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Droplet interactions during combustion of unsupported droplet clusters in microgravity: Numerical study of droplet interactions at low Reynolds number.

机译:无重力液滴簇在微重力中燃烧过程中的液滴相互作用:低雷诺数下液滴相互作用的数值研究。

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The present work developed a numerical model to study the combustion of well-characterized drop clusters in microgravity environment using direct numerical simulation by the means of Fire Dynamic Simulator---a CFD model of fire-driven fluid flow. The computational research investigated the combustion of clusters of droplets of different sized and asymmetric three-dimensional configurations in zero gravity environments for zero relative Reynolds numbers. One of the aspects studied is droplet interaction during evaporation and combustion over the lifetime of the droplet. The model developed accounts for variable gas-phase thermophysical properties, unity Lewis number, Stefan velocities and includes the gas-phase radiative transfer (solved by a finite volume method) for finite rate reaction. Mass burning rates are calculated for each droplet in an array and compared to mass burning rate of similar single droplet, the ratio of these two being a correction factor eta. Single droplet combustion has been studied to evaluate and validate the model output. It was found that single droplet combustion does follow the d2-law, mass burning rates being in excellent qualitative agreement with current theories and experimental data. Direct numerical results of multiple droplet combustion were obtained and compared with a point source method as well as with experimental and numerical models developed in the past. Data obtained with proposed method provided results consistent with and in qualitative agreement with multiple droplets combustion theories and experimental investigations. Quantitatively, the numerical model results were in the range of 85% to 95% of the results provided by the investigations found in the literature for droplet array combustion models and in the range of 85% to 90% when compared with single droplet combustion models.; The numerical simulation along with the future proposed experiment described in the project is a unique combination of investigative methods that will provide support for future investigations and for understanding of droplet interaction phenomena.
机译:本工作开发了一个数值模型,以利用火动力仿真器(一种由火驱动的流体流动的CFD模型)进行直接数值模拟,研究在微重力环境下特性良好的液滴团簇的燃烧。计算研究针对零相对雷诺数在零重力环境下研究了不同尺寸和非对称三维构型的液滴簇的燃烧。研究的方面之一是在液滴的整个生命周期内在蒸发和燃烧过程中的液滴相互作用。开发的模型考虑了可变的气相热物理性质,统一的Lewis数,Stefan速度,并包括了用于有限速率反应的气相辐射传递(通过有限体积法求解)。计算阵列中每个液滴的质量燃烧速率,并将其与相似的单个液滴的质量燃烧速率进行比较,二者之比为校正因子eta。已经研究了单滴燃烧以评估和验证模型输出。发现单滴燃烧确实遵循d2-定律,质量燃烧速率与当前理论和实验数据具有极好的定性一致性。获得了多滴燃烧的直接数值结果,并将其与点源方法以及过去开发的实验和数值模型进行了比较。用所提出的方法获得的数据提供的结果与多滴燃烧理论和实验研究相吻合,并且在质量上与之吻合。定量地,数值模型结果在液滴阵列燃烧模型的文献中提供的调查结果的85%至95%范围内,而与单液滴燃烧模型相比则在85%至90%的范围内。 ;该项目中描述的数值模拟以及未来拟议的实验是研究方法的独特组合,将为将来的研究和理解液滴相互作用现象提供支持。

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