JonsidneyB,
I created an account to reply to this thread! I've wondered the same kinds of things as you about scaling effects on BC, rifling marks etc.
As for the scaling effects, I've written an entire 2 part article about it. You can find it on my website:
http://bryanlitz.bravehost.com/
On the bottom left, there's a couple links under "Understanding Long Range Bullets". You want 'Part 1: The nature of scale'.
As for the rifling marks, The answer may be different than you think....
At first thought, you might think the roughness adds drag, right? On second thought, the bullets spinning, so the air flow isn't hitting the grooves perpendicular,like you said). However, the bullets forward motion slows down faster than it's rotational speed, so downrange the speeds don't match up, and there's drag again, right...?
Here's what I think about the effect of riflings on bullet drag...
The grooves are small enough to be burried in the boundary layer where the air isn't moving at full speed, so if there is added skin friction drag, it's negligable. However, there is a bigger effect at work.
A boundary layer can be laminar or turbulent, depending on the length, speed, and surface roughness of the projectile,the projectile's 'Reynolds number'). Now, there's less skin friction drag in a laminar boundary layer than a turbulent boundary layer. So laminar is always better, right? Not always. The case where a turbulent boundary layer is desireable is when you have an adverse pressure gradient, and you want the flow to stay attached to the body, like along a boat-tail, or the back of a racecar, airplane, etc. If the flow stays attached along the tapered boat-tail, the bullet has less base drag. But it's harder for the boundary layer to stay attached if it's laminar. In other words, the extra skin friction drag of the turbulent boundary layer is mroe than made up for by the fact that the turbulent boundary layer is more energetic, and can stay better attached to the tapered afterbody,boat-tail), and yeild less base drag,much more important than difference in skin friction).
It's hard to predict exactly when transition,from turbulent to laminar) will occur, but the things that foster transition are: length, speed, and surface roughness. The riflings are the perfect height of surface roughness to cause boundary layer transition, and help keep the flow attached along the boat-tail. Wind tunnel models will often use artificial roughness strips on the leading edges of subscale aircraft and missile models to trigger early transition in an attempt to match the flow charachteristics of larger scale airframes.,getting off topic, sorry...)
Back to riflings and boat-tails...
I'm not saying that boat-tails would be completely ineffective with a laminar boundary layer, but by working with a turbulent boundary layer,thanks in part to the 'surface roughness' riflings), the boat-tail can perhaps opperate at a steeper angle. For example, laminar flow might separate from a 4 degree boat-tail. However, a turbulent boundary layer might stay attached to a 8 or 9 degree boat-tail, yielding less base drag than the 4 degree boat-tail. The trick is finding the steepest boat-tail angle you can get away with, while maintaining attached flow. If the flow separates, the bullet might as well be a flat-base from a base drag point of view.
If all this sounds like I'm talking 'smack', did you ever wonder why golf balls have dimples? It's for the EXACT reason I'm talking about. The dimples cause boundary layer transition which enables the flow to stay attached a little farther around the back of the ball, and have a smaller area of detached flow, ie, less base drag.
In conclusion, I believe that if riflings have any effect at all on the overall drag of a bullet, it's a net decrease in drag. The riflings help to transition the boundary layer to turbulent, thus enableing the flow to negotiate steeper boat-tail angles, and decrease the area of separated flow behind the bullet, which decreases base drag.
-Bryan
Reference:
1. Modern Exterior Ballistics By Robert McCoy page 77
2. Basic Fluid Mechanics By David Wilcox
3. Also see:
This link
and
this other link