Global ETD Search

1	Effect Of Hydraulic Parameters On The Formation Of Vortices At Intake Structures Baykara, Ali 01 January 2013 (has links) (PDF) The aim of this experimental study was to investigate the hydraulic conditions at which air-entraining vortices would form in front of horizontal intakes and to determine the ways of eliminating the formation of these vortices by testing anti-vortex devices. For these reasons, a series of experiments were conducted in an experimental setup composed of a reservoir having the dimensions of 3.10 m x 3.10 m x 2.20 m and a pump connected to the intake pipe. Within the reservoir, between the concrete side walls adjustable plexiglass side walls were placed to provide the desired wall clearance for the intake pipes. Six pipes of different diameters / 5 cm, 10 cm, 14.4 cm, 19.4 cm, 25 cm and 30 cm were horizontally mounted on the front side of the reservoir one by one, and for each case, a wide range of discharges was provided from the reservoir by the pump. Under symmetrical approach flow conditions and zero bottom wall clearance, the experiments were repeated for each intake pipe and the &ldquo / critical submergence depths&rdquo / for the tested discharges were determined. At some of the discharges, the effect of horizontal plates located on the top of the pipe entrance as anti-vortex devices on the elimination of the vortices was investigated. The measured critical submergence depths were related in dimensionless form to the relevant dimensionless parameters and empirical equations were derived. These equations were compared with similar ones available in the literature and it was shown that the agreement between them was quite good. TC Hydraulic Engineering 1-978
2	Computational Modelling Of Free Surface Flow In Intake Structures Using Flow 3d Software Aybar, Akin 01 June 2012 (has links) (PDF) Intakes are inlet structures where fluid is accelerated to a certain flow velocity to provide required amount of water into a hydraulic system. Intake size and geometry affects the formation of flow patterns, which can be influential for hydraulic performance of the whole system. An experimental study is conducted by measuring velocity field in the hydraulic model of the head pond of a hydropower plant to investigate vortex formation. Vortex strength based on potential flow theory is calculated from the measured velocity field. It was shown that vortex strength increases with the submergence Froude number. The free surface flow in the head pond is simulated using Flow-3D software. Vortex strength calculations are repeated using the computational velocity distributions and compared to experimentally obtained values. Similar computations were carried on with some idealized pond geometries such as rectangular and circular. TC Hydraulic Engineering 1-978
3	Flow Control Over a Circular Arc Airfoil by Periodic Blowing Rullan, Jose M. 04 November 2004 (has links) The flow over sharp-edged wings is almost always separated. The control of separated flows is possible and benefits can be achieved but only in a time average sense. A new design of an actuator was designed and tested which can achieve a wide range velocity of without frequency dependence, is free of oscillating components as well as free of secondary frequencies and therefore can be scaled up easily, unlike a traditional synthetic jet. The actuator can achieve a considerable amount of jet vectoring, thus aligning the disturbance with the leading edge shear layer. Results indicate that unsteady mini-jet actuation is an effective actuation device capable of increasing the lift in the stall region of the airfoil. Moreover, pressure measurements showed that two parameters could be altered to maximize the lift. The momentum coefficient needed a minimum value to exert influence and the actuating frequency need not be at exact the natural shedding frequency to improve the lift and can be operated at harmonics of the natural shedding frequency and obtain improvements. / Master of Science vortex formation jet pulsation separated flow flow control Sharp edge airfoil
4	Experiments in Vortex Formation of Plunging & Flapping Flat Plates Stanley, Daniel C. January 2008 (has links) No description available. Fluid Dynamics vortex formation low Reynolds number fluid dynamics formation parameter formation time formation number
5	Confined Aerosol Jet in Fiber Classification and Dustiness Measurement Dubey, Prahit 08 September 2015 (has links) No description available. Mechanics Dustiness Measurement Dustiness Tester Baron Fiber Classifier Vortex Formation Confined Turbulent Jet Impingement Turbulent Mixing
