Global ETD Search

681	Drooped Strings and Dressed Mesons: Implications of Gauge-Gravity Duality for the Properties of Heavy-Light Mesons at Finite Temperature Moomaw, Peter 22 December 2009 (has links) No description available. Particle Physics Physics AdS/CFT holography String Theory quark-gluon plasma mesons drag coefficient heavy-light mesons Gauge-Gravity duality meson spectrum Drooped string Drooping string Dressed meson kinematics, finite temperature
682	Modeling, Simulation and Correlation of Drag losses in a Power Transfer Unit of an All- Wheel Drive System / Modellering, simulering och korrelation av dragförluster i en kraftöverföringsenhet i ett fyrhjulsdrivsystem Venkatesan, Balaji Srinivasan January 2020 (has links) A Power Transfer Unit (PTU) of an All-Wheel Drive System is a hypoid gear transmission unit that distributes the power from the vehicle transmission to all wheels of the vehicle. This thesis aims at increasing the fidelity of the analytical power loss calculation methods through test data correlation and develop a 1D simulation model that can be used to evaluate the drag losses in the PTU at early design stages. Firstly, the analytical methods to predict the frictional losses and oil churning losses due to the hypoid gearset, rolling bearings and seals immersed in oil are studied. Several drag loss tests with different combinations of internal components, bearing preloads and with/without the presence of oil were previously conducted on the PTU at different speeds and temperatures at zero torque. The power losses are computed in ROMAX Energy and Excel using different analytical methods available in the literature for each component in the PTU. Then the results from the drag loss tests are segregated component-wise for data correlation with the losses evaluated previously. Based on the data correlation, modification factors are introduced for all analytical methods to match the segregated test results. The demand in the automotive industry to reduce time to market is high. Hence, system-level simulation was chosen as a solution to assess the system efficiency at early concept design stage, saving a lot of time and aid the detailed design. 1D simulation technique is used to study the total power loss of the PTU to optimize its design. The thesis is aimed at developing a 1D system model of the PTU in a commercial tool called LMS AMESim, to evaluate the total power loss of the unit. Inbuilt component models from the software library are used to build a sketch of a simplified lumped mass model of the physical system. The model is simulated in a time domain temporal analysis. The total power loss results simulated using AMESim are compared to the efficiency tests results conducted at different torque levels and ROMAX results. Comparisons between the simulations and test data shows that the system model is accurate and can be used in predicting the power losses in the PTU in the early design stages. This model can also be used to study the influential factors through sensitivity analysis of different parameters which can be done as an extension to the current scope of this work. / En kraftöverföringsenhet (PTU) i ett fyrhjulsdriftsystem är en hypoidväxellådsöverföringsenhet som fördelar kraften från växellådan till alla hjul i fordonet. Det rapporterade arbetet syftar till att öka konfidensen i de analytiska beräkningsmetoderna för effektförlust genom testdatakorrelation och genom att utveckla en 1D-simuleringsmodell som kan användas för att utvärdera dragförlusterna i PTUn i tidiga designfaser. För det första studeras analysmetoderna för att förutsäga friktionsförluster och plaskförluster på grund av hypoidväxeln, rullager och tätningar nedsänkta i olja. Flera ”Drag Loss”-tester med olika kombinationer av interna komponenter, lagerförspänningar och med / utan närvaro av olja utfördes tidigare på PTU vid olika hastigheter och temperaturer utan pålagt moment. Effektförlusterna beräknas i ROMAX Energy med olika analysmetoder tillgängliga i litteraturen för varje komponent i PTU. Sedan separeras resultaten från dragförlusttesterna komponentmässigt för datakorrelation med de tidigare utvärderade förlusterna. Baserat på datakorrelationen införs modifieringsfaktorer för alla analysmetoder för att matcha de segregerade testresultaten. Efterfrågan inom fordonsindustrin att minska tiden till marknaden är hög. Därför väljs simulering på systemnivå som en lösning för att bedöma systemeffektiviteten i ett tidigt konceptdesignfas, vilket sparar mycket tid och underlättar den detaljerade designen. 