International Journal of Aerospace Engineering

Research Article

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

Table 1

Mach number versus rolling rate (RPS).
MachRPS
0.14147.6
0.4421.6
0.65685.1
0.85895.9
0.875922.3
0.9948.6
0.951001.3
1.01054.0
1.051106.7
1.11159.4
1.21264.8