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Extensive measurements using hot-wire anemometry were carried out for single jet, tandem jets, and side-by-side jets for a velocity ratio of 2, and a jet spacing of 4 for the latter two cases. The measurements yielded axial mean velocity, turbulence intensities, and Reynolds stresses for four downstream stations for the single jet and two downstream stations for the double jet. A preliminary study of the one-dimensional frequency spectra and flow visualization using a tuft wire were also performed. An analytical study using a momentum-integral approach was also carried out in order to predict the gross jet properties such as the jet trajectories, the jet growth, and the mean jet velocity and the mean jet temperature. The jets showed considerable influence on each other for the jet spacing of four jet diameters. An upward shift of the merged jet trajectory, and a widening of the jet crosssection in both directions for the tandem jets as compared to the single jet, were observed. Good correlation between the mean velocity gradients and Reynolds shear stresses were found to exist. The detailed flow structure was found to be very similar for the single jet and tandem jet cases for the downstream stations. The distribution of the one-dimensional energy spectra showed spatial and/or configurational dependence; however, no discernible variation of the frequency corresponding to the peak energy was observed. The flow visualization study showed the existence of circulatory flow in the cross-planes. The analytical study gave results which agreed very well with experimental data. / Ph. D.

published_or_final_version / Mechanical Engineering / Doctoral / Doctor of Philosophy

We have surveyed 84 Class 0, Class I, and flat-spectrum protostars in mid-infrared [Si II], [Fe II], and [S I] line emission, and 11 of these in far-infrared [O I] emission. We use the results to derive their mass. outflow rates, (M) over dot(w). Thereby we observe a strong correlation of (M) over dot(w) with bolometric luminosity, and with the inferred mass accretion rates of the central objects, (M) over dot(a), which continues through the Class 0 range the trend observed in Class II young stellar objects. Along this trend from large to small mass. flow rates, the different classes of young stellar objects lie in the sequence Class 0-Class I/flat-spectrum-Class II, indicating that the trend is an evolutionary sequence in which (M) over dot(a) and (M) over dot(w) decrease together with increasing age, while maintaining rough proportionality. The survey results include two that. are key tests of magnetocentrifugal outflow-acceleration mechanisms: the distribution of the outflow/accretion branching ratio b = (M) over dot(w)/(M) over dot(a), and limits on the distribution of outflow speeds. Neither rules out any of the three leading outflow-acceleration, angular-momentum-ejection mechanisms, but they provide some evidence that disk winds and accretion-powered stellar winds (APSWs) operate in many protostars. An upper edge observed in the branching-ratio distribution is consistent with the upper bound of b = 0.6 found in models of APSWs, and a large fraction (31%) of the sample have a. branching ratio sufficiently small that only disk winds, launched on scales as large as several au, have been demonstrated to account for them.

In this thesis the jet energy scale uncertainty of small and large radius jets at the ATLAS detector is evaluated in-situ using gamma-jet events. The well calibrated photon in the gamma-jet events is used to probe the energy scale of the jets. The studies of the jet energy scale of small radius jets are performed using 4.7 fb^-1 of data collected at sqrt{s} = 7 TeV in 2011. The gamma-jet methods which were developed are then adapted and applied to large radius jets, using 20.3 fb^-1 of data collected at sqrt{s} = 8 TeV in 2012. The new jet energy scale uncertainties are found to be ~1 % for |eta| < 0.8, rising to 2-3 % for |eta| > 0.8. These uncertainties are significantly lower than the 3-6 % precision which has previously been achieved at ATLAS using track jets as a reference object. Due to the increase in precision, uncertainties due to pile-up and the topology of the jet also had to be evaluated. The total energy scale uncertainties for large radius jets are reduced by ~1-2 % (0.5-1 %) for |eta| < 0.8 (> 0.8). This reduction will be beneficial to analyses using large radius jets and it is specifically shown to benefit the t-tbar resonance search in the semi-leptonic channel. The t-tbar search looks for events with two top quarks in the final state, where one decays leptonically and the other hadronically. The hadronically decaying top quark is reconstructed using a large radius jet, and the jet energy scale uncertainty is a dominant source of uncertainty in the analysis. In addition to the studies of the jet energy scale of large radius jets, the first derivation of a calibration, and jet energy scale uncertainties derived with gamma-jet events, are shown for Variable R jets. The Variable R jet algorithm is a new type of jet algorithm with a radius that is inversely proportional to the size of the jet, making it useful for the study of high momentum top quarks. It is shown that similar methods can be used to calibrate and assess the uncertainties of Variable R jets as are used for standard, fixed radius jets at the ATLAS detector, although some adaptations will be necessary. The studies provide a basis for the calibration of Variable R jets in the future.

