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首页> 外文期刊>Numerical Heat Transfer, Part A: Applications >Studies of the Effect of Spray Inlet Conditions on the Flow and Flame Structures of Ethanol-Spray Combustion by Large-Eddy Simulation
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Studies of the Effect of Spray Inlet Conditions on the Flow and Flame Structures of Ethanol-Spray Combustion by Large-Eddy Simulation

机译:大涡模拟研究喷雾入口条件对乙醇喷雾燃烧流动和火焰结构的影响

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Large-eddy simulation (LES) of ethanol spray-air combustion with a poly-dispersed initial droplet size distribution is presented here by using an Eulerian-Lagrangian approach, a sub-grid-scale kinetic energy stress model, and a filtered finite-rate combustion model with a sub-grid scale reaction rate called the second-order moment (SOM) combustion model, proposed by our research group. The simulation results are validated in detail by experiments. Furthermore, the flow and flame structures of spray combustion with different spray cone angles and cone angle thickness are studied. The results show that for the case of smaller spray cone angle thickness, the coherent structures in the high temperature zone tend to shed more clearly. High temperature develops around the coherent structures in the region of high vapor concentration, but not inside the large vortices. For the spray combustion with larger spray cone angle thickness, the vortex shedding at the outside of the flame zone is faster than that with smaller spray cone angle thickness. The instantaneous temperature maps of different spray flame structures with smaller cone angle thickness indicate the existence of small flame islands, expressing the droplet-group combustion, which is not observed in single-phase jet combustion and not obvious in the case of larger cone angle thickness.View full textDownload full textRelated var addthis_config = { ui_cobrand: "Taylor & Francis Online", services_compact: "citeulike,netvibes,twitter,technorati,delicious,linkedin,facebook,stumbleupon,digg,google,more", pubid: "ra-4dff56cd6bb1830b" }; Add to shortlist Link Permalink http://dx.doi.org/10.1080/10407782.2012.672865
机译:使用欧拉-拉格朗日方法,亚网格规模动能应力模型和滤波后的有限速率,对乙醇喷雾空气燃烧具有多分散初始液滴尺寸分布的大涡模拟(LES)进行了介绍。由研究小组提出的具有次网格规模反应速率的燃烧模型,称为二阶矩(SOM)燃烧模型。通过实验对仿真结果进行了详细验证。此外,研究了具有不同喷雾锥角和锥角厚度的喷雾燃烧的流动和火焰结构。结果表明,在较小的喷雾锥角厚度的情况下,高温区域的相干结构倾向于更清楚地脱落。在高蒸气浓度的区域中,在相干结构周围会产生高温,但在大涡旋内部则不会。对于具有较大喷雾锥角厚度的喷雾燃烧,火焰区域外侧的涡旋脱落比具有较小喷雾锥角厚度的涡流更快。锥角厚度较小的不同喷雾火焰结构的瞬时温度图表明存在小火焰岛,表示液滴群燃烧,这在单相射流燃烧中未观察到,而在锥角厚度较大的情况下不明显查看全文下载全文相关变量var addthis_config = {ui_cobrand:“泰勒和弗朗西斯在线”,servicescompact:“ citeulike,netvibes,twitter,technorati,delicious,linkedin,facebook,stumbleupon,digg,google,更多”,发布ID:“ ra- 4dff56cd6bb1830b“};添加到候选列表链接永久链接http://dx.doi.org/10.1080/10407782.2012.672865

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