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A 3D COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF THE WELLS TURBINE

机译:汽轮机的3D计算流体动力学分析

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摘要

This paper deals with the application of Computational Fluid Dynamics (CFD) to the turbulent analysis of the Wells Turbine. The objectives of this work were twofold; firstly to develop and benchmark the 3D CFD model and then to use this model to analyse the airflow through the turbine. The model was analysed as My turbulent compressible flow using the Fluent~(TM) CFD code. The computational model was first bencbmarked against previously published experimental and CFD data for two similar turbines. The computational model accurately predicted the non-dimensional torque and non-dimensional pressure drop, while the efficiency predictions were lower than the experimental results. Predicted location of turbine stall also corresponded well with experimental results. Potential causes for differences between the computational and experimental results are suggested. The computational model was then analysed at both high and low tip Mach number settings and also with and without the tip gap, and these results were discussed.
机译:本文将计算流体动力学(CFD)应用于Wells Turbine的湍流分析中。这项工作的目标是双重的。首先开发3D CFD模型并对其进行基准测试,然后使用该模型分析通过涡轮的气流。使用FluentTM CFD代码将模型分析为My湍流可压缩流。该计算模型首先针对先前发布的两个相似涡轮机的实验和CFD数据进行了标注。该计算模型准确地预测了无量纲的扭矩和无量纲的压降,而效率的预测却低于实验结果。涡轮失速的预测位置也与实验结果很好地吻合。建议了计算和实验结果之间差异的潜在原因。然后在高和低尖端马赫数设置下以及有无尖端间隙的情况下分析计算模型,并对这些结果进行了讨论。

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