Estudo das interações de eIF5A com a maquinaria de tradução e com o complexo Ribosome Quality Control, utilizando modelo de Saccharomyces cerevisiae

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Projeto de adaptação do sistema de injeção do túnel transônico para ensaios em bocais de foguete

In this work, the project of a new experimental facility to be installed at the Aerodynamics Division of the Institute of Aeronautics and Space is presented. This new facility will provide means to perform experimental campaigns to analyze the flow behavior at different rocket nozzle concepts using cold gas that will be obtained from a modification of the Pilot Transonic Wind Tunnel air system. The new installation will enable less expensive experiments in a more secure environment, since the cold gas experimental procedures do not demand fuel storage and burn and security procedures are much less severe. Furthermore, experiments can be carried with different types of sensors, commonly used in wind tunnel tests. Also, the optical access is facilitated enabling the use of optical techniques for the characterization of flow properties inside the nozzles, such as pressure and temperature sensitive painting. The full project design and the operation conditions will be showed, as also some technical considerations about the flor behavior in the facility

Projeto de adaptação do sistema de injeção do túnel transônico para ensaios em bocais de foguete

In this work, the project of a new experimental facility to be installed at the Aerodynamics Division of the Institute of Aeronautics and Space is presented. This new facility will provide means to perform experimental campaigns to analyze the flow behavior at different rocket nozzle concepts using cold gas that will be obtained from a modification of the Pilot Transonic Wind Tunnel air system. The new installation will enable less expensive experiments in a more secure environment, since the cold gas experimental procedures do not demand fuel storage and burn and security procedures are much less severe. Furthermore, experiments can be carried with different types of sensors, commonly used in wind tunnel tests. Also, the optical access is facilitated enabling the use of optical techniques for the characterization of flow properties inside the nozzles, such as pressure and temperature sensitive painting. The full project design and the operation conditions will be showed, as also some technical considerations about the flor behavior in the facility

Relationship between body size and flying-related structures in Neotropical social wasps (Polistinae, Vespidae, Hymenoptera)

Body size influences wing shape and associated muscles in flying animals which is a conspicuous phenomenon in insects, given their wide range in body size. Despite the significance of this, to date, no detailed study has been conducted across a group of species with similar biology allowing a look at specific relationship between body size and flying structures. Neotropical social vespids are a model group to study this problem as they are strong predators that rely heavily on flight while exhibiting a wide range in body size. In this paper we describe the variation in both wing shape, as wing planform, and mesosoma muscle size along the body size gradient of the Neotropical social wasps and discuss the potential factors affecting these changes. Analyses of 56 species were conducted using geometric morphometrics for the wings and lineal morphometrics for the body; independent contrast method regressions were used to correct for the phylogenetic effect. Smaller vespid species exhibit rounded wings, veins that are more concentrated in the proximal region, larger stigmata and the mesosoma is proportionally larger than in larger species. Meanwhile, larger species have more elongated wings, more distally extended venation, smaller stigmata and a proportionally smaller mesosoma. The differences in wing shape and other traits could be related to differences in flight demands caused by smaller and larger body sizes. Species around the extremes of body size distribution may invest more in flight muscle mass than species of intermediate sizes.

SET overexpression decreases cell detoxification efficiency: ALDH2 and GSTP1 are downregulated, DDR is impaired and DNA damage accumulates

