Bryan Litz Ballistics
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The overturning moment experienced by a bullet in flight is well understood and documented. It's the reason why bullets need to be spun; in order to not 'overturn' or tumble. The aerodynamic force applied at the center of pressure, which is forward of the center of gravity for a bullet, will 'overturn' the bullet if it's not spun fast enough.
The magnitude of the overturning moment depends on many things including several aerodynamic properties which have severe changes near the speed of sound (transonic speed). This is also well documented, and manifests for some bullets as tumbling near Mach 1.
It can be confusing because, in supersonic flight, the bullet's forward velocity decays much faster than it's rotational velocity. Therefore, aerodynamic overturning moment is diminishing faster than the bullets spin rate, and stability does improve as the bullet goes downrange; to a point.
So one might wonder how stability becomes 'challenged' at transonic speed. The reason is because the aero properties (in laymans terms) just go crazy near Mach 1. So even though the bullet's forward speed has slowed more than it's rotation, the dramatic transient in aero coefficients near Mach 1 can still challenge the stability of the bullet.
This is not just theory, it's been measured and published by numerous credible sources.
Catshooter,
This forum was established as a place for shooters to ask ballistics questions and have educational and productive discussions. Your posts on this topic have contained a mixture of false information and berating of forum members. This type of conduct will not be tolerated.
-Bryan
The magnitude of the overturning moment depends on many things including several aerodynamic properties which have severe changes near the speed of sound (transonic speed). This is also well documented, and manifests for some bullets as tumbling near Mach 1.
It can be confusing because, in supersonic flight, the bullet's forward velocity decays much faster than it's rotational velocity. Therefore, aerodynamic overturning moment is diminishing faster than the bullets spin rate, and stability does improve as the bullet goes downrange; to a point.
So one might wonder how stability becomes 'challenged' at transonic speed. The reason is because the aero properties (in laymans terms) just go crazy near Mach 1. So even though the bullet's forward speed has slowed more than it's rotation, the dramatic transient in aero coefficients near Mach 1 can still challenge the stability of the bullet.
This is not just theory, it's been measured and published by numerous credible sources.
CatShooter said:The BS stops here.
Catshooter,
This forum was established as a place for shooters to ask ballistics questions and have educational and productive discussions. Your posts on this topic have contained a mixture of false information and berating of forum members. This type of conduct will not be tolerated.
-Bryan