS 37 3.1 GENERAL 37 3.2 RHEOMETRY 37 3.3 DIRECT DETERMINATION OF PUMPING PRESSURE 40 3.4 SAMPLING AND PRODUCTION OF LUBRICATING MATERIAL 42 3.5 MEASUREMENT OF FILTRATE AMOUNT 45 3.6 ANALYTICAL DETERMINATION OF LUBRICATING LAYER THICKNESS 47 3.7 SMALL-SCALE PUMPING 49 3.8 FULL-SCALE PUMPING 50 3.9 NUMERICAL METHOD 56 3.9.1 MATERIAL MODEL 56 3.9.2 NUMERICAL IMPLEMENTATION 58 4 CHARACTERISATION OF CONCRETE PUMPABILITY 63 4.1 GENERAL 63 4.2 MIXTURE DESIGN PARAMETERS 63 4.3 COMPARISON BETWEEN REFERENCE AND DESIGN MORTARS 65 4.4 RESULTS AND DISCUSSION 65 4.4.1 RHEOLOGICAL BEHAVIOUR OF CONCRETES AND DESIGN MORTARS 65 4.4.2 INFLUENCE OF WALL ROUGHNESS ON RHEOLOGICAL PARAMETERS 67 4.4.3 PREDICTION OF PUMPING PRESSURE 72 4.5 SUMMARY 74 5 LUBRICATING LAYER THICKNESS AND CONCRETE FLOW 75 5.1 GENERAL 75 5.2 MIXTURE DESIGN PARAMETERS 75 5.3 RESULTS AND DISCUSSION 76 5.3.1 CONCRETE FLOW TYPE 76 5.3.2 PREDICTION AND VERIFICATION OF PUMPING PRESSURE 77 5.3.3 QUANTIFICATION OF LUBRICATING LAYER THICKNESS 79 5.4 SUMMARY 82 6 FULL-SCALE PUMPING EXPERIMENTS 83 6.1 GENERAL 83 6.2 MIXTURES AND DESIGN PARAMETERS 83 6.3 RESULTS AND DISCUSSION 85 6.3.1 PRESSURE LOSS AND PRESSURE-FLOW RATE CURVES 85 6.3.2 NUMERICAL SIMULATION RESULTS 86 6.3.3 PRESSURE PREDICTION USING MODIFIED NOMOGRAM 88 6.3.4 COMPARISON BETWEEN PREDICTED AND ACTUAL PRESSURE-FLOW RATE CURVES 90 6.4 SUMMARY 92 7 EFFECT OF PUMPING ON FRESH PROPERTIES OF CONCRETE AND FILTRATE FORMATION 95 7.1 GENERAL 95 7.2 MIXTURES DESIGN PARAMETERS 95 7.3 INFLUENCE OF PUMPING ON PROPERTIES OF FRESH CONCRETE 97 7.4 INFLUENCE OF CONCRETE PROPERTIES ON KINETICS OF FILTRATE FORMATION 98 7.5 IMPACT OF FILTRATE AMOUNT ON PUMPABILITY 101 7.6 SUMMARY 104 8 CHALLENGES RELATED TO PUMPING OF CONCRETE 105 8.1 GENERAL 105 8.2 PRIMING GROUT 105 8.3 PIPELINE GEOMETRY 108 8.4 BLOCKAGES 113 8.5 FILLING DEGREE OF PUMP PISTONS 116 8.6 TEMPERATURE CONTROL 117 8.7 VERTICAL PUMPING 118 8.8 CLEANING THE PIPELINE 119 8.9 SUMMARY 120 9 FINAL CONCLUSIONS AND OUTLOOK 121 9.1 GENERAL 121 9.2 CONCRETE FLOW TYPE 121 9.3 LUBRICATING LAYER PROPERTIES 121 9.4 RHEOLOGICAL DEVICES 122 9.5 FILTRATE FORMATION 122 9.6 NUMERICAL SIMULATIONS 122 9.7 MODIFIED NOMOGRAM 123 9.8 RELEVANCE OF PUMPING EXPERIMENTS 123 9.9 INFLUENCE OF PUMPING ON FRESH CONCRETE PROPERTIES 124 9.10 GENERATED DATABASE 124 9.11 IMPROVING NUMERICAL MODEL 124 9.12 TODAY AND TOMORROW 124 BIBLIOGRAPHY 127 APPENDIX A 135 A.1 MATERIALS DESCRIPTION, CHAPTERS 4 AND 5 135 A.2 MATERIALS DESCRIPTION, CHAPTERS 6, 7 AND 8 136 APPENDIX B 137 APPENDIX C 141 LIST OF SELECTED PUBLICATIONS 143 JOURNALS 143 CONFERENCE PAPERS 143 CURRICULUM VITAE 145 / Das Pumpen stellt die effektivste Methode für das Fördern und Einbringen von Frischbeton auf der Baustelle dar. Trotz der in den letzten Jahren erreichten deutlichen Fortschritte auf betontechnologischem Gebiet existieren für die Beurteilung der Pumpbarkeit von Beton bisher weder offiziell gültige Vorschriften noch abgesicherte theoretische Grundlagen, die eine zielsichere Vorhersage des Pumpverhaltens von Normal- als auch Hochleistungsbetonen ermöglichen. Die vorliegende Arbeit schließt entsprechende Wissenslücken und befasst sich gezielt