·2,447,543篇论文数据，部分数据来源于NoteExpress
The unsteady flow field near the leading edge of an oscillating sweptback wing is obtained by using 3-D subsonic lifting surface theory.
本文应用三元亚音速升力面理论求出了后掠翼前缘附近的流场。
youdao
应用推荐
模块上移
模块下移
不移动