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Evaluation of spray impact on a sphere with a two-fluid nozzle

机译:用双流体喷嘴对球体喷雾撞击的评价

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The generation of a secondary aerosol after impact, consisting of smaller droplets at a given velocity and mass flow, is relevant for various applications. Thus far, the investigations and modelling approaches on spray impact are based on extrapolation of the single-droplet impingement or empirical correlations. The validity of the models presented is limited to the given experimental setup and conditions such as initial droplet size, velocity and the impact surface characteristics. The aim of this work was to empirically evaluate the spray impact of a two-fluid nozzle on a sphere. A small-scale nozzle was used, which produced a primary aerosol with a mass median diameter of about 12 mu m (liquid-to-gas mass flow ratio = 1, gas pressure: Delta p(G) = 5 bar). After impact on a sphere, a multimodal distribution was observed and a higher mass flowrate of droplets in the small micrometer range (2 and 3 mu m) was produced for a liquid mass flow rate in the range of 1.2-6 kg/h and an atomizing gas mass flow rate of 1-4 kg/h. For easier observation, a geometrically similar, larger nozzle was used, which produced an aerosol with a mass median diameter of about 80 mu m (liquid-to-gas mass flow ratio = 4, gas pressure: Delta p(G) = 1 bar). The measured droplet size after impact is smaller for a lower liquid-to-gas mass flow ratio and increased atomizing gas inlet pressure. Droplet formation mechanisms such as splashing, crown formation and spreading on the sphere surface were observed. A characteristic film with large variations in thickness was generated.
机译:在给定速度和质量流动下的较小液滴组成的抗冲击后的二次气溶胶的产生与各种应用相关。到目前为止,喷雾冲击的研究和建模方法基于单滴冲击的外推或经验相关性。所呈现的模型的有效性仅限于给定的实验设置和条件,例如初始液滴尺寸,速度和冲击表面特性。这项工作的目的是经常评估双流体喷嘴在球体上的喷雾冲击。使用小尺寸喷嘴,其制造了大量中值直径为约12μm的主要气溶胶(液 - 气体质量流量= 1,气体压力:Delta P(g)= 5巴)。在对球体上冲击后,观察到多模峰分布,并且在1.2-6kg / h的范围内的液体质量流速产生液体质量流速的液体中液滴的较高质量流量。雾化气体质量流量为1-4 kg / h。为了更容易观察,使用几何相似的较大喷嘴,其产生了大规模中值直径为约80μm的气溶胶(液 - 气质量流量= 4,气体压力:Delta P(g)= 1巴)。撞击后的测量液滴尺寸对于较低的液 - 气体质量流量比和增加的雾化气体入口压力较小。观察液滴形成机制,例如飞溅,冠形成和在球面上展开。产生具有大变化的特征膜。

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