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Comprehensive Study of the Initial Diameter for Combustion of n-Heptane/iso-Octane Mixture Droplets

机译:正庚烷/异辛烷混合物液滴燃烧初始直径的综合研究

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This paper reports a comprehensive study of n-heptane/iso-octane mixture droplets burning in atmospheric pressure air under conditions that promote spherical symmetry. The initial droplet diameter (D_o) range studied (0.5 mm to ~ 4.8 mm) included pure n-heptane, iso-octane, and equi-volume (50/50) heptane/iso-octane mixtures. The data show that as D_o increases, a transition occurs from steady burning with essentially no influence of D_o on the burning rate to where the burning rate decreases as D_o is further increased. The droplet mixture fraction was observed to have little effect on early burning behavior, resulted in earlier extinction for larger initial droplet sizes containing iso-octane. Detailed spherically symmetric, isolated droplet model predictions were compared with and used to interpret the experimental observations. The model considered numerically reduced detailed kinetics involving 298 species and 1916 detailed reactions, non-luminous, radiative transport, variable physical properties and unsteady liquid and gas phase effects. The simulations indicate that depending on the initial droplet diameter, two distinctly different combustion behaviors are observed the 50/50 n-heptane/iso-octane blend. Smaller droplets undergo a single stage burn to completion. At larger droplet sizes, the initial burning is observed to transition through radiative extinction to a cool flame droplet burning mode driven by negative temperature coefficient kinetics. The cool flame droplet burning period is decreased as iso-octane fraction is increased and is completely suppressed for pure iso-octane conditions. The predicted flame standoff ratios are somewhat larger than, but qualitatively in agreement with the experimental measurements. For both experiments and predictions, the high temperature flame standoff ratio is observed to be independent of the initial droplet diameter. The flame stand-off ratio for cool flame droplet burning conditions exhibits an inverse dependence on initial drop diameter, consistent with increasing heat loss from the reaction zone.
机译:本文报道了在促进球形对称的条件下在大气压空气中燃烧的正庚烷/异辛烷混合物液滴的综合研究。研究的初始液滴直径(D_O)范围(0.5mm至〜4.8mm)包括纯正庚烷,异辛烷和等体积(50/50)庚烷/异辛烷混合物。数据表明,随着D_O的增加,从稳定燃烧发生的过渡,基本上没有D_O对燃烧速率的燃烧速率的影响,因为D_O进一步增加了燃烧速率。观察到液滴混合物分数对早期燃烧行为几乎没有影响,导致含有异辛烷的较大初始液滴尺寸的早期消光。详细的球形对称,与孤立的液滴模型预测进行了比较并用于解释实验观察。该模型被认为是数值减少的详细动力学,涉及298种和1916年的细致反应,非发光,辐射传输,可变物理性质和不稳定的液体和气相效应。该模拟表明,根据初始液滴直径,观察到两个明显不同的燃烧行为,观察到50/50正庚烷/异辛烷共混物。较小的液滴经历单级刻录到完成。在较大的液滴尺寸下,观察到初始燃烧以通过辐射灭绝转换到由负温度系数动力学驱动的冷火焰液滴燃烧模式。随着异辛烷馏分的增加,冷却火焰液滴燃烧周期降低,并且对于纯的异辛烷条件完全抑制。预测的火焰支座比率略大于,但与实验测量相一致地具有定性。对于实验和预测,观察到高温火焰梯级比例与初始液滴直径无关。用于冷火焰液滴燃烧条件的火焰脱扣比表现出对初始落叶直径的逆依赖性,这与来自反应区的热损失增加一致。

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