Research Article
Prediction and Analysis of the Aerodynamic Characteristics of a Spinning Projectile Based on Computational Fluid Dynamics
Figure 6
Comparison of aerodynamic coefficients, coefficient of (a) zero yaw drag, (b) quadratic yaw drag, (c) normal force derivative, (d) Magnus force, (e) pitching moment derivative, (f) rolling damping moment.
(a) |
(b) |
(c) |
(d) |
(e) |
(f) |