风力机用带和不带襟翼叶冠流动特性数值研究

IF 1.5 Q4 ENERGY & FUELS
L. Ramayee, K. Supradeepan
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引用次数: 0

摘要

与传统的风力涡轮机相比,有冠的风力涡轮机在转子的圆周上增加了防护罩,增强了风力。本文旨在为风力涡轮机设计一个更短的翼型横截面外壳,以提高平均速度,减少阻力,风管材料体积和塔负荷。利用ANSYS Fluent软件对小型风力机运行工况下单独叶冠和带襟翼叶冠的特性进行了数值模拟。采用单因素法(OFAT)分析了翼罩长径L/D比和角度对性能的影响,找到了最佳值。然后在优化后的翼罩出口处加入襟翼进行分析。结果表明,与单个长叶冠相比,带襟翼叶冠的平均速度提高,质量流量增加,阻力增大。为了降低阻力系数,采用实验设计方法对其外形几何参数进行了分析。结果表明,叶冠L/D比对平均速度有显著影响。最佳组合为叶冠L/D =0.4,叶冠角=9°,襟翼L/D =0.2,襟翼角=16°,径向距离为0.2 r。所提出的组合有助于得到加速度系数为1.78,阻力系数为1.84,材料体积为0.7×10−3 m3。结果表明,最佳的叶冠L/D比值在0.3 ~ 0.6之间,加速系数较高,材料体积较小,长度较短。通过对翼盖各截面受力分析,研究了单独翼盖和带翼盖的阻力。结果表明,负阻力作用于翼罩内前缘。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical study on flow characteristics of shroud with and without flap for wind turbine applications
Shrouded wind turbines have the shroud added to the rotor’s circumference, enhancing wind power compared to conventional wind turbines. This article aims to design a shorter aerofoil cross-sectional enclosure for the wind turbine that improves average velocity and reduces drag, duct material volume, and tower load. Numerical simulations were performed to understand the characteristics of shroud alone and shroud with flap using ANSYS Fluent in the operating regime of the small wind turbine. The influence of the shroud’s length-to-diameter L/D ratio and angle on the performance was analyzed using a one-factor-at-a-time (OFAT) approach, and the optimum values were found. Then the analysis was performed by including the flap at the exit of an optimized shroud. The shroud with flap results showed enhanced average velocity, increased mass flow rate, and higher drag forces than a single long shroud. In order to reduce the drag coefficient, the enclosure geometrical parameters were analyzed using the Design of Experiments (DOE) approach. The results show that the shroud L/D ratio significantly affects the average velocity. Moreover, the optimum combination was found as shroud L/D ratio=0.4, shroud angle=9°, flap L/D ratio=0.2, flap angle=16°, and radial distance of 0.2R. The proposed combination helps to get an acceleration factor of 1.78, a drag coefficient of 1.84, and a material volume of 0.7×10−3 m3. It was found that the optimal ratio of shroud L/D could be between 0.3 and 0.6, resulting in a higher acceleration factor, lower material volume, and shorter length. The drag forces acting in the shroud alone and shroud with flap were studied by analyzing the forces in every section. The results show that the negative drag force acts in the shroud’s inner leading edge.
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来源期刊
Wind Engineering
Wind Engineering ENERGY & FUELS-
CiteScore
4.00
自引率
13.30%
发文量
81
期刊介绍: Having been in continuous publication since 1977, Wind Engineering is the oldest and most authoritative English language journal devoted entirely to the technology of wind energy. Under the direction of a distinguished editor and editorial board, Wind Engineering appears bimonthly with fully refereed contributions from active figures in the field, book notices, and summaries of the more interesting papers from other sources. Papers are published in Wind Engineering on: the aerodynamics of rotors and blades; machine subsystems and components; design; test programmes; power generation and transmission; measuring and recording techniques; installations and applications; and economic, environmental and legal aspects.
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