Calculation of the characteristic diagram of an axial fan using CFD

T. Wolfanger, M. Lenartz
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Abstract

The characteristic curves of a ventilator with adjustable blade angle were calculated using CFD. The characteristic curve is valid for a certain blade angle of a single stage ventilator and was measured on a test stand according to DIN 24163. To evaluate the critical points for the calculation of the characteristic curves, a number of blade angles have been considered. It turned out that the points with the maximum deviation between measurement and calculation were lying close to the optimum efficiency point of the fan operation in the vicinity of the separation line. For further studies of the influence of mesh resolution, turbulence modelling and geometric modelling, one operation point showing relatively large deviations from the measurements was chosen. For this operation point, a successive refinement of the mesh was done to get a grid independent solution. The mesh of the grid independent solution was used to study the influence of several turbulence models including two equation k-ε and k-ω models and a ω based Reynolds stress model and the influence of the blade tip gap. Finally, one curve from the characteristic diagram was recalculated using the best performing turbulence model and the results were compared to measurements.
用CFD计算轴流风机的特性图
利用CFD计算了叶片角度可调通风机的特性曲线。该特性曲线适用于单级通风机一定叶片角度下的特性曲线,并根据DIN 24163在试验台上进行了测量。为了评估计算特性曲线的临界点,考虑了多个叶片角度。结果表明,测量值与计算值偏差最大的点位于分离线附近风机运行最佳效率点附近。为了进一步研究网格分辨率、湍流建模和几何建模的影响,选择了一个与测量值偏差较大的操作点。针对该操作点,对网格进行逐次细化,得到与网格无关的解。利用网格独立解的网格,研究了两种方程k-ε和k-ω模型以及基于ω的雷诺应力模型等湍流模型和叶尖间隙的影响。最后,利用性能最好的湍流模型重新计算了特征图中的一条曲线,并将计算结果与实测结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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