Alcohol and tobacco consumption are risk factors for head and neck squamous cell carcinoma (HNSCC). Aldehyde dehydrogenase 2 (ALDH2) and glutathione Stransferase pi 1 (GSTP1) are important enzymes for cellular detoxification and low efficiencies are implicated in cancer. We assessed the potential role of SET protein overexpression, a histone acetylation modulator accumulated in HNSCC, in gene regulation and protein activity of ALDH2 and GSTP1. SET was knocked down in HN13, HN12 and Cal27, and overexpressed in HEK293 cells; ethanol and cisplatin were the chemical agents. Cells with SET overexpression (HEK293/SET, HN13 and HN12) showed lower ALDH2 and GSTP1 mRNA levels and trichostatin A increased them (real-time PCR). Ethanol upregulated GSTP1 and ALDH2 mRNAs, whereas cisplatin upregulated GSTP1 in HEK293 cells. SET-chromatin binding revealed SET interaction with ALDH2 and GSTP1 promoters, specifically via SET NAP domain; ethanol and cisplatin abolished SET binding. ALDH2 and GSTP1 efficiency was assessed by enzymatic and comet assay. A lower ALDH2 activity was associated with greater DNA damage (tail intensity) in HEK293/SET compared with HEK293 cells, whereas HN13/siSET showed ALDH2 activity higher than HN13 cells. HN13/siSET cells showed increased tail intensity. Cisplatin-induced DNA damage response showed negative relationship between SET overexpression and BRCA2 recruitment. SET downregulated repair genes ATM, BRCA1 and CHEK2 and upregulated TP53. Cisplatin-induced cell-cycle arrest occurred in G0/G1 and S in HEK293 cells, whereas HEK293/SET showed G2/M stalling. Overall, cisplatin was more cytotoxic for HN13 than HN13/siSET cells. Our data suggest a role for SET in cellular detoxification, DNA damage response and genome integrity.

Simulazione numerica di fenomeni aeroelastici con applicazione alle strutture civili

Il presente lavoro tratta lo studio dei fenomeni aeroelastici di interazione fra fluido e struttura, con il fine di provare a simularli mediante l’ausilio di un codice agli elementi finiti. Nel primo capitolo sono fornite alcune nozioni di fluidodinamica, in modo da rendere chiari i passaggi teorici fondamentali che portano alle equazioni di Navier-Stokes governanti il moto dei fluidi viscosi. Inoltre è illustrato il fenomeno della formazione di vortici a valle dei corpi tozzi dovuto alla separazione dello strato limite laminare, con descrizione anche di alcuni risultati ottenuti dalle simulazioni numeriche. Nel secondo capitolo vengono presi in rassegna i principali fenomeni di interazione fra fluido e struttura, cercando di metterne in luce le fondamenta della trattazione analitica e le ipotesi sotto le quali tale trattazione è valida. Chiaramente si tratta solo di una panoramica che non entra in merito degli sviluppi della ricerca più recente ma fornisce le basi per affrontare i vari problemi di instabilità strutturale dovuti a un particolare fenomeno di interazione con il vento. Il terzo capitolo contiene una trattazione più approfondita del fenomeno di instabilità per flutter. Tra tutti i fenomeni di instabilità aeroelastica delle strutture il flutter risulta il più temibile, soprattutto per i ponti di grande luce. Per questo si è ritenuto opportuno dedicargli un capitolo, in modo da illustrare i vari procedimenti con cui si riesce a determinare analiticamente la velocità critica di flutter di un impalcato da ponte, a partire dalle funzioni sperimentali denominate derivate di flutter. Al termine del capitolo è illustrato il procedimento con cui si ricavano sperimentalmente le derivate di flutter di un impalcato da ponte. Nel quarto capitolo è presentato l’esempio di studio dell’impalcato del ponte Tsing Ma ad Hong Kong. Sono riportati i risultati analitici dei calcoli della velocità di flutter e di divergenza torsionale dell’impalcato e i risultati delle simulazioni numeriche effettuate per stimare i coefficienti aerodinamici statici e il comportamento dinamico della struttura soggetta all’azione del vento. Considerazioni e commenti sui risultati ottenuti e sui metodi di modellazione numerica adottati completano l’elaborato.

Comparison between 2.5-D and 3-D realistic models for wind field adjustment

[EN]In previous works, many authors have widely used mass consistent models for wind field simulation by the finite element method. On one hand, we have developed a 3-D mass consistent model by using tetrahedral meshes which are simultaneously adapted to complex orography and to terrain roughness length. In addition, we have included a local refinement strategy around several measurement or control points, significant contours, as for example shorelines, or numerical solution singularities. On the other hand, we have developed a 2.5-D model for simulating the wind velocity in a 3-D domain in terms of the terrain elevation, the surface temperature and the meteorological wind, which is consider as an averaged wind on vertical boundaries...

