Prediction and Analysis of the Aerodynamic Characteristics of a Spinning Projectile Based on Computational Fluid Dynamics

Table 2

Notation and formula of six aerodynamic coefficients.

Coefficient	Name	Formula
CD0	Zero-yaw drag coefficient	,
CD2	Yaw drag coefficient
CLα	Lift coefficient derivative
CYpα	Magnus force coefficient derivative
CMα	Overturning moment coefficient derivative
Clp	Spin damping moment coefficient derivative