Lift and Drag Forces With Respect to Azimuth Position of a Darrieus Wind Turbine

Sajid Ali, Sang-Moon Lee, C. Jang
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Abstract

Tangential force is the most important parameter for driving the blade of a straight bladed H-Darrieus wind turbine forward. The direction of this force is very critical as it may move the blade forward (positive force) or it can also oppose the rotation (negative force). The direction of tangential force depends upon the distribution of two fundamental aerodynamic forces around the wind turbine blade i.e. Lift and drag. Current study aims to understand the impact of lift and drag forces on the tangential force variation with respect to (w.r.t) azimuth position. Commercial CFD software SC/tetra was employed in order to solve the unsteady Reynold-averaged Navier stokes (URANS) equations around the blades. Results show that very small portion (maximum 20% during rotation) of the drag force is actually converted into useful tangential force whereas rest of the drag force is converted into either normal force or negative tangential force (waste of energy). On the other hand, out of all the generated lift force, 70–90 percent is seemed to be beneficial for moving the blade forward and rest of the lift force also tries to oppose the motion (almost 15%). Overall, it was found that only 50–60 percent of the resultant force (lift + drag) acting on the blade, is actually useful to move the blade forward. The study was conducted at seven different tip speed ratios (TSRs) i.e. 1, 2, 2.28, 3, 3.5, 4 and 5 with NACA 0015 airfoil. Relatively higher fluctuations were observed in the distribution of forces at low values of TSRs (1 and 2) as compared to high values of TSRs (4 and 5). The results presented here are only limited to NACA 0015 whereas same methodology can be adopted for other blade profiles in future as well.
升力和阻力与达里厄斯风力机的方位位置有关
切向力是驱动直叶H-Darrieus风力机叶片前进的最重要参数。这个力的方向是非常关键的,因为它可以移动叶片向前(正力)或它也可以反对旋转(负力)。切向力的方向取决于风力机叶片周围两个基本气动力的分布,即升力和阻力。本研究旨在了解升力和阻力对切向力随(w.r.t)方位位置变化的影响。采用商用CFD软件SC/tetra对叶片周围的非定常雷诺平均纳维斯托克斯(URANS)方程进行求解。结果表明,很小一部分阻力(旋转时最大20%)实际上转化为有用的切向力,而其余的阻力转化为法向力或负切向力(浪费能量)。另一方面,在所有产生的升力中,70 - 90%似乎有利于叶片向前移动,其余的升力也试图反对运动(几乎15%)。总的来说,它被发现只有50 - 60%的合力(升力+阻力)作用在叶片上,实际上是有用的移动叶片向前。该研究是在七个不同的尖端速比(tsr)即1,2,2.28,3,3.5,4和5与NACA 0015翼型进行。与tsr值较高(4和5)相比,tsr值较低(1和2)时的力分布波动相对较大。本文给出的结果仅局限于NACA 0015,未来同样的方法也可以用于其他叶片型面。
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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