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Modeling and detailed numerical simulation of the primary breakup of a gasoline surrogate jet under non-evaporative operating conditions

机译:非蒸发操作条件下汽油代理喷射初级分解的建模与详细数值模拟

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The injection and atomization of gasoline fuels are critical to the performance of gasoline direct injection engines. Due to the complex nature of the primary breakup of the liquid jet in the near field, high-level details are often difficult to measure in experiments. In the present study, detailed numerical simulations are performed to investigate the primary breakup of a gasoline surrogate jet under non-evaporative "Spray G" operating conditions. The Spray G injector and operating conditions, developed by the Engine Combustion Network (ECN), represent the early phase of spray-guided gasoline injection. To focus the computational resources on resolving the primary breakup, simplifications have been made on the injector geometry. The effect of the internal flow on the primary breakup is modeled by specifying a nonzero injection angle at the inlet. The nonzero injection angle results in an increase of the jet penetration speed and also a deflection of the liquid jet. A parametric study on the injection angle is performed, and the numerical results are compared to the experimental data to identify the injection angle that best represents the Spray G conditions. The nonzero injection angle introduces an azimuthally non-uniform velocity in the liquid jet, which in turn influences the instability development on the jet surfaces and also the deformation and breakup of the jet head. The asymmetric primary breakup dynamics eventually lead to an azimuthal variation of droplet size distributions. The number of droplets varies significantly with the azimuthal angle, but interestingly, the probability density functions (PDF) of droplet size for different azimuthal angles collapse to a self-similar profile. The self-similar PDF is fitted with both lognormal and gamma distribution functions. Analysis has also been conducted to estimate the percentage and statistics of the tiny droplets that are under resolved in the present simulation. The PDF of the azimuthal angle is also presented, which is also shown to exhibit a self-similar form that varies little over time. The PDF of the azimuthal angle is well represented by a hyperbolic tangent function. Finally, a model is developed to predict the droplet number as a function of droplet diameter, azimuthal angle where a droplet is located, and time. (C) 2020 Elsevier Ltd. All rights reserved.
机译:汽油燃料的注射和雾化对汽油直喷发动机的性能至关重要。由于近场液体射流初级分解的复杂性,在实验中通常难以测量高级细节。在本研究中,进行详细的数值模拟,以研究在非蒸发“喷射G”操作条件下汽油替代射流的主要分解。喷射G喷射器和由发动机燃烧网络(ECN)开发的操作条件代表了喷射引导汽油喷射的早期阶段。要将计算资源集中在解决初级分析上,则在喷射器几何中取出了简化。通过在入口处指定非零喷射角来建模内部流对初级分解的影响。非零注射角导致喷射穿透速度的增加以及液体射流的偏转。执行对注射角的参数研究,并将数值结果与实验数据进行比较,以识别最能代表喷射G条件的注射角度。非零注射角度在液体射流中引入方位而至的速度,这反过来影响喷射表面上的不稳定发育以及喷射头的变形和破碎。非对称初级分手动态最终导致液滴尺寸分布的方位角变化。液滴的数量随方位角而变化,但有趣的是,不同方位角的液滴尺寸的概率密度函数(PDF)塌陷到自相似的轮廓。自相似的PDF配有Lognormal和伽马分布函数。还进行了分析以估计本模拟中未分辨的微小液滴的百分比和统计。还提出了方位角角的PDF,其也被示出表现出一种随时间几乎不变的自相似形式。方位角角的PDF通过双曲线切线功能表示良好。最后,开发了一种模型以将液滴数预测为液滴直径的函数,所以液滴的方位角和时间。 (c)2020 elestvier有限公司保留所有权利。

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