1D-simuleringsteknik används för att studera PTUns totala effektförlust för att optimera dess design. Arbetet syftar till att utveckla en 1D-systemmodell av PTU i ett kommersiellt verktyg som heter LMS AMESim, för att utvärdera enhetens totala effektförlust. Inbyggda komponentmodeller från programvarubiblioteket används för att skapa en skiss av en förenklad modell av det fysiska systemet. De totala effektförlusterna beräknade med AMESim jämförs med effektivitetstestresultaten vid olika vridmomentnivåer och ROMAX-resultat. Från korrelationen med testresultaten observeras att systemmodellen är korrekt och kan användas för att förutsäga effektförlusterna i PTU i de tidiga designstadierna. Denna modell kan också användas för att studera de viktigaste faktorerna genom känslighetsanalys av olika parametrar, vilket kan göras som en förlängning av detta arbete. 1-D simulation System simulation ROMAX Energy LMS AMESim Power loss Hypoid gear Power Transfer Unit Efficiency and Drag Loss Tests 1-D simulering systemsimulering ROMAX Energy LMS AMESim effektförlust hypoidväxel kraftöverföringsenhet effektivitet och dragförlusttester Engineering and Technology Teknik och teknologier
683	Development, Modelling and Control of a Multirotor Vehicle Mikkelsen, Markus January 2015 (has links) The interest of drones in all forms has exploded in the recent years. The development of multirotor vehicles such as quadcopters and octocopters, has reached a point where they are cheap and versatile enough to start becoming a part of everyday life. It is clear to say that the future applications seem limitless. This thesis goes through the steps of development, modelling and control design of an octocopter system. The developed octocopter builds on a concept of using the mini computer Raspberry Pi together with the code generation functionality of Matlab/Simulink. The mathematical modelling of the octocopter includes the thrust and torques generated by the propellers, added with gyroscopic torque. These are combined with the aerodynamic effects caused by incoming air. The importance of modelling the later mentioned effects has increased with the demand of precise controlled extreme manoeuvres. A full state feedback based hybrid controller scheme is designed against a linearized model, which makes use of the motor dynamics. The controllers show good performance in simulations and are approved for flight tests, which are conducted on two separate occasions. The octocopter makes two successful flights, proving that the concept can be applied on multirotor vehicles. However, there is a miss-match between the mathematical model and the physical octocopter, leaving questions for future work. Multirotor Octocopter Blade flapping Induced drag Gyroscopic torque Drone Modelling Control Code generation Raspberry Pi Matlab Simulink Simulations Flight tests Control Engineering Reglerteknik Embedded Systems Inbäddad systemteknik Robotics Robotteknik och automation Vehicle Engineering Farkostteknik Aerospace Engineering Rymd- och flygteknik
684	The Effect of a Splitter Plate on the Flow around a Surface-Mounted Finite Circular Cylinder 2011 September 1900 (has links) Splitter plates are passive flow control devices for reducing drag and suppressing vortex shedding from bluff bodies. Most studies of splitter plates involve the flow around an “infinite” circular cylinder, however, in the present study the flow around a surface-mounted finite-height circular cylinder, with a wake-mounted splitter plate, was studied experimentally in a low-speed wind tunnel using a force balance and single-component hot-wire anemometry. Four circular cylinders of aspect ratios AR = 9, 7, 5 and 3 were tested for a Reynolds number range of Re = 1.9×10^4 to 8.2×10^4. The splitter plates had lengths, relative to the cylinder diameter, of L/D = 1, 1.5, 2, 3, 5 and 7, thicknesses ranging from T/D = 0.10 and 0.15, and were the same height as the cylinder being tested. The cylinders were partially immersed in a flat-plate turbulent boundary layer, where the range of boundary layer thickness relative to the cylinder diameter was δ/D = 1.4 to 1.5. Measurements were made of the mean drag force coefficient, the Strouhal number at the mid-height position, and the Strouhal number and power spectra along the cylinder height. For all four finite circular cylinders, the splitter plates were effective at reducing the magnitude of the Strouhal number, and weakening or even suppressing vortex shedding, depending on the specific combination of AR and L/D. Compared to the case of an infinite circular cylinder, the splitter plate is less effective at reducing the mean drag force coefficient of a finite circular cylinder. The largest drag reduction was obtained for the cylinder of AR = 9 and splitter plates of L/D = 1 to 3, while negligible drag reduction occurred for the shorter cylinders.
