双向水平轴潮流能水轮机翼型优化设计OA
Optimized design of bidirectional horizontal-axis tidal turbine airfoils
为适应潮流能的双向性和水平轴潮流能水轮机的可靠性,本文以NACA0012翼型为基础翼型,通过截取、拼接构造完全对称翼型,并构建以翼型升阻比为优化目标的自动寻优模型.该模型基于翼型类别形状函数变换参数化方法,并结合ICEM网格划分、Fluent数值模拟和多岛遗传算法,最终得到适用于水平轴潮流能水轮机双向运行的高升阻比翼型.优化后的完全对称翼型相比基础翼型更加扁平,最大相对厚度减少了49.65%.同时,升力系数提高了10.77%,且升阻比提升46.24%.通过分析翼型表面压力分布,发现优化后的翼型能有效地抑制翼型吸力面的流动分离现象,使翼型整体水动性能得到大幅提升.研究成果可为水平轴潮流能水轮机叶片翼型优化研究提供参考.
To address the bidirectionality and reliability of horizontal-axis tidal-current-energy-powered turbines,an automatic optimization model is constructed to optimize the lift-to-drag ratio of the airfoil.The optimized airfoil airfoil,is a fully symmetric airfoil that was constructed by modulating(intercepting and splicing)the NACA0012 airfoil,which serves as the base airfoil.The model employs the class-shape transformation parameterization method for the airfoil shape,integrating ANSYS ICEM CFD meshing,Fluent-based numerical simulation,and a multi-island genetic algorithm.This combined approach obtains a high lift-to-drag-ratio airfoil suitable for the bidirectional operation of horizontal-axis tidal-current-energy hydraulic turbines.Compared with the base airfoil(NACA0012),the optimized,fully symmetric airfoil is flatter,and its maximum relative thickness is reduced by 49.65%.This structural change resulted in a 10.77%increase in the lift coefficient and a notable 46.24%improvement in the lift-to-drag ratio.An analysis of the pressure distribution on the surface of the airfoil reveals that the optimized airfoil design effectively inhibits the flow-separation phenomenon on its suction surface,thereby significantly improving the overall hydrodynamic performance of the airfoil.Overall,this study provides a valuable reference for the optimization of the shapes of blade airfoils in horizontal-axis tidal-current-energy hydraulic turbines.
王树齐;卞百福;唐吉;刘峰
江苏科技大学 船舶与海洋工程学院,江苏 镇江 212100江苏科技大学 船舶与海洋工程学院,江苏 镇江 212100江苏科技大学 船舶与海洋工程学院,江苏 镇江 212100哈尔滨工程大学 船舶工程学院,黑龙江 哈尔滨 150001
海洋科学
潮流能水轮机完全对称翼型CST参数化多岛遗传算法优化设计数值模拟升阻比压力系数
tidal current energycompletely symmetrical airfoilCST parameterizationmulti-island genetic algo-rithmoptimization designnumerical simulationlift-to-drag ratiopressure coefficient
《哈尔滨工程大学学报》 2026 (1)
28-34,7
国家自然科学基金项目(51709137).
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