Algebraic Flame Surface Density Modelling of High Pressure Turbulent Premixed Bunsen Flames

被引:12
|
作者
Rasool, R. [1 ]
Chakraborty, N. [2 ]
Klein, M. [1 ]
机构
[1] Bundeswehr Univ Munich, Dept Aerosp Engn, Werner Heisenberg Weg 39, D-85577 Neubiberg, Germany
[2] Newcastle Univ, Sch Engn, Stephenson Bldg,Claremont Rd, Newcastle Upon Tyne NE1 7RU, Tyne & Wear, England
基金
英国工程与自然科学研究理事会;
关键词
High pressure turbulent combustion; A-priori DNS analysis; Algebraic FSD modelling; Large eddy simulation; Bunsen flames; LARGE-EDDY SIMULATION; BURNER FLAMES; FUNCTION TRANSPORT; A-PRIORI; CONTEXT; COMBUSTION; CURVATURE;
D O I
10.1007/s10494-020-00128-y
中图分类号
O414.1 [热力学];
学科分类号
摘要
Performance of representative algebraic flame surface density (FSD) models have been a-priori assessed based on a direct numerical simulation database consisting of four turbulent premixed Bunsen flames at four different pressure levels. Results indicate that for a given resolution of the flame front, the considered algebraic FSD closures perform in a qualitatively similar manner irrespective of pressure variation. However, for a given computational mesh, the performance deteriorates as flame thickness decreases with increasing pressure. Additionally, the contribution of the subgrid scale surface-filtered density-weighted tangential diffusion component of the displacement speed tends to increase with pressure increment, further complicating the modelling of FSD. Further analysis also indicate that the inner cut-off scale normalized by the thermal flame thickness increases with increasing pressure, possibly due to the presence of Darrieus-Landau instability which is more likely to occur at higher pressure due to a larger ratio of hydrodynamic length scale to thermal flame thickness.
引用
收藏
页码:1313 / 1327
页数:15
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