A study on the fluid dynamics of domestic Gas burners

Domestic gas burners are investigated experimentally and numerically in order to further understand the fluid dynamics processes that drive the cooking appliance performances. In particular, a numerical simulation tool has been developed in order to predict the onset of two flame instabilities which may deteriorate the performances of the burner: the flame back and flame lift. The numerical model has been firstly validated by comparing the simulated flow field with a data set of experimental measurements. A prediction criterion for the flame back instability has been formulated based on isothermal simulations without involving the combustion modelization. This analysis has been verified by a Design Of Experiments investigation performed on different burner prototype geometries. On the contrary, the formulation of a prediction criterion regarding the flame lift instability has required the use of a combustion model in the numerical code. In this analysis, the structure and aerodynamics of the flame generated by a cooking appliance has thus been characterized by experimental and numerical investigations, in which, by varying the flow inlet conditions, the flame behaviour was studied from a stable reference case toward a complete blow-out.

A LES study of a modified Ahmed body geometry

A numerical study using Large Eddy Simulation Coherent Structure Model (LES-CSM), of the flow around a simplified Ahmed body, has been done in this work of thesis. The models used are two salient geometries from the experimental investigation performed in [1], and consist, in particular, in two notch-back body geometries. Six simulation are carried out in total, changing Reynolds number and back-light angle of the model’s rear part. The Reynolds numbers used, based on the height of the models and the free stream velocity, are Re = 10000, Re = 30000 and Re = 50000. The back-light angles of the slanted surface with respect to the horizontal roof surface, that characterizes the vehicle, are taken as B = 31.8◦ and B = 42◦ respectively. The experimental results in [1] have shown that, depending on the parameter B, asymmetric and symmetric averaged flow over the back-light and in the wake for a symmetric geometry can be observed. The aims of the present work of master thesis are principally two. The first aim is to investigate and confirm the influence of the parameter B on the presence of the asymmetry of the averaged flow, and confirm the features described in the experimental results. The second important aspect is to investigate and observe the influence of the second variable, the Reynolds number, in the developing of the asymmetric flow itself. The results have shown the presence of the mentioned asymmetry as well as an influence of the Reynolds number on it.

Separation control by means of oriented DBD plasma actuators: an experimental analysis in a wind tunnel

This thesis provides an experimental analysis of the effectiveness of oriented DBD plasma actuators over a NACA 0015 airfoil at low Reynolds numbers. Tests were performed in partnership with the Department of Electrical Engineering of Bologna University, in the wind tunnel of the Applied Aerodynamics Laboratory of Aerospace Engineering faculty. Lift coefficient measurements were carried out in order to verify how an oriented plasma jet succeeds in prevent boundary layer separation. Both actuators’ chord wise position and plasma jet orientation angle have been investigated to examine which configurations lead to the best results. A particular attention has been paid also to the analysis of results in steady and unsteady plasma actuation. Questa tesi offre un’analisi sperimentale sull’efficacia di attuatori al plasma orientabili, basati su una tecnologia DBD, installati su un profilo alare NACA 0015, a bassi numeri di Reynolds. Le prove sono state condotte in collaborazione con il Dipartimento di Ingegneria Elettrica dell’Università di Bologna, nella galleria del vento del Laboratorio di Aerodinamica Applicata della Facoltà di Ingegneria Aerospaziale di Forlì. Per verificare come un getto orientabile di plasma riesca a prevenire la separazione dello strato limite, sono state eseguite misure sul coefficiente di portanza. Sono state indagate sia la posizione degli attuatori lungo la corda che l’angolo con cui è orientato il getto di plasma, per vedere quali configurazioni conducono ai migliori risultati. Una particolare attenzione è stata riservata all’analisi dei risultati ottenuti con plasma continuo e pulsato.

