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Large eddy simulations of ventilated micro hydrokinetic turbine at design and off-design operating conditions

机译:设计和非设计工况下的通风微流体动力涡轮的大型涡流模拟

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Multiphase large eddy simulations (LES) were conducted for ventilated micro hydrokinetic turbine operating at design and off-design operational conditions. The simulations were performed with and without aeration at the design tip-speed ratio of 1.86 and at off-design tip-speed ratios of 1.2 and 2.7. The spatial and temporal characteristics of oxygen dissolution into the water were examined. The nominal value of power generation for the tip-speed ratio of 1.2 decreased slightly with aeration, while it increased slightly at the tip-speed ratio of 1.86 and 2.7. Slight increase in thrust was also observed for each case. The standard deviation of both power and thrust coefficient were increased more than 47% with air injection at the tip-speed ratio of 1.2, while the standard deviation of the thrust coefficient decreases by approximately 18% at the tip-speed ratio of 1.86 and 2.7. The suppression of small eddies and the early dissipation of tip vortices in multiphase simulations in the cases of the tip-speed ratio of 1.86 and 2.7 can be related to more stable turbine operation with aeration. It is demonstrated here that micro hydrokinetic turbines can be used effectively for aeration purposes at wide range of operating conditions.
机译:对在设计和非设计运行条件下运行的通风微流体动力涡轮机进行了多相大涡模拟(LES)。在有和没有充气的情况下进行了仿真,设计尖端速度比为1.86,非设计尖端速度比为1.2和2.7。检查了氧气溶解在水中的时空特征。尖端速度比为1.2时的发电标称值随充气而略有下降,而尖端速度比为1.86和2.7时则略有增加。在每种情况下,推力也略有增加。顶速比为1.2时,空气注入时功率和推力系数的标准偏差都增加了47%以上,而顶速比为1.86和2.7时,推力系数的标准偏差下降了约18%。 。在叶端速比为1.86和2.7的情况下,在多相模拟中抑制小涡流和叶尖涡流的早期散失可能与涡轮机更稳定的充气运行有关。在此证明,微型流体动力涡轮机可以有效地用于各种工作条件下的充气目的。

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