计算模型维数对风力机翼型气动性能预测的影响
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国家重点基础研究发展计划(973计划)资助项目(2007CB714605)


Effects of the Calculation Models with Different Dimension on the Aerodynamic Performance Prediction for Wind Turbine Airfoil
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    摘要:

    为了研究二维与三维计算对风力机翼型气动性能预测的影响,采用数值求解N-S方程的方法,对DU93-W-210二维翼型和三维直叶片进行了数值模拟,并将气动性能的计算结果与实验值进行比较。结果表明:当翼型表面气流未发生分离时,二维翼型与三维直叶片周围的流场结构相同,二者之间的气动性能无明显差异,三维直叶片可被简化为二维翼型;当气流分离时,三维直叶片周围的流场结构具有明显的三维流动效果,气动性能更接近实验值,三维直叶片不能简化为二维翼型,而且三维直叶片的展向长度不宜过小,取2~4倍弦长为最佳。

    Abstract:

    In order to analyze the influence of different dimensions on aerodynamic performance prediction of wind turbine airfoil, the flow fields surrounding 2-D airfoil of DU93-W-210 and 3-D straight blade were simulated by solving the N-S equations. Experimental results were compared to predict aerodynamic performances. The results revealed that if the flow did not separate, the aerodynamic performance and streamline between the 2-D airfoil and 3-D straight blade were similar, and the 3-D straight blade could be simplified into 2-D airfoil. If it separated, the flow field of 3-D straight blade had significant 3-D flow effects, the predicted aerodynamic performance was closer to experimental value than 2-D airfoil, but the 3-D straight blade could not be simplified into 2-D airfoil. The best span wise length of 3-D straight blade was 2~4 times of the chord.

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李银然,李仁年,王秀勇,李德顺.计算模型维数对风力机翼型气动性能预测的影响[J].农业机械学报,2011,42(2):115-119.

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