6 resultados para OF-PRESSURE TRAJECTORIES
em AMS Tesi di Laurea - Alm@DL - Università di Bologna
Resumo:
La crescente attenzione verso un utilizzo attento, sostenibile ed economicamente efficiente della risorsa idrica rende di primaria importanza il tema delle perdite idriche e della gestione efficiente dei sistemi idrici. La richiesta di controlli dell’uso dell’acqua è stata avanzata a livello mondiale. Il problema delle perdite idriche nei Paesi industrializzati è stato così affrontato con specifiche normative e procedure di best practice gestionale per avanzare una valutazione delle perdite idriche e una limitazione degli sprechi e degli usi impropri. In quest’ambito, la pressione gioca un ruolo fondamentale nella regolazione delle perdite reali. La regolazione delle pressioni nelle diverse ore del giorno consente, infatti, di poter agire su queste ultime perdite, che aumentano all’aumentare della pressione secondo una cosiddetta legge di potenza. La motivazione della presente tesi è originata dalla necessità di quantificare il livello di perdita idrica in un sistema acquedottistico in relazione alla pressione all’interno del sistema stesso. Per avere una stima realistica che vada al di là della legge della foronomia, si vuole valutare l’influenza della deformabilità della condotta in pressione fessurata sull’entità delle perdite idriche, con particolare attenzione alle fessurazioni di tipo longitudinale. Tale studio è condotto tramite l’introduzione di un semplice modello di trave alla Winkler grazie al quale, attraverso un’analisi elastica, si descrive il comportamento di una generica condotta fessurata longitudinalmente e si valuta la quantità d’acqua perduta. I risultati ottenuti in condizioni specifiche della condotta (tipo di materiale, caratteristiche geometriche dei tubi e delle fessure, etc.) e mediante l’inserimento di opportuni parametri nel modello, calibrati sui risultati forniti da una raffinata modellazione tridimensionale agli elementi finiti delle medesime condotte, verranno poi confrontati con i risultati di alcune campagne sperimentali. Gli obiettivi del presente lavoro sono, quindi, la descrizione e la valutazione del modello di trave introdotto, per stabilire se esso, nonostante la sua semplicità, sia effettivamente in grado di riprodurre, in maniera realistica, la situazione che si potrebbe verificare nel caso di tubo fessurato longitudinalmente e di fornire risultati attendibili per lo studio delle perdite idriche. Nella prima parte verrà approfondito il problema della perdite idriche. Nella seconda parte si illustrerà il semplice modello di trave su suolo elastico adottato per l’analisi delle condotte in pressione fessurate, dopo alcuni cenni teorici ai quali si è fatto riferimento per la realizzazione del modello stesso. Successivamente, nella terza parte, si procederà alla calibrazione del modello, tramite il confronto con i risultati forniti da un’analisi tridimensionale agli elementi finiti. Infine nella quarta parte verrà ricavata la relazione flusso-pressione con particolare attenzione all’esponente di perdita, il cui valore risulterà superiore a quello predetto dalla teoria della foronomia, e verrà verificata l’effettiva validità del modello tramite un confronto con i risultati sperimentali di cui è stata fatta menzione in precedenza.
Resumo:
This dissertation presents a calibration procedure for a pressure velocity probe. The dissertation is divided into four main chapters. The first chapter is divided into six main sections. In the firsts two, the wave equation in fluids and the velocity of sound in gases are calculated, the third section contains a general solution of the wave equation in the case of plane acoustic waves. Section four and five report the definition of the acoustic impedance and admittance, and the practical units the sound level is measured with, i.e. the decibel scale. Finally, the last section of the chapter is about the theory linked to the frequency analysis of a sound wave and includes the analysis of sound in bands and the discrete Fourier analysis, with the definition of some important functions. The second chapter describes different reference field calibration procedures that are used to calibrate the P-V probes, between them the progressive plane wave method, which is that has been used in this work. Finally, the last section of the chapter contains a description of the working principles of the two transducers that have been used, with a focus on the velocity one. The third chapter of the dissertation is devoted to the explanation of the calibration set up and the instruments used for the data acquisition and analysis. Since software routines were extremely important, this chapter includes a dedicated section on them and the proprietary routines most used are thoroughly explained. Finally, there is the description of the work that has been done, which is identified with three different phases, where the data acquired and the results obtained are presented. All the graphs and data reported were obtained through the Matlab® routine. As for the last chapter, it briefly presents all the work that has been done as well as an excursus on a new probe and on the way the procedure implemented in this dissertation could be applied in the case of a general field.
