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襟翼改型对风力机专用翼型气动特性的影响研究

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采用数值模拟方法研究襟翼改型对S809翼型气动特性的影响,并对襟翼的增升机理进行探讨。研究结果表明,在中小攻角范围内,安装角度为 90 °和60 °的襟翼具有一定的增升效果,可使最大升力系数分别提高 5。66%和 3。95%;通过分析翼型压力系数分布,发现尾缘附近压力面压力变大,导致升力系数提高;但是在大攻角下改型襟翼导致升力系数减小。
Research on the influence of modified flaps on the aerodynamic characteristics of wind turbine special airfoil
The influence of flap modification on the aerodynamic characteristics of S809 airfoil for wind turbines was studied by numerical simulation method,and the principal of lift enhancement of flap was discussed.The results show that the flaps with inclined angles of 90° and 60° had a certain lifting effect at low-to-moderate angles of attack,and could increase the maximum lift coefficient by 5.66%and 3.95%,respectively.By analyzing the distribution of pressure coefficients of airfoils,it was found that the pressure of the pressure surface near the tail edge became larger,resulting in an increase in the lift coefficient.However,the modification of the flaps at big angles of attack led to a decrease in the lift coefficient.

wind turbine airfoilaerodynamic characteristicsGurney flapinclined angle

黄智峰、蒋笑、王海鹏

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江西理工大学 能源与机械工程学院 江西 南昌 330013

风力机翼型 气动特性 襟翼 安装角度

江西省教育厅科学技术研究项目

GJJ170570

2024

能源工程
浙江省能源研究所 浙江省能源研究会

能源工程

影响因子:0.314
ISSN:1004-3950
年,卷(期):2024.44(1)
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