等温十字射流大涡模拟:初步结果

B.T. Kannan , P. Ssheshan , Sundararaj Senthilkumar
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引用次数: 6

摘要

本文对高雷诺数为1.7 × 105的十字形喷嘴向静止空气中喷射的湍流等温射流进行了数值研究。采用开源CFD工具OpenFOAM®进行数值模拟。采用三维长方体区域模拟非定常湍流流场。通过求解滤波后的Navier-Stokes方程和Smagorinsky子网格尺度模型进行了仿真。将大涡模拟(LES)结果与实验数据进行了比较,验证了射流物理特性。用平均轴向速度衰减逆曲线和可视化方法描述了十字形喷嘴湍流射流的流场。利用涡度大小的等面等高线来显示涡旋结构。十字形喷管形成的旋涡结构与轴对称喷管明显不同。从喷嘴向下游移动时,螺旋结构的形状会发生变化。十字形射流在近场区表现出复杂的涡度动力学。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Large Eddy Simulation of isothermal cruciform jet flow: Preliminary results

The present work is a numerical study of a turbulent isothermal jet issuing from cruciform nozzle into still air at a high Reynolds number of 1.7 × 105. The numerical simulation was carried out by using open source CFD tool OpenFOAM®. Three-dimensional cuboid shaped domain was used to simulate the unsteady turbulent flow field. The simulation was carried out by solving the filtered Navier–Stokes equations along with Smagorinsky sub-grid scale model. The Large Eddy Simulation (LES) solutions are compared with experimental data for validation of the jet flow physics. The flow field of turbulent jet from cruciform nozzle are described in terms of inverse mean axial velocity decay and visualizations. The vortical structures are visualized using iso-surface contours of vorticity magnitude. The vortical structures develop from the cruciform nozzle is significantly different from axisymmetric nozzles. The vortical structures show changes in shape as they move downstream from the nozzle. The cruciform jet shows complex vorticity dynamics in the near field region.

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