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风力机翼型多目标气动性能优选设计方法
发表时间：2013-03-31 浏览量：1365 下载量：658
| 全部作者： | 卓文涛，戴韧，杨爱玲，刘雪骄，李莹 |
| 作者单位： | 上海理工大学能源与动力工程学院 |
| 摘 要： | 以翼型升阻比和气动噪声作为翼型主要优选目标，建立风力机翼型的多目标优选设计方法，包括利用Bezier曲线对翼型几何进行参数化建模，使用位势流动与边界层迭代（interactive boundary-layer，IBL）的流动分析方法计算翼型流场，采用Brooks-Pope-Marcolini（BPM）翼型自噪声半经验模型预测气动噪声，利用均匀试验优选方法求得优选翼型。以S809翼型为例，对翼型进行优选设计计算，结果表明优选翼型在设计工况下，升阻比提高，噪声降低，优选翼型获得比原始翼型更好的气动性能。 |
| 关 键 词： | 风能；风力机翼型；升阻比；气动噪声；优选设计 |
| Title： | Multi-objective optimization design method of aerodynamic performance for wind turbine airfoil |
| Author： | ZHUO Wentao, DAI Ren, YANG Ailing, LIU Xuejiao, LI Ying |
| Organization： | School of Energy and Power Engineering, University of Shanghai for Science and Technology |
| Abstract： | In this paper, taking lift-drag ratio and aerodynamic noise of the airfoil as the optimization objectives, the multi-objective optimization method of wind turbine airfoil was established, including describing airfoil geometry using Bezier curves, calculating airfoil flow field using interactive boundary layer (IBL) flow analysis method, predicting aerodynamic noise using the Brooks-Pope-Marcolini (BPM) airfoil self-noise semi-empirical model for predicting aerodynamic noise, and getting the optimized airfoil using uniform design optimization method. Taking S809 airfoil as an example, through the optimum design caculation on its airfoil, the results showed that the lift-drag ratio of optimized airfoil was increased and the acoustic level was decreased in operating conditions, and optimized airfoil got much better aerodynamic performance than the original airfoil. |
| Key words： | wind energy; wind turbine airfoil; lift-drag ratio; aerodynamic noise; optimum design |
| 发表期数： | 2013年3月第6期 |
| 引用格式： | 卓文涛，戴韧，杨爱玲，等. 风力机翼型多目标气动性能优选设计方法[J]. 中国科技论文在线精品论文，2013，6（6）：543-548. |
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