M
mks
Guest
The pressure wave would be bowed over the bullet nose at some unknown angles, constantly changing, during flight. Same would hold for other shockwaves generated at bearing and base.
On the other hand, the pressure wave far from the bullet has an angle defined by the mach number
angle = arcsin(1/Mach #)
Ckaven,
What are you trying to find out about the pressure wave?
Keith
Last edited by a moderator: