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3d Analysis of Lift and Moment Adaptation via Control Surface Deployments on a 5 MW Wind Turbine Blade

机译:通过5 MW风力涡轮机叶片上的控制面展开进行升力和力矩适应的3d分析

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This paper investigates the impact of deploying control surfaces on a model 5 MW offshore wind turbine blade. The wind turbine blade is modeled in 3D based on NRELs 5 MW wind turbine and incorporates varying airfoil shapes and structural twist along the blade length. Lift and aero-dynamic moment at various angle of attack settings are simulated and analyzed. Partial span-wise trailing-edge 3D control surfaces are modeled, simulated and analyzed at various control angles. Results depict the onset of stall around 22 degrees and a larger lift gain versus 10-15 degrees for standard 2D airfoils. Mid-flap controller enhances lift by a factor 2 and mitigates moment a factor of around 7 while end-flap controller enhances lift by a factor of around 1.024 and mitigates moment by a factor of around 2. The results and comparisons obtained serve as one of many instruments for gauging, designing, analyzing, and optimizing wind turbine systems.
机译:本文研究了部署控制面对5 MW型号海上风力涡轮机叶片的影响。风力涡轮机叶片基于NREL 5 MW风力涡轮机进行3D建模,并沿叶片长度融合了不同的翼型形状和结构扭曲。模拟和分析了在各种迎角设置下的升力和气动力矩。在各种控制角度对部分翼展方向后缘3D控制表面进行建模,模拟和分析。结果显示失速发生在22度左右,升力增益比标准2D机翼的10-15度大。中襟翼控制器将升力提高2倍,并将力矩降低约7倍,而尾翼控制器将升力提高约1.024倍,并将力矩降低约2倍。获得的结果和比较结果之一是测量,设计,分析和优化风力涡轮机系统的许多仪器。

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