This is a complex subject matter, which is precisely the sort of thing this forum was created to discuss.
If there is a general statement to be made about bullet design and transonic stability, it would be that: shorter, fatter bullets with small, shallow BT's or no BT tend to remain most stable at transonic speed. Going up in altitude also results in more stability in transonic, so some bullets which may tumble at transonic at sea level could fly thru fine at 5,000 feet altitude.
The obvious problem with this general statement is that LR shooters don't typically want to shoot short fat bullets, we like the long pointy bullets.
So when selecting a bullet for Extreme Long Range (ELR) where bullets will encounter transonic speed, you have to decide if you want to push transonic far downrange with a long pointy bullet that will be questionable at transonic speed, or select a low BC bullet that will hit transonic at a shorter range, but remain stable as it flies at this speed.
Most ELR shooters favor the high BC option, and there is a lot of grey area as to how these bullets will fly thru transonic. Most will experience some degree of yaw as they fly thru transonic. The technical term is called 'limit cycle yaw' which is a fancy name for 'trim'. In a place where stability is challenged, as in transonic flight, the bullet isn't stable in perfect point forward flight, but can 'trim' at a small yaw angle which puts the bullet in equilibrium for that condition. The yaw isn't a steady pointing to one side, rather a dynamic coning motion around the bullets flight path.
Limit cycle yaw causes 'induced drag' on the bullet, which is proportional to the magnitude of limit cycle yaw angle. Many bullets can fly straight and remain accurate thru transonic even though their drag is +10% or greater than it's 'zero yaw' drag. You can suppress the magnitude of the limit cycle yaw angle by using faster twist rates. Doing so allows the bullet to fly thru transonic with lower angles, and therefore lower drag.
This is why transonic drag and trajectory prediction can be such a grey area; drag can literally be affected by twist rate.
As to what bullet features contribute to limit cycle yaw, it's difficult to say because the entire stability condition is determined by a complex interaction of the bullets mass and aerodynamic properties.
One feature of bullet design that's been identified as having an affect is the camfer at the base of the bullet. At the very base, or heel of a bullet, there is a 0.010" to 0.020" camfer, or radius. The presence of this radius actually causes the bullet to fly with greater limit cycle yaw angles. I first became aware of this by reading an AIAA paper (
http://arc.aiaa.org/doi/abs/10.2514/6.2009-3851). I then repeated the experiment by taking some typical bullets that had about 0.020" heal, and cutting that heal off in a lathe. Note, just the small heal was cut off, not the entire boat tail. It amounted to less than 4 grains of material. These bullets I called 'square heal bullets'. I then performed the following comparison. I measured the BC of the un-altered bullets from a 1:12" and 1:8" twist barrel thru transonic speed. For these unaltered bullets, there was noticably (~7%) more drag for the 1:12" twist compared to the 1:8" twist. I then fired the square heal bullets thru both barrels under the same conditions, and observed that there was no difference in transonic drag for these bullets fired from the 1:12" and 1:8". The square heal bullets exhibited the same drag from both barrels that the un-altered bullets had from the 1:8".
So my results matched with the AIAA paper; removing the heal allows the bullet to fly with less limit cycle yaw.
This is a long answer to your question, but it goes to show that sometimes even minor features of a bullets shape can have a substantial effect on it's transonic flight. I don't think any generalizations can be made, which is why I'm working on testing bullets thru various twist rate barrels to determine their transonic flight quality. The end objective for me is to experimentally determine transonic effects for bullets, so it can be described in models used in ballistics software to predict more accurate trajectories thru transonic.
BTW, if you're interested in reading more about the square base experiment and my other tests on how stability affects BC (supersonic and transonic), how twist rate affects MV, precision, etc. it's all published in: 'Modern Advancements in Long Range Shooting'.
-Bryan