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首页> 外文期刊>Combustion theory and modelling >Large eddy simulations of partially premixed ethanol dilute spray flames using the flamelet generated manifold model
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Large eddy simulations of partially premixed ethanol dilute spray flames using the flamelet generated manifold model

机译:使用小火焰生成歧管模型对部分预混合乙醇稀释喷雾火焰进行大涡模拟

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The paper presents Large Eddy Simulations (LESs) for the Sydney ethanol piloted turbulent dilute spray flames ETF2, ETF6, and ETF7. The Flamelet Generated Manifold (FGM) approach is employed to predict mixing and burning of the evaporating fuel droplets. A methodology to match the experimental inflow spray profiles is presented. The spray statistical time-averaged results show reasonable agreement with mean and RMS data. The Particle Size Distribution (PSD) shows a good match downstream of the nozzle exit and up to x/D = 10. At x/D = 20 and 30 the PSD is under-predicted for droplets with mean diameter D10 > 20m and over-predicted for the smaller size droplets. The simulations reasonably predict the reported mean flame structure and length. The effect of increasing the carrier velocity (ETF2-ETF7) or decreasing the liquid fuel injection mass flow rate (ETF2-ETF6) is found to result in a leaner, shorter flame and stronger spray-flow interactions. Higher tendency to local extinction is observed for ETF7 which is closer to blow-off compared to ETF2 and has higher scalar dissipation rates, higher range of Stokes number, and faster droplet response. The possible sources of LES-FGM deviations from the measurements are discussed and highlighted. In particular, the spray time-averaged statistical error contribution is quantified and the impact of the inflow uncertainty is studied. Sensitivity analysis to the pre-vaporized nozzle fuel mass fraction show that such small inflow perturbations (by +/- 2% for the ETF2 flame) have a strong impact on the flame structure, and the droplets' dynamics. Conditional scatter plots show that the flame exhibits wide range of mixing conditions and bimodal mixing lines particularly at upstream locations (x/D<20), where the injected droplets are still penetrating the centerline. This is relaxed further downstream as droplets gradually evaporate and burn in a diffusion like mode.
机译:本文介绍了针对悉尼乙醇引燃湍流稀薄喷雾火焰ETF2,ETF6和ETF7的大型涡模拟(LESs)。火焰产生歧管(FGM)方法用于预测蒸发的燃料滴的混合和燃烧。提出了一种与实验流入喷雾分布相匹配的方法。喷雾统计的时间平均结果与平均值和RMS数据显示出合理的一致性。粒径分布(PSD)在喷嘴出口的下游显示出良好的匹配,并且高达x / D =10。在x / D = 20和30时,对于平均直径D10> 20m的液滴,PSD预测不足。预测较小尺寸的液滴。该模拟合理地预测了所报告的平均火焰结构和长度。发现增加载流子速度(ETF2-ETF7)或降低液体燃料喷射质量流量(ETF2-ETF6)的效果导致更稀薄,更短的火焰和更强的喷雾流相互作用。对于ETF7,观察到了更高的局部灭绝趋势,与ETF2相比更接近吹灭,并且具有更高的标量耗散率,更大的斯托克斯数范围和更快的液滴响应。讨论并强调了LES-FGM与测量值偏差的可能来源。特别是,对喷雾时间平均的统计误差贡献进行了量化,并研究了流入不确定性的影响。对预蒸发喷嘴燃料质量分数的敏感性分析表明,如此小的流入扰动(对于ETF2火焰为+/- 2%)对火焰结构和液滴的动力学有很大影响。条件散点图显示,火焰表现出广泛的混合条件和双峰混合线,特别是在上游位置(x / D <20)处,在该位置喷射的液滴仍渗透中心线。随着液滴逐渐蒸发并以类似扩散的方式燃烧,其在下游进一步松弛。

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