Numerical and semi-analytical models of sliding masses: application to the 1783 Scilla tsunamigenic landslide

The Scilla rock avalanche occurred on 6 February 1783 along the coast of the Calabria region (southern Italy), close to the Messina Strait. It was triggered by a mainshock of the Terremoto delle Calabrie seismic sequence, and it induced a tsunami wave responsible for more than 1500 casualties along the neighboring Marina Grande beach. The main goal of this work is the application of semi-analtycal and numerical models to simulate this event. The first one is a MATLAB code expressly created for this work that solves the equations of motion for sliding particles on a two-dimensional surface through a fourth-order Runge-Kutta method. The second one is a code developed by the Tsunami Research Team of the Department of Physics and Astronomy (DIFA) of the Bologna University that describes a slide as a chain of blocks able to interact while sliding down over a slope and adopts a Lagrangian point of view. A wide description of landslide phenomena and in particular of landslides induced by earthquakes and with tsunamigenic potential is proposed in the first part of the work. Subsequently, the physical and mathematical background is presented; in particular, a detailed study on derivatives discratization is provided. Later on, a description of the dynamics of a point-mass sliding on a surface is proposed together with several applications of numerical and analytical models over ideal topographies. In the last part, the dynamics of points sliding on a surface and interacting with each other is proposed. Similarly, different application on an ideal topography are shown. Finally, the applications on the 1783 Scilla event are shown and discussed.

Tradurre la letteratura per l'infanzia: proposta di traduzione di Flip Flap Safari di Axel Scheffler

This thesis is a proposed translation of the picture book Flip Flap Safari, written by the German author Axel Scheffler and published in 2014. The translation is presented along with an analysis and a commentary in which I analyse and examine the main translation problems of this kind of literature. and I explain the reasons behind my solutions. The translation of a picture book is a creative challenge because it requires translator to use their linguistic and cultural skills together with their imagination and to evaluate the phonetic dimension of the source text and reproduce in the target language. In the first part of my thesis I will introduce an overview of children’s literature in Italy and I will then focus on Flip Flap Safari, analysing the text and providing biographical information about its author-illustrator Axel Scheffler. In the second part of my thesis I will present my translation of the book, which will be followed by a reflection about the main problems I had to face during the translation process.

Generic wind estimation and compensation based on residual generators and higher-order sliding mode schemes

This master thesis proposes a solution to the approach problem in case of unknown severe microburst wind shear for a fixed-wing aircraft, accounting for both longitudinal and lateral dynamics. The adaptive controller design for wind rejection is also addressed, exploiting the wind estimation provided by suitable estimators. It is able to successfully complete the final approach phase even in presence of wind shear, and at the same time aerodynamic envelope protection is retained. The adaptive controller for wind compensation has been designed by a backstepping approach and feedback linearization for time-varying systems. The wind shear components have been estimated by higher-order sliding mode schemes. At the end of this work the results are provided, an autonomous final approach in presence of microburst is discussed, performances are analyzed, and estimation of the microburst characteristics from telemetry data is examined.

Experimental Study on Friction between Saline Ice and Steel

Understanding the interaction of sea ice with offshore structures is of primary importance for the development of technology in cold climate regions. The rheological properties of sea ice (strength, creep, viscosity) as well as the roughness of the contact surface are the main factors influencing the type of interaction with a structure. A device was developed and designed and small scale laboratory experiments were carried out to study sea ice frictional interaction with steel material by means of a uniaxial compression rig. Sea-ice was artificially grown between a stainless steel piston (of circular cross section) and a hollow cylinder of the same material, coaxial to the former and of the same surface roughness. Three different values for the roughness were tested: 1.2, 10 and 30 μm Ry (maximum asperities height), chosen as representative values for typical surface conditions, from smooth to normally corroded steel. Creep tests (0.2, 0.3, 0.4 and 0.6 kN) were conducted at T = -10 ºC. By pushing the piston head towards the cylinder base, three different types of relative movement were observed: 1) the piston slid through the ice, 2) the piston slid through the ice and the ice slid on the surface of the outer cylinder, 3) the ice slid only on the cylinder surface. A cyclic stick-slip motion of the piston was detected with a representative frequency of 0.1 Hz. The ratio of the mean rate of axial displacement to the frequency of the stick-slip oscillations was found to be comparable to the roughness length (Sm). The roughness is the most influential parameter affecting the amplitude of the oscillations, while the load has a relevant influence on the their frequency. Guidelines for further investigations were recommended. Marco Nanetti - seloselo@virgilio.it