mit dem Pumpen moderner Betone. Grundlegenden Erkenntnisgewinn stellt die Entwicklung einer wissenschaftlich fundierten, baustellengerechten Prüfmethodik zur Charakterisierung und Vorhersage des Pumpverhaltens von Frischbeton dar. Der Untersuchungsfokus richtet sich auf die Wirkung der sich beim Pumpvorgang ausbildenden Gleitschicht. Ein umfangreiches Untersuchungsprogramm gestattet die Erfassung und Quantifizierung der Eigenschaften dieser Schicht. Sie bestimmen infolge deutlicher Reduzierung der Reibung an der Grenzfläche zwischen Rohrwandung und Beton die Betonströmung entscheidend. Bewiesen wird, dass Betonzusammensetzung und rheologische Eigenschaften der Gleitschicht maßgebende Auswirkungen auf den Pumpvorgang haben, da sich die pumpdruckinduzierte Scherspannung in dieser Schicht konzentriert. Weiterhin erfolgt sowohl eine analytische als auch numerische Charakterisierung der Betonströmung im Rohr. Nachgewiesen wird, dass sich beim Pumpvorgang betonspezifisch unterschiedliche Strömungsarten einstellen, die bereits bei niedrigen Durchflussmengen definiert sind: Pfropfenströmung in hochduktilen Betonen, partielle Scherung des Kernbetons in Normalbetonen und signifikante Scherung in selbstverdichtenden Betonen. Aus großtechnisch durchgeführten Pumpversuchen gewonnene Ergebnisse werden dem derzeit vorhandenen, verbesserungsbedürftigen Betondruck-Leistungs-Nomogramm zur Einstellung von Parametern an der Betonpumpe gegenübergestellt. Die Vorhersagekapazität des Nomogramms kann durch den Ersatz der Ausbreit- bzw. Setzfließmaßangaben mit Viskositätsangaben der Gleitschicht erweitert und verifiziert werden. Des Weiteren werden baustellenbezogene Herausforderungen im Gesamtprozess des Betonpumpvorgangs, u. a. Vorbereitung der Rohrleitung vor dem Pumpen, Auftreten von Stopfern und Endreinigung exemplarisch dargestellt sowie Empfehlungen für die Praktiker erarbeitet. Schließlich wird der Transfer der in dieser Arbeit entwickelten wissenschaftlich basierten und anwendungsbereiten Methodik als Teil des zukünftigen Konzeptes für die in-situ Rheologie-Überwachung hinsichtlich einer angestrebten vollständigen Automatisierung von Fertigungs- und Einbringprozessen von Beton mit Nachdruck empfohlen.:ZUSAMMENFASSUNG V ABSTRACT VII VORWORT DES HERAUSGEBERS IX DANKSAGUNG XI SYMBOLS XVII INTRODUCTION 1 1.1 FLASHLIGHTS ON HISTORY 1 1.2 MOTIVATION 1 1.3 RESEARCH FIELD 3 1.4 RESEARCH CONCEPT 6 1.5 ECONOMIC RELEVANCE 8 1.6 STRUCTURE AND BOUNDARIES OF THE THESIS 10 STATE OF THE ART 13 2.1 GENERAL 13 2.2 CONCRETE FLOW IN PIPELINE 13 2.3 INFLUENCE OF CONCRETE RHEOLOGY ON PUMPING BEHAVIOUR 16 2.3.1 CEMENT HYDRATION 16 2.3.2 MIXTURE COMPOSITION 17 2.3.2.1 WATER-TO-BINDER RATIO AND PASTE VOLUME 18 2.3.2.2 AGGREGATES 20 2.3.2.3 ADMIXTURES AS PUMPING AIDS 22 2.3.3 HYDRODYNAMIC INTERACTIONS 25 2.3.4 SHEAR HISTORY 27 2.3.5 TEMPERATURE 28 2.4 FORMATION OF LUBRICATING LAYER 30 2.4.1 FLOW-INDUCED PARTICLE MIGRATION 30 2.4.2 PROPERTIES 31 2.4.3 EXPERIMENTAL CHARACTERISATION 32 2.5 BOUNDARY CONDITIONS 32 2.6 PUMPING EQUIPMENT 34 2.7 PRIMING 35 3 APPLIED METHODS 37 3.1 GENERAL 37 3.2 RHEOMETRY 37 3.3 DIRECT DETERMINATION OF PUMPING PRESSURE 40 3.4 SAMPLING AND