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Study on Performance of Wind Mill by Adding Winglet in Turbine Blade: Virtual Analysis

机译:汽轮机叶片中翼坯的性能研究:虚拟分析

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This research paper discusses the performance evaluation of wind mill by attaching winglet in turbine blade. Five winglet parameters namely winglet height, curvature radius, cant angle, sweep angle and twist angle are considered in this analysis, to get hold of how these parameters have influenced on lift coefficient and drag coefficient. Fifteen combinations of winglet model were modeled in Solid works and virtual analyses were carried out to identify the best winglet model that yield higher power output in the wind mill. Aerodynamic analysis was also carried out to study the performance of winglet at the tip of the rotor blade to account for the fluid forces with blades comprising different winglet configurations. The numerical investigation revealed that by adding a winglet to the base line turbine blade increases the co-efficient of lift by 2.3% resulting 2% to 3% rise in power output, and the reductions in vortex formation at tip of the blade in the total drag by 10.4%. From the analysis results, it is found that the sweep angle, cant angle and twist angle have influenced the windmill performance to extent of 2% increase, the coefficient of lift and 6% decrease in the coefficient of drag.
机译:本研究论文通过在涡轮叶片中附着小翼探讨了挡风机的性能评价。在该分析中考虑了五个小翼参数即小翼,曲率半径,不能角度,扫描角度和扭转角度,以掌握这些参数如何影响升力系数和拖动系数。 WINGLET模型的十五种组合在实木中建模,并进行了虚拟分析,以识别最佳翅翼模型,从而在缠绕磨机中产生更高功率输出。还进行了空气动力学分析,以研究转子叶片尖端的小翼的性能,以解释具有不同小翼型构造的叶片的流体力。数值研究表明,通过向基线涡轮机叶片添加小翼增加升力的共同效率为2.3%,导致功率输出的2%至3%升高,总计叶片尖端涡旋形成中的涡流形成减少拖累10.4%。从分析结果来看,发现扫掠角,角度和扭转角度影响了风车性能,在增加2%的程度上增加,升力系数和拖拉系数减少了6%。

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