6	Time-Resolved Analysis of Circulation Control over Supercritical Airfoil using Digital Particle Image Velocimetry (DPIV) Hussain, Mian M. 07 January 2005 (has links) Active pneumatic flow control methods as applied to aerospace applications have shown noteworthy improvements in lift compared to traditional means. The General Aviation Circulation Control (GACC) concept currently under investigation at NASA's Langley Research Center (LaRC) is an attempt at addressing some of the fundamental obstacles related to the successful development and implementation of such techniques. The primary focus of research in the field of high lift pneumatic devices is to investigate ways of obtaining significant improvements in the lift coefficient without resorting to moving surfaces. Though it has been demonstrated that the lift coefficient can be amplified in a variety of ways, the chosen method for the current work is via enhanced circulation stemming from a trailing edge Coanda jet. A secondary objective is to reduce the amount energy expenditure used in these pneumatic techniques by implementing time-variant flow. This paper describes experimental observations of the flow behavior at the trailing edge of a modified water tunnel based supercritical airfoil model that exploits both steady and pulsed Coanda driven circulation control. A total of 10 sets of data, excluding a baseline case of no Coanda jet, were sampled with five cases each for steady and pulsed flow, the latter at a reduced frequency, f+, of 1. Two cases of equal momentum coefficient but with varying forced frequencies were isolated for further study in an attempt to accurately compare the resultant flow dynamics of each method. All measurements were taken at a zero-lift angle of attack by means of a non-invasive time accurate flow visualization technique (DPIV). Vorticity behavior was investigated using Tecplot® and a MATLAB® program was developed to quantify the Strouhal Number of time-averaged velocity fluctuations moving aft of the Coanda surface for each case. / Master of Science Vortex Formation Jet Pulsation Flow Visualization Flow Control Coanda Effect DPIV Circulation Control Wing (CCW)
7	Experimental Investigation of the Effects of a Passing Shock on Compressor Stator Flow Langford, Matthew David 07 May 2003 (has links) A stator cascade was developed to simulate the flow conditions within a close-stage-spacing transonic axial compressor. Experiments were conducted in a linear transonic blowdown cascade wind tunnel with an inlet Mach number of 0.65. The bow shock from the downstream rotor was simulated by a single moving normal shock generated with a shock tube. First, steady pressure data were gathered to ensure that the stator cascade operated properly without the presence of the shock. Next, the effects of the passing shock on the stator flow field were investigated using shadowgraph photography and Digital Particle Image Velocimetry (DPIV). Measurements were taken for three different shock strengths. In every case studied, a vortex formed near the stator trailing edge as the shock impacted the blade. The size of this vortex was shown to be directly related to the shock strength, and the vortex remained present in the trailing edge flow field throughout the cycle duration. Analysis of the DPIV data showed that the vortex acts as a flow blockage, with the extent of this blockage ranging from 2.9% of the passage for the weakest shock, to 14.3% of the passage for the strongest shock. The vortex was also shown to cause flow deviation up to 75° for the case with the strongest shock. Further analysis estimated that the total pressure losses due to shock-induced vorticity ranged from 46% to 113% of the steady wake losses. Finally, the total pressure loss purely due to the upstream-propagating normal shock was estimated to be roughly 0.22%. / Master of Science Particle Image Velocimetry Vortex Formation Unsteady Losses Rotor Bow Shock Compressor Cascade
8	Large Eddy Simulation of Impinging Jets Hällqvist, Thomas January 2006 (has links) This thesis deals with Large Eddy Simulation (LES) of impinging air jets. The impinging jet configuration features heated circular jets impinging onto a flat plate. The problem addressed here is of generic nature, with applications in many engineering devices, such as cooling of components in gas turbines, in cars and electronic devices. The flow is inherently unsteady and contains relatively slowly varying coherent structures. Therefore, LES is the method of choice when the Reynolds number is large enough to exclude Direct Numerical Simulations (DNS). The present LES model is a basic model without explicit Sub-Grid-Scale (SGS) modeling and without explicit filtering. Instead, the numerical scheme is used to account for the necessary amount of dissipation. By using the computational grid as a filter the cutoff wavenumber depends explicitly on the grid spacing. The underlying computational grid is staggered and constructed in a Cartesian coordinate system. Heat transfer is modeled by the transport equation for a passive scalar. This is possible due to the negligible influence of buoyancy which implies constant density throughout the flow field. The present method provides accurate results for simple geometries in an efficient manner. A great variety of inlet conditions have been considered in order to elucidate how the dynamics of the flow and heat transfer are affected. The considered studies include top-hat and mollified mean velocity profiles subjected to random and sinusoidal perturbations