PRODUCTION OF LUBRICATING MATERIAL 42 3.5 MEASUREMENT OF FILTRATE AMOUNT 45 3.6 ANALYTICAL DETERMINATION OF LUBRICATING LAYER THICKNESS 47 3.7 SMALL-SCALE PUMPING 49 3.8 FULL-SCALE PUMPING 50 3.9 NUMERICAL METHOD 56 3.9.1 MATERIAL MODEL 56 3.9.2 NUMERICAL IMPLEMENTATION 58 4 CHARACTERISATION OF CONCRETE PUMPABILITY 63 4.1 GENERAL 63 4.2 MIXTURE DESIGN PARAMETERS 63 4.3 COMPARISON BETWEEN REFERENCE AND DESIGN MORTARS 65 4.4 RESULTS AND DISCUSSION 65 4.4.1 RHEOLOGICAL BEHAVIOUR OF CONCRETES AND DESIGN MORTARS 65 4.4.2 INFLUENCE OF WALL ROUGHNESS ON RHEOLOGICAL PARAMETERS 67 4.4.3 PREDICTION OF PUMPING PRESSURE 72 4.5 SUMMARY 74 5 LUBRICATING LAYER THICKNESS AND CONCRETE FLOW 75 5.1 GENERAL 75 5.2 MIXTURE DESIGN PARAMETERS 75 5.3 RESULTS AND DISCUSSION 76 5.3.1 CONCRETE FLOW TYPE 76 5.3.2 PREDICTION AND VERIFICATION OF PUMPING PRESSURE 77 5.3.3 QUANTIFICATION OF LUBRICATING LAYER THICKNESS 79 5.4 SUMMARY 82 6 FULL-SCALE PUMPING EXPERIMENTS 83 6.1 GENERAL 83 6.2 MIXTURES AND DESIGN PARAMETERS 83 6.3 RESULTS AND DISCUSSION 85 6.3.1 PRESSURE LOSS AND PRESSURE-FLOW RATE CURVES 85 6.3.2 NUMERICAL SIMULATION RESULTS 86 6.3.3 PRESSURE PREDICTION USING MODIFIED NOMOGRAM 88 6.3.4 COMPARISON BETWEEN PREDICTED AND ACTUAL PRESSURE-FLOW RATE CURVES 90 6.4 SUMMARY 92 7 EFFECT OF PUMPING ON FRESH PROPERTIES OF CONCRETE AND FILTRATE FORMATION 95 7.1 GENERAL 95 7.2 MIXTURES DESIGN PARAMETERS 95 7.3 INFLUENCE OF PUMPING ON PROPERTIES OF FRESH CONCRETE 97 7.4 INFLUENCE OF CONCRETE PROPERTIES ON KINETICS OF FILTRATE FORMATION 98 7.5 IMPACT OF FILTRATE AMOUNT ON PUMPABILITY 101 7.6 SUMMARY 104 8 CHALLENGES RELATED TO PUMPING OF CONCRETE 105 8.1 GENERAL 105 8.2 PRIMING GROUT 105 8.3 PIPELINE GEOMETRY 108 8.4 BLOCKAGES 113 8.5 FILLING DEGREE OF PUMP PISTONS 116 8.6 TEMPERATURE CONTROL 117 8.7 VERTICAL PUMPING 118 8.8 CLEANING THE PIPELINE 119 8.9 SUMMARY 120 9 FINAL CONCLUSIONS AND OUTLOOK 121 9.1 GENERAL 121 9.2 CONCRETE FLOW TYPE 121 9.3 LUBRICATING LAYER PROPERTIES 121 9.4 RHEOLOGICAL DEVICES 122 9.5 FILTRATE FORMATION 122 9.6 NUMERICAL SIMULATIONS 122 9.7 MODIFIED NOMOGRAM 123 9.8 RELEVANCE OF PUMPING EXPERIMENTS 123 9.9 INFLUENCE OF PUMPING ON FRESH CONCRETE PROPERTIES 124 9.10 GENERATED DATABASE 124 9.11 IMPROVING NUMERICAL MODEL 124 9.12 TODAY AND TOMORROW 124 BIBLIOGRAPHY 127 APPENDIX A 135 A.1 MATERIALS DESCRIPTION, CHAPTERS 4 AND 5 135 A.2 MATERIALS DESCRIPTION, CHAPTERS 6, 7 AND 8 136 APPENDIX B 137 APPENDIX C 141 LIST OF SELECTED PUBLICATIONS 143 JOURNALS 143 CONFERENCE PAPERS 143 CURRICULUM VITAE 145

Thesis (MScEng)--Stellenbosch University, 2012. / ENGLISH ABSTRACT: The optimal design of a heat exchanger for a specified heat transfer, pressure drop and set of ambient conditions entails minimising space, weight, material usage and overall cost. However, the variables which influence the performance as well as the overall cost of a heat exchanger are not related in a simple way and it is not obvious which variables play the most important roles (Perry & Green, 1997:11-44). Air cooled heat exchangers (ACHEs) are normally designed in three stages, by different experts in the field, and with the aid of specially designed software. This project