Cette thèse est consacrée à l'étude des propriétés aéroacoustiques de jets supersoniques impactant une paroi par simulation des grandes échelles. Ces simulations sont réalisées à partir des équations de Navier-Stokes 3-D instationnaires compressibles exprimées pour des coordonnées cartésiennes ou cylindriques. Afin de résoudre ces équations, des schémas numériques de différenciation spatiale et d'intégration temporelle peu dispersifs et peu dissipatifs sont utilisés. Les écoulements étudiés étant supersoniques, une procédure de capture de choc est également implémentée afin de supprimer les oscillations de Gibbs de part et d'autre des chocs.Dans un premier temps, un jet rond libre et quatre jets ronds impactant une paroi avec un angle de 90 degrés sont simulés sur des maillages cylindriques. Ces jets sont supersoniques, sous-détendus, et sont caractérisés par un nombre de Reynolds calculé à partir du diamètre du jet de Re=60.000, et par un nombre de Mach parfaitement détendu de Mj=1.56. Les résultats du jet libre sont tout d'abord présentés. Ils sont comparés aux résultats de plusieurs études expérimentales et de modèles afin de valider l'approche numérique utilisée. Notamment, les différentes composantes acoustiques spécifiques aux jets sous-détendus comme le bruit de choc large-bande et le bruit de screech sont observées et analysées. Les résultats obtenus pour les quatre jets impactant une paroi sont ensuite examinés. Dans ce cas, la présence d'une boucle de rétroaction aéroacoustique entre les lèvres de la buse et la paroi est montrée. Pour finir, le comportement aérodynamique et aéroacoustique des jets est étudié, et comparé à différentes études numériques et expérimentales de la littérature. Quatre jets plans supersoniques idéalement détendus impactant une paroi avec un angle de 90 degrés sont ensuite calculés. Ils ont un nombre de Reynolds évalué à partir de la hauteur de la buse de Re=50.000 et un nombre de Mach de Mj=1.28. Une boucle de rétroaction aéroacoustique entre la buse et la paroi est de nouveau mise en évidence. Une combinaison de modèles associant un modèle d'onde stationnaire aérodynamique-acoustique et un modèle de stabilité de jet plan 2-D avec des couches de mélange infiniment minces est alors proposée. Ce modèle permet de déterminer à la fois les fréquences les plus probables de la boucle de rétroaction aéroacoustique et leurs natures plane ou sinueuse.Enfin, les simulations de deux jets plans supersoniques impactant une paroi avec des angles de 60 et 75 degrés sont réalisées grâce à l'utilisation de deux maillages cartésiens, par une méthode de recouvrement de maillages. Les modifications des propriétés de la boucle de rétroaction aéroacoustique lorsque l'angle d'impact dévie de 90 degrés sont ainsi étudiées. / In this PhD work, supersonic impinging jets are simulated using large-eddy simulation in order to investigate their aerodynamic and acoustic fields. In practice, the unsteady compressible Navier-Stokes equations are solved on Cartesian or cylindrical meshes. Low-dissipation and low-dispersion numerical methods are used for spatial differentiation and time integration. As the jets are supersonic, a shock-capturing filtering is also applied in order to avoid Gibbs oscillations near shocks.A free round jet and four round jets impinging normally on a flat plate are first simulated on cylindrical meshes. They are underexpanded, and have a Reynolds number based on the nozzle diameter of Re=60.000 and a fully expanded Mach number of Mj=1.56. The results for the free jet are first presented. They are compared with experimental results and predictions given by models in order to validate the numerical setup. Acoustic