Funktionelle Analyse der Gliazellwanderung im Drosophila-Embryo

Gliazellen kommen in allen höheren Organismen vor und sind sowohl für die korrekte Entwicklung, als auch für die Funktionalität des adulten Nervensystems unerlässlich. Eine der mannigfachen Funktionen dieses Zelltyps ist die Umhüllung von Axonen im zentralen und peripheren Nervensystem (ZNS und PNS). Um eine vollständige Umhüllung zu gewährleisten, wandern Gliazellen während der Neurogenese zum Teil über enorme Distanzen von ihrem Entstehungsort aus. Dies trifft insbesondere auf die Gliazellen zu, durch deren Membranausläufer die distalen Axonbereiche der peripheren Nerven isoliert werden.rnIn dieser Arbeit wurde die Migration von Gliazellen anhand des Modelorganismus Drosophila untersucht. Ein besonderes Interesse galt dabei der Wanderung einer distinkten Population von Gliazellen, den sogenannten embryonalen Peripheren Gliazellen (ePG). Die ePGs werden überwiegend im sich entwickelnden ventralen Bauchmark geboren und wandern anschließend entlang der peripheren Nerventrakte nach dorsal aus, um diese bis zum Ende der Embryogenese zu umhüllen und dadurch die gliale Blut-Nerv-Schranke zu etablieren. Das Hauptziel dieser Arbeit bestand darin, neue Faktoren bzw. Mechanismen aufzudecken, durch welche die Migration der ePGs reguliert wird. Dazu wurde zunächst der wildtypische Verlauf ihrer Wanderung detailliert analysiert. Es stellte sich heraus, dass in jedem abdominalen Hemisegment eine invariante Anzahl von 12 ePGs von distinkten neuralen Vorläuferzellen generiert wird, die individuelle Identitäten besitzen und mittels molekularer Marker auf Einzelzellebene identifiziert werden können. Basierend auf der charakteristischen Lage der Zellen erfolgte die Etablierung einer neuen, konsistenten Nomenklatur für sämtliche ePGs. Darüber hinaus offenbarten in vivo Migrationsanalysen, dass die Wanderung individueller ePGs stereotyp verläuft und demzufolge weitestgehend prädeterminiert ist. Die genaue Kenntnis der wildtypischen ePG Migration auf Einzelzellebene diente anschließend als Grundlage für detaillierte Mutantenanalysen. Anhand derer konnte für den ebenfalls als molekularen Marker verwendeten Transkriptionsfaktor Castor eine Funktion als zellspezifische Determinante für die korrekte Spezifizierung der ePG6 und ePG8 nachgewiesen werden, dessen Verlust in einem signifikanten Migrationsdefekt dieser beiden ePGs resultiert. Des Weiteren konnte mit Netrin (NetB) der erste diffusible und richtungsweisende Faktor für die Migration von ePGs enthüllt werden, der in Interaktion mit dem Rezeptor Uncoordinated5 speziell die Wanderung der ePG6 und ePG8 leitet. Die von den übrigen Gliazellen unabhängige Navigation der ePG6 und ePG8 belegt, dass zumindest die Migration von Gruppen der ePGs durch unterschiedliche Mechanismen kontrolliert wird, was durch die Resultate der durchgeführten Ablationsexperimente bestätigt wird. rnFerner konnte gezeigt werden, dass während der frühen Gliogenese eine zuvor unbekannte, von Neuroblasten bereitgestellte Netrinquelle an der initialen Wegfindung der Longitudinalen Gliazellen (eine Population Neuropil-assoziierter Gliazellen im ZNS) beteiligt ist. In diesem Kontext erfolgt die Signaldetektion bereits in deren Vorläuferzelle, dem Longitudinalen Glioblasten, zellautonom über den Rezeptor Frazzled. rnFür künftige Mutantenscreens zur Identifizierung weiterer an der Migration der ePGs beteiligter Faktoren stellt die in dieser Arbeit präsentierte detaillierte Beschreibung eine wichtige Grundlage dar. Speziell in Kombination mit den vorgestellten molekularen Markern liefert sie die Voraussetzung dafür, individuelle ePGs auch im mutanten Hintergrund zu erfassen, wodurch selbst subtile Phänotypen überhaupt erst detektiert und auf Einzelzellebene analysiert werden können. Aufgrund der aufgezeigten voneinander unabhängigen Wegfindung, erscheinen Mutantenanalysen ohne derartige Möglichkeiten wenig erfolgversprechend, da Mutationen vermutlich mehrheitlich die Migration einzelner oder weniger ePGs beeinträchtigen. Letzten Endes wird somit die Aussicht verbessert, weitere neuartige Migrationsfaktoren im Modellorganismus Drosophila zu entschlüsseln, die gegebenenfalls bis hin zu höheren Organismen konserviert sind und folglich zum Verständnis der Gliazellwanderung in Vertebraten beitragen.

