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Aerodynamic performance of a blunt trailing-edge airfoil affected by vortex generators and a trailing-edge wedge

机译:受涡流发生器和后缘楔形影响的钝后缘翼型的空气动力学性能

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Vortex generators and trailing-edge wedges are proposed to be adopted simultaneously to enhance aerodynamic performance of a blunt trailing-edge airfoil for wind turbines. To understand the impact and physics of these two devices on airfoil performance, investigation was carried out by numerical simulation on DU97-W-300 using CFD. Three-dimensional models, including baseline models, models fitted with vortex generators, models equipped with a trailing-edge wedge and models with both devices, were built and validated through the comparison between the simulation results and experimental data. The main aerodynamic parameters were obtained to evaluate the efficiency of these two accessories. Furthermore, pressure distributions with and without the two devices were presented, and the structures of induced vortices, as well as their interaction in downstream region were also analysed. The simulation shows that vortex generators and the trailing-edge wedge work well in concert. The combined effects of the two devices on airfoil performance are positive, especially in enhancement of lift and the restriction of drag. In addition, trailing-edge wedges are suitable for blunt trailing-edge airfoils due to their strength. And the wedge with a height under 1% chord yields a significant increase in maximum lift coefficient at the cost of an acceptable drag increment.
机译:建议同时采用涡流发生器和后缘楔块,以增强用于风力涡轮机的钝性后缘翼型的空气动力学性能。为了了解这两种设备对翼型性能的影响和物理特性,使用CFD对DU97-W-300进行了数值模拟,以进行研究。通过模拟结果和实验数据之间的比较,建立并验证了三维模型,包括基线模型,装配有涡流发生器的模型,装配有后缘楔形的模型以及带有这两种设备的模型。获得了主要的空气动力学参数,以评估这两个附件的效率。此外,还介绍了有和没有这两种装置时的压力分布,还分析了诱导涡旋的结构以及它们在下游区域的相互作用。仿真表明,涡流发生器和后缘楔形件可以很好地协同工作。这两种装置对翼型性能的综合影响是积极的,尤其是在提升力和阻力限制方面。另外,由于后缘楔块的强度,因此它们适合于钝的后缘翼型。并且,高度低于1%的楔形块会以可接受的阻力增量为代价,显着提高最大升力系数。

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