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 |
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.