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Turbulent premixed propane/air and methane/air flames were studied using planar Rayleigh scattering and particle image velocimetry on a stabilized Bunsen type burner. The fuel-air equivalence ratio was varied from Φ=0.7 to 1.0 for propane flames, and from Φ=0.6 to 1.0 for methane flames. The non-dimensional turbulence intensity, u'/SL (ratio of fluctuation velocity to laminar burning velocity), covered the range from 3 to 24, equivalent to conditions of corrugated flamelets and thin reaction zones regimes. Temperature gradients decreased with the increasing u'/SL and levelled off beyond u'/SL > 10 for both propane and methane flames. Flame front thickness increased slightly as u'/SL increased for both mixtures, although the thickness increase was more noticeable for propane flames, which meant the thermal flame front structure was being thickened. A zone of higher temperature was observed on the average temperature profile in the preheat zone of the flame front as well as some instantaneous temperature profiles at the highest u'/SL. Curvature probability density functions were similar to the Gaussian distribution at all u'/SL for both mixtures and for all the flame sections. The mean curvature values decreased as a function of u'/SL and approached zero. Flame front thickness was smaller when evaluated at flame front locations with zero curvature than that with curvature. Temperature gradients and FSD were larger when the flame curvature was zero. The combined thickness and FSD data suggest that the curvature effect is more dominant than that of the stretch by turbulent eddies during flame propagation. Integrated flame surface density for both propane and methane flames exhibited no dependance on u'/SL regardless of the FSD method used for evaluation. This observation implies that flame surface area may not be the dominant factor in increasing the turbulent burning velocity and the flamelet assumption may not be valid under the conditions studied. Dκ term, the product of diffusivity evaluated at conditions studied and the flame front curvature, was a magnitude smaller than or the same magnitude as the laminar burning velocity.

Turbulent premixed propane/air and methane/air flames were studied using planar Rayleigh scattering and particle image velocimetry on a stabilized Bunsen type burner. The fuel-air equivalence ratio was varied from Φ=0.7 to 1.0 for propane flames, and from Φ=0.6 to 1.0 for methane flames. The non-dimensional turbulence intensity, u'/SL (ratio of fluctuation velocity to laminar burning velocity), covered the range from 3 to 24, equivalent to conditions of corrugated flamelets and thin reaction zones regimes. Temperature gradients decreased with the increasing u'/SL and levelled off beyond u'/SL > 10 for both propane and methane flames. Flame front thickness increased slightly as u'/SL increased for both mixtures, although the thickness increase was more noticeable for propane flames, which meant the thermal flame front structure was being thickened. A zone of higher temperature was observed on the average temperature profile in the preheat zone of the flame front as well as some instantaneous temperature profiles at the highest u'/SL. Curvature probability density functions were similar to the Gaussian distribution at all u'/SL for both mixtures and for all the flame sections. The mean curvature values decreased as a function of u'/SL and approached zero. Flame front thickness was smaller when evaluated at flame front locations with zero curvature than that with curvature. Temperature gradients and FSD were larger when the flame curvature was zero. The combined thickness and FSD data suggest that the curvature effect is more dominant than that of the stretch by turbulent eddies during flame propagation. Integrated flame surface density for both propane and methane flames exhibited no dependance on u'/SL regardless of the FSD method used for evaluation. This observation implies that flame surface area may not be the dominant factor in increasing the turbulent burning velocity and the flamelet assumption may not be valid under the conditions studied. Dκ term, the product of diffusivity evaluated at conditions studied and the flame front curvature, was a magnitude smaller than or the same magnitude as the laminar burning velocity.

[pt] O presente trabalho apresenta um estudo numérico da transferência de energia por radiação e sua interação com as propriedades radiantes cinzas e espectrais dos gases produtos da combustão e da fuligem que são formados em um processo de combustão turbulenta. Assim, utilizam-se sistemas de forno/- queimador que operam em regime de chama não pré-misturada de maneira a avaliar, através da dinâmica dos fluidos computacional (CFD), a influência que exercem os diversos modelos de propriedades radiantes sobre a representação da termoquímica do escoamento reativo. Com o objetivo de identificar as principais características e deficiências que apresentam cada um destes modelos, foram considerados dois cenários. O primeiro, correspondente a um problema de radiação unidimensional de um sistema homogêneo e não isotérmico onde são estudados, modelos de propriedades radiantes (i) disponíveis em um software comercial de CFD e (ii) aqueles que foram implementados neste trabalho. Além disso, foi empregado um código numérico que determina as propriedades radiantes espectrais de gases produtos da combustão e da fuligem através de uma abordagem de banda estreita. Para este fim, este código foi acoplado com o software de CFD. Em seguida, dois queimadores de porte laboratorial são empregados de forma a avaliar a capacidade preditiva dos modelos de propriedades radiantes: o primeiro queima propano gasoso e ar enriquecido com oxigênio e o segundo utiliza querosene líquido e oxigênio como reagentes. Dados experimentais de fluxo de calor radiante e de fração volumétrica da fuligem são utilizados para comparação com os resultados obtidos da simulação. Para ambas as configurações de queimador foi também estudado o modelo de Moss-Brookes para previsão da formação/consumo da fuligem. Os resultados obtidos demonstraram o bom desempenho da maioria dos modelos de propriedades radiantes estudados. Em particular, a abordagem de banda estreita foi o que melhor previu a radiação térmica. Além disso, a sua utilização com o modelo de Moss-Brookes levou à melhor previsão da fração volumétrica da fuligem. / [en] This work presents a numerical study of radiation heat transfer and its interaction with gray and spectral radiation of combustion products and soot that are formed in a turbulent combustion process. Different burner/furnace systems operating in a non-premixed combustion regime were used in order to evaluate, through computational fluid dynamics (CFD), the influence of several radiant properties models. Aiming to identify the key features and shortcomings that exhibit each of these models, two scenarios were considered. The first corresponds to a 1-D radiation problem where radiative properties models of a homogeneous non isothermal system are studied as (i) available CFD commercial software and (ii) those implemented in this work. Moreover, a numerical code was used in order to determine, through a narrow band approach, the spectral radiative properties of soot and combustion products. For this purpose, this code was coupled with the CFD software. Then, two laboratory-scale burners are used to assess the predictive capacity of radiative properties models: the first, burning propane and enriched air oxygen, and the second uses kerosene and oxygen as reactants. Measurements of radiant heat flux and soot volumetric fraction are used for comparison with simulation results. For both configurations, the performance of the Moss-Brookes model for predicting the soot production was also studied. The results of this study demonstrated the good performance of the majority of the radiant properties models studied. Particularly, the narrow band approach was the model that provided the best thermal radiation prediction. Moreover, the combination of the narrow band approach with the Moss-Brookes model lead to the best prediction of soot volume fraction.