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Analysis of Tip Clearance Vortices in a Rotating Axial Fan by Large-Eddy Simulation

机译:大涡模拟分析轴流风扇叶尖间隙涡

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In this paper the flow in a low-speed axial fan at a Reynolds number of 9.36×105 based on the outer casing diameter is investigated by large-eddy simulation(LES)using a cut-cell method based Cartesian flow solver for compressible and viscous flows.The computation includes one of five blades using a periodic boundary condition in azimuthal direction.The paper focuses on the capability of the Cartesian flow solver to efficiently and accurately predict the flow field in axial fans.Simulations with two diffierent grid resolutions and volume flow rates have been performed.Instantaneous and mean flow field results for the fan focusing on the phenomena near the tip-gap region including the tip-gap vortex will be discussed.
机译:本文基于大涡模拟(LES),采用基于切格法的笛卡尔流量解算器对可压缩和粘滞性进行大涡模拟,研究了基于外壳直径的低速轴流风机在9.36×105雷诺数下的流动。该计算包括在方位角方向上使用周期性边界条件的五个叶片中的一个叶片。本文着重于笛卡尔流量解算器有效且准确地预测轴流风扇中流场的能力。具有两种不同的网格分辨率和体积流量的模拟将讨论风扇的瞬时和平均流场结果,重点关注尖端间隙区域(包括尖端间隙涡)附近的现象。

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