685	Dinosaurier, drakar, vapen, rymdskepp, aliens, eld, monster, farliga djur : Om att passa in i samhället eller hitta hem utanför. / Dinosaurs, dragons, weapons, spaceships, aliens, fire, monsters, dangerous animals : To fit into society or to find your home outside. Pettersson, Mattias January 2019 (has links) I denna text vill jag, som undertiteln skvallrar, prata om att passa in i samhället eller hitta hem utanför. Arbetet har den enkla strukturen att det börjar med att prata om hinder man kan ha för att ”passa in”, såsom att inte klara prestations-pressen man känner från en osynlig makt, eller helt enkelt av att bryta från normen (här med fokus på att vara bög eller queer). Vidare via min och andras historier kring att ha sitt psyke eller sina känslor som en grundläggande parameter i sitt konstnärskap, och går sen avslutningsvis ut i några andra alternativa vägar att hitta hem utanför; drag och frivillig enkelhet. Varsågod. / Dinosaurs, dragons, weapons, spaceships, aliens, fire, monsters, dangerous animals. Never interested me. That's why they interest me. Through intuitive sculpting, stories about my traumas, lusts and needs are formed, and about the society they exist in. I can see a tension towards the boy I never was/the man I never became, and a longing after to now approach him om my own terms. The sculptures are crooked, weak, broken, naive and weird, and in this becomes a vital space where that is allowed. The pieces are standing with the underdogs. In a movement upwards. fit in queer gay men feminine men drag straight acting downshifting dragons spaceship alien gender roles ceramics sculpture safe space naivism outsider art mental illness working class anxiety depression stress norms emotions straight acting scew masculinity masc for masc fantasy mcqueen rupauls dragrace blue abstract art passa in hitta hem queer bögar feminina killar drag frivillig enkelhet drakar rymdskepp aliens könsroller keramik skulptur trygga rum tryggt rum naivism outsiderart psykisk ohälsa arbetarklass ångest depression stress normer känslostyrd straightacting skevhet manlighet fantasy mcqueen rupauls dragrace blå abstrakt konst Arts Konst
686	Development of Sensors and Microcontrollers for Underwater Robots Jebelli, Ali January 2014 (has links) Nowadays, small autonomous underwater robots are strongly preferred for remote exploration of unknown and unstructured environments. Such robots allow the exploration and monitoring of underwater environments where a long term underwater presence is required to cover a large area. Furthermore, reducing the robot size, embedding electrical board inside and reducing cost are some of the challenges designers of autonomous underwater robots are facing. As a key device for reliable operation-decision process of autonomous underwater robots, a relatively fast and cost effective controller based on Fuzzy logic and proportional-integral-derivative method is proposed in this thesis. It efficiently models nonlinear system behaviors largely present in robot operation and for which mathematical models are difficult to obtain. To evaluate its response, the fault finding test approach was applied and the response of each task of the robot depicted under different operating conditions. The robot performance while combining all control programs and including sensors was also investigated while the number of program codes and inputs were increased. AUV Autonomous Underwater Vehicles ADC Analog to Digital Converter Cd Drag coefficient of the object DOF Degree of Freedom KT Thrust coefficient Fd Force of drag g Acceleration of gravity h Height of the fluid above the object KQ Torque coefficient mb Buoyant mass NN Neural network P Proportional controller PI Proportional-integral controller PID ρ Density of the fluid Q Torque of the propeller ROV Remotely Operated Vehicles RPM Speed of the motor or propeller SDO Serial data output SMC Sliding mode control Measured thrust T° Temperature v AV Advance speed of the propeller
687	Transition delay in boundary-layer flows via reactive control / Fördröjning av laminärt-turbulent omslag i gränsskiktströmning genom reaktiv kontroll Fabbiane, Nicolò January 2016 (has links) Transition delay in boundary-layer flows is achieved via reactive control of flow instabilities, i.e. Tollmien-Schlichting (TS) waves. Adaptive and model-based control techniques are investigated by means of direct numerical simulations (DNS) and experiments. The action of actuators localised in the wall region is prescribed based on localised measurement of the disturbance field; in particular, plasma actuators and surface hot-wire sensors are considered. Performances and limitations of this control approach are evaluated both for two-dimensional (2D) and three-dimensional (3D) disturbance scenarios. The focus is on the robustness properties of the investigated control techniques; it is highlighted that static model-based control, such as the linear-quadratic- Gaussian (LQG) regulator, is very sensitive to model-inaccuracies. The reason for this behaviour is found in the feed-forward nature of the adopted sensor/actuator scheme; hence, a second, downstream sensor is introduced and actively used to recover robustness via an adaptive filtered-x least-mean-squares (fxLMS) algorithm. Furthermore, the model of the flow required by the control algorithm is reduced to a time delay. This technique, called delayed-x least-mean-squares (dxLMS) algorithm, allows taking a step towards a