Dynamics Analysis of Separation Mechanism for Rotating Projectiles at the End of Trajectory

Table 6

Aerodynamic parameters for different angles of attack.

δ (°)	Cd	CL (10^−4)	Rx (N)	Ry (N)	Rz (N)
0	0.43	1.78	17.8	0.008	0.025
4	0.44	8.39	18.8	0.033	0.042
8	0.44	10.24	18.9	0.040	0.060

Note. C_d represents the drag coefficient, C_L represents the lift coefficient, R_x represents the drag force, R_y represents the lift force, and R_z represents the side force.