Bret, you get into these discussions by saying uninformed nonsense such as this.
< A 12-6 takes less HP than a 12-4, so arguably a 12-6 is less load. That's the problem with the 12-4 on the ST46, it doesn't have enough poop to run fast enough with a 12-4 (and still have an responsiveness left). The 12-6 puts can pull the airplane with much less shaft HP, so the ST still be happy.
The faster it is spinning, the less efficient the prop, so the more HP is required from the engine to get sufficient HP into the airframe. We are talking 8700 RPM or so with a 12-6 inflight, VS, ~11,000 with the 12-4. All else being equal (which is isn't since they are the same type prop), that would be almost twice the parasitic drag. >
Even the most casual aviation enthusiast knows that as you increase pitch, you increase load on the engine. That is just a fundamental fact of life . Don't believe it, get in any airplane with a controllable pitch prop on it and start cranking the pitch up and watch the manifold pressure go up along with the CHT and EGT..
I never professed to be an expert, but I sure do know that it takes more HP to spin a 6" pitch at a given RPM than it takes to spin a 4" pitch at the same RPM.
As for a 4-2 break, the engine has to be loaded and slowed down enough in order for the ignition to be capable of burning the too rich charge.
As for a 'wet two', the mixture isn't as far off as in a 4-2 mode so the change is very limited.
The only 'add' to be had from the break is an increase in torque due to the engine being slowed down enough to allow ignition on every revolution.
Phil