components specific to underexpanded jets such as broadband shock-associated noise and screech noise are obtained. The results for the four impinging jets are then examined. An aeroacoustic feedback mechanism establishing between the nozzle lips and the flat plate is found to generate tones. Finally, the flow and acoustic properties of the jets are studied and compared with numerical and experimental data.Four ideally expanded jets impinging normally on a flat plate are then simulated. They have a Reynolds number based on the nozzle height of Re=50.000 and a Mach number of Mj=1.28. An aeroacoustic feedback mechanism is again observed between the nozzle lips and the flat plate. A combination of models based on an aeroacoustic feedback model and a vortex sheet model of the jet is then proposed. The model appears able to predict the most likely tone frequencies of the feedback mechanism, and the symmetric or antisymmetric nature of the corresponding jet oscillation.Finally, two ideally expanded jets impinging on a flat plate with angles between the jet direction and the plate of 60 and 75 degrees are simulated using two Cartesian meshes. The effects of the angle of impact on the properties of the aeroacoustic feedback mechanism are finally studied.

Cette thèse est une contribution expérimentale à l’étude des résonances aéroacoustiques des jets sous-détendus : le Screech. Diverses méthodes expérimentales sont utilisées à ces fins, telles que la mesure de pression acoustique, la strioscopie et Vélocimétrie par Image des Particules, et associées à des techniques classiques de post-traitement comme les décompositions en mode de Fourier et aux valeurs propres. Ces Techniques permettent d’évaluer les effets d’épaisseur de la lèvre de la buse sur l’écoulement, et fournissent des informations sur les différences de comportement d’un même jet montrant des modes oscillatoires différents. Enfin, on entreprend d’étudier la présence de divers mécanismes de fermeture de la boucle de résonance pour divers modes de screech. La présence d’ondes intrinsèques du jet, se propageant vers l’aval pour les modes axisymétrique (A2) et hélicoïdal (C) suggèrent que ces ondes puissent jouer un rôle dans la résonance. La signature de ces ondes n’est en revanche pas attestée pour les modes battants (B). Ces résultats semblent donc indiquer que plusieurs mécanismes de rétroaction différents puissent être à l’oeuvre dans la résonance du jet sous-détendus. / This work provides an experimental contribution to the study of the Screech phenomenon. Various experimental techniques such as microphones array, Schlieren and Particle Image Velocimetry (PIV) together with advanced post-processing techniques like azimuthal Fourier decomposition and Proper Orthogonal Decomposition (POD) are employed. These techniques enable the evaluation of the lip thickness effects on the jets generated by two different round nozzles. The differences on the flow aerodynamics and acoustics are discussed. Then, we carry out experiments to analyse the effects of the different dominant Screech modes (B and C) on the flow characteristics. No noticeable differences are found in the mean fields. However, the fluctuation fields shows the contrary: B mode has larger fluctuation. In the last part, we investigate the Screech closure mechanism. The signature of upstream jet waves is revealed in the axisymmetric (A2) and helical (C) mode. However, the mode B does not present evidence of this instability in the flow, indicating that its closure mechanism may be bonded to another kind of waves. The conclusion from the results is that the Screech phenomenon seems be driven by different closure mechanisms.

