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Modification of k-ω Turbulence Model for Predicting Airfoil Aerodynamic Performance

Modification of k-ω Turbulence Model for Predicting Airfoil Aerodynamic Performance
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摘要 Predicting wind turbine S825 airfoil's aerodynamic performance is crucial to improving its energy efficiency and reducing its environmental impact. In this paper, a numerical simulation on the wind turbine S825 airfoil is con- ducted with k-to turbulence model at different attack angles. By comparing with experimental data, a new method of modifying k-to model is proposed. A modifying function is proposed to limit the production term in ω equation based on fluid rotation and deformation. This method improves turbulent viscosity and decreases separating re- gion when the airfoil works at large separating conditions. The predictive accuracy could be improved by using the modified k-to turbulence model.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第3期221-228,共8页 热科学学报(英文版)
基金 supported by the National Natural Science Foundation of China(No.51420105008,No.51376001) the National Basic Research Program of China(2012CB720205,2014CB046405)
关键词 S825 airfoil SEPARATION k-ω model aerodynamic performance NON-EQUILIBRIUM 湍流模型 面积预测 气动性能 翼型 修改 风力涡轮机 分离条件 能源效率
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