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首页> 外文期刊>International Journal of Computational Engineering Science(IJCES) >3-D COMPUTATIONAL FLUID DYNAMIC ANALYSIS OF EFFECT OF TIP CLEARANCE ON THE PERFORMANCE OF IMPULSE TURBINE FOR WAVE ENERGY CONVERSION
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3-D COMPUTATIONAL FLUID DYNAMIC ANALYSIS OF EFFECT OF TIP CLEARANCE ON THE PERFORMANCE OF IMPULSE TURBINE FOR WAVE ENERGY CONVERSION

机译:尖端间隙对脉冲能量转换对波能性能影响的3-D计算流体动力学分析

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摘要

This paper depicts numerical analysis on impulse turbine of 0.6 m diameter with fixed guide vanes for wave energy conversion. From the earlier investigations, it is found that one of the reasons for the mismatch between computed and experimental data is due to neglecting tip clearance effect. Hence, a three-dimensional (3-D) model with tip clearance has been generated with structured grids to predict the internal flow and performance of the turbine. As a result, it is found that the comparison between computed and experimental data is good. Computation has been carried out for various tip clearances to understand the effect of tip clearance leakage flow on such unconventional turbine. The change in flow behavior in the turbine blade passage due to tip clearance flow has been studied by comparing the results with without tip clearance, which is impossible by experiments. It is predicted that the efficiency of the turbine has been reduced about 4%, due to tip clearance flow at higher flow coefficients.
机译:本文描述了直径为0.6 m的带有固定导向叶片的脉冲式涡轮机用于波能转换的数值分析。从较早的研究中发现,计算数据和实验数据之间不匹配的原因之一是由于忽略了尖端间隙效应。因此,已使用结构化网格生成了具有尖端间隙的三维(3-D)模型,以预测涡轮的内部流量和性能。结果,发现计算数据与实验数据之间的比较是良好的。已经对各种叶尖间隙进行了计算,以了解叶尖间隙泄漏流对这种非常规涡轮机的影响。通过比较无叶尖间隙的结果,研究了由于叶尖间隙流动而导致的涡轮叶片通道流动特性的变化,这是无法通过实验进行的。据预测,由于叶尖间隙流量较高,涡轮机的效率已降低了约4%。

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