Open Access

表4

气动优化设计模型

模型字符表示含义数量
目标函数CD阻力系数1
设计变量α
Xwing
TW
巡航迎角
FFD控制点的Z向位移
机翼扭转角
1
224
7
约束CL=0.116
t≥0.9tini
TW0
定升力系数约束
机翼厚度约束
翼根扭转角约束
1
245
1

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