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Application of the Eulerian subgrid Probability Density Function method in the Large Eddy Simulation of a partially premixed swirl flame

机译:欧拉次网格概率密度函数法在部分预混旋流火焰大涡模拟中的应用

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摘要

A gas turbine model combustor is studied using Large Eddy Simulation with a transported Probability Density Function approach solved by the Eulerian stochastic field method. The chemistry is represented by a reduced methane mechanism containing 15 steps and 19 species while the subgrid scale stresses and scalar fluxes are modelled, respectively, via a dynamic Smagorinsky model and a gradient diffusion approximation. The test case comprises a partially premixed swirl flame in a complex geometry. Four stochastic fields are utilised in the simulations, which are performed for two different combustor operating conditions involving a stable and an unstable flame. Good agreement between the simulation and measurement data is shown in a comparison of mean velocity, temperature and species mass fraction profiles, as well as scatter plots of the instantaneous thermochemical properties. In conclusion, the predictive capabilities of the employed Large Eddy Simulation method are successfully demonstrated in this work.
机译:利用大涡模拟研究了燃气轮机模型燃烧器,并通过欧拉随机场法求解了运输概率密度函数法。化学过程以甲烷的还原机理为代表,该机理包含15个步骤和19个物种,而亚网格尺度应力和标量通量分别通过动态Smagorinsky模型和梯度扩散近似建模。测试用例包括部分预混的复杂几何形状的旋流火焰。在模拟中利用了四个随机场,它们是针对涉及稳定火焰和不稳定火焰的两种不同燃烧器运行条件而执行的。通过比较平均速度,温度和物质质量分数分布图以及瞬时热化学性质的散点图,可以看出模拟数据与测量数据之间的一致性。总之,这项工作成功地证明了所采用的大涡模拟方法的预测能力。

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