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Design of a Small Horizontal Axis Wind Turbine

机译:小型水平轴风力发电机的设计

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摘要

Wind turbine rotor is the most significant part of a wind turbine. The design of wind turbine rotor blades can be achieved by many methods. The blade element momentum theory (BEMT) is one such method. Despite its simplicity, the BEMT gives quite accurate results. In the current work, wind turbine blades for small horizontal axis wind turbine were designed using Schmitz formulas for optimum rotor theory in conjunction with BEMT. The current design used the SG6043 airfoil. A low wind speed of 6 m/s is set for the design. The blade is divided into a number of equal length elements. MATLAB code iterates the solution to calculate the chord length and twist angle for each blade element until convergence. In each iteration, the angle of attack, as well as the lift and drag coefficients, are interpolated from airfoil data files at maximum glide ratio (Lift-to-Drag ratio). Blade element momentum theory is used to characterize the performance of the designed rotor. Wilson-Walker method for the correction of Thrust coefficient and axial induction factor is used in the calculation. Typical power coefficient vs. tip-speed ratio is reported with a maximum power coefficient of 0.53 is at a tip-speed ratio of around 6.
机译:风力涡轮机转子是风力涡轮机最重要的部分。风力涡轮机转子叶片的设计可以通过许多方法实现。刀片元素动量理论(BEMT)是一种这样的方法。尽管它很简单,但Bemt提供了非常准确的结果。在当前的工作中,使用Schmitz公式设计了用于小横轴风力涡轮机的风力涡轮机叶片,可与Bemt一起使用施密茨公式。目前的设计使用SG6043翼型。为设计设定了6米/秒的低风速。刀片分为多个相等的长度元件。 MATLAB代码迭代解决方案以计算每个刀片元件的弦长和扭转角度,直到收敛。在每次迭代中,攻击角度以及提升和拖动系数以最大的滑动比(升力与阻力比)从翼型数据文件内插。刀片元件动量理论用于表征设计转子的性能。用于校正推力系数和轴向诱导因子的威尔逊沃克方法用于计算。典型的功率系数与尖端速比报告,最大功率系数为0.53,尖端速度比为约6。

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