提高升力性能的改进型垂直轴潮汐水轮机研究

N. Arini, S. Turnock, M. Tan
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引用次数: 6

摘要

本文对采用改型翼型的达里厄斯垂直轴潮汐水轮机的设计进行了数值研究。在二维CFD模型中,采用k-?湍流模型,逆风插值方案,并使用OpenFOAM进行模拟。涡轮机有三片叶片对称排列。叶片为NACA 0012翼型,后缘区域进行了改进以提高升力性能。在尾缘距弦长15%处截断尾缘进行修改。在涡轮设计评估之前,对单正常翼型和钝翼型进行了建模和研究。对单翼型模型采用c结构网格,对垂直轴潮汐涡轮机模型采用混合网格进行网格划分。单翼型仿真结果表明,钝型NACA0012的升力系数比普通翼型高12%,钝型垂直轴潮汐涡轮的压力系数量级比普通NACA0012翼型垂直轴潮汐涡轮显著提高2倍。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A study of modified vertical axis tidal turbine to improve lift performance
A design of Darrieus vertical axis tidal turbine using modified airfoil was studied numerically in this work. The turbine design was evaluated in 2D CFD model using k-? turbulence model, upwind interpolation scheme and simulated using OpenFOAM. The turbine had three blades which were arranged symmetrically. The blades were of NACA 0012 airfoil which had been modified in the trailing edge region to increase its lift performance. The modification was made by truncating the trailing edge at the 15% of chord length from the trailing edge. Single normal and blunt airfoil were modelled and investigated prior to the turbine design evaluation. For generating the mesh, C-structured grid was employed to the single airfoil model and hybrid mesh to the vertical axis tidal turbine model. From the single airfoil simulations, it was found that blunt NACA0012 had 12% higher lift coefficient than normal airfoil and the pressure coefficient magnitude of blunt vertical axis tidal turbine significantly rise two times from vertical axis tidal turbine using normal NACA0012 airfoil.
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