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Numerical optimization and experimental validation for a tidal turbine blade with leading-edge tubercles

机译:具有前沿结节的潮汐涡轮机叶片的数值优化和实验验证

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摘要

Recently the leading-edge tubercles on the pectoral fins of humpback whales have attracted the attention of researchers who wish to exploit this feature in the design of turbine blades to improve the blade performance. The main objective of this paper is therefore to make a further investigation into this biomimetic design inspiration through a fundamental research study involving a hydrofoil section, which represents a straightened tidal turbine blade, with and without the leading-edge tubercles, using computational and experimental methods. Firstly a computational study was conducted to optimise the design of the leading-edge tubercles by using commercial CFD code, ANSYS-CFX. Based on this study the optimum tubercle configuration for a tidal turbine blade with S814 foil cross-section was obtained and investigated further. A 3D hydrofoil model, which represented a "straightened" tidal turbine blade, was manufactured and tested in the Emerson Cavitation Tunnel of Newcastle University to investigate the effect of various tubercle options on the lift and drag characteristics of the hydrofoil. The experiments involved taking force measurements using a 3-component balance device and flow visualisation using a Particle Image Velocimetry (PIV) system. These tests revealed that the leading-edge tubercles may have significant benefits on the hydrodynamic performance of the hydrofoil in terms of an improved lift-to-drag ratio performance as well as reducing the tip vortex which is main cause of the undesirable end-effect of 3D foils. The study explores further potential benefits of the application of leading-edge tubercles on tidal turbine blades.
机译:最近,座头鲸的胸鳍上的前沿结节吸引了研究人员的注意力,他们希望在涡轮叶片的设计中利用这一特征来改善叶片性能。因此,本文的主要目的是通过计算和实验方法,通过一项涉及翼型截面的基础研究,对仿生设计的灵感进行进一步研究,该翼型截面代表了带有和不具有前沿结节的潮汐涡轮叶片的拉直状态。 。首先,通过商业CFD代码ANSYS-CFX进行了计算研究,以优化前沿结节的设计。基于这项研究,获得了具有S814箔横截面的潮汐涡轮机叶片的最佳结节构型,并进行了进一步研究。在纽卡斯尔大学的艾默生气蚀隧道中制造并测试了代表“拉直”潮汐涡轮机叶片的3D水翼模型,以研究各种结节选项对水翼的升力和阻力特性的影响。实验涉及使用三分量平衡装置进行力测量,以及使用粒子图像测速(PIV)系统进行流动可视化。这些测试表明,前缘结节可能对水翼的水动力性能具有显着的好处,因为它具有改善的升阻比性能以及减少尖端涡流的作用,而尖端涡流是造成不希望有的最终结果的主要原因。 3D箔纸。该研究探索了在潮汐涡轮机叶片上应用前沿结核的进一步潜在益处。

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