pitching-moment inertia俯仰转动惯量
pitching-moment derivative俯仰力矩导数
pitching connection moment纵摇扭转力矩
pitching-moment link测俯仰力矩杆
pitching-moment equation俯仰力矩方程
pitching-moment curve俯仰力矩曲线
pitching-moment equilibrium俯仰力矩平衡
fuselage pitching-moment contribution机身俯仰力矩
pitching-moment weight beam俯仰力矩测量杆
The coefficients of drag, lift, pitching moment, pressure center are calculated by the integral of every wing surface according to the flow field parameters. The results accord with the aerodynamic theory.
依据流场参数,对翼的各个面进行气动力积分,计算出不同马赫数和不同攻角下的阻力系数、升力系数、俯仰力矩系数和压力中心系数,通过分析,计算结果符合空气动力学基本规律。
参考来源 - 高超声速弹箭尾翼（弹翼）的气动力与气动热研究