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Analysis of Aerodynamic Performance for Wind Turbine Based on Amended Calculation of BEM Theory

机译:基于BEM理论修正计算的风力涡轮机空气动力学性能分析

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Effects of tip losses, hub losses, amended attack angle, and amended thrust coefficient are taken into consideration to analyze aerodynamic performance of wind turbine blades based on the blade element momentum (BEM) theory. Based on amended calculation of BEM theory, a program code is developed by software named Matlab. Using a 1500 kW wind turbine as an example, aerodynamic information, performance coefficients and blade load distributions are calculated. Compared with the well-known international wind power design software called Garrad Hassan (GH) Bladed, the results have good consistency, which further verifies amendments to the model algorithms and accuracy of the calculation. As a result, the amended calculation of BEM theory can reflect blade aerodynamic performance characteristics under actual operating condition, which has good reference and practicality for the wind turbine design and evaluation.
机译:考虑到尖端损耗,集线器损失,修改的攻角和修改推力系数的影响,分析了基于叶片元件动量(BEM)理论的风力涡轮机叶片的空气动力学性能。基于BEM理论的修正计算,由名为MATLAB的软件开发的程序代码。使用1500 kW风力涡轮机作为示例,计算空气动力学信息,性能系数和刀片负载分布。与称为Garrad Hassan(GH)的知名国际风电设计软件相比,结果具有良好的一致性,这进一步验证了模型算法的修改和计算的准确性。结果,BEM理论的修正计算可以反映实际操作条件下的叶片空气动力学性能特征,对风力涡轮机设计和评估具有良好的参考和实用性。

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