Mechanistic study of the effects of 8-oxo-7,8-dihydroguanine (8-oxoG) on reporter gene expression in mammalian cells

DNA damage causes replication errors, leading to genetic instability or cell death. Besides that, many types of DNA base modifications have been shown to interfere with transcriptional elongation if they are located in the transcribed DNA strand of active genes, acting as roadblocks for RNA polymerases. It is widely assumed that transcription blockage by endogenous DNA damage is responsible for the early cell senescence in organs and accelerated ageing observed in individuals with compromised nucleotide excision repair.rnThe aims of this work were to design new experimental systems for testing transcription blocking potentials of DNA base modifications in an individual gene and to apply these test systems to the investigation of the effects of a frequent endogenously generated base modification, namely 8-oxo-7,8-hydroxyguanine (8-oxoG), on the gene transcription in cells. Several experimental strategies were employed for this purpose. First, I constructed an episomal vector encoding for a short-lived EGFP-ODC fusion protein and measured expression of the reporter gene in permanently transfected clonal cell lines exposed to DNA damaging agents. Second, the expression of plasmid-borne EGFP gene damaged with photosensitisers to obtain one or several oxidative purine modifications per plasmid molecule was determined in transiently transfected human and mouse host cells in an approach known as “host cell reactivation”. As a prerequisite for these experiments, a robust method of precise quantitative measurement of the EGFP gene expression in transiently transfected cells by flow cytometry was developed and validated. Third, I elaborated a very efficient procedure for insertion of synthetic oligonucleotides carrying 8-oxoG into plasmid DNA, avoiding any unwanted base damage and strand breaks. The consequences of 8-oxoG placed in defined positions in opposing DNA strands of the EGFP gene for transcription were measured by host cell reactivation in cells with functional 8-oxoguanine DNA glycosylase (OGG1) gene and in OGG1 null cells.rnThe results obtained in Ogg1-/- cells demonstrated that unrepaired 8-oxoG, even if situated in the transcribed DNA strand, does not have any negative effect on the reporter gene transcription. On the other hand, as few as one 8-oxoG was sufficient to cause a significant decrease of the gene expression in OGG1-proficient cell lines, i.e. in the presence of base excision repair. For two analysed positions of 8-oxoG in the plasmid DNA, the inhibition of gene transcription by the base modification correlated with the efficiency of its excision by purified OGG1 protein under cell-free conditions. Based on these findings, it has to be concluded that the observed decrease of transcription is mediated by excision of the base modification by OGG1 and probably caused by the repair-induced single-strand breaks. The mechanism of transcription inhibition by 8-oxoG is therefore clearly distinct from stalling of elongating RNA polymerase II complexes at the modified base.

Contributo sperimentale alla ridefinizione della diffusione in parete della camera di prova della galleria del vento Dallara

