翼型厚度对风力涡轮机叶片截面旋转增加的影响研究

Nathan Oliveira Assis, Daniel Sampaio Souza
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引用次数: 0

摘要

。了解风力涡轮机的空气动力对其设计具有重要意义。旋转增强是在旋转叶片的模拟和实验中观察到的现象。这种现象解决了空气动力载荷的增加。众所周知,科里奥利力造成的径向涡度的破坏与分离区域的缩小有关,因此与旋转效应有关。本文研究了翼型厚度对旋翼增振效果的影响。采用计算流体力学(CFD)方法,将科里奥利力和离心力作为Navier-Stokes方程的源项,并假设其在展向上具有周期性。结果表明,改进后的翼型升力系数对旋转效应的敏感性较低。至于阻力系数,修改翼型显示增加,而原来的翼型有一个减少。在攻角较大的情况下,涡度破坏项的分布较轻
本文章由计算机程序翻译,如有差异,请以英文原文为准。
ESTUDO DO EFEITO DA ESPESSURA DO AEROFÓLIO SOBRE O AUMENTO ROTACIONAL EM SEÇÕES DE PÁS DE TURBINA EÓLICA
. Understanding the aerodynamic forces on wind turbines is of major importance for their design. Rotational augmentation is a phenomenon observed in simulations and experiments with rotating blades. This phenomenon addresses the increase in aerodynamic load. It is known that the destruction of the radial vorticity attributed to the Coriolis force is related to the reduction of the separation region and, therefore, associated with the rotational effects. This paper describes investigations on the influence of airfoil thickness on the effects of rotational augmentation. Analyzes were performed using Computational Fluid Dynamics (CFD) considering Coriolis and centrifugal force as source terms in the Navier-Stokes equations and assuming periodicity in the spanwise direction. The results showed that the modified airfoil’s lift coefficient is less sensitive to rotational effects. As for the drag coefficient, the modified airfoil showed an increase, while the original airfoil had a reduction. The distribution of the vorticity destruction term was milder than in other cases with higher angles of attack
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