and top-hat profiles superimposed with solid body rotation. It has been found that the shape of the mean inlet velocity profile has a decisive influence on the development of the flow and scalar fields, whereas the characteristics of the imposed artificial disturbances (under consideration) have somewhat weaker effect. In order to obtain results unequivocally comparable to experimental data on turbulent impinging jets both space and time correlations of the inflow data must be considered, so also the spectral content. This is particularly important if the region of interest is close to the velocity inlet, i.e. for small nozzle-to-plate spacings. Within this work mainly small nozzle-toplate spacings are considered (within the range of 0.25 and 4 nozzle diameters), which emphasizes the importance of the inflow conditions. Thus, additional to the basic methods also turbulent inflow conditions, acquired from a precursor pipe simulation, have been examined. Both for swirling and non-swirling flows. This method emulates fully developed turbulent pipe flow conditions and is the best in the sense of being well defined, but it demands a great deal of computing power and is also rather inflexibility. In case of the basic randomly perturbed methods the top-hat approach has been found to produce results in closest agreement with those originating from turbulent inlet conditions. In the present simulations the growth of individual instability modes is clearly detected. The character of the instability is strongly influenced by the imposed boundary conditions. Due to the lack of correlation random superimposed fluctuations have only a weak influence on the developing flow field. The shape of the mean profile, on the other hand, influences both the growth rate and the frequency of the dominant modes. The top-hat profile yields a higher natural frequency than the mollified. Furthermore, for the top-hat profile coalescence of pairs of vortices takes place within the shear-layer of the axial jet, whereas for the mollified profile (for the considered degree of mollification) it takes place within the wall jet. This indicates that the transition process is delayed for smoother profiles. The amount of wall heat transfer is directly influenced by the character of the convective vortical structures. For the mollified cases wall heat transfer originates predominantly from the dynamics of discrete coherent structures. The influence from eddy structures is low and hence Reynolds analogy is applicable, at least in regions of attached flow. The top-hat and the turbulent inflow conditions yield a higher rate of incoherent small scale structures. This strongly affects the character of wall heat transfer. Also the applied level of swirl at the velocity inlet has significant influence on the rate of heat transfer. The turbulence level increases with swirl, which is positive for heat transfer, and so also the spreading of the jet. The latter effect has a negative influence on wall heat transfer, particularly in the center most regions. This however depends also on the details of the inflow data. / QC 20100831 Impinging jet large eddy simulation heat transfer vortex formation circular jet forcing inflow conditions implicit modeling. Fluid mechanics Strömningsmekanik
9	Investigation par Calcul numérique de la région en « S » des courbes caractéristiques d’une turbine-pompe réversible / CFD Investigation of the S-shape region of the characteristic curves of reversible pump-turbines Jacquet, Clément 21 June 2017 (has links) Les Stations de Transfert de l’Énergie par Pompage (STEP) munies de turbines-pompes réversibles de type Francis (TP) permettent de stocker et de restituer de grandes quantités d’énergie avec des rendements très élevés. Celles-ci apparaissent comme un moyen viable d’assurer la réactivité et la stabilité du réseau électrique vis-à-vis de l’augmentation croissante des sources d’énergie renouvelables intermittentes. Pour répondre aux nouveaux besoins en régulation du réseau électrique, la technologie actuelle des STEP doit être adaptée. Accroître la réactivité requiert d’optimiser les procédures de démarrage et d’arrêt des machines. Dans les quadrants turbine, turbine-frein et pompe inverse, les TP de haute chute ont des courbes caractéristiques présentant la forme d’un « S ». Cette forme particulière peut engendrer des coups de béliers lors des phases d’arrêts d’urgences, exposant les conduites à de sévères surpressions et dépressions. De plus, pour ces points de fonctionnement associés au « S » les écoulements sont fortement instationnaires et induisent des fluctuations de pression responsables de chargements dynamiques sur les parties mécaniques. Les objectifs de ce travail sont la modélisation et la compréhension des phénomènes hydrauliques complexes liés au « S ». Des simulations numériques instationnaires sont réalisées en utilisant le modèle de turbulence SAS-SST. Moins couteux que les modèles LES, ce modèle permet de résoudre d’une partie du spectre turbulent et ainsi de prendre en compte les principaux effets instationnaires. Trois