基于深度学习的翼型参数化建模方法
沈剑雄1(
),刘迎圆1(),王乐勤2
),刘迎圆1(),王乐勤2
Deep learning-based method for parametrized modeling of airfoil
Jianxiong SHEN1(),Yingyuan LIU1(),Leqin WANG2
),Yingyuan LIU1(),Leqin WANG2
图9. 原始翼型与拟合翼型的表面压力系数对比
Fig.9. Comparison of surface pressure coefficient between original airfoil and fitted airfoil
