Numerical results of symmetric arc airfoil and NACA65A006 airfoil show that aerodynamic efficiency of adaptive airfoil is better than that of bi objective optimization airfoil.
本文计算了对称圆弧翼型和NACA 6 5 A0 0 6翼型。 计算结果表明，自适应翼型比双目标优化的翼型有更好的气动特性。
Numerical results of symmetric arc airfoil and NACA65A006 airfoil show that aerodynamic efficiency of adaptive airfoil is better than that of bi objective optimization airfoil.
本文计算了对称圆弧翼型和NACA 6 5 A0 0 6翼型。 计算结果表明，自适应翼型比双目标优化的翼型有更好的气动特性。
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