Orientador: Wei-Liang Qian / Resumo: O sucesso da descrição hidrodinâmica das colisões de íons pesados relativísticos desempenha um papel vital para entender as propriedades da matéria QCD. A essência da evolução hidrodinâmica, em geral, foi atribuída à resposta dinâmica às condições iniciais flutuantes. Em particular, as características observadas nas correlações de duas partículas, referidas como ``cume'' e ``ombro'', mostraram ser reproduzidas com sucesso por simulações hidrodinâmicas com condições iniciais flutuantes evento a evento, mas não por condições iniciais médias. Posteriormente, leva ao entendimento atual, através de extensos estudos de análise hidrodinâmica/transporte baseada em eventos por eventos, que as correlações de duas partículas para o momento transversal inferior podem ser interpretadas principalmente em termos de harmônicos de fluxo $ v_n $. Notavelmente, o fluxo triangular, $ v_3 $, é atribuído principalmente à aparência da estrutura do ``ombro'' no lado externo da partícula acionadora. Além disso, entende-se que esses coeficientes harmônicos estão intimamente associados aos correspondentes $ \varepsilon_n $, as anisotropias da distribuição inicial de energia. No entanto, a linearidade entre $ v_n $ e $ \varepsilon_n $ se torna menos evidente para harmônicos maiores que $ n = 2 $. Isso sugere que as próprias flutuações de evento a evento carregam informações importantes, além da linearidade observada. Se alguém se restringe apenas à análise das relações/correlações médias de eventos entr... (Resumo completo, clicar acesso eletrônico abaixo) / Doutor

This thesis aims at improving our knowledge on swirl combustors. The work presented here is based on Large Eddy Simulations (LES) coupled to an advanced combustion model: the Conditional Moment Closure (CMC). Numerical predictions have been systematically compared and validated with detailed experimental datasets. In order to analyze further the physics underlying the large numerical datasets, Proper Orthogonal Decomposition (POD) has also been used throughout the thesis. Various aspects of the aerodynamics of swirling flames are investigated, such as precession or vortex formation caused by flow oscillations, as well as various combustion aspects such as localized extinctions and flame lift-off. All the above affect flame stabilization in different ways and are explored through focused simulations. The first study investigates isothermal air flows behind an enclosed bluff body, with the incoming flow being pulsated. These flows have strong similarities to flows found in combustors experiencing self-excited oscillations and can therefore be considered as canonical problems. At high enough forcing frequencies, double ring vortices are shed from the air pipe exit. Various harmonics of the pulsating frequency are observed in the spectra and their relation with the vortex shedding is investigated through POD. The second study explores the structure of the Delft III piloted turbulent non-premixed flame. The simple configuration allows to analyze further key combustion aspects of combustors, with further insights provided on the dynamics of localized extinctions and re-ignition, as well as the pollutants emissions. The third study presents a comprehensive analysis of the aerodynamics of swirl flows based on the TECFLAM confined non-premixed S09c configuration. A periodic component inside the air inlet pipe and around the central bluff body is observed, for both the inert and reactive flows. POD shows that these flow oscillations are due to single and double helical vortices, similar to Precessing Vortex Cores (PVC), that develop inside the air inlet pipe and whose axes rotate around the burner. The combustion process is found to affect the swirl flow aerodynamics. Finally, the fourth study investigates the TECFLAM configuration again, but here attention is given to the flame lift-off evident in experiments and reproduced by the LES-CMC formulation. The stabilization process and the pollutants emission of the flame are investigated in detail.