Research Article
Unsteady Vibration Aerodynamic Modeling and Evaluation of Dynamic Derivatives Using Computational Fluid Dynamics
Figure 1
Five motion states of aircraft after disturbance.
(a) Steady linear flight |
(b) Static instability |
(c) Static neutral stability |
(d) Static stability, dynamic stability |
(e) Static stability, dynamic neutral stability |
(f) Static stability, dynamic instability |