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2D and 3D numerical modelling of internal flow of Pressure-swirl atomizer

机译:压力 - 旋流雾化器内部流动的2D和3D数值模型

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摘要

This paper compares 2D axisymmetric and 3D numerical models used to predict the internal flow of a pressure-swirl atomizer using a commercial software Ansys Fluent 18.1. The computed results are compared with experimental data in terms of spray cone angle (SCA), discharge coefficient (CD), internal air-core dimensions and swirl velocity profile. The swirl velocity was experimentally studied using a Laser Doppler Anemometry in a scaled transparent model of the atomizer. The internal air-core was visualized at high temporal and spatial resolution by a high-speed camera with backlit illumination. The internal flow was numerically treated as transient two-phase flow. The gas-liquid interface was captured with Volume of Fluid scheme. The numerical solver used both laminar and turbulent approach. Turbulence was modelled using k-ε, k-ω, Reynolds Stress model (RSM) and coarse Large Eddy Simulation (LES). The laminar solver was capable to predict all the parameters with an error less than 5% compared with the experimental results in both 2D and 3D simulation. However, it overpredicted the velocity of the discharged liquid sheet. The LES model performed similarly to the laminar solver, but the liquid sheet velocity was 10% lower. The two-equation models k-ε and k-ω overpredicted the turbulence viscosity and the internal air-core was not predicted.
机译:本文比较2D轴对称和3D数字模型用于预测的压力 - 旋流的内部流雾化器使用商业软件ANSYS FLUENT 18.1。所计算的结果与在喷雾锥角(SCA),流量系数(CD),内部空芯的尺寸和回旋速度分布方面的实验数据进行比较。在雾化器的经缩放的透明模型使用激光多普勒测速仪的回旋速度进行实验研究。内部空芯在由高速照相机带背光照明高时空分辨率可视化。内部流进行数值视为瞬时两相流。气液界面与流体方案的卷捕获。数值求解器使用这两种层流和湍流的方法。紊流用的k-ε,K-ω,雷诺应力模型(RSM)和粗大涡模拟(LES)建模。层状解算器是能够向所有预测有错误的参数小于5%,在2D和3D仿真的实验结果进行比较。然而,它overpredicted排出液薄片的速度。在LES模型中进行类似的层状解算器,但液体片速度为10%以下。两个方程模型的k-ε和k-ωoverpredicted湍流粘度和未预测的内部空芯。

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