self-tuning controller; by introducing a third sensor it is possible to compute on-line the suitable time-delay model with no previous knowledge of the controlled system. This self-tuning approach is successfully tested by in-flight experiments on a motor-glider. Lastly, the transition delay capabilities of the investigated control con- figuration are confirmed in a complex disturbance environment. The flow is perturbed with random localised disturbances inside the boundary layer and the laminar-to-turbulence transition is delayed via a multi-input-multi-output (MIMO) version of the fxLMS algorithm. A positive theoretical net-energy- saving is observed for disturbance amplitudes up to 2% of the free-stream velocity at the actuation location, reaching values around 1000 times the input power for the lower disturbance amplitudes that have been investigated. / I den här avhandlingen har reglertekniska metoder tillämpats för att försena omslaget från ett laminärt till ett turbulent gränsskikt genom att dämpa tillväxten av små instabiliteter, så kallade Tollmien-Schlichting vågor. Adaptiva och modellbaserade metoder för reglering av strömning har undersökts med hjälp av numeriska beräkningar av Navier-Stokes ekvationer, vindtunnelexperiment och även genom direkt tillämpning på flygplan. Plasmaaktuatorer och varmtrådsgivare vidhäftade på ytan av plattan eller vingen har använts i experimenten och modellerats i beräkningarna. Prestanda och begränsningar av den valda kontrollstrategin har utvärderats för både tvådimensionella och tredimensionella gränsskiktsinstabiliteter. Fokus har varit på metodernas robusthet, där vi visar att statiska metoder som linjär-kvadratiska regulatorer (LQG) är mycket känsliga för avvikelser från den nominella modellen. Detta beror främst på att regulatorer agerar i förkompenseringsläge (”feed-foward”) på grund av strömningens karaktär och placeringen av givare och aktuatorer. För att minska känsligheten mot avvikelser och därmed öka robustheten har en givare införts nedströms och en adaptiv fXLMS algoritm (filtered-x least-mean-squares) har tillämpats. Vidare har modelleringen av fXLMS-algoritmen förenklats genom att ersätta överföringsfunktionen mellan aktuatorer och givare med en lämplig tidsfördröjning. Denna metod som kallas för dxLMS (delayed-x least-mean-squares) kräver att ytterligare en givare införs långt uppströms för att kunna uppskatta hastigheten på de propagerande instabilitetsvågorna. Denna teknik har tillämpats framgångsrikt för reglering av gränsskiktet på vingen av ett segelflygplan. Slutligen har de reglertekniska metoderna testas för komplexa slumpmässiga tredimensionella störningar som genererats uppströms lokalt i gränsskiktet. Vi visar att en signifikant försening av laminärt-turbulentomslag äger rum med hjälp av en fXLMS algoritm. En analys av energibudgeten visar att för ideala aktuatorer och givare kan den sparade energiåtgången på grund av minskad väggfriktion vara upp till 1000 gånger större än den energi som använts för reglering. flow control drag reduction net energy saving adaptive control model-based control optimal control flat-plate boundary layer laminar-to- turbulent transition plasma actuator direct numerical simulation in-flight experiments strömningsstyrning friktionsreduktion netto energibesparing adaptiv styrning modellbaserad styrning optimal kontroll gränsskikt öve en plan platta laminärt till turbulent omslag plasma aktuator DNS flyg prov
688	Simulation aux grandes échelles des lits fluidisés circulants gaz-particule / Development of Large Eddy Simulation Approach for Simulation of Circulating Fluidized Beds Özel, Ali 18 October 2011 (has links) Les simulations numériques des équations d’Euler deux-fluides réalisé sur des maillages grossiers éliminent les structures fins d’écoulement gaz-solide dans les lits fluidisés. Pour précisément estimer l’hydrodynamique globale de lit, il faut proposer une modélisation qui prend en compte les effets de structure non-résolue. Dans ce but, les maillages sont raffinés pour obtenir le résultat de simulation pleinement résolue ce que les grandeurs statistiques ne modifient plus avec un autre raffinement pour le lit fluidisé périodique dilué gaz-particules sur une géométrie 3D cartésienne et ce résultat est utilisé pour tests "a priori". Les résultats de tests "a priori" montrent que l’équation filtrée de la quantité de mouvement est effectuée mais il faut prendre en compte le flux de la fraction volumique de solide de sous-maille en raison de l’interaction locale de la vitesse du gaz et la fraction volumique de solide pour la force traniée. Nous proposons les modèles fonctionnels et structurels pour le flux de la fraction volumique de solide de sous-maille. En plus, les modèles fermetures du tenseur de sous-maille de la phase dispersée sont similaires aux modèles classiquement utilisés en écoulement turbulent monophasique. Tous les modèles sont validés par test "a priori" et "a posteriori" / Eulerian two fluid approach is generally used to simulate gas-solid flows in industrial circulating fluidized beds. Because of limitation of computational resources, simulations of large vessels are usually performed by using too coarse grid. Coarse grid simulations can not resolve fine flow scales which can play an important role in the dynamic behaviour of the beds. In particular, cancelling out the particle segregation effect of small scales leads to an inadequate modelling of the mean interfacial momentum transfer