Numerical and Experimental study of the effect of increasing aspect ratio of self-starting force to vertical axis wind turbine

H. Seifi, S. Kouravand, Mohsen Seifi Davari, S. Mohammadzadeh
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引用次数: 2

Abstract

Three airfoils NACA0015, NACA0018 and NACA0021 were selected and in the Q-Blade software, the coefficients of shear, post and the maximum ratio of the exponential coefficients were determined and, finally, the Airfoil Nakata 0015 at a speed of 5 and 10 meters per second, was selected and best. Fluent software was used to solve it, based on the finite volume method. For numerical analysis, the turbulence method K-ω SST was validated with experimental results. The wind turbine schematics was designed in Catia software and the height of the blades was 35 and 75 centimeters, the radius of the blade was 18.5 cm and the length of the airfoil 6.4 Cm is. The results show that in order to operate the turbine of porous blade windings at 35 cm height at speeds of 1, 2, 3, 4, 5, 7, 7.45, 8.25, 8.5 m / s 50% 50%, 33%, 50%, 50%, 60%, 57%, 55%, 50%, and for setting up a porous blade wind turbine at a height of 75 cm at a speed of one, two, three, four, Five, seven, 7.45, 8.25, 8.5, 9, 9.5 m / s 66.6%, 75%, 80%, 71.4%, 66.6%, 76.9%, 80%, 82%, 89%, 100% of the launching force Smooth wind turbine is required at the same height.
增大自启动力展弦比对垂直轴风力机影响的数值与实验研究
选择了NACA0015、NACA0018和NACA0021三种翼型,并在Q-Blade软件中确定了剪切系数、后期系数和指数系数的最大比值,最终选择了速度为5和10米/秒的中田翼型0015。基于有限体积法,采用Fluent软件进行求解。在数值分析中,用实验结果验证了湍流度方法K-ω SST。在Catia软件中设计风力机原理图,叶片高度分别为35和75厘米,叶片半径为18.5厘米,翼型长度为6.4厘米。结果表明,以多孔的涡轮叶片运行绕组在35厘米高度的速度1,2,3,4,5,7,7.45,8.25,8.5 m / s 50% 50%, 33%, 50%, 50%, 60%, 57%, 55%, 50%,和建立一个多孔叶片风力涡轮机的高度75厘米的速度一,二,三,四,五,七,7.45,8.25,8.5,9日,9.5 m / s 66.6%, 75%, 80%, 71.4%, 66.6%, 76.9%, 80%, 82%, 89%, 100%的启动力量平滑风力涡轮机是必需的在相同的高度。
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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