Now were getting some input.:thumbsup: So other than the brief mention from TD I'm getting the impression that most are more concerned about the benefits of the increased volume that the turbo puts out than a reduction in back pressure.
I backed away from the discussion as I know what I'm wanting to say but can't get the message out all are talking the same thing but from different angles. Airflow dynamics do play a role here, we arent filling a static chamber, P over V laws do not change, if one goes up the other has to go down, a larger more efficent wheel will net more flow. Since my air compressor analogy fell flat (no pun intended)

lets try this, 2 jet engines, something I've spent 28 years previous to this one working on,
2 turbines; 1 small, & 1 large both capable of making say 1500 shp, but the bigger one is capable of 3000 shp, you might eek out more hp from the small one and get say 1750 shp out of it, but putting signifcant stress on it to make that and no safety margin left in it, or go with safety margin of the bigger one but underload it and run inefficiently fuel wise and run it also at 1750. The larger the turbine the slower it spins yet both are making same shp.
Or design a jet capable of producing power for 1750 shp, maximizing flow for power demand/projected max hp, my point that seems to be getting lost in translation is we have upped power request from the 6.5, yet GM designed the GM-X to meet the demand for 195 shp,
Yes it is backpressure, yes it is flow out of the turbo into the engine, yes it is overlap, yes it is charge air density, yes it is dispacement it is all of those things, we can debate the individual pieces and parts, but that isn't how an engine works, it is all about total flow dynamics and power to ground after it all happens, air flow is the key impediments to that are bad ergo flow loss through an IC, backpressure out the back of the engine, you can do things to make the trade off tolerable but there is a trade to be sure, you have to manage it.
We aren't completely dealing with a fixed compression into a fixed cyl, yes one stroke =X psi & cfm, but increase the number of strokes with rpm, and push from the turbo that range of availble power shifts to occur at different points of operating range from what it once did, ergo n/a 6.2 flywheel more/less peaks at 135 shp, 6.5 n/a a little more 150 IIRC, 6.5 turbo stock 195, peaked & tweaked 6.5 single turbo 300+, 6.5 dual turbo peaked & tweaked estimated 500+ or 153 mph capable all that was done to those same essential blocks is add more fuel & cfm of air, boost psi remains fairly similar with all, with exception of n/a's where physical dispalcement is changed.
I'm not a scientist, nor do I play one on TV, it's been a while since I stayed in a Holiday Inn Express, maybe I need to do that and have a fresh go at explaining how I think it all happens.

Just a knuckle dragging field service guy that dabbles in engine repair, turbines once as a profession, Diesel locomotives as profession now, and a plethora of other vehicular contrivances as a hobby over the years, gasoline-Diesel-and even pedal powered.