Analisi e valutazione delle performance acustiche degli aeromobili nella fase di atterraggio

Nella tesi si analizzano le principali fonti del rumore aeronautico, lo stato dell'arte dal punto di vista normativo, tecnologico e procedurale. Si analizza lo stato dell'arte anche riguardo alla classificazione degli aeromobili, proponendo un nuovo indice prestazionale in alternativa a quello indicato dalla metodologia di certificazione (AC36-ICAO) Allo scopo di diminuire l'impatto acustico degli aeromobili in fase di atterraggio, si analizzano col programma INM i benefici di procedure CDA a 3° rispetto alle procedure tradizionali e, di seguito di procedure CDA ad angoli maggiori in termini di riduzione di lunghezza e di area delle isofoniche SEL85, SEL80 e SEL75.

Hybrid foundations for offshore wind turbines

Nowadays offshore wind turbines represents a valid answer for energy production but with an increasing in costs mainly due to foundation technology required. Hybrid foundations composed by suction caissons over which is welded a tower supporting the nacelle and the blades allows a strong costs reduction. Here a monopod configuration is studied in a sandy soil in a 10 m water depth. Bearing capacity, sliding resistance and pull-out resistance are evaluated. In a second part the installation process occurring in four steps is analysed. considering also the effect of stress enhancement due to frictional forces opposing to penetration growing at skirt sides both inside and outside. In a three dimensional finite element model using Straus7 the soil non-linearity is considered in an approximate way through an iterative procedure using the Yokota empirical decay curves.

A Phase Space Box-counting based Method for Arrhythmia Prediction from Electrocardiogram Time Series

Arrhythmia is one kind of cardiovascular diseases that give rise to the number of deaths and potentially yields immedicable danger. Arrhythmia is a life threatening condition originating from disorganized propagation of electrical signals in heart resulting in desynchronization among different chambers of the heart. Fundamentally, the synchronization process means that the phase relationship of electrical activities between the chambers remains coherent, maintaining a constant phase difference over time. If desynchronization occurs due to arrhythmia, the coherent phase relationship breaks down resulting in chaotic rhythm affecting the regular pumping mechanism of heart. This phenomenon was explored by using the phase space reconstruction technique which is a standard analysis technique of time series data generated from nonlinear dynamical system. In this project a novel index is presented for predicting the onset of ventricular arrhythmias. Analysis of continuously captured long-term ECG data recordings was conducted up to the onset of arrhythmia by the phase space reconstruction method, obtaining 2-dimensional images, analysed by the box counting method. The method was tested using the ECG data set of three different kinds including normal (NR), Ventricular Tachycardia (VT), Ventricular Fibrillation (VF), extracted from the Physionet ECG database. Statistical measures like mean (μ), standard deviation (σ) and coefficient of variation (σ/μ) for the box-counting in phase space diagrams are derived for a sliding window of 10 beats of ECG signal. From the results of these statistical analyses, a threshold was derived as an upper bound of Coefficient of Variation (CV) for box-counting of ECG phase portraits which is capable of reliably predicting the impeding arrhythmia long before its actual occurrence. As future work of research, it was planned to validate this prediction tool over a wider population of patients affected by different kind of arrhythmia, like atrial fibrillation, bundle and brunch block, and set different thresholds for them, in order to confirm its clinical applicability.

