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Computational characterization of the vortex generated by a Vortex Generator on a flat plate for different vane angles

机译:涡流发生器在平板上针对不同叶片角度产生的涡旋的计算表征

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Vortex generators (VGs) are usually employed to improve the aerodynamic performance for both spatial or energy issues; such as aircrafts and wind turbine blades. These structures present poor aerodynamic performance in the sections close to the hub enabling the lift to decay under critical conditions. One way to overcome this drawback is the use of VGs, avoiding or delaying the boundary layer separation. The main goal of this work is to characterize the size of the primary vortex generated by a single VG on a flat plate by Computational Fluid Dynamics simulations using OpenFOAM code. This is performed by assessing the half-life radius of the vortex and comparing it with experimental results. In addition, a prediction model based on two elementary parameters has been developed to describe in a simple way the evolution of the size of the primary vortex downstream of the vane for four different incident angles. (C) 2017 Elsevier Masson SAS. All rights reserved.
机译:涡流发生器(VG)通常用于改善空间或能量问题的空气动力学性能。例如飞机和风力涡轮机叶片。这些结构在靠近轮毂的区域中表现出较差的空气动力学性能,从而使举升在关键条件下衰减。克服此缺点的一种方法是使用VG,避免或延迟边界层分离。这项工作的主要目的是通过使用OpenFOAM代码进行计算流体动力学模拟,表征单个VG在平板上产生的一次涡旋的大小。这是通过评估涡旋的半衰期半径并将其与实验结果进行比较来完成的。另外,已经开发了基于两个基本参数的预测模型,以简单的方式描述了针对四个不同入射角的叶片下游初级涡旋尺寸的演变。 (C)2017 Elsevier Masson SAS。版权所有。

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