Esta tese objetiva caracterizar o escoamento provocado pela incidência de um jato vertical em um fundo plano, descrevendo assim as características médias e flutuantes das pressões a partir da investigação experimental. O modelo utilizado é composto por um jato retangular posicionado, perpendicularmente, a uma distância de 0,92 m do fundo plano de um canal. Utilizando transdutores de pressão instalados na posição de incidência do jato, adquiriu-se os valores de pressão “instantânea” a uma frequência de 128 Hz durante 10 minutos. Foram ensaiadas cinco (5) vazões: 25 l/s (Fr1 = 7,12), 30 l/s (Fr1 = 8,51), 36,6 l/s (Fr1 = 10,35), 42,7 l/s (Fr1 = 12,12) e 50l/s (Fr1 = 14,23), além de vinte (20) diferentes espessuras de colchão d'água. Com os dados de pressão, efetuou-se análises no domínio do tempo, da frequência e da posição. No domínio do tempo, analisou-se a variação dos parâmetros estatísticos essenciais (média, desvio padrão, assimetria e curtose) bem como a identificação de valores máximo e mínimos das pressões. No domínio da frequência, procurou-se avaliar por meio da análise espectral a identificação de frequências significativas associadas à energia macroturbulenta. No que tange à análise no domínio da posição buscou-se analisar a faixa de influência do jato junto ao fundo, a região de subpressões e o alcance das pressões dinâmicas. Outro aspecto importante abordado é a apresentação dos resultados em gráficos adimensionalizados, o que confere ao estudo um caráter geral dentro da faixa de valores ensaiados. Os resultados definem um colchão mínimo de água da ordem de 3 vezes a altura crítica do escoamento, para o amortecimento das pressões dinâmicas. A análise dos momentos estatísticos demonstra que a distribuição das pressões não segue a distribuição normal. Dentro disso, estão disponibilizados coeficientes estatísticos de probabilidade para a determinação das pressões extremas. Ainda, estão definidas quatro zonas a jusante do impacto do jato: Zona I - região do impacto, Zona II - reflexão do jato, Zona III - Acomodação do escoamento e por fim, a Zona IV - caracterizada pelo fim da influência do jato. Além disso, uma análise deste escoamento sob a perspectiva da formação de um ressalto hidráulico é realizada, indicando que apenas os parâmetros utilizados, não descrevem o escoamento como tal. Esta tese é produto da parceria entre Laboratório de Obras Hidráulicas do Instituto de Pesquisas Hidráulicas da Universidade Federal do Rio Grande do Sul (LOH/IPH/UFRGS) e o Laboratório de Hidráulica Experimental e Recursos Hídricos de Furnas Centrais Elétricas S. A. (LAHE/FURNAS). / This thesis aims to characterize the flow prompted by the incidence of a vertical jet on a flat bottom, thus describing the mean and floating characteristics of the pressures from the experimental investigation. The model used is comprised of a rectangular jet positioned perpendicularly at a distance of 0.92 m from the flat bottom of a channel. Using pressure transducers installed in the jet incidence position, the "instantaneous" pressure values were acquired at a frequency of 128 Hz for 10 minutes. Five (5) discharges were tested: 25 l/s (Fr1 = 7.12), 30 l/s (Fr1 = 8.51), 36.6 l/s (Fr1 = 10.35), 42.7 l/s (Fr1 = 12.12) and 50 1/s (Fr1 = 14.23), as well as twenty (20) different waterbed thicknesses. The pressure data were analyzed in terms of time, frequency and position domains. In the time domain, the variation of the essential statistical parameters (mean, standard deviation, asymmetry and kurtosis) was analyzed, as well as the identification of maximum and minimum pressure values. In the frequency domain, it was sought to assess, by means of the spectral analysis, the identification of significant frequencies associated with macroturbulent energy. Regarding the analysis in the position domain, this study aimed to analyze the range of influence of the jet near the bottom, the region of subpressions and the reach of the dynamic pressures. Another important aspect is the presentation of the results in dimensionless graphs, which grants the study a general character within the range of values tested. The results define a minimum waterbed of the order of 3 times the critical height of the flow for the damping of the dynamic pressures. Statistical moments analysis shows that the distribution of pressures does not follow the normal distribution. Therein, probability statistical coefficients are available for the determination of extreme pressures. Also, four zones are defined downstream of the impact of the jet: Zone I - region of impact, Zone II - reflection of the jet, Zone III - accommodation of the flow and, finally, Zone IV - characterized by the end of the influence of the jet. Furthermore, an analysis of this flow from the perspective of the formation of a hydraulic jump is conducted, indicating that the parameters used alone do not describe the flow as such. This thesis is a product of the partnership between the Hydraulic Works Laboratory of the Hydraulic Research Institute of the Federal University of Rio Grande do Sul (LOH/IPH/UFRGS) and the Laboratory of Experimental Hydraulics and Hydraulic Resources of Furnas Centrais Elétricas SA (LAHE/FURNAS).

