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.
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。
2
The aerodynamic forces on any control surface produce a moment about the hinge.
在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
3
The aerodynamic terms in the force and moment equations have all been replaced by the state variables of which they are functions. and control forces and moments.