Joseph Nicolas Cugnot built the first primitive car in 1769 and approximately one hundred year later the first automotive race took place. Thanks to this, for the first time the aerodynamics principles began to be applied to cars. The aerodynamic study of a car is important to improve the performance on the road, or on the track. It purposely enhances the stability in the turns and increases the maximum velocity. However, it is also useful, decrease the fuel consumption, in order to reduce the pollution. Given that cars are a very complex body, the aerodynamic study cannot be conducted following an analytical method, but it is possible, in general, to choose between two different approaches: the numerical or the experimental one. The results of numerical studies depend on the computers’ potential and on the method use to implement the mathematical model. Today, the best way to perform an aerodynamic study is still experimental, which means that in the first phase of the design process the study is performed in a wind tunnel and in later phases directly on track. The automotive wind tunnels are singular mainly due to the test chamber, which typically contains a ground simulation system. The test chamber can have different types of walls: open walls, closed walls, adaptive walls or slotted walls. The best solution is to use the slotted walls because they minimize the interference between the walls and the streamlines, the interaction between the flow and the environment, and also to contain the overall costs. Furthermore, is necessary minimize the boundary layer at the walls, without accelerating the flow, in order to provide the maximum section of homogeneous flow. This thesis aims at redefining the divergent angle of the Dallara Automobili S.P.A. wind tunnel’s walls, in order to improve the overall homogeneity. To perform this study it was necessary to acquire the pressure data of the boundary layer, than it was created the profile of the boundary layer velocity and, to minimize the experimental errors, it was calculated the displacement thickness. The results obtained shows, even if the instrument used to the experiment was not the best one, that the boundary layer thickness could be minor in case of a low diffusion angle. So it is convenient to perform another experiment with a most sensitive instrument to verified what is the better wall configuration.

Dynamics and control issues of multi-rotor platforms

This thesis deals with the analytic study of dynamics of Multi--Rotor Unmanned Aerial Vehicles. It is conceived to give a set of mathematical instruments apt to the theoretical study and design of these flying machines. The entire work is organized in analogy with classical academic texts about airplane flight dynamics. First, the non--linear equations of motion are defined and all the external actions are modeled, with particular attention to rotors aerodynamics. All the equations are provided in a form, and with personal expedients, to be directly exploitable in a simulation environment. This has requited an answer to questions like the trim of such mathematical systems. All the treatment is developed aiming at the description of different multi--rotor configurations. Then, the linearized equations of motion are derived. The computation of the stability and control derivatives of the linear model is carried out. The study of static and dynamic stability characteristics is, thus, addressed, showing the influence of the various geometric and aerodynamic parameters of the machine and in particular of the rotors. All the theoretic results are finally utilized in two interesting cases. One concerns the design of control systems for attitude stabilization. The linear model permits the tuning of linear controllers gains and the non--linear model allows the numerical testing. The other case is the study of the performances of an innovative configuration of quad--rotor aircraft. With the non--linear model the feasibility of maneuvers impossible for a traditional quad--rotor is assessed. The linear model is applied to the controllability analysis of such an aircraft in case of actuator block.

Testing of subgrid scale (SGS) models for large-eddy simulation (LES) of turbulent channel flow

Sub-grid scale (SGS) models are required in order to model the influence of the unresolved small scales on the resolved scales in large-eddy simulations (LES), the flow at the smallest scales of turbulence. In the following work two SGS models are presented and deeply analyzed in terms of accuracy through several LESs with different spatial resolutions, i.e. grid spacings. The first part of this thesis focuses on the basic theory of turbulence, the governing equations of fluid dynamics and their adaptation to LES. Furthermore, two important SGS models are presented: one is the Dynamic eddy-viscosity model (DEVM), developed by \cite{germano1991dynamic}, while the other is the Explicit Algebraic SGS model (EASSM), by \cite{marstorp2009explicit}. In addition, some details about the implementation of the EASSM in a Pseudo-Spectral Navier-Stokes code \cite{chevalier2007simson} are presented. The performance of the two aforementioned models will be investigated in the following chapters, by means of LES of a channel flow, with friction Reynolds numbers $Re_\tau=590$ up to $Re_\tau=5200$, with relatively coarse resolutions. Data from each simulation will be compared to baseline DNS data. Results have shown that, in contrast to the DEVM, the EASSM has promising potentials for flow predictions at high friction Reynolds numbers: the higher the friction Reynolds number is the better the EASSM will behave and the worse the performances of the DEVM will be. The better performance of the EASSM is contributed to the ability to capture flow anisotropy at the small scales through a correct formulation for the SGS stresses. Moreover, a considerable reduction in the required computational resources can be achieved using the EASSM compared to DEVM. Therefore, the EASSM combines accuracy and computational efficiency, implying that it has a clear potential for industrial CFD usage.