摘要
基于三维N-S方程,分别选用k-ε、k-ω、RSM和LES四种湍流模型对风力机专用S827翼型进行了数值模拟,对比了不同湍流模型对气动模拟精度的影响,得到了雷诺数为4×106时,该翼型在-4°~10°攻角下的升力和阻力特性曲线以及压力分布图,并与NREL的气动数据进行对比,结果表明,RSM湍流模型更适用于风力机专用翼型的数值模拟。
Different turbulence models such as k-ε、k-ω、RSM and LES are used to simulate airfoil S827 based on 3D N-S equation, and the computational results are compared. The lift and drag coefficients and pressure distribution are obtained within attack angle from -4° to 10° when Re equals 4×106. Through the comparison with NREL aerodynamic data, it is revealed that RSM turbulence model is more useful for the numerical simulation of special airfoil of wind turbine.
出处
《西华大学学报(自然科学版)》
CAS
2007年第6期61-62,65,共3页
Journal of Xihua University:Natural Science Edition
基金
甘肃省科技攻关项目(No2S052-004-03)