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Improvement of wind turbine aerodynamic performance by vanquishing stall with active multi air jet blowing

机译:通过主动多气动喷射吹塑燃烧摊位的风力涡轮机空气动力学性能

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The effects of jet blowing on blade suction side of NREL phase VI horizontal axis wind turbine (HAWT) for alleviation of degraded flow due to boundary layer separation were investigated. A 3D innovative multi jet blade is simulated using FLUENT 18.2 software applying SST k -u turbulence model. The spanwise blade portions for jets are outer, middle and inner. Furthermore, twelve jets with 0.04 local chord width have deployed in four chordwise locations of x/c = 0.1, x/c = 0.3, x/c = 0.5 and x/c = 0.7. The torque is sensitive to some dimensionless parameters such as Tip Speed Ratio (TSR) and jet velocity ratio (VR). At the best condition, torque increases about two times with respect to baseline blade. The jet velocity ratios are 1.2, 2.0, 2.4, 2.8, and 3.2. Applying changes in jet parameters, the flow pattern and quality improved. Also, the aerodynamic torque synergy of combinations of two, three and four jets were compared with that of a single jet and the direct relationship between the number of activated jets and the increase in torque was proved. The results showed that jets in blade outer part, have more effects in aerodynamic performance of rotor than the other blade portions. T1 jet produced the highest increase in torque. ? 2021 Elsevier Ltd. All rights reserved.
机译:研究了喷射对叶片抽吸侧的NREL相VI水平轴风风力涡轮机(HAWT)的影响,以减轻由于边界层分离引起的降解流动。使用Pluent 18.2软件应用SST K -U湍流模型模拟3D创新多射流刀片。用于喷射的翼展叶片部分是外部,中间和内部的。此外,在X / C = 0.1,X / C = 0.3,X / C = 0.5和X / C = 0.7的四个弦曲线位置,X / C = 0.5和X / C = 0.7的四个弦弦宽度部署了12个弦乐件。扭矩对一些无量纲参数敏感,例如尖端速度比(TSR)和喷射速度比(VR)。在最佳条件下,扭矩相对于基线刀片增加了大约两次。喷射速度比为1.2,2.0,2.4,2.8和3.2。应用射流参数的变化,流量模式和质量提高。而且,将两个,三个和四个喷射器的组合的空气动力扭矩协同作用与单次射流的组合,并证明了活化喷射器的数量与扭矩增加之间的直接关系。结果表明,叶片外部的喷射,在转子的空气动力学性能方面具有比其他刀片部分的空气动力学性能更多。 T1喷射产生扭矩的最高增加。还是2021 elestvier有限公司保留所有权利。

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