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Unsteady RANS for Simulation of High Swirling Non-Premixed Methane-Air Flame

机译:用于高涡旋非预混甲烷空气火焰模拟的非稳态RANS

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Highly swirled non-premixed methane-air combustion is studied using Unsteady RANS. The increased CPU power at present times makes RANS solutions a viable design methodology for industrial applications. LES, Large Eddy Simulation, is still a bit far away from being the routine approach as a design tool in industry. The confined non-premixed TECFLAM S09C flame is investigated because of its similarity with gas turbine engine combustors. A block structured hexahedral computational mesh is used for the whole domain for higher numerical accuracy. A first-order accurate Euler Implicit technique is used for the temporal discretization of the transient terms. Realizable k-c turbulence model is employed in order to account for the turbulent flow effects on the flow field and chemical reactions. Results of fast and two step reactions are compared with finite rate chemistry. Results show that, the best solution is obtained by using Finite Rate Eddy Dissipation Model. The infinitely fast chemistry approach is not capable of predicting the reaction delay that is clearly observed in the experiments. Instead, the fast chemistry approach show reaction zones in the close vicinity of the swirler where the fuel-air mixing is not well achieved for the reactions to take place in such a short distance. The flow field is directly affected by the heat release rate that is determined by the fuel air mixing and combustion model.
机译:使用非稳态RANS研究了高度涡旋的非预混合甲烷-空气燃烧。目前,不断增强的CPU能力使RANS解决方案成为工业应用的可行设计方法。 LES(大型涡流仿真)与作为工业设计工具的常规方法相比还有一段距离。研究了密闭的非预混TECFLAM S09C火焰,因为它与燃气轮机燃烧室相似。块结构的六面体计算网格用于整个域,以实现更高的数值精度。一阶精确的Euler隐式技术用于瞬时项的时间离散化。为了解决湍流对流场和化学反应的影响,采用了可实现的k-c湍流模型。快速反应和两步反应的结果与有限速率化学进行了比较。结果表明,采用有限速率涡流耗散模型可获得最佳解。无限快速的化学方法无法预测在实验中清楚观察到的反应延迟。相反,快速化学方法显示出旋流器附近的反应区,在该区域中,燃油和空气的混合不能很好地实现在如此短的距离内进行反应。流场直接受由燃料空气混合和燃烧模型确定的放热率影响。

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