Studio e ottimizzazione della ipersostentazione del velivolo V-173

Studio della ipersostentazione di un velivolo non convenzionale degli anni ‘40, il Vought V-173 Flying Pancake. Per realizzare l’intero lavoro si sono adoperati dei software di fluidodinamica computazionale come Flow Simulation di SolidWorks e il programma JavaFoil, inoltre, si è scelto l’ambiente Matlab di supporto ai calcoli e per rappresentare i risultati ottenuti a seguito delle simulazioni, realizzando script e funzioni per l’approssimazione di questi e la loro successiva raffigurazione grafica. In particolar modo, a partire dal modello tridimensionale in SolidWorks del V-173 si sono ricreate le curve CL-α e CD-α a partire dai punti ottenuti dalle simulazioni per diverse configurazioni del velivolo. In una prima fase si è valutata l’aerodinamica del velivolo ‘pulito’ senza la presenza delle eliche e di ipersostentatori, successivamente si sono seguite due strade diverse per valutare il comportamento del velivolo: nel primo caso si sono eseguiti studi dell’aerodinamica del Pancake in presenza degli ipersostentatori già presenti sul velivolo (i plain flap), proponendo soluzioni alternative per migliorare l’ipersostentazione del V-173 tramite spillamenti (slots) e diverse configurazioni di vortex generator che energizzassero lo strato limite e ottimizzassero le prestazioni del velivolo con particolare attenzione alla fase di atterraggio. In secondo luogo, tenendo in considerazione che il Pancake è un aeroplano bielica, si è voluta studiare l’influenza delle due eliche sulla sua aerodinamica: dopo aver riprodotto nel modo più verosimile entrambe le eliche utilizzando SolidWorks si è fatto uno studio di massima ricavando risultati che potessero indicare la compatibilità tra elica e velivolo a seguito dei risultati sperimentali ottenuti con Flow Simulation.

Valutazione sperimentale del campo aerodinamico prodotto da rasaerba industriali: un'indagine parametrica

L’azienda GGP, leader europeo nella produzione di rasaerba e prodotti per il giardinaggio, ha avviato, in collaborazione con il Laboratorio di aerodinamica sperimentale della Facoltà di ingegneria dell’Università di Bologna, uno studio atto alla valutazione delle prestazioni dei rasaerba commercializzati, al fine di comprendere quali siano le vie percorribili per ottenere un miglioramento delle prestazioni associate. Attualmente il metodo utilizzato per compiere tali valutazioni consiste nel far percorrere al rasaerba un percorso di lunghezza prestabilita e valutare il peso dell’erba raccolta nel sacco. Tale approccio presenta delle forti limitazioni in quanto le prove non sono per loro natura ripetibili. Si pensi ad esempio alla non uniformità del terreno e all’altezza dell’erba. È pertanto necessario un approccio in grado di definire con maggior precisione e ripetibilità le prestazioni dei macchinari rasaerba. Tra le diverse prestazioni c’è la capacità della macchina di trattare una portata di aria più elevata possibile garantendo un’elevata aspirazione dell’erba tagliata. Da questo punto vista la geometria della lama riveste un’importanza particolare. Per valutare le prestazioni della singola lama, è stato realizzato un “test-rig lame”, uno strumento con cui è possibile trattare il flusso per renderlo misurabile e valutare la portata d’aria attraverso semplici misure di pressione. Una volta costruito il “test-rig”, sono stati individuati i parametri geometrici delle lame che influenzano la portata, quali apertura, corda e calettamento del flap della lama. Lo studio svolto si limita a valutare gli effetti causati dalla sola geometria della lama prescindendo dalla forma della voluta, in quanto la sua interazione con la lama risulta di grande complessità. Si è quindi avviata una campagna di test sperimentali effettuati su lame caratterizzate da diversi valori dei parametri, che l’azienda stessa ha prodotto e fornito al laboratorio, al fine di trovare relazioni funzionali tra la portata elaborata e la geometria delle lame.