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粗糙度對(duì)風(fēng)力機(jī)翼型氣動(dòng)性能影響的數(shù)值預(yù)測(cè)
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國(guó)家重點(diǎn)基礎(chǔ)研究發(fā)展計(jì)劃(973計(jì)劃)資助項(xiàng)目


Numerical Prediction of the Effect of Surface Roughness on Aerodynamic Performance of a Wind Turbine Airfoil
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    摘要:

    采用二維不可壓縮N-S方程和SST k-ω湍流模型研究了風(fēng)力機(jī)翼型DU 95-W-180在粗糙表面時(shí)的空氣動(dòng)力學(xué)性能,,在整個(gè)翼型表面均勻分布不同高度的粗糙帶時(shí),,得到了該翼型的升力和阻力特性曲線,,以及最敏感的粗糙度,;同時(shí),,研究了在翼型壓力面和吸力面的不同位置布置粗糙帶時(shí),,粗糙帶位置對(duì)翼型的升力和阻力特性的影響,,通過(guò)分析得到了該翼型對(duì)粗糙帶的最敏感位置,,并進(jìn)一步分析了翼型兩個(gè)敏感位置的粗糙度對(duì)翼型升力特性,、阻力特性和升阻比的影響,。

    Abstract:

    The two-dimensional incompressible N-S equations and the SST k-ω turbulence model were used to study the aerodynamic performance of a wind turbine airfoil under rough surface conditions. The DU 95-W-180 airfoil that is widely used in wind turbines was chosen as the object. The studies were mainly done as described: the lift coefficient and the drag coefficient of the airfoil under different roughness heights on full surface and different roughness tape locations were computed, the trend of the lift coefficient and the drag coefficient with the roughness height and the roughness tape location were analyzed, the critical value of the roughness height and the roughness tape location,the trends of the lift coefficient, the drag coefficient and the ratio of lift coefficient and drag coefficient with the roughness height at the critical locations were also analyzed and the results were gained.

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李德順,李仁年,楊從新,王秀勇,李銀然.粗糙度對(duì)風(fēng)力機(jī)翼型氣動(dòng)性能影響的數(shù)值預(yù)測(cè)[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2011,42(5):111-115. Li Deshun, Li Rennian, Yang Congxin, Wang Xiuyong, Li Yinran. Numerical Prediction of the Effect of Surface Roughness on Aerodynamic Performance of a Wind Turbine Airfoil[J]. Transactions of the Chinese Society for Agricultural Machinery,2011,42(5):111-115.

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