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CFD analysis of an innovative combined lift and drag (CLD) based modified Savonius water turbine

机译:基于创新的提升与阻力(CLD)组合式改良Savonius水轮机的CFD分析

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Savonius water turbine is a popular turbine that can be used for energy extraction from free stream flows in rivers or manmade channels and also from tidal and ocean currents. The present study aims at developing a new combined lift-drag (CLD) based blade design for a conventional two-bladed Savonius water turbine. The semicircular blade is replaced with a straight blade section starting from the turbine axis and ending with an airfoil blade section at the leading edge. The blade lengths are adjusted within the overall diameter of an established conventional Savonius water turbine, taken from available literature. This innovative design is considered as the base model. The base model is then gradually modified and optimized using ANSYS Fluent 14 CFD software by considering design parameters - gap width ratio and overlap ratio. The evolved optimal design is then further studied for two more turbine diameters, one of which is taken from another prominent literature. All the performance analyses are carried out through flow physics study of the turbines. It has been found that the maximum coefficient of power (C-p) obtained for the CLD Savonius turbine is 0.284 obtained at a tip speed ratio 0.6 for an overall turbine diameter 260 mm, gap width ratio 8.45%, and overlap ratio 46.9%. The contributions of the individual blade sections on the CLD turbine performance have also been appreciated. Finally, the CLD design is compared with an established Savonius turbine design to highlight the significant importance of the present design.
机译:Savonius水轮机是一种流行的水轮机,可用于从河流或人造河道中的自由水流以及潮汐和洋流中提取能量。本研究旨在为常规的两叶片Savonius水轮机开发一种新的基于举升-拖曳(CLD)组合的叶片设计。从涡轮机轴开始,到前缘的翼型叶片部分结束,用直叶片部分代替半圆形叶片。根据现有文献,在已建立的常规Savonius水轮机的总直径范围内调节叶片长度。此创新设计被视为基本模型。然后,通过考虑设计参数-间隙宽度比和重叠比,使用ANSYS Fluent 14 CFD软件逐步修改和优化基本模型。然后,针对另外两个涡轮机直径进一步研究了改进的最佳设计,其中一个直径取自另一本著名的文献。所有性能分析都是通过涡轮机的流动物理研究进行的。已经发现,对于总直径为260mm的涡轮,间隙宽度比为8.45%,重叠比为46.9%,对于CLD Savonius涡轮而言,在叶尖速度比为0.6时获得的最大功率系数(C-p)为0.284。各个叶片部分对CLD涡轮机性能的贡献也得到了认可。最后,将CLD设计与已建立的Savonius涡轮机设计进行了比较,以强调本设计的重要意义。

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