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)