首页> 外文会议>ASME Fluids Engineering Division summer meeting >THE EFFECT OF ADVANCE RATIO, SOLIDITY, AND WAKE INTERACTIONS ON A 2D VERTICAL AXIS TURBINE
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THE EFFECT OF ADVANCE RATIO, SOLIDITY, AND WAKE INTERACTIONS ON A 2D VERTICAL AXIS TURBINE

机译:提前比,固结度和尾波相互作用对二维垂直轴涡轮的影响

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In recent years there has been an increased effort to utilize hydrokinetic devices to harvest energy from both wind and tidal flows. Vertical axis turbines utilization is of particular interest in tidal flows. A major disadvantage in vertical axis turbines is that they are less efficient than horizontal axis turbines. To increase the efficiency of the vertical axis turbines, 2D CFD simulations are completed in an effort to better understand the physics behind the operation of these turbines. Specifically, the effect of advance ratio, solidity, and wake interactions were investigated. Simulations were completed in OpenFOAM using the k-ω SST turbulence model at a nominal Reynolds number of 500,000 using a NACA 0015 airfoil. To simulate the motion of the turbine, Arbitrary Mesh Interfacing (AMI) was used. For all of the parameters tested, it was found that the geometric effective angle of attack seen by the turbine blades had a significant impact on the power extracted from the flow. The range of effective angles of attack was found to decrease as the advance ratio increased. In spite of this, a severe loss in the power coefficient occurred at an advance ratio of 2.5 during which the blade experienced dynamic stall. This effect was also seen when the number of turbine blades was changed to four, at a solidity of 1.08. Results indicate that wake interactions between subsequent blades have a large impact on performance especially when the wake interaction alters the flow direction sufficiently to create conditions for dynamic stall.
机译:近年来,加大了利用流体动力学装置从风和潮汐流中收集能量的努力。垂直轴涡轮机的利用在潮汐流中特别重要。垂直轴涡轮机的主要缺点是它们的效率低于水平轴涡轮机。为了提高垂直轴涡轮机的效率,已完成2D CFD仿真,以更好地了解这些涡轮机运行背后的物理原理。具体来说,研究了前进比,坚固性和尾流相互作用的影响。使用k-ωSST湍流模型在OpenFOAM中使用NACA 0015翼型在标称雷诺数为500,000的情况下完成了仿真。为了模拟涡轮机的运动,使用了任意网格接口(AMI)。对于所有测试参数,发现涡轮叶片看到的几何有效攻角对从流中提取的功率有重大影响。发现有效攻角的范围随着前进比的增加而减小。尽管如此,在前进比为2.5时,功率系数出现了严重的损失,在此期间叶片经历了动态失速。当涡轮叶片的数量更改为四个时,其坚固性为1.08,也可以看到这种效果。结果表明,后续叶片之间的尾流相互作用对性能有很大影响,特别是当尾流相互作用充分改变流向以创造动态失速条件时。

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