combines these thermal, mechanical and cost estimation processes into a MS Excel model which makes it easier to see the influence that design parameters have on the overall cost of the heat exchanger. A thermal model was created to design an API 661 (2006) ACHE. The results from this model compared well with those of HTRI Xchanger Suite 6.0 software, with HTRI being more conservative in its design mode. A mechanical design model was then developed, which uses as inputs the outputs of the thermal design. The output from this mechanical design model is the minimum material thicknesses based on the stress criteria of Appendix 13 of ASME VIII div 1 (2007) Boiler and Pressure Vessel Code. An experiment on a finned tube bundle was performed in a wind tunnel facility to determine performance characteristics and compare these to existing correlations in literature. The results showed that both the heat transfer coefficient (h) and loss coefficient (Eu) correlations proposed by Ganguli et al. (1985) closely predict the measured data, and were consequently used in the thermal design model. During this experiment it was also shown that the tube bundle reached 8 % - 9 % of its allowable internal fouling factor, due to rust build up inside the tubes, and in a testing period of only nine days. The thermal and mechanical models were then combined with a cost estimation process to perform both a thermal and mechanical parametric study. The thermal study showed that to obtain an optimal solution, the design must attempt to maximise the length, increase the width rather than the number of bays, make use of two bundles per bay with fewer but larger fans and employ a large number of tube rows with the least number of tube passes. These guidelines were used to create an initial design; Excel Solver was then applied to locate the optimum combination of bundle length and width that result in the minimum heat exchanger cost. Two mechanical considerations were investigated, both requiring additional welding and thus increased welding cost. Firstly the use of stay plates result in reduced required plate thicknesses according to the stress criteria since it provides additional stiffness in the header box design. Secondly the use of more (but smaller) nozzles as opposed to less (but larger) nozzles was also considered. The mechanical parametric study showed no specific trends, but both considerations should still be checked as it can be cost beneficial in a specific design. / AFRIKAANSE OPSOMMING: Optimale ontwerp van ’n warmteoordraer vir ’n gespesifiseerde warmteoordrag, drukval en stel van omgewingstoestande behels die minimalisering van ruimte, gewig, materiaalverbruik en algehele koste. Die veranderlikes wat egter die werkverrigting, sowel as die algehele koste, van ’n warmteoordraer beïnvloed, hou nie in ’n eenvoudige sin met mekaar verband nie, en dit is nie vanselfsprekend watter veranderlikes die belangrikste rolle speel nie (Perry & Green, 1997:11-44). Lugverkoelde warmteoordraers (air-cooled heat exchangers of ACHEs) word normaalweg in drie fases ontwerp deur verskillende kundiges in die veld en met behulp van spesiaal ontwerpte