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Comparative study of the performances of twisted two-bladed and three-bladed airfoil shaped H-Darrieus turbines by computational and experimental methods

机译:用计算和实验方法对比研究扭曲的两叶和三叶翼型H-Darrieus涡轮的性能

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摘要

The vertical axis H-Darrieus turbines are simple in construction, self-starting, omni-directional, and self-regulating at a!! wind speeds. A comparative study of the performances of twisted two-bladed and three-bladed airfoil shaped H-Darrieus turbines was made. The models of the turbines were designed, fabricated, and tested in a subsonic wind tunnel. The power coefficients (C_p) and torque coefficients (C,) were evaluated for ten numbers of height-to-diameter (H/D) ratios. Both C_p and C, of the two-bladed turbine were higher than the three-bladed turbine. The maximum C_p for the two-bladed turbine was 0.237 and that for the three-bladed turbine was 0.151. The performances of the turbines were also compared computationally through 2D steady-state CFD simulations using Fluent 6.2 software. The agreement between the computational and experimental C_p was within ± 5.86%. The contour plots of static and dynamic pressures and velocity magnitudes were generated for chord Reynolds number of 8.5×10~4. At any position on the blade, dynamic pressure, velocity and also the velocity gradient between the ends were higher for the two-bladed turbine than the three-bladed turbine.
机译:垂直轴H-Darrieus涡轮机结构简单,可自动启动,全向且可自动调节!风速。对扭曲的两叶和三叶翼型H-Darrieus涡轮的性能进行了比较研究。涡轮机的模型是在亚音速风洞中设计,制造和测试的。针对十个高径比(H / D)比率,评估了功率系数(C_p)和扭矩系数(C1)。两叶涡轮的C_p和C均高于三叶涡轮。两叶涡轮的最大C_p为0.237,三叶涡轮的最大C_p为0.151。还使用Fluent 6.2软件通过2D稳态CFD仿真对涡轮机的性能进行了计算比较。计算和实验C_p之间的一致性在±5.86%之内。对于8.5×10〜4的和弦雷诺数,生成了动静压力和速度幅值的等高线图。在叶片的任何位置上,两叶片式涡轮机的动压,速度以及两端之间的速度梯度均高于三叶片式涡轮机。

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