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Computational analysis of shrouded wind turbine configurations using a 3-dimensional RANS solver

机译:使用3维RANS求解器的带罩风轮机配置的计算分析

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The use of a shroud is known to improve performance. In this work, the flow physics and performance of shrouded turbines is assessed by solving the Reynolds Averaged Navier-Stokes equations supplemented with a transition model. Shroud geometries are evaluated for their augmentation of mass flow through the turbine. Initial assessments are performed using axisymmetric calculations of annular wings with high-lift airfoils as cross sections. The mass flow amplification factor is defined as a performance parameter and is found to increase nearly linearly with radial lift force. From a selection of considered airfoils, the Selig S1223 high-lift airfoil is found to best promote mass flow rate. Full three-dimensional simulations of shrouded wind turbines are performed for selected shroud geometries. The results are compared to open turbine solutions. Augmentation ratios of up to 1.9 are achieved. Peak augmentation occurs at the highest wind speed for which the flow over the blade stays attached. Flowfields are examined in detail and the following aspects are investigated: regions with flow separation, the development of velocity profiles, and the interaction between the turbine wake and shroud boundary layer. The sensitivity of the solutions to rotation rate is examined. (C) 2014 Elsevier Ltd. All rights reserved.
机译:已知使用护罩可提高性能。在这项工作中,通过求解补充了过渡模型的雷诺平均Navier-Stokes方程来评估带罩涡轮的流动物理特性和性能。评估护罩的几何形状以增加通过涡轮的质量流量。初始评估是通过以高升翼型为横截面的环形机翼的轴对称计算来进行的。将质量流量放大系数定义为性能参数,并且发现其随径向提升力几乎呈线性增加。从一系列经过考虑的翼型中,发现Selig S1223高升力翼型可以最大程度地提高质量流量。对于选定的罩几何形状,对罩式风力涡轮机进行了完整的三维模拟。将结果与开放式涡轮机解决方案进行比较。达到高达1.9的增强率。峰值增加发生在最高风速时,叶片上的气流保持附着。详细研究了流场,并研究了以下方面:具有流动分离的区域,速度分布的形成以及涡轮机尾流和护罩边界层之间的相互作用。检查溶液对转速的敏感性。 (C)2014 Elsevier Ltd.保留所有权利。

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