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Towards accurate CFD simulations of vertical axis wind turbines at different tip speed ratios and solidities: Guidelines for azimuthal increment, domain size and convergence

机译:在不同的叶尖速比和强度下实现垂直轴风力涡轮机的精确CFD模拟:方位角增量,域大小和收敛的准则

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The accuracy of CFD simulations of vertical axis wind turbines (VAWTs) is known to be significantly associated with the computational parameters, such as azimuthal increment, domain size and number of turbine revolutions before reaching a statistically steady state condition (convergence). A detailed review of the literature, however, indicates that there is a lack of extensive parametric studies investigating the impact of the computational parameters. The current study, therefore, intends to systematically investigate the impact of these parameters, on the simulation results to guide the execution of accurate CFD simulations of VAWTs at different tip speed ratios (lambda) and solidities (sigma). The evaluation is based on 110 CFD simulations validated with wind tunnel measurements for two VAWTs. Instantaneous moment coefficient, C-m, and power coefficient, C-p, are studied for each case using unsteady Reynolds-averaged Navier-Stokes (URANS) simulations with the 4-equation transition SST turbulence model. The results show that the azimuthal increment d theta is largely dependent on tip speed ratio. For moderate to high lambda, the minimum requirement for d theta is 0.5 degrees while this decreases to 0.1 degrees at low to moderate lambda. The need for finer time steps is associated to the flow complexities related to dynamic stall on turbine blades and blade-wake interactions at low lambda. In addition, the minimum distance from the turbine center to the domain inlet and outlet is 15 and 10 times the turbine diameter, respectively. It is also shown that 20-30 turbine revolutions are required to ensure statistically converged solutions. The current findings can serve as guidelines towards accurate and reliable CFD simulations of VAWTs at different tip speed ratios and solidities.
机译:已知垂直轴风力涡轮机(VAWT)的CFD模拟精度与计算参数显着相关,例如方位角增量,域大小和达到统计稳定状态条件(收敛)之前的涡轮转数。然而,对文献的详细回顾表明,缺乏广泛的参数研究来研究计算参数的影响。因此,当前的研究旨在系统地研究这些参数对模拟结果的影响,以指导在不同的叶尖速度比(λ)和固体(sigma)下对VAWT进行精确的CFD模拟。该评估基于对两个VAWT的风洞测量进行验证的110个CFD模拟。使用具有四方程过渡SST湍流模型的非稳态雷诺平均Navier-Stokes(URANS)模拟,针对每种情况研究了瞬时力矩系数C-m和功率系数C-p。结果表明,方位角增量d theta在很大程度上取决于叶尖速度比。对于中至高的λ,d theta的最低要求为0.5度,而在中至低的λ时,最低要求降至0.1度。需要更细的时间步长与涡轮机叶片动态失速和低λ叶片-尾流相互作用相关的流动复杂性有关。另外,从涡轮中心到区域入口和出口的最小距离分别是涡轮直径的15倍和10倍。还显示出需要20-30次涡轮旋转才能确保统计收敛解。当前的发现可以作为在不同的叶尖速比和强度下对VAWT进行准确可靠的CFD模拟的指南。

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