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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