Dans cette thèse la mesure du rapport des sections efficaces de production de bosons W et Z en association avec un jet au LHC est effectuée.Le rapport des sections efficaces est mesuré à l'aide des données issues de collisions proton-proton au LHC à une énergie dans le centre de masse de 7 TeV, recueillies par l'expérience ATLAS en 2010, correspondant à une luminosité intégrée d'environ 40 pb-1. L'analyse est effectuée à l’aide de bosons W et Z se désintégrant dans le canal muon.Il s'agit de la première mesure du rapport des taux de production de bosons W et Z associés à un jet réalisée à une si haute énergie dans le centre de masse, la mesure est la également la première effectuée au LHC. Cette mesure constitue un test très important des calculs théoriques perturbatifs et tire avantage des annulations partielles ou totales de diverses incertitudes expérimentales.La mesure sert aussi pour les recherches de nouveaux phénomènes de physique au LHC à contraindre les bruits de fonds ayant les mêmes signatures topologiques.La valeur du rapport de mesuré est présentée en fonction de différents seuils d’impulsion transverse de jet cumulatifs et est trouvé, a l’intérieur de la précision statistique, en bon accord avec prédictions pertubatives de QCD aux LO et NLO. / In this thesis an investigation of the ratio of the production cross section of W and Z bosons in association with one jet at LHC is performed.The cross-section ratio is measured with LHC proton-proton collision data at a center-of-mass energy of 7 TeV, collected by the ATLAS experiment in 2010, corresponding to an integrated luminosity of approximately 40 pb-1. The analysis is performed selecting W and Z bosons decaying in the muon channel.It is the first time the ratio of W and Z bosons production associated with one jet is measured at such a high center-of-mass energy, the measurement is the first one at the LHC. This measurement constitutes a very important test of perturbative theoretical calculations based on the advantage of the partial and full cancellations of various uncertainties.It also serves as constraining backgrounds with similar topological signatures in the search for new physics phenomena at the LHC. The measured ratio value is presented as a function of cumulative jet transverse momentum thresholds and found, within statistical precision, to agree well with perturbative LO and NLO QCD predictions.

La recherche du boson de Higgs ainsi que celle de nouvelle physique auprès du LHC requiert une excellente compréhension des processus du Modèle Standard du fait de leurs signatures expérimentales similaires. La capacité de mesurer le plus précisément possible l'énergie des objets reconstruits dans les détecteurs est par ailleurs primordiale à la fois pour effectuer des mesures de précision et pour accroître la sensibilité des analyses à des signaux de physique au-delà du Modèle Standard. Les travaux présentés dans cette thèse s'attachent à ces deux points par l'étude d'événements contenant un ou plusieurs jets associés à un boson Z avec le détecteur ATLAS. D'une part, ces événements sont utilisés pour améliorer la calibration en énergie des jets de faible impulsion transverse, d'une importance capitale pour les analyses utilisant le dénombrement de jets ou leur veto. D'autre part la section efficace différentielle de production de ces événements est mesurée en fonction de nombreuses observables et comparée à diverses prédictions théoriques. Ces mesures pourront être utilisées pour améliorer les prédictions qui servent de modèles de bruit de fond dans des analyses sur le boson de Higgs et de recherche de physique au-delà du Modèle Standard.