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Numerical modeling of hollow-cone fuel atomization, vaporization and wall impingement processes under high ambient temperatures

机译:高环境温度下空心锥燃料雾化,汽化和壁撞击过程的数值模拟

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摘要

In the following paper, a numerical study of the atomization, vaporization and wall impingement processes of hollow-cone fuel spray from high-pressure swirl injectors under various ambient temperature conditions was carried out. Also, the availability of applied models and the effect of ambient temperature on spray characteristics is discussed. The Linearized Instability Sheet Atomization (LISA) model combined with the Aerodynamically Progressed Taylor Analogy Breakup (APTAB) model, the improved Abramzon model and the Gosman model are used to calculate the atomization, vaporization and wall impingement processes of hollow-cone fuel spray, respectively. Spray models are implemented with the modified KIVA code. The calculation results of the spray characteristics under two ambient temperatures, including spray tip penetration, spray structure and radial distance after spray-wall impingement are compared to the experimental results obtained by the Laser Induced Exciplex Fluorescence (LIEF) technique. The droplet size distribution, ambient gas velocity field, vapor phase distribution and fuel film mass generated by spray-wall impingement, measurements which are generally difficult to obtain by experimental methods, are also calculated and discussed. Quantitative discussions on the effect of the ambient temperature on the spray development process are conducted. It is shown that the applied models are applicable even in the high ambient temperature condition.
机译:在下面的论文中,对在各种环境温度条件下从高压旋流喷射器喷出的中空锥状燃料喷雾的雾化,汽化和壁撞击过程进行了数值研究。此外,还讨论了应用模型的可用性以及环境温度对喷雾特性的影响。线性化不稳定性片雾化(LISA)模型与空气动力学进行的泰勒模拟分解(APTAB)模型,改进的Abramzon模型和Gosman模型相结合,分别用于计算中空锥燃油喷雾的雾化,汽化和壁撞击过程。 。喷涂模型使用修改后的KIVA代码实现。将两种环境温度下的喷雾特性计算结果(包括喷嘴尖端穿透力,喷雾结构和撞击壁后的径向距离)与通过激光诱导激基荧光(LIEF)技术获得的实验结果进行了比较。还计算和讨论了通过喷雾壁撞击产生的液滴尺寸分布,环境气体速度场,气相分布和燃料膜质量,以及通常难以通过实验方法获得的测量值。进行了有关环境温度对喷雾显影过程影响的定量讨论。结果表明,所应用的模型即使在高温环境下也适用。

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