between phases and particulate shear stresses by secondary effect. Then, an appropriate modelling ac counting for influences of unresolved structures has to be proposed for coarse-grid simu-lations. For this purpose, computational grids are refined to get mesh-independent result where statistical quantities do not change with further mesh refinement for a 3-D peri-odic circulating fluidized bed. The 3-D periodic circulating fluidized is a simple academic configuration where gas-solid flow conducted with A-type particles is periodically driven along the opposite direction of the gravity. The particulate momentum and agitation equations are filtered by the volume averaging and the importance of additional terms due to the averaging procedure are investigated by budget analyses using the mesh independent result. Results show that the filtered momentum equation of phases can be computed on coarse grid simulations but sub-grid drift velocity due to the sub-grid correlation between the local fluid veloc- ity and the local particle volume fraction and particulate sub-grid shear stresses must be taken into account. In this study, we propose functional and structural models for sub- grid drift velocity, written in terms of the difference between the gas velocity-solid volume fraction correlation and the multiplication of the filtered gas velocity with the filtered solid volume fraction. Particulate sub-grid shear stresses are closed by models proposed for single turbulent flows. Models’ predictabilities are investigated by a priori tests and they are validated by coarse-grid simulations of 3-D periodic circulating, dense fluidized beds and experimental data of industrial scale circulating fluidized bed in manner of a posteriori tests Lit fluidisé circulant Modèle à deux-fluides filtré Force de traînée Contrainte Cinétiques de sous-maille Modèles fonctionnels Modèles structurels Etude "a priori" Etude "a posteriori Circulating fluidized bed Filtered two-fluid model Drag force Solid subgrid kinetic stress Functional model Structural model A priori test A posteriori test
689	A Theory and Analysis of Planing Catamarans in Calm and Rough Water Zhou, Zhengquan 16 May 2003 (has links) A planing catamaran is a high-powered, twin-hull water craft that develops the lift which supports its weight, primarily through hydrodynamic water pressure. Presently, there is increasing demand to further develop the catamaran's planing and seakeeping characteristics so that it is more effectively applied in today's modern military and pleasure craft, and offshore industry supply vessels. Over the course of the past ten years, Vorus (1994,1996,1998,2000) has systematically conducted a series of research works on planing craft hydrodynamics. Based on Vorus' planing monohull theory, he has developed and implemented a first order nonlinear model for planing catamarans, embodied in the computer code CatSea. This model is currently applied in planing catamaran design. However, due to the greater complexity of the catamaran flow physics relative to the monohull, Vorus's (first order) catamaran model implemented some important approximations and simplifications which were not considered necessary in the monohull work. The research of this thesis is for relieving the initially implemented approximations in Vorus's first order planing catamaran theory, and further developing and extending the theory and application beyond that currently in use in CatSea. This has been achieved through a detailed theoretical analysis, algorithm development, and careful coding. The research result is a new, complete second order nonlinear hydrodynamic theory for planing catamarans. A detailed numerical comparison of the Vorus's first order nonlinear theory and the second order nonlinear theory developed here is carried out. The second order nonlinear theory and algorithms have been incorporated into a new catamaran design code (NewCat). A detailed mathematical formulation of the base first order CatSea theory, followed by the extended second order theory, is completely documented in this thesis. vortex strength distribution random wave nonlinear wave high speed jet flow water jet fast ship vessel design drag and resistance dynamic lift high speed craft Planing craft planing boat impact hydrodynamics steady planing seakeeping slender body theory time marching singular integral special function ship motion
690	Comparative Hydrodynamic Testing of Small Scale Models Acosta, Jared 19 December 2008 (has links) Early in the ship design process, naval architects must often evaluate and compare multiple hull forms for a specific set of requirements. Analytical tools are useful for quick comparisons, but they usually specialize in a specific hull type and are therefore not adequate for comparing dissimilar hull types. Scale model hydrodynamic testing is the traditional evaluation method, and is applicable to most hull forms. Scale model tests are usually performed on the largest model possible in order to achieve the most accurate performance predictions. However, such testing is very resource intensive, and is therefore not a cost effective method of evaluating multiple hull forms. This thesis explores the testing of small scale models. It is hypothesized that although the data acquired by these tests will not be accurate enough for performance predictions, they will be accurate enough to rank the performance of the multiple hull forms being evaluated.

Search results