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首页> 外文期刊>International journal of engine research >The effect of fuel on high velocity evaporating fuel sprays: Large-Eddy simulation of Spray A with various fuels
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The effect of fuel on high velocity evaporating fuel sprays: Large-Eddy simulation of Spray A with various fuels

机译:燃料对高速蒸发燃料喷雾的影响:各种燃料喷雾A的大涡模拟

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Lagrangian particle tracking and Large-Eddy simulation were used to assess the effect of different fuels on spray characteristics. In such a two-way coupled modeling scenario, spray momentum accelerates the gaseous phase into an intense, multiphase jet near the nozzle. To assess fuel property effects on liquid spray formation, the non-reacting Engine Combustion Network Spray A baseline condition was chosen as the reference case. The validated Spray A case was modified by replacing n -dodecane with diesel, methanol, dimethyl ether, or propane assuming 150?MPa injection pressure. The model features and performance for various fuels in the under-resolved near-nozzle region are discussed. The main findings of the paper are as follows. (1) We show that, in addition to the well-known liquid penetration ( L liq ) , and vapor penetration ( L vap ) , for all the investigated fuels, the modeled multiphase jets exhibit also a third length scale L core , with discussed correspondence to a potential core part common to single phase jets. (2) As a characteristic feature of the present model, L core is noted to correlate linearly with L liq and L vap for all the fuels. (3) A separate sensitivity test on density variation indicated that the liquid density had a relatively minor role on L liq . (4) Significant dependency between fuel oxygen content and the equivalence ratio ( Φ ) distribution was observed. (5) Repeated simulations indicated injection-to-injection variations below 2% for L liq and 4% for L vap . In the absence of experimental and fully resolved numerical near-nozzle velocity data, the exact details of L core remain as an open question. In contrast, fuel property effects on spray development have been consistently explained herein.
机译:拉格朗日粒子跟踪和大涡模拟用于评估不同燃料对喷雾特性的影响。在这种双向耦合建模场景中,喷涂动量将气相加速到喷嘴附近的强烈的多相喷射中。为了评估对液体喷雾形成的燃料性能影响,选择非反应发动机燃烧网络喷射基线状况作为参考情况。通过用柴油,甲醇,二甲醚或丙烷替换N-DodeCane,通过假设150〜MPa注射压力来改变验证的喷雾案例。讨论了在解析的近喷嘴区域中各种燃料的模型特征和性能。本文的主要结果如下。 (1)我们表明,除了众所周知的液体渗透(L LIQ)和蒸汽渗透(L LIQ)之外,对于所有调查的燃料,所建模的多相喷射器也表现出第三长度尺度L核心,并讨论对应于单相喷射的潜在核心部分的对应。 (2)作为本模型的特征,应注意与所有燃料的L LIQ和L VAP线性相关联。 (3)密度变异的单独灵敏度试验表明,液体密度在L LIQ上具有相对较小的作用。 (4)观察到燃料氧含量与等效比(φ)分布之间的显着依赖性。 (5)重复模拟表明L LIQ的注射进样变化低于2%,L LIQ的4%,L VAP为4%。在没有实验和完全解决的数值近喷嘴速度数据的情况下,L核心的确切细节仍然是一个打开的问题。相比之下,本文始终解释了对喷雾开发的燃料性能影响。

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