pitch rate
·2,447,543篇论文数据，部分数据来源于NoteExpress
考虑了不同飞行攻角、不同燃料流率下气动参数，包括升力系数、阻力系数和俯仰力矩系数的变化规律。
The change rules of aerodynamic parameters including lift coefficient, drag coefficient and pitch moment coefficient have been analyzed when Angle of attack and fuel flow rate is changed.
youdao
应用推荐
模块上移
模块下移
不移动