Analysis of Angular Velocities, Surrounding Air Pressure and Velocities of Various Designed Micro Vertical Axis Savonius Wind Turbines by the Computational Fluid Dynamics (CFD) Method

W. Manosroi, T. Tangtrakool, C. Lhaosornthong
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Abstract

The objective of this study is to analyze angular velocities, surrounding air pressure and velocities of various micro vertical axis Savonius wind turbine prototypes by the Computational Fluid Dynamics (CFD) method. The angular velocities of turbines are the basic parameters for determining the major parameters of the wind turbines, such as efficiency, torque, power and electricity etc. Eight models of the micro vertical axis Savonius wind turbine made of acrylic were designed by varying three parameters including the turbine distance between the pivot point and the tip, the distance between the apex curvature and the center plane curvature and the cross section types (circular, square, triangular and trapezoid). The eight models were divided into three groups including two models (B1, B2) with two different cross section types (triangle and rectangular) in the first group, three models (C1, C2, C3) with three different distances from the curvature tip to the centerline of 110, 85 and 40 millimeters in the second group and three models (D1, D2, D3) with different distances between the pivot point and the tip in the third group. Then, the angular velocities, the surrounding air pressure and velocities of the micro vertical axis Savonius wind turbine at the five wind speeds at 5.59, 7.67, 9.76, 10.45 and 11.84 m/s were measured and evaluated by the ANSYS program. The simulation by the CFD method of the angular velocities of the designed wind turbines was compared with the experimental results. Some discrepancies due to the absence of friction in the CFD results were observed. However, discrepancies between the simulation and the experimental results were decreased when the wind speed was increased due to the increase of torque and force in the experimental results which has overcome the turbine core friction. It has indicated that at the highest wind speed (11.84 m/s), the designed micro vertical axis Savonius circular cross section wind turbine with the curvature of the distance from the apex curvature to the center plane at 110 millimeters gave the highest turbine angular velocity of 441 rpm. At this highest turbine velocity by the CFD simulation, the high surrounding air pressure was not the smallest and the low turbine surrounding air pressure area was not the largest. This might be due to the effect of the suitable apex curvature distance to the center plane causing the efficient air flow to overcome the effect of the surrounding air pressure. The wind turbine of the second group gave the highest angular velocities followed by the first and the third group. These designed micro vertical axis Savonius wind turbines can be used as a preliminary model for the design and construction of the micro wind turbine to generate electricity at low wind speed region, such as Thailand.
用计算流体力学(CFD)方法分析不同设计的微型垂直轴Savonius风力机的角速度、周围空气压力和速度
本研究的目的是利用计算流体动力学(CFD)方法分析各种微型垂直轴Savonius风力机样机的角速度、周围空气压力和速度。风力机角速度是确定风力机效率、转矩、功率、电量等主要参数的基本参数。通过改变涡轮机枢轴点到尖端的距离、顶点曲率到中心平面曲率的距离以及截面类型(圆形、正方形、三角形和梯形)三个参数,设计了8个亚克力材料的微型垂直轴Savonius风力发电机模型。8个模型分为3组,第一组为2个模型(B1、B2),具有三角形和矩形两种不同的截面类型;第二组为3个模型(C1、C2、C3),曲率尖端距中心线110、85和40毫米有3个不同的距离;第三组为3个模型(D1、D2、D3),枢轴点距尖端有不同的距离。在此基础上,利用ANSYS软件分别测量了在5.59、7.67、9.76、10.45和11.84 m/s 5种风速下,Savonius微型垂直轴风力机的角速度、周围空气压力和风速。利用CFD方法对设计的风力机进行了角速度模拟,并与实验结果进行了比较。由于不考虑摩擦,计算结果中出现了一些差异。然而,随着风速的增加,由于实验结果中扭矩和力的增加,克服了涡轮堆芯摩擦,模拟结果与实验结果的差异减小。结果表明,在最高风速(11.84 m/s)下,设计的微垂直轴Savonius圆形截面风力机,从顶点曲率到中心平面的距离曲率为110 mm时,风力机的最大角速度为441 rpm。通过CFD模拟,在此最高涡轮速度下,高涡轮周围空气压力并不是最小的,低涡轮周围空气压力面积也不是最大的。这可能是由于适当的顶点曲率距离中心平面的影响,使有效的气流克服了周围空气压力的影响。第二组风力涡轮机的角速度最高,其次是第一组和第三组。这些设计的微型垂直轴Savonius风力涡轮机可以作为设计和建造微型风力涡轮机的初步模型,用于在泰国等低风速地区发电。
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