Tidal Turbine Benchmarking Project: Stage I - Steady Flow Experiments

S.W. Tucker Harvey, Xiaosheng Chen, D. Rowe, J. McNaughton, C.R. Vogel, K. Bhavsar, T. Allsop, J. Gilbert, H. Mullings, T. Stallard, A. Young, I. Benson, R. Willden
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Abstract

The tidal turbine benchmarking project, funded by the UK's EPSRC and the Supergen ORE Hub, has conducted a large laboratory scale experiment on a highly instrumented 1.6m diameter tidal rotor. The turbine is instrumented for the measurement of spanwise distributions of flapwise and edgewise bending moments using strain gauges and a fibre Bragg optical system, as well as overall rotor torque and thrust. The turbine was tested in well-defined flow conditions, including grid-generated freestream turbulence, and was towed through the 12.2m wide, 5.4m deep long towing tank at Qinetiq’s Haslar facility. The turbine scale was such that blade Reynolds numbers were Re=3x10^5 and therefore post-critical, whilst turbine blockage was kept low at 3.1. In order to achieve higher levels of freestream turbulence a 2.4m by 2.4m turbulence grid was towed 5m upstream of the turbine. Measurements to characterise the grid generated turbulence were made at the rotor plane using an Acoustic Doppler Velocimeter and a five-hole pressure probe. An elevated turbulence of 3.1% with homogeneous flow speed across the rotor plane was achieved using the upstream turbulence grid. The experimental tests are well defined and repeatable, and provide relevant data for validating models intended for use in the design and analysis of full-scale turbines. This paper reports on the first experimental stage of the tidal benchmarking programme, including the design of the rotor and comparisons of the experimental results to blade resolved numerical simulations.
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潮汐涡轮机基准项目:第一阶段-稳定流动实验
由英国EPSRC和Supergen ORE Hub资助的潮汐涡轮机基准项目已经在一个高度仪器化的直径1.6米的潮汐转子上进行了大型实验室规模的实验。涡轮的仪器用于测量扇形和边缘弯矩的展向分布,使用应变片和光纤布拉格光学系统,以及整体转子扭矩和推力。涡轮机在明确的流动条件下进行了测试,包括电网产生的自由流湍流,并在Qinetiq的Haslar设施中通过12.2米宽,5.4米深的拖曳水箱。涡轮尺度是这样的,叶片雷诺数Re=3 × 10^5,因此是后临界,而涡轮堵塞保持在3.1的低水平。为了获得更高水平的自由流湍流,在涡轮上游5m处拖曳了一个2.4m × 2.4m的湍流网格。利用声学多普勒测速仪和五孔压力探头,在旋翼面上对网格产生的湍流进行了测量。采用上游湍流栅格,在均匀的旋翼平面上实现了3.1%的湍流提升。实验测试具有良好的定义和可重复性,并为验证用于全尺寸涡轮机设计和分析的模型提供了相关数据。本文报道了潮汐基准程序的第一阶段实验,包括转子的设计和实验结果与叶片解析数值模拟的比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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