Resumo:
A new method for the evaluation of the efficiency of parabolic trough collectors, called Rapid Test Method, is investigated at the Solar Institut Jülich. The basic concept is to carry out measurements under stagnation conditions. This allows a fast and inexpensive process due to the fact that no working fluid is required. With this approach, the temperature reached by the inner wall of the receiver is assumed to be the stagnation temperature and hence the average temperature inside the collector. This leads to a systematic error which can be rectified through the introduction of a correction factor. A model of the collector is simulated with COMSOL Multipyisics to study the size of the correction factor depending on collector geometry and working conditions. The resulting values are compared with experimental data obtained at a test rig at the Solar Institut Jülich. These results do not match with the simulated ones. Consequentially, it was not pos-sible to verify the model. The reliability of both the model with COMSOL Multiphysics and of the measurements are analysed. The influence of the correction factor on the rapid test method is also studied, as well as the possibility of neglecting it by measuring the receiver’s inner wall temperature where it receives the least amount of solar rays. The last two chapters analyse the specific heat capacity as a function of pressure and tem-perature and present some considerations about the uncertainties on the efficiency curve obtained with the Rapid Test Method.
Resumo:
In the recent years, autonomous aerial vehicles gained large popularity in a variety of applications in the field of automation. To accomplish various and challenging tasks the capability of generating trajectories has assumed a key role. As higher performances are sought, traditional, flatness-based trajectory generation schemes present their limitations. In these approaches the highly nonlinear dynamics of the quadrotor is, indeed, neglected. Therefore, strategies based on optimal control principles turn out to be beneficial, since in the trajectory generation process they allow the control unit to best exploit the actual dynamics, and enable the drone to perform quite aggressive maneuvers. This dissertation is then concerned with the development of an optimal control technique to generate trajectories for autonomous drones. The algorithm adopted to this end is a second-order iterative method working directly in continuous-time, which, under proper initialization, guarantees quadratic convergence to a locally optimal trajectory. At each iteration a quadratic approximation of the cost functional is minimized and a decreasing direction is then obtained as a linear-affine control law, after solving a differential Riccati equation. The algorithm has been implemented and its effectiveness has been tested on the vectored-thrust dynamical model of a quadrotor in a realistic simulative setup.
Resumo:
Numerous types of acute respiratory failure are routinely treated using non-invasive ventilatory support (NIV). Its efficacy is well documented: NIV lowers intubation and death rates in various respiratory disorders. It can be delivered by means of face masks or head helmets. Currently the scientific community’s interest about NIV helmets is mostly focused on optimising the mixing between CO2 and clean air and on improving patient comfort. To this end, fluid dynamic analysis plays a particularly important role and a two- pronged approach is frequently employed. While on one hand numerical simulations provide information about the entire flow field and different geometries, they exhibit require huge temporal and computational resources. Experiments on the other hand help to validate simulations and provide results with a much smaller time investment and thus remain at the core of research in fluid dynamics. The aim of this thesis work was to develop a flow bench and to utilise it for the analysis of NIV helmets. A flow test bench and an instrumented mannequin were successfully designed, produced and put into use. Experiments were performed to characterise the helmet interface in terms of pressure drop and flow rate drop over different inlet flow rates and outlet pressure set points. Velocity measurements by means of Particle Image Velocimetry were performed. Pressure drop and flow rate characteristics from experiments were contrasted with CFD data and sufficient agreement was observed between both numerical and experimental results. PIV studies permitted qualitative and quantitative comparisons with numerical simulation data and offered a clear picture of the internal flow behaviour, aiding the identification of coherent flow features.