This information can then be used to calculate the Pitch and Yaw StabilityDerivatives.
这个参数可以用来计算飞机仰角和偏航的加速回中稳定微调能力。
2
Aerodynamic force, moments, and longitudinal stabilityderivatives are estimated by three-dimensional low-order panel method.
涉及的气动力、力距和纵向稳定导数等则由三维低阶板块法计算获得。
3
The dynamic stabilityderivatives which are used for analysis and prediction the characters of spin are acquired in routine flow field usually, which has no effect of rotation.