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Impact of geometry on spray combustion in an enclosure

机译:几何形状对外壳喷射燃烧的影响

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The objective of this work was to study an effect of the combustion chamber geometry/length on characteristics of a spray flame such as its shape, height, and structure along with the flow field parameters. The study was aimed at assisting andoptimizing the design process of the combustion chamber. Chemically reactive computational fluid dynamics (CFD) modeling was applied to predicting the impact of geometry, as a tool for these studies. The CFD computer code used to predict the industrialspray combustion process, was originally developed for the aerospace engineering applications. The code numerical method utilizes, among others, unique third order of accuracy spatial approximations, a second order of accuracy temporal approximation, andthe pressure implicit with splitting of operators (PISO) approach, which makes the solution convergent and exceptionally stable and efficient. A series of numerical tests was performed to identify the most efficient numerical procedure out of a suite ofnumerical approaches. Based on the spray combustion predictions, it has been found that the chamber length/height has a significant impact on the flame penetration/length, and some influence on the spray structure in the initial section, due to theaerodynamic suction effect of the chamber exhaust.
机译:这项工作的目的是研究燃烧室几何/长度对喷雾火焰的特性的影响,例如其形状,高度和结构以及流场参数。该研究旨在协助和迭代燃烧室的设计方法。将化学反应性计算流体动力学(CFD)建模应用于预测几何形状的影响,作为这些研究的工具。用于预测IndustriondsPray燃烧过程的CFD计算机代码最初是为航空航天工程应用开发的。代码数值方法在其外,具有精度空间近似的独特的三阶,准确度时间近似的二阶阶数,以及拆分操作者(PISO)方法的压力隐含,这使得解决方案会聚和特别稳定和高效。进行一系列数值测试以识别出在套房套件中的最有效的数值程序。基于喷雾燃烧预测,已经发现腔室长度/高度对火焰穿透/长度具有显着影响,并且由于腔室排气的术后动力学抽吸效果,对初始部分的喷雾结构产生一些影响。

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