Design optimization of three‐dimensional geometry of a micro horizontal axis wind turbine blade using the response surface method

PAMM Pub Date : 2024-01-27 DOI:10.1002/pamm.202300248
Riyadh Bekkai, R. Laouar, R. Mdouki
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Abstract

This study presents an aerodynamic design optimization of a micro micro‐horizontal‐axis wind turbine (HAWT). To obtain an optimal design, it is essential to understand the design parameters and select the responsible factors that affect the blade efficiency. The aim of this work is to redesign a 3D micro‐HAWT to improve aerodynamic performance, through improving the distribution of chord length and twist angle along the blade. Performance analysis and flow visualization of the initial design and the optimal design were carried out using CFD analyzer. In the blade optimization design, eight significant input parameters were selected, five to characterize the chord length distribution and three to represent the twist angle along the blade. To maximize the efficiency, design points that are created by Design of Experiment (DoE) are evaluated through (Multi‐Objective‐Genetic Algorithm) MOGA method. The results showed a reduction on the separation effect area on the optimal blade surface compared to the initial one. The use of response surface optimization (RSO), when combined with CFD simulation, has proven beneficial in selecting the optimal HAWT design. Finally, the open source software (Qblade) was used to investigate and to compare the performance of the initial and optimum design. An efficiency enhancement of approximately 3.6% is achieved at tip speed ration TSR = 3.4.
利用响应面法优化微型水平轴风力涡轮机叶片的三维几何设计
本研究介绍了微型水平轴风力涡轮机(HAWT)的空气动力学优化设计。要获得最佳设计,必须了解设计参数并选择影响叶片效率的相关因素。这项工作的目的是重新设计三维微型 HAWT,通过改善叶片弦长和扭转角的分布来提高气动性能。使用 CFD 分析仪对初始设计和优化设计进行了性能分析和流动可视化。在叶片优化设计中,选择了 8 个重要的输入参数,其中 5 个用于描述叶片弦长分布,3 个用于表示沿叶片的扭转角。为了最大限度地提高效率,通过(多目标遗传算法)MOGA 方法对实验设计(DoE)创建的设计点进行了评估。结果表明,与初始叶片相比,最佳叶片表面的分离效应面积有所减少。事实证明,将响应面优化(RSO)与 CFD 模拟相结合,有利于选择最佳的 HAWT 设计。最后,使用开源软件(Qblade)对初始设计和优化设计的性能进行了研究和比较。在顶端速度比 TSR = 3.4 时,效率提高了约 3.6%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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