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LES Simulation of a Turbulent Methane/Air Premixed bluff body flame with Non-Adiabatic Flamelet Progress Variable Approach

机译:LES仿真湍流甲烷/空气预混诈唬体火焰,具有非绝热轰炸机进度可变方法

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A Large Eddy Simulation of a CH_4/Air premixed bluff body flame is performed by means of a progress variable/flame surface density/probability density function approach. In particular, both mean and variance of the progress variable are transported. Its subgrid spatially filtered gradient contributes to model the flame surface density (that introduces the effect of the subgrid flame reaction zone) and to presume a probability density function (that introduces the effect of subgrid fluctuations on chemistry). Chemistry is tabulated in terms of laminar premixed flames and enthalpy is included as a new coordinate in their tabulation to take into account heat losses in the flowfield. The filtered mass, momentum, enthalpy and scalar equations mentioned above are integrated by means of an explicit scheme using finite differences, 2nd-order accurate in space and third order in time, over a cylindrical non-uniform grid using a staggered approach. The bluff-body geometry is modeled by using the Immersed Boundary Method. The predictions of velocity and temperature are compared with available experimental data.
机译:通过进度可变/火焰表面密度/概率密度函数方法执行CH_4 /空气预混诈唬体火焰的大涡模拟。特别地,运输进度变量的均值和方差。其底下空间过滤的梯度有助于模拟火焰表面密度(引入亚底填充火焰反应区的效果)并假设概率密度函数(引入亚底波动对化学的影响)。化学在层流预混火焰方面列出,焓被包括在其制表中的新坐标,以考虑流场中的热量损失。上面提到的过滤的质量,动量,焓和标量方程通过使用有限差异,在空间和第三顺序的时间和第三顺序的时间和第三顺序的时间,在使用交错方法的圆柱形非均匀网格上进行整合。通过使用浸没的边界法建模诈唬体几何形状。将速度和温度的预测与可用的实验数据进行比较。

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