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Single and multicomponent droplet models for spray applications

机译:用于喷涂的单组分和多组分液滴模型

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An unsteady, spherically symmetric, single component, diffusion controlled gas phase droplet combustion model was developed first, by solving numerically the time dependent equations of energy and species. Results indicated that flame to droplet diameter ratio (flame standoff ratio) increased throughout the droplet burning period, its value being much smaller than that of the quasi-steady case, where it assumes a large constant value. Effects of fuels on important combustion characteristics suggested that combustion parameters were influenced primarily by the fuel boiling point. Droplet mass burning rate variation was smallest for ethanol in comparison with methyl linoleate (biodiesel) and n-heptane. Also, effects of fuels on CO, NO, CO_2, and H_2O concentrations were determined from the point of view of getting a qualitative trend.For multicomponent spherical combustion of a heptane-dodecane droplet, it was observed that the mass fraction of heptane decreased abruptly to a minimum value as the droplet surface was approached. For a 200μm hexane-decane droplet (at its boiling point), vaporising in conditions of 1 atm and 1000K with Le_1=10, it was observed that mixing of air and fuel vapour resulted in a higher concentration of hexane at the droplet surface at the end of droplet lifetime thereby altering the vaporisation behaviour. Other conditions remaining same, an increase in Lewis number resulted in a higher mass fraction of hexane being present at the droplet surface. A detailed multicomponent (MC) droplet vaporisation model (diffusion limit model with convection and no internal liquid circulation) was also evolved by numerically solving the transient-diffusive equations of species and energy for a 280μm (heptane-dodecane) droplet vaporising at 1 atm and 1000 K with Re_σ=100, and Le_1=10. The present MC model was compared with other existing models and was found to be simpler and quite accurate. The submodels developed in the present work can be implemented in spray analysis.
机译:首先通过数值求解能量和物质的时间相关方程,建立了一个不稳定的,球对称的,单组分,扩散控制的气相液滴燃烧模型。结果表明,在整个液滴燃烧期间,火焰与液滴的直径比(火焰阻滞比)增加,其值远小于准恒定情况下的近似恒定值(假定为大恒定值)。燃料对重要燃烧特性的影响表明,燃烧参数主要受燃料沸点的影响。与亚油酸甲酯(生物柴油)和正庚烷相比,乙醇的液滴质量燃烧速率变化最小。另外,从定性的观点出发,研究了燃料对CO,NO,CO_2和H_2O浓度的影响。对于庚烷-十二烷液滴的多组分球形燃烧,观察到庚烷的质量分数急剧下降。接近液滴表面时的最大值。对于200μm的己烷-癸烷液滴(在其沸点),在1个大气压和1000K的条件下蒸发,且Le_1 = 10时蒸发,观察到空气和燃料蒸气的混合会导致液滴表面的己烷浓度更高。液滴寿命的结束,从而改变了汽化行为。其他条件保持不变,路易斯数的增加导致在液滴表面存在较高质量的己烷。通过数值求解在1个大气压下蒸发的280μm(庚烷-十二烷)液滴的物种和能量的瞬态扩散方程,还建立了详细的多组分(MC)液滴蒸发模型(具有对流且没有内部液体循环的扩散极限模型)。 Re_σ= 100且Le_1 = 10时为1000K。将当前的MC模型与其他现有模型进行了比较,发现该模型更为简单且非常准确。本工作中开发的子模型可以在喷雾分析中实现。

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