The aerodynamic efficiency is compared with bi objective optimization airfoil's, to identify the advantage of adaptive airfoil.
为验证自适应翼型增益的效果，计算了双目标优化翼型的气动特性。
A new type of fitness function suitable to bi \ | objective optimization problems is suggested.
提出了一种新的适用于双目标优化的适应函数的构造方法。
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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