configurations de turbine-pompe de même vitesse spécifique (nq=40) sont étudiées. Une seule (grande) ouverture de directrices est retenue pour chaque configuration. Les points de fonctionnement considérés couvrent une large gamme de conditions d’opération, allant du fonctionnement en régime continu (rendement élevé) jusqu’au débit nul, en passant par le point d’emballement. Les résultats des calculs sont comparés aux mesures expérimentales. La bonne corrélation entre valeurs numériques et expérimentales valide la pertinence du modèle numérique. Les analyses des performances de la machine et des fluctuations de pression permettent d’identifier les régions de l’écoulement associées aux principales instabilités. Enfin, les visualisations de l’écoulement couplées à une étude des mécanismes de dissipation de l’énergie mettent en évidence les principaux phénomènes à l’origine de la forme en « S » des courbes caractéristiques. / Pumped Storage Plants (PSP) using reversible Francis pump-turbines can store large amounts of energy with high efficiency. They therefore appear as a cost-effective tool to provide stability to the energy production network against the intermittency of renewable energy sources. Nevertheless, start-up and shutdown procedures still need to be improved to increase the reactivity of the PSP. Reversible high head pump-turbines have characteristic curves that exhibit an S-Shape in the turbine, turbine-brake and reverse pump quadrants. This S-Shape may be responsible for surge transient phenomena in the case of an emergency shutdown (for large guide vane opening). Moreover, for operating point in the S-Shape region, the flow is highly unsteady and leads to a high level of pressure fluctuations and strong dynamic loadings on the mechanical parts. The objective of the current work is to perform a comprehensive study of the complex hydraulic phenomena linked with the S-Shape. Unsteady numerical computations are carried out using the turbulence model SAS-SST. Such a model can resolve part of the turbulent spectrum while maintaining affordable computational cost. It therefore offers an interesting alternative to more expensive LES computations. Three different configurations of pump-turbine with the same specific speed (nq=40) are investigated. Several operating conditions from optimal efficiency point to zero discharge condition for a given large guide vane opening are studied. Numerical results show good agreement with the experimental data. Accuracy of the numerical model is thus assessed. The investigations of the global performances of the pump-turbine and the pressure pulsations help to identify the region of the flow which are associated with the main instabilities. Finally, flow visualizations linked with the analysis of the mechanisms of energy dissipation reveal the major flow phenomena at the origin of the S-Shape. Pompe-Turbine Phénomènes transitoires Simulations numériques Structure tourbillonnaires Fluctuations de pression Pump-turbine Unsteady phenomena CFD computations Vortex formation Pressure pulsations 620
10	Ein Beitrag zur Entwicklung neuartiger keramischer Wärmeübertrager für Rekuperatorbrenner Eder, Robert 17 February 2015 (has links) (PDF) Die Effektivität keramischer Wärmeübertrager kann durch eine feinere Strukturierung der Oberflächen gesteigert werden. Dies kann durch die Integration textiler Urformen anstatt der konventionell im Schlickguss hergestellten gröberen Geometrien erfolgen. Für Strukturierungen in Form von wandgebundenen Halbbögen werden die Ergebnisse umfangreicher experimenteller und numerischer Untersuchungen zu den wärmetechnischen und strömungsmechanischen Eigenschaften vorgestellt. Basierend auf den Erkenntnissen der mittels numerischer Simulation durchgeführten Parameterstudie werden verschiedene Empfehlungen für eine optimierte Anordnung der Halbbögen gegeben, um das Verhältnis von Wärmeübergang zur Druckverlust zu verbessern. Die experimentellen Ergebnisse belegen die Richtigkeit der gewählten Randbedingungen und Vereinfachungen im numerischen Modell. Des Weiteren wurden die Strömungsstrukturen mit laserdiagnostischen Messmethoden umfangreich charakterisiert. PIV LDA Laserdiagnostik Wärmerückgewinnung Abgas Industriegasbrenner Rekuperator Wärmeübertrager Wärmetauscher SiC Keramik Wärmerückgewinnung Siliziumkarbid Silizium infiltriert Wirbelbildung konvektiver Wärmeübergang numerische Simulation Wärmeübertragung Wärmeverluste Energeieffizienz CO2 Abgastemperatur Strukturierte Oberfläche Strömung Grenzschicht Turbulator PIV LDA laser diagnostics heat recovery waste gas industrial gas burner recuperator heat exchangers heat exchanger SiC ceramic heat recovery silicon carbide silicon infiltrated vortex formation convective heat transfer numerical simulation heat transfer heat losses Energeieffizienz CO2 exhaust gas temperature structured surface flow boundary layer turbulator cfd vortex shedding Large eddy simulation les ddc:620 ddc:624 Brenner <Feuerung> Rekuperator Keramischer Werkstoff Textilien Verbundwerkstoff Herstellung

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