programmatuur. Hierdie studie kombineer dié termiese, meganiese en kosteberamingsprosesse in ’n MS Excel-model, wat dit makliker maak om van te stel wat die invloed wat ontwerpparameters op die algehele koste van die hitteruiler is. ’n Termiese model is geskep om ’n “API 661 (2006) ACHE” te ontwerp. Die resultate van hierdie model het goed vergelyk met dié van die HTRI Xchanger Suite 6.0-program, met HTRI meer konserwatiew in die ontwerp af. Na die termiese model geskep is, is ’n meganieseontwerp-model ontwikkel, wat as insette die uitsette van die termiese ontwerp gebruik het. Die uitset van hierdie meganieseontwerp-model is die minimum materiaaldikte gebaseer op die spanningskriteria van Bylae 13 van “ASME VIII div 1 (2007) Boiler and Pressure Vessel Code.” Daar is ’n eksperiment op ’n vinbuisbundel in ’n windtonnelfasiliteit uitgevoer om werkverrigtingskarakteristieke te bepaal en dit met bestaande korrelasies in die literatuur te vergelyk. Die resultate het getoon dat sowel die warmteoordragskoëffisiënt (h) en die verlieskoeffisient (Eu) korrelasies, voorgestel deur Ganguli et al. (1985), die data wat gemeet is akkuraat voorspel, en gevolglik is die korrelasies in die termieseontwerp-model gebruik. Gedurende die eksperiment is ook getoon dat die buisbundel 8 % - 9 % van sy toelaatbare interne-aanpakkingfaktor bereik het vanweë roesopbou binne-in die buise, en dit in ’n toetsingtydperk van slegs nege dae. Die termiese en meganiese modelle was toe gekombineer met ’n kosteberamingsproses om ’n termiese sowel as ’n meganiese parametriese studie uit te voer. Die termiese studie het getoon dat, om ’n optimale oplossing te verkry, die ontwerp moet poog om die lengte te maksimeer; die wydte eerder as die aantal strate (bays) te vermeerder; van twee bundels per straat gebruik te maak met minder, maar groter waaiers; en ’n groot aantal buisrye met die kleinste hoeveelheid buisdeurvloeiweë in te span. Hierdie riglyne is gebruik in ’n aanvanklike ontwerp, waarna die Excel Solver gebruik is om die optimale kombinasie van bundellengte en –wydte vas te stel met die oog op die laagste moontlike warmteoordraerkoste. Twee meganiese oorwegings is ondersoek wat albei addisionele sweiswerk sou vereis en dus tot verhoogde sweiskoste sou lei. Eerstens lei die gebruik van ankerplate (stay plates) tot ’n vermindering in die vereiste plaatdiktes volgens die spanningskriteria, aangesien dit addisionele stewigheid in die spruitstukhouerontwerp bied. Tweedens is die gebruik van meer (maar kleiner) spuitstukke teenoor minder (maar groter) spuitstukke ook oorweeg. Die meganiese parametriese studie het geen spesifieke voorkeurneigings getoon nie, maar altwee oorgewings moet nog getoets word want dit kan koste voordelig word in 'n spesifieke ontwerp.

For decades, duplex filters have been put to use virtually unmodified. Technologies, handling and use of materials show enormous potential for improvement. Filter element emoval/replacement is performed according to a complex process sequence. With the newly developed Duplex Filter, the market demands concerning simple filter element removal/replacement, as well as weight and pressure loss reduction are fully met.

Modern construction practices require proper knowledge to predict concrete pumping pressure, especially in high-volume and high-rise applications. Despite the progress made over the last decades, the spread of concrete pumping to high-rise construction has been hampered by the lack of standardized operating procedures and performance criteria. By and large, the guidelines available today focus predominantly on pumping Conventional Vibrated Concrete (CVC), while ambiguity still surrounds pumping Self-Consolidating Concrete (SCC) and other types of Highly-Workable Concrete (HWC). This PhD dissertation focuses on the fundamental principles relevant to the flow of high-strength SCC in pumping pipes, and it aims to develop methods to predict and reduce the required pumping pressure. The flow pattern of SCC in pipes is analytically investigated, providing a numerical approach to predict the pumping pressure based on the properties of both concrete and the lubrication layer, the pipe diameter, and the flow rate. The analytical results are further validated through full-scale pumping tests executed at the laboratory of the Université de Sherbrooke. Through this phase 26 optimal concrete mixtures were pumped in a 30-m pumping circuit to investigate the interactions between the concrete properties and pressure loss. The same tests are also employed to empirically correlate pressure loss with rheological and tribological properties of concrete at different flow rates. The resulting correlations furnish instrumental models capable of computing pressure loss for a wide range of concrete properties. In another application, the experimental results are analyzed to identify the influence of pumping on concrete properties with time. Full-scale pumping results are statistically analyzed in order to establish a quantitative description of the most influential parameters governing the concrete flow in pipes. As a result, concrete pipe flow is statically modeled, allowing the computation of pressure loss at different flow rates based on the the rheological and tribological properties of the concrete and the pipe diameter. Another statistical model is derived to calculate the pressure loss as a function of the V-funnel flow time, granting the advantage of predicting the pressure loss on job sites without the need for complex rheological and tribological measurements. In light of the research findings of the previous phases, a new simple test method called the pipe flow test (PFT) is developed in the context of this research, specifically for predicting pipe flow pressure loss. With preceding research phases as insights, the final stage of this project is directed toward mix design optimization faced with the challenge of reducing the pumping pressure and meeting the strength requirements of high-strength SCC. Ultimately, the research findings emanating from this investigation provide practical guidelines and conclusive models to predict and reduce pumping pressure for a wide scope of concrete mixtures and pipe diameters.

[pt] O presente trabalho analisa a transferência de calor e a perda de carga em escoamento turbulento através das regiões anulares lisas e aletadas. Os coeficientes de transferência de calor foram obtidos experimentalmente, utilizando-se a teoria de trocadores de calor. Também foram determinados os coeficientes de perda de carga associados a cada uma das geometrias analisadas. Os experimentos foram realizados em um trocador de calor bi-tubular concêntrico. Água (fluído quente) escoava através do tubo interno, enquanto ar (fluido frio) fluía através da região anular. Medindo-se as vazões e temperaturas na entrada e saída da seção de teste do trocador de calor, obtém-se a efetividade da mesma e, consequentemente, o coeficiente global de transferência de calor (médio). As condições de contorno adotadas foram de temperatura uniforme na superfície externa do tubo interno e de isolamento térmico na superfície externa do tubo interno e de isolamento térmico na superfície externa da região anular. Com o objetivo de obter-se condições de escoamento completamente desenvolvido, o trocador de calor possui um comprimento, a montante da seção de testes, de aproximadamente trinta diâmetros hidráulicos. Os coeficientes de transferência de calor e de perda de carga são apresentados de forma adimensional, como função do número de Reynolds do escoamento, os resultados obtidos para as regiões anulares lisas e aletadas são comparados entre si. O propósito de tal comparação foi o de estudar a influencia das aletas na perda de carga e na taxa de transferência de calor. No caso das regiões aletadas, verifica-se que a eficiência das aletas influencia a transferência de calor. Deste modo, realizou-se uma análise bi-dimensional de transferência de calor nas aletas para obter-se a eficiência das mesmas e, consequentemente, a eficiência das regiões aletadas. Também é mostrado que o desempenho térmico da região depende principalmente do número de Nusselt e da eficiência da mesma. Tais parâmetros são apresentados, em última análise, como funções do número de Reynolds e da geometria do problema. / [en] The present work is concerned with the turbulent heat transfer and pressure drop in smooth and finned annular ducts. Average heat transfer coeeficients have been obtained by means of the heat exchanger theory. In addition, friction factors have also been determined. The experiments were performed by utiling four double-pipe heat exchangers. The average heat transfer coefficients, for air flowing in the annular section, were fertmined by measuring the overall heat transfer coefficients of the heat exchangers. In order to aatain fully developed conditions, the heat exchangers had a starting length of 30 hydrualic diameters. The thermal boundary conditions consisted of uniform temperature on the inner surface, the outer surface being insulate. The heat transfer coefficients and friction factors are presented in dimensinless forms, as functions of the Reynolds number of the fow. The results for smooth and finned annular ducts were compared. The purpose of such comparison was to study the influence of the fins on the pressure drop and heat transfer rate. In the case of the finned annular ducts, it is shown that fin efficiency has some influence on the heat transfer rates. Then a two-dimensional heat transfer analysis was performed in order to obtain the fin efficiency and the annular region efficiency. It is also shown that the overall thermal performance of finned surfaces depends mainly of the Nusselt number and on the region efficiency. These parameters are presented as functiond